Started by upstream project "ESP_bPreBuilt" build number 77 originally caused by: Started by user galbramc Running as galbramc [EnvInject] - Loading node environment variables. Building remotely on viggen in workspace /Users/jenkins/workspace/ESP_bPreBuilt [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] Done Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_bPreBuilt Cleaning local Directory . Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-07-27T23:59:51.894 -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 2518 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP doesn't exist Cleaning local Directory JenkinsESP Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-07-27T23:59:51.894 -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 882 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023 doesn't exist Cleaning local Directory CAPS/training/2023 Checking out svn+ssh://acdl.mit.edu/home/svnroot/CAPS/training/2023 at revision '2024-07-27T23:59:51.894 -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 4251 No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ [GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [viggen] is in [[macys, macys_VM, master, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-rhel7, reynolds-ubuntu16, reynolds-ubuntu18, reynolds-ubuntu20]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [viggen] is in [[viggen]] Run condition [Execution node ] enabling perform for step [Execute shell] [ESP_bPreBuilt] $ /bin/bash -ex /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jenkins6693457005200018732.sh + arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_PreBuilt.sh + source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_Env.sh ++ export OCCTREF=7.8 ++ OCCTREF=7.8 ++ AFLR_VERSION=11.5.15 ++ SU2_VERSION=8.0.1 ++ TETGEN_VERSION=1.6.0 ++ VSP_VERSION=3.38.0 ++ export PYTHON_VERSION=3.11.9 ++ PYTHON_VERSION=3.11.9 ++ export MPLBACKEND=agg ++ MPLBACKEND=agg ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ [[ viggen == \r\e\y\n\o\l\d\s ]] ++ [[ '' == *\.\i\f\o\r\t ]] ++ '[' -f /opt/intel/oneapi/setvars.sh ']' ++ source /opt/intel/oneapi/setvars.sh ++ '[' -f /Users/jenkins/.bashrc ']' ++ export CAPS_OUTLEVEL=0 ++ CAPS_OUTLEVEL=0 ++ export ESP_UDC_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/personalUdc ++ ESP_UDC_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/personalUdc ++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/ ++ ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/ ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/ ++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/ ++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia ++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.8 != '' ]] ++ [[ '' != '' ]] ++ [[ viggen == *\r\e\y\n\o\l\d\s* ]] ++ [[ viggen == *\m\a\c\y\s* ]] ++ [[ viggen == *\v\i\g\g\e\n* ]] ++ export EMPnumProc=2 ++ EMPnumProc=2 ++ export OMP_NUM_THREADS=2 ++ OMP_NUM_THREADS=2 ++ source /Users/jenkins/.bash_profile ++++ /opt/homebrew/bin/brew shellenv +++ eval 'export HOMEBREW_PREFIX="/opt/homebrew"; export HOMEBREW_CELLAR="/opt/homebrew/Cellar"; export HOMEBREW_REPOSITORY="/opt/homebrew"; export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}"; [ -z "${MANPATH-}" ] || export MANPATH=":${MANPATH#:}"; export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";' ++++ export HOMEBREW_PREFIX=/opt/homebrew ++++ HOMEBREW_PREFIX=/opt/homebrew ++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ export HOMEBREW_REPOSITORY=/opt/homebrew ++++ HOMEBREW_REPOSITORY=/opt/homebrew ++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ '[' -z '' ']' ++++ export INFOPATH=/opt/homebrew/share/info: ++++ INFOPATH=/opt/homebrew/share/info: +++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]] +++ . /opt/homebrew/etc/profile.d/bash_completion.sh ++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']' ++++ return +++ export NETCDF_PATH=/opt/homebrew +++ NETCDF_PATH=/opt/homebrew ++ [[ viggen == *\m\a\c\y\s* ]] ++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \m\a\c\y\s ]] ++ export CASARCH=. ++ CASARCH=. ++ '[' '!' -z '' ']' +++ ls -d '/Users/jenkins/util/ESP/OpenCASCADE-.?' ls: /Users/jenkins/util/ESP/OpenCASCADE-.?: No such file or directory ++ export CASROOT= ++ CASROOT= ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/udunits/udunits2.xml ++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//lib:/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib ++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//lib:/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib ++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.15 ++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.15 ++ [[ viggen == *\m\a\c\y\s* ]] ++ export AFLR_ARCH=MacOSX-arm64 ++ AFLR_ARCH=MacOSX-arm64 ++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ export CART3D_ARCH=OSX64_ICC ++ CART3D_ARCH=OSX64_ICC ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS ++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ export SEACAS=/Users/jenkins/util/sandialabs/seacas ++ SEACAS=/Users/jenkins/util/sandialabs/seacas ++ [[ viggen == \v\i\g\g\e\n ]] ++ export NETCDFINC=/opt/homebrew/include ++ NETCDFINC=/opt/homebrew/include ++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.1 ++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.1 ++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']' +++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl ++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH; PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB; PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT; PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT; PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;' +++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin +++ export PATH +++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 +++ export PERL5LIB +++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_LOCAL_LIB_ROOT +++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"' +++ export PERL_MB_OPT +++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_MM_OPT ++ export PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ export PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ [[ viggen == \m\a\c\y\s* ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin ++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python ++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config ++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/virtualenv ++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-*' ++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-*' ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/virtualenv +++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-cc +++ python-config --includes ++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11' ++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11' +++ python-config --help ++ [[ Usage: /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]] +++ python-config --ldflags --embed ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation' ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ export PYTHONUNBUFFERED=true ++ PYTHONUNBUFFERED=true ++ export PYTHONFAULTHANDLER=true ++ PYTHONFAULTHANDLER=true ++ python --version Python 3.11.9 ++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/data ++ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/data + unset PYTHONINC + unset PYTHONLIB + unset ESP_BLOC + unset ESP_ROOT + unset ESP_ARCH + unset AWAVE ++ uname -s + [[ Darwin == *\D\a\r\w\i\n* ]] + DESKTOP=/Users/jenkins/Desktop + OSI=macos ++ uname -m + ARCH=arm64 + wget --tries=3 https://acdl.mit.edu/ESP/archive/ESP126-macos-arm64.tgz --2024-07-28 00:00:08-- https://acdl.mit.edu/ESP/archive/ESP126-macos-arm64.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: 522032067 (498M) [application/x-gzip] Saving to: ‘ESP126-macos-arm64.tgz’ 0K .......... .......... .......... .......... .......... 0% 7.39M 67s 50K .......... .......... .......... .......... .......... 0% 26.6M 43s 100K .......... .......... .......... .......... .......... 0% 81.5M 31s 150K .......... .......... .......... .......... .......... 0% 15.8M 31s 200K .......... .......... .......... .......... .......... 0% 309M 25s 250K .......... .......... .......... .......... .......... 0% 39.0M 23s 300K .......... .......... .......... .......... .......... 0% 263M 20s 350K .......... .......... .......... .......... .......... 0% 24.0M 20s 400K .......... .......... .......... .......... .......... 0% 303M 18s 450K .......... .......... .......... .......... .......... 0% 60.3M 17s 500K .......... .......... .......... .......... .......... 0% 50.4M 16s 550K .......... .......... .......... .......... .......... 0% 48.7M 16s 600K .......... .......... .......... .......... .......... 0% 33.0M 16s 650K .......... .......... .......... .......... .......... 0% 60.2M 15s 700K .......... .......... .......... .......... .......... 0% 231M 14s 750K .......... .......... .......... .......... .......... 0% 21.0M 15s 800K .......... .......... .......... .......... .......... 0% 170M 14s 850K .......... .......... .......... .......... .......... 0% 27.1M 14s 900K .......... .......... .......... .......... .......... 0% 33.4M 15s 950K .......... .......... .......... .......... .......... 0% 20.0M 15s 1000K .......... .......... .......... .......... .......... 0% 22.4M 15s 1050K .......... .......... .......... .......... .......... 0% 19.8M 16s 1100K .......... .......... .......... .......... .......... 0% 16.3M 16s 1150K .......... .......... .......... .......... .......... 0% 19.9M 17s 1200K .......... .......... .......... .......... .......... 0% 13.4M 18s 1250K .......... .......... .......... .......... .......... 0% 19.2M 18s 1300K .......... .......... .......... .......... .......... 0% 16.3M 18s 1350K .......... .......... .......... .......... .......... 0% 15.5M 19s 1400K .......... .......... .......... .......... .......... 0% 21.2M 19s 1450K .......... .......... .......... .......... .......... 0% 14.5M 20s 1500K .......... .......... .......... .......... .......... 0% 18.5M 20s 1550K .......... .......... .......... .......... .......... 0% 16.0M 20s 1600K .......... .......... .......... .......... .......... 0% 15.3M 20s 1650K .......... .......... .......... .......... .......... 0% 17.4M 21s 1700K .......... .......... .......... .......... .......... 0% 14.3M 21s 1750K .......... .......... .......... .......... .......... 0% 14.2M 22s 1800K .......... .......... .......... .......... .......... 0% 12.8M 22s 1850K .......... .......... .......... .......... .......... 0% 11.9M 22s 1900K .......... .......... .......... .......... .......... 0% 11.6M 23s 1950K .......... .......... .......... .......... .......... 0% 11.7M 23s 2000K .......... .......... .......... .......... .......... 0% 11.3M 24s 2050K .......... .......... .......... .......... .......... 0% 14.2M 24s 2100K .......... .......... .......... .......... .......... 0% 10.6M 25s 2150K .......... .......... .......... .......... .......... 0% 10.9M 25s 2200K .......... .......... .......... .......... .......... 0% 8.71M 26s 2250K .......... .......... .......... .......... .......... 0% 12.5M 26s 2300K .......... .......... .......... .......... .......... 0% 10.5M 27s 2350K .......... .......... .......... .......... .......... 0% 7.93M 27s 2400K .......... .......... .......... .......... .......... 0% 10.3M 28s 2450K .......... .......... .......... .......... .......... 0% 7.98M 29s 2500K .......... .......... .......... .......... .......... 0% 6.31M 29s 2550K .......... .......... .......... .......... .......... 0% 6.49M 30s 2600K .......... .......... .......... .......... .......... 0% 4.50M 32s 2650K .......... .......... .......... .......... .......... 0% 9.49M 32s 2700K .......... .......... .......... .......... .......... 0% 5.46M 33s 2750K .......... .......... .......... .......... .......... 0% 6.56M 34s 2800K .......... .......... .......... .......... .......... 0% 8.67M 34s 2850K .......... .......... .......... .......... .......... 0% 4.44M 36s 2900K .......... .......... .......... .......... .......... 0% 5.38M 37s 2950K .......... .......... .......... .......... .......... 0% 4.97M 38s 3000K .......... .......... .......... .......... .......... 0% 5.98M 39s 3050K .......... .......... .......... .......... .......... 0% 12.7M 39s 3100K .......... .......... .......... .......... .......... 0% 12.4M 39s 3150K .......... .......... .......... .......... .......... 0% 11.5M 39s 3200K .......... .......... .......... .......... .......... 0% 9.60M 39s 3250K .......... .......... .......... .......... .......... 0% 11.7M 39s 3300K .......... .......... .......... .......... .......... 0% 13.5M 39s 3350K .......... .......... .......... .......... .......... 0% 9.75M 39s 3400K .......... .......... .......... .......... .......... 0% 10.4M 39s 3450K .......... .......... .......... .......... .......... 0% 9.65M 39s 3500K .......... .......... .......... .......... .......... 0% 10.1M 39s 3550K .......... .......... .......... .......... .......... 0% 12.0M 39s 3600K .......... .......... .......... .......... .......... 0% 8.57M 40s 3650K .......... .......... .......... .......... .......... 0% 12.4M 40s 3700K .......... .......... .......... .......... .......... 0% 8.96M 40s 3750K .......... .......... .......... .......... .......... 0% 20.3M 40s 3800K .......... .......... .......... .......... .......... 0% 34.2M 39s 3850K .......... .......... .......... .......... .......... 0% 24.2M 39s 3900K .......... .......... .......... .......... .......... 0% 27.1M 39s 3950K .......... .......... .......... .......... .......... 0% 43.8M 38s 4000K .......... .......... .......... .......... .......... 0% 25.5M 38s 4050K .......... .......... .......... .......... .......... 0% 42.8M 38s 4100K .......... .......... .......... .......... .......... 0% 21.4M 38s 4150K .......... .......... .......... .......... .......... 0% 32.0M 37s 4200K .......... .......... .......... .......... .......... 0% 23.6M 37s 4250K .......... .......... .......... .......... .......... 0% 27.9M 37s 4300K .......... .......... .......... .......... .......... 0% 22.0M 37s 4350K .......... .......... .......... .......... .......... 0% 17.0M 37s 4400K .......... .......... .......... .......... .......... 0% 27.1M 37s 4450K .......... .......... .......... .......... .......... 0% 17.6M 36s 4500K .......... .......... .......... .......... .......... 0% 22.6M 36s 4550K .......... .......... .......... .......... .......... 0% 24.0M 36s 4600K .......... .......... .......... .......... .......... 0% 17.5M 36s 4650K .......... .......... .......... .......... .......... 0% 20.2M 36s 4700K .......... .......... .......... .......... .......... 0% 22.7M 36s 4750K .......... .......... .......... .......... .......... 0% 25.6M 36s 4800K .......... .......... .......... .......... .......... 0% 27.4M 35s 4850K .......... .......... .......... .......... .......... 0% 14.8M 35s 4900K .......... .......... .......... .......... .......... 0% 1.32M 39s 4950K .......... .......... .......... .......... .......... 0% 16.9M 39s 5000K .......... .......... .......... .......... .......... 0% 8.20M 39s 5050K .......... .......... .......... .......... .......... 1% 9.76M 39s 5100K .......... .......... .......... .......... .......... 1% 13.8M 39s 5150K .......... .......... .......... .......... .......... 1% 15.3M 39s 5200K .......... .......... .......... .......... .......... 1% 10.8M 39s 5250K .......... .......... .......... .......... .......... 1% 13.8M 39s 5300K .......... .......... .......... .......... .......... 1% 17.3M 39s 5350K .......... .......... .......... .......... .......... 1% 11.7M 39s 5400K .......... .......... .......... .......... .......... 1% 15.0M 39s 5450K .......... .......... .......... .......... .......... 1% 11.3M 39s 5500K .......... .......... .......... .......... .......... 1% 9.92M 39s 5550K .......... .......... .......... .......... .......... 1% 8.59M 39s 5600K .......... .......... .......... .......... .......... 1% 7.74M 39s 5650K .......... .......... .......... .......... .......... 1% 9.24M 39s 5700K .......... .......... .......... .......... .......... 1% 7.73M 40s 5750K .......... .......... .......... .......... .......... 1% 8.39M 40s 5800K .......... .......... .......... .......... .......... 1% 11.3M 40s 5850K .......... .......... .......... .......... .......... 1% 2.84M 41s 5900K .......... .......... .......... .......... .......... 1% 12.8M 41s 5950K .......... .......... .......... .......... .......... 1% 13.7M 41s 6000K .......... .......... .......... .......... .......... 1% 20.3M 41s 6050K .......... .......... .......... .......... .......... 1% 15.6M 41s 6100K .......... .......... .......... .......... .......... 1% 10.4M 41s 6150K .......... .......... .......... .......... .......... 1% 14.3M 41s 6200K .......... .......... .......... .......... .......... 1% 10.6M 41s 6250K .......... .......... .......... .......... .......... 1% 11.4M 41s 6300K .......... .......... .......... .......... .......... 1% 13.3M 41s 6350K .......... .......... .......... .......... .......... 1% 11.7M 41s 6400K .......... .......... .......... .......... .......... 1% 14.9M 41s 6450K .......... .......... .......... .......... .......... 1% 12.9M 41s 6500K .......... .......... .......... .......... .......... 1% 13.3M 41s 6550K .......... .......... .......... .......... .......... 1% 11.4M 41s 6600K .......... .......... .......... .......... .......... 1% 11.7M 41s 6650K .......... .......... .......... .......... .......... 1% 12.1M 41s 6700K .......... .......... .......... .......... .......... 1% 22.5M 40s 6750K .......... .......... .......... .......... .......... 1% 38.5M 40s 6800K .......... .......... .......... .......... .......... 1% 96.1M 40s 6850K .......... .......... .......... .......... .......... 1% 23.0M 40s 6900K .......... .......... .......... .......... .......... 1% 344M 40s 6950K .......... .......... .......... .......... .......... 1% 30.0M 39s 7000K .......... .......... .......... .......... .......... 1% 40.8M 39s 7050K .......... .......... .......... .......... .......... 1% 35.0M 39s 7100K .......... .......... .......... .......... .......... 1% 32.0M 39s 7150K .......... .......... .......... .......... .......... 1% 32.5M 39s 7200K .......... .......... .......... .......... .......... 1% 32.1M 38s 7250K .......... .......... .......... .......... .......... 1% 42.5M 38s 7300K .......... .......... .......... .......... .......... 1% 32.0M 38s 7350K .......... .......... .......... .......... .......... 1% 34.3M 38s 7400K .......... .......... .......... .......... .......... 1% 38.4M 38s 7450K .......... .......... .......... .......... .......... 1% 32.7M 38s 7500K .......... .......... .......... .......... .......... 1% 31.9M 37s 7550K .......... .......... .......... .......... .......... 1% 23.9M 37s 7600K .......... .......... .......... .......... .......... 1% 38.4M 37s 7650K .......... .......... .......... .......... .......... 1% 27.6M 37s 7700K .......... .......... .......... .......... .......... 1% 25.8M 37s 7750K .......... .......... .......... .......... .......... 1% 25.6M 37s 7800K .......... .......... .......... .......... .......... 1% 35.0M 37s 7850K .......... .......... .......... .......... .......... 1% 27.2M 37s 7900K .......... .......... .......... .......... .......... 1% 25.6M 36s 7950K .......... .......... .......... .......... .......... 1% 24.3M 36s 8000K .......... .......... .......... .......... .......... 1% 31.6M 36s 8050K .......... .......... .......... .......... .......... 1% 2.89M 37s 8100K .......... .......... .......... .......... .......... 1% 10.2M 37s 8150K .......... .......... .......... .......... .......... 1% 18.5M 37s 8200K .......... .......... .......... .......... .......... 1% 18.4M 37s 8250K .......... .......... .......... .......... .......... 1% 21.1M 37s 8300K .......... .......... .......... .......... .......... 1% 22.0M 37s 8350K .......... .......... .......... .......... .......... 1% 22.6M 37s 8400K .......... .......... .......... .......... .......... 1% 18.2M 37s 8450K .......... .......... .......... .......... .......... 1% 56.4M 36s 8500K .......... .......... .......... .......... .......... 1% 31.3M 36s 8550K .......... .......... .......... .......... .......... 1% 24.5M 36s 8600K .......... .......... .......... .......... .......... 1% 19.9M 36s 8650K .......... .......... .......... .......... .......... 1% 44.3M 36s 8700K .......... .......... .......... .......... .......... 1% 13.7M 36s 8750K .......... .......... .......... .......... .......... 1% 38.8M 36s 8800K .......... .......... .......... .......... .......... 1% 23.5M 36s 8850K .......... .......... .......... .......... .......... 1% 15.0M 36s 8900K .......... .......... .......... .......... .......... 1% 12.1M 36s 8950K .......... .......... .......... .......... .......... 1% 14.4M 36s 9000K .......... .......... .......... .......... .......... 1% 13.8M 36s 9050K .......... .......... .......... .......... .......... 1% 18.4M 36s 9100K .......... .......... .......... .......... .......... 1% 12.0M 36s 9150K .......... .......... .......... .......... .......... 1% 17.5M 36s 9200K .......... .......... .......... .......... .......... 1% 15.4M 36s 9250K .......... .......... .......... .......... .......... 1% 14.2M 36s 9300K .......... .......... .......... .......... .......... 1% 15.3M 36s 9350K .......... .......... .......... .......... .......... 1% 12.5M 36s 9400K .......... .......... .......... .......... .......... 1% 16.1M 36s 9450K .......... .......... .......... .......... .......... 1% 12.4M 36s 9500K .......... .......... .......... .......... .......... 1% 15.5M 36s 9550K .......... .......... .......... .......... .......... 1% 14.8M 36s 9600K .......... .......... .......... .......... .......... 1% 8.77M 36s 9650K .......... .......... .......... .......... .......... 1% 10.4M 36s 9700K .......... .......... .......... .......... .......... 1% 7.73M 36s 9750K .......... .......... .......... .......... .......... 1% 7.90M 36s 9800K .......... .......... .......... .......... .......... 1% 13.3M 36s 9850K .......... .......... .......... .......... .......... 1% 10.4M 36s 9900K .......... .......... .......... .......... .......... 1% 10.1M 36s 9950K .......... .......... .......... .......... .......... 1% 11.1M 36s 10000K .......... .......... .......... .......... .......... 1% 12.5M 36s 10050K .......... .......... .......... .......... .......... 1% 10.4M 36s 10100K .......... .......... .......... .......... .......... 1% 9.63M 36s 10150K .......... .......... .......... .......... .......... 2% 10.7M 36s 10200K .......... .......... .......... .......... .......... 2% 7.16M 36s 10250K .......... .......... .......... .......... .......... 2% 6.90M 37s 10300K .......... .......... .......... .......... .......... 2% 5.38M 37s 10350K .......... .......... .......... .......... .......... 2% 5.24M 37s 10400K .......... .......... .......... .......... .......... 2% 6.68M 37s 10450K .......... .......... .......... .......... .......... 2% 11.4M 37s 10500K .......... .......... .......... .......... .......... 2% 16.0M 37s 10550K .......... .......... .......... .......... .......... 2% 11.3M 37s 10600K .......... .......... .......... .......... .......... 2% 12.9M 37s 10650K .......... .......... .......... .......... .......... 2% 11.1M 37s 10700K .......... .......... .......... .......... .......... 2% 11.7M 37s 10750K .......... .......... .......... .......... .......... 2% 11.2M 37s 10800K .......... .......... .......... .......... .......... 2% 12.8M 37s 10850K .......... .......... .......... .......... .......... 2% 10.5M 37s 10900K .......... .......... .......... .......... .......... 2% 13.4M 37s 10950K .......... .......... .......... .......... .......... 2% 11.3M 37s 11000K .......... .......... .......... .......... .......... 2% 27.1M 37s 11050K .......... .......... .......... .......... .......... 2% 29.7M 37s 11100K .......... .......... .......... .......... .......... 2% 25.4M 37s 11150K .......... .......... .......... .......... .......... 2% 29.9M 37s 11200K .......... .......... .......... .......... .......... 2% 22.7M 37s 11250K .......... .......... .......... .......... .......... 2% 19.3M 37s 11300K .......... .......... .......... .......... .......... 2% 21.2M 37s 11350K .......... .......... .......... .......... .......... 2% 15.5M 37s 11400K .......... .......... .......... .......... .......... 2% 15.5M 37s 11450K .......... .......... .......... .......... .......... 2% 19.1M 37s 11500K .......... .......... .......... .......... .......... 2% 14.5M 37s 11550K .......... .......... .......... .......... .......... 2% 21.3M 37s 11600K .......... .......... .......... .......... .......... 2% 15.4M 37s 11650K .......... .......... .......... .......... .......... 2% 21.7M 37s 11700K .......... .......... .......... .......... .......... 2% 14.9M 37s 11750K .......... .......... .......... .......... .......... 2% 20.4M 37s 11800K .......... .......... .......... .......... .......... 2% 23.8M 36s 11850K .......... .......... .......... .......... .......... 2% 14.7M 36s 11900K .......... .......... .......... .......... .......... 2% 18.0M 36s 11950K .......... .......... .......... .......... .......... 2% 27.4M 36s 12000K .......... .......... .......... .......... .......... 2% 22.1M 36s 12050K .......... .......... .......... .......... .......... 2% 18.0M 36s 12100K .......... .......... .......... .......... .......... 2% 92.8M 36s 12150K .......... .......... .......... .......... .......... 2% 24.2M 36s 12200K .......... .......... .......... .......... .......... 2% 25.8M 36s 12250K .......... .......... .......... .......... .......... 2% 27.6M 36s 12300K .......... .......... .......... .......... .......... 2% 34.1M 36s 12350K .......... .......... .......... .......... .......... 2% 24.7M 36s 12400K .......... .......... .......... .......... .......... 2% 29.7M 36s 12450K .......... .......... .......... .......... .......... 2% 25.7M 36s 12500K .......... .......... .......... .......... .......... 2% 22.8M 35s 12550K .......... .......... .......... .......... .......... 2% 25.3M 35s 12600K .......... .......... .......... .......... .......... 2% 21.7M 35s 12650K .......... .......... .......... .......... .......... 2% 34.1M 35s 12700K .......... .......... .......... .......... .......... 2% 24.6M 35s 12750K .......... .......... .......... .......... .......... 2% 29.6M 35s 12800K .......... .......... .......... .......... .......... 2% 27.2M 35s 12850K .......... .......... .......... .......... .......... 2% 16.7M 35s 12900K .......... .......... .......... .......... .......... 2% 19.3M 35s 12950K .......... .......... .......... .......... .......... 2% 17.6M 35s 13000K .......... .......... .......... .......... .......... 2% 16.0M 35s 13050K .......... .......... .......... .......... .......... 2% 15.4M 35s 13100K .......... .......... .......... .......... .......... 2% 15.4M 35s 13150K .......... .......... .......... .......... .......... 2% 11.8M 35s 13200K .......... .......... .......... .......... .......... 2% 14.3M 35s 13250K .......... .......... .......... .......... .......... 2% 16.8M 35s 13300K .......... .......... .......... .......... .......... 2% 17.6M 35s 13350K .......... .......... .......... .......... .......... 2% 11.4M 35s 13400K .......... .......... .......... .......... .......... 2% 10.2M 35s 13450K .......... .......... .......... .......... .......... 2% 10.7M 35s 13500K .......... .......... .......... .......... .......... 2% 15.5M 35s 13550K .......... .......... .......... .......... .......... 2% 20.3M 35s 13600K .......... .......... .......... .......... .......... 2% 34.1M 35s 13650K .......... .......... .......... .......... .......... 2% 35.4M 35s 13700K .......... .......... .......... .......... .......... 2% 19.1M 35s 13750K .......... .......... .......... .......... .......... 2% 391M 35s 13800K .......... .......... .......... .......... .......... 2% 42.5M 35s 13850K .......... .......... .......... .......... .......... 2% 16.8M 34s 13900K .......... .......... .......... .......... .......... 2% 192M 34s 13950K .......... .......... .......... .......... .......... 2% 19.2M 34s 14000K .......... .......... .......... .......... .......... 2% 16.7M 34s 14050K .......... .......... .......... .......... .......... 2% 15.9M 34s 14100K .......... .......... .......... .......... .......... 2% 11.8M 34s 14150K .......... .......... .......... .......... .......... 2% 15.4M 34s 14200K .......... .......... .......... .......... .......... 2% 11.5M 34s 14250K .......... .......... .......... .......... .......... 2% 16.7M 34s 14300K .......... .......... .......... .......... .......... 2% 12.4M 34s 14350K .......... .......... .......... .......... .......... 2% 10.7M 34s 14400K .......... .......... .......... .......... .......... 2% 14.3M 34s 14450K .......... .......... .......... .......... .......... 2% 10.1M 34s 14500K .......... .......... .......... .......... .......... 2% 16.7M 34s 14550K .......... .......... .......... .......... .......... 2% 12.5M 34s 14600K .......... .......... .......... .......... .......... 2% 11.7M 34s 14650K .......... .......... .......... .......... .......... 2% 15.4M 34s 14700K .......... .......... .......... .......... .......... 2% 15.4M 34s 14750K .......... .......... .......... .......... .......... 2% 16.7M 34s 14800K .......... .......... .......... .......... .......... 2% 10.7M 34s 14850K .......... .......... .......... .......... .......... 2% 8.42M 34s 14900K .......... .......... .......... .......... .......... 2% 13.8M 34s 14950K .......... .......... .......... .......... .......... 2% 11.7M 34s 15000K .......... .......... .......... .......... .......... 2% 13.3M 34s 15050K .......... .......... .......... .......... .......... 2% 14.3M 34s 15100K .......... .......... .......... .......... .......... 2% 9.17M 35s 15150K .......... .......... .......... .......... .......... 2% 12.9M 35s 15200K .......... .......... .......... .......... .......... 2% 9.92M 35s 15250K .......... .......... .......... .......... .......... 3% 11.0M 35s 15300K .......... .......... .......... .......... .......... 3% 10.7M 35s 15350K .......... .......... .......... .......... .......... 3% 7.90M 35s 15400K .......... .......... .......... .......... .......... 3% 9.91M 35s 15450K .......... .......... .......... .......... .......... 3% 8.06M 35s 15500K .......... .......... .......... .......... .......... 3% 10.7M 35s 15550K .......... .......... .......... .......... .......... 3% 11.1M 35s 15600K .......... .......... .......... .......... .......... 3% 9.65M 35s 15650K .......... .......... .......... .......... .......... 3% 12.2M 35s 15700K .......... .......... .......... .......... .......... 3% 34.1M 35s 15750K .......... .......... .......... .......... .......... 3% 36.0M 35s 15800K .......... .......... .......... .......... .......... 3% 54.1M 35s 15850K .......... .......... .......... .......... .......... 3% 41.4M 35s 15900K .......... .......... .......... .......... .......... 3% 36.4M 35s 15950K .......... .......... .......... .......... .......... 3% 34.6M 34s 16000K .......... .......... .......... .......... .......... 3% 32.1M 34s 16050K .......... .......... .......... .......... .......... 3% 27.1M 34s 16100K .......... .......... .......... .......... .......... 3% 22.9M 34s 16150K .......... .......... .......... .......... .......... 3% 55.1M 34s 16200K .......... .......... .......... .......... .......... 3% 22.6M 34s 16250K .......... .......... .......... .......... .......... 3% 25.6M 34s 16300K .......... .......... .......... .......... .......... 3% 27.6M 34s 16350K .......... .......... .......... .......... .......... 3% 25.4M 34s 16400K .......... .......... .......... .......... .......... 3% 24.4M 34s 16450K .......... .......... .......... .......... .......... 3% 22.8M 34s 16500K .......... .......... .......... .......... .......... 3% 29.6M 34s 16550K .......... .......... .......... .......... .......... 3% 19.3M 34s 16600K .......... .......... .......... .......... .......... 3% 21.2M 34s 16650K .......... .......... .......... .......... .......... 3% 18.1M 34s 16700K .......... .......... .......... .......... .......... 3% 17.3M 34s 16750K .......... .......... .......... .......... .......... 3% 12.9M 34s 16800K .......... .......... .......... .......... .......... 3% 14.4M 34s 16850K .......... .......... .......... .......... .......... 3% 11.3M 34s 16900K .......... .......... .......... .......... .......... 3% 12.5M 34s 16950K .......... .......... .......... .......... .......... 3% 8.99M 34s 17000K .......... .......... .......... .......... .......... 3% 9.87M 34s 17050K .......... .......... .......... .......... .......... 3% 12.1M 34s 17100K .......... .......... .......... .......... .......... 3% 8.98M 34s 17150K .......... .......... .......... .......... .......... 3% 11.8M 34s 17200K .......... .......... .......... .......... .......... 3% 10.7M 34s 17250K .......... .......... .......... .......... .......... 3% 10.2M 34s 17300K .......... .......... .......... .......... .......... 3% 8.97M 34s 17350K .......... .......... .......... .......... .......... 3% 9.20M 34s 17400K .......... .......... .......... .......... .......... 3% 13.3M 34s 17450K .......... .......... .......... .......... .......... 3% 24.2M 34s 17500K .......... .......... .......... .......... .......... 3% 38.5M 34s 17550K .......... .......... .......... .......... .......... 3% 31.9M 34s 17600K .......... .......... .......... .......... .......... 3% 22.3M 34s 17650K .......... .......... .......... .......... .......... 3% 32.8M 34s 17700K .......... .......... .......... .......... .......... 3% 20.2M 34s 17750K .......... .......... .......... .......... .......... 3% 38.6M 34s 17800K .......... .......... .......... .......... .......... 3% 29.6M 34s 17850K .......... .......... .......... .......... .......... 3% 19.3M 34s 17900K .......... .......... .......... .......... .......... 3% 16.8M 34s 17950K .......... .......... .......... .......... .......... 3% 19.2M 34s 18000K .......... .......... .......... .......... .......... 3% 13.9M 34s 18050K .......... .......... .......... .......... .......... 3% 21.5M 34s 18100K .......... .......... .......... .......... .......... 3% 20.2M 34s 18150K .......... .......... .......... .......... .......... 3% 22.6M 34s 18200K .......... .......... .......... .......... .......... 3% 19.3M 34s 18250K .......... .......... .......... .......... .......... 3% 24.1M 34s 18300K .......... .......... .......... .......... .......... 3% 25.8M 33s 18350K .......... .......... .......... .......... .......... 3% 19.3M 33s 18400K .......... .......... .......... .......... .......... 3% 27.6M 33s 18450K .......... .......... .......... .......... .......... 3% 19.0M 33s 18500K .......... .......... .......... .......... .......... 3% 25.8M 33s 18550K .......... .......... .......... .......... .......... 3% 24.0M 33s 18600K .......... .......... .......... .......... .......... 3% 35.5M 33s 18650K .......... .......... .......... .......... .......... 3% 23.9M 33s 18700K .......... .......... .......... .......... .......... 3% 62.8M 33s 18750K .......... .......... .......... .......... .......... 3% 332M 33s 18800K .......... .......... .......... .......... .......... 3% 28.0M 33s 18850K .......... .......... .......... .......... .......... 3% 46.4M 33s 18900K .......... .......... .......... .......... .......... 3% 39.1M 33s 18950K .......... .......... .......... .......... .......... 3% 29.2M 33s 19000K .......... .......... .......... .......... .......... 3% 30.2M 33s 19050K .......... .......... .......... .......... .......... 3% 25.6M 33s 19100K .......... .......... .......... .......... .......... 3% 27.3M 33s 19150K .......... .......... .......... .......... .......... 3% 25.9M 33s 19200K .......... .......... .......... .......... .......... 3% 24.1M 33s 19250K .......... .......... .......... .......... .......... 3% 25.7M 33s 19300K .......... .......... .......... .......... .......... 3% 25.6M 33s 19350K .......... .......... .......... .......... .......... 3% 25.5M 32s 19400K .......... .......... .......... .......... .......... 3% 24.1M 32s 19450K .......... .......... .......... .......... .......... 3% 18.3M 32s 19500K .......... .......... .......... .......... .......... 3% 27.3M 32s 19550K .......... .......... .......... .......... .......... 3% 27.6M 32s 19600K .......... .......... .......... .......... .......... 3% 16.8M 32s 19650K .......... .......... .......... .......... .......... 3% 27.5M 32s 19700K .......... .......... .......... .......... .......... 3% 20.3M 32s 19750K .......... .......... .......... .......... .......... 3% 19.3M 32s 19800K .......... .......... .......... .......... .......... 3% 13.3M 32s 19850K .......... .......... .......... .......... .......... 3% 15.4M 32s 19900K .......... .......... .......... .......... .......... 3% 21.4M 32s 19950K .......... .......... .......... .......... .......... 3% 16.0M 32s 20000K .......... .......... .......... .......... .......... 3% 24.0M 32s 20050K .......... .......... .......... .......... .......... 3% 22.9M 32s 20100K .......... .......... .......... .......... .......... 3% 21.3M 32s 20150K .......... .......... .......... .......... .......... 3% 25.2M 32s 20200K .......... .......... .......... .......... .......... 3% 198M 32s 20250K .......... .......... .......... .......... .......... 3% 31.5M 32s 20300K .......... .......... .......... .......... .......... 3% 34.2M 32s 20350K .......... .......... .......... .......... .......... 4% 31.7M 32s 20400K .......... .......... .......... .......... .......... 4% 31.6M 32s 20450K .......... .......... .......... .......... .......... 4% 20.2M 32s 20500K .......... .......... .......... .......... .......... 4% 37.5M 32s 20550K .......... .......... .......... .......... .......... 4% 23.9M 32s 20600K .......... .......... .......... .......... .......... 4% 14.6M 32s 20650K .......... .......... .......... .......... .......... 4% 19.3M 32s 20700K .......... .......... .......... .......... .......... 4% 16.7M 32s 20750K .......... .......... .......... .......... .......... 4% 18.1M 32s 20800K .......... .......... .......... .......... .......... 4% 19.2M 32s 20850K .......... .......... .......... .......... .......... 4% 14.1M 32s 20900K .......... .......... .......... .......... .......... 4% 16.4M 32s 20950K .......... .......... .......... .......... .......... 4% 11.3M 32s 21000K .......... .......... .......... .......... .......... 4% 17.3M 32s 21050K .......... .......... .......... .......... .......... 4% 10.4M 32s 21100K .......... .......... .......... .......... .......... 4% 12.3M 32s 21150K .......... .......... .......... .......... .......... 4% 13.2M 32s 21200K .......... .......... .......... .......... .......... 4% 11.6M 32s 21250K .......... .......... .......... .......... .......... 4% 13.5M 32s 21300K .......... .......... .......... .......... .......... 4% 15.3M 32s 21350K .......... .......... .......... .......... .......... 4% 12.3M 32s 21400K .......... .......... .......... .......... .......... 4% 13.1M 32s 21450K .......... .......... .......... .......... .......... 4% 7.68M 32s 21500K .......... .......... .......... .......... .......... 4% 11.7M 32s 21550K .......... .......... .......... .......... .......... 4% 8.79M 32s 21600K .......... .......... .......... .......... .......... 4% 6.54M 32s 21650K .......... .......... .......... .......... .......... 4% 8.80M 32s 21700K .......... .......... .......... .......... .......... 4% 6.03M 32s 21750K .......... .......... .......... .......... .......... 4% 7.73M 32s 21800K .......... .......... .......... .......... .......... 4% 5.53M 32s 21850K .......... .......... .......... .......... .......... 4% 2.38M 33s 21900K .......... .......... .......... .......... .......... 4% 11.8M 33s 21950K .......... .......... .......... .......... .......... 4% 11.4M 33s 22000K .......... .......... .......... .......... .......... 4% 11.7M 33s 22050K .......... .......... .......... .......... .......... 4% 12.8M 33s 22100K .......... .......... .......... .......... .......... 4% 13.2M 33s 22150K .......... .......... .......... .......... .......... 4% 14.5M 33s 22200K .......... .......... .......... .......... .......... 4% 9.86M 33s 22250K .......... .......... .......... .......... .......... 4% 15.7M 33s 22300K .......... .......... .......... .......... .......... 4% 12.3M 33s 22350K .......... .......... .......... .......... .......... 4% 15.1M 33s 22400K .......... .......... .......... .......... .......... 4% 13.6M 33s 22450K .......... .......... .......... .......... .......... 4% 13.0M 33s 22500K .......... .......... .......... .......... .......... 4% 15.8M 33s 22550K .......... .......... .......... .......... .......... 4% 12.3M 33s 22600K .......... .......... .......... .......... .......... 4% 14.3M 33s 22650K .......... .......... .......... .......... .......... 4% 15.9M 33s 22700K .......... .......... .......... .......... .......... 4% 13.0M 33s 22750K .......... .......... .......... .......... .......... 4% 36.2M 33s 22800K .......... .......... .......... .......... .......... 4% 32.1M 33s 22850K .......... .......... .......... .......... .......... 4% 42.7M 33s 22900K .......... .......... .......... .......... .......... 4% 23.0M 33s 22950K .......... .......... .......... .......... .......... 4% 31.4M 33s 23000K .......... .......... .......... .......... .......... 4% 49.8M 33s 23050K .......... .......... .......... .......... .......... 4% 17.7M 32s 23100K .......... .......... .......... .......... .......... 4% 22.2M 32s 23150K .......... .......... .......... .......... .......... 4% 21.1M 32s 23200K .......... .......... .......... .......... .......... 4% 18.1M 32s 23250K .......... .......... .......... .......... .......... 4% 21.2M 32s 23300K .......... .......... .......... .......... .......... 4% 22.4M 32s 23350K .......... .......... .......... .......... .......... 4% 16.9M 32s 23400K .......... .......... .......... .......... .......... 4% 17.9M 32s 23450K .......... .......... .......... .......... .......... 4% 19.2M 32s 23500K .......... .......... .......... .......... .......... 4% 20.8M 32s 23550K .......... .......... .......... .......... .......... 4% 19.7M 32s 23600K .......... .......... .......... .......... .......... 4% 15.0M 32s 23650K .......... .......... .......... .......... .......... 4% 23.7M 32s 23700K .......... .......... .......... .......... .......... 4% 13.7M 32s 23750K .......... .......... .......... .......... .......... 4% 23.3M 32s 23800K .......... .......... .......... .......... .......... 4% 16.4M 32s 23850K .......... .......... .......... .......... .......... 4% 17.9M 32s 23900K .......... .......... .......... .......... .......... 4% 16.4M 32s 23950K .......... .......... .......... .......... .......... 4% 23.8M 32s 24000K .......... .......... .......... .......... .......... 4% 12.0M 32s 24050K .......... .......... .......... .......... .......... 4% 12.7M 32s 24100K .......... .......... .......... .......... .......... 4% 13.0M 32s 24150K .......... .......... .......... .......... .......... 4% 98.2M 32s 24200K .......... .......... .......... .......... .......... 4% 22.3M 32s 24250K .......... .......... .......... .......... .......... 4% 31.4M 32s 24300K .......... .......... .......... .......... .......... 4% 38.1M 32s 24350K .......... .......... .......... .......... .......... 4% 26.9M 32s 24400K .......... .......... .......... .......... .......... 4% 41.5M 32s 24450K .......... .......... .......... .......... .......... 4% 28.7M 32s 24500K .......... .......... .......... .......... .......... 4% 17.3M 32s 24550K .......... .......... .......... .......... .......... 4% 32.9M 32s 24600K .......... .......... .......... .......... .......... 4% 25.8M 32s 24650K .......... .......... .......... .......... .......... 4% 19.8M 32s 24700K .......... .......... .......... .......... .......... 4% 19.1M 32s 24750K .......... .......... .......... .......... .......... 4% 18.2M 32s 24800K .......... .......... .......... .......... .......... 4% 13.8M 32s 24850K .......... .......... .......... .......... .......... 4% 13.4M 32s 24900K .......... .......... .......... .......... .......... 4% 16.6M 32s 24950K .......... .......... .......... .......... .......... 4% 11.1M 32s 25000K .......... .......... .......... .......... .......... 4% 12.5M 32s 25050K .......... .......... .......... .......... .......... 4% 16.4M 32s 25100K .......... .......... .......... .......... .......... 4% 12.2M 32s 25150K .......... .......... .......... .......... .......... 4% 15.5M 32s 25200K .......... .......... .......... .......... .......... 4% 15.1M 32s 25250K .......... .......... .......... .......... .......... 4% 25.1M 32s 25300K .......... .......... .......... .......... .......... 4% 42.2M 32s 25350K .......... .......... .......... .......... .......... 4% 25.9M 32s 25400K .......... .......... .......... .......... .......... 4% 86.7M 32s 25450K .......... .......... .......... .......... .......... 5% 20.0M 32s 25500K .......... .......... .......... .......... .......... 5% 80.4M 32s 25550K .......... .......... .......... .......... .......... 5% 21.3M 32s 25600K .......... .......... .......... .......... .......... 5% 20.6M 32s 25650K .......... .......... .......... .......... .......... 5% 32.7M 31s 25700K .......... .......... .......... .......... .......... 5% 23.1M 31s 25750K .......... .......... .......... .......... .......... 5% 19.1M 31s 25800K .......... .......... .......... .......... .......... 5% 19.7M 31s 25850K .......... .......... .......... .......... .......... 5% 15.7M 31s 25900K .......... .......... .......... .......... .......... 5% 22.3M 31s 25950K .......... .......... .......... .......... .......... 5% 15.1M 31s 26000K .......... .......... .......... .......... .......... 5% 19.1M 31s 26050K .......... .......... .......... .......... .......... 5% 21.9M 31s 26100K .......... .......... .......... .......... .......... 5% 17.5M 31s 26150K .......... .......... .......... .......... .......... 5% 19.7M 31s 26200K .......... .......... .......... .......... .......... 5% 18.6M 31s 26250K .......... .......... .......... .......... .......... 5% 20.7M 31s 26300K .......... .......... .......... .......... .......... 5% 18.1M 31s 26350K .......... .......... .......... .......... .......... 5% 16.2M 31s 26400K .......... .......... .......... .......... .......... 5% 18.2M 31s 26450K .......... .......... .......... .......... .......... 5% 11.4M 31s 26500K .......... .......... .......... .......... .......... 5% 13.0M 31s 26550K .......... .......... .......... .......... .......... 5% 15.9M 31s 26600K .......... .......... .......... .......... .......... 5% 11.8M 31s 26650K .......... .......... .......... .......... .......... 5% 15.7M 31s 26700K .......... .......... .......... .......... .......... 5% 12.5M 31s 26750K .......... .......... .......... .......... .......... 5% 18.0M 31s 26800K .......... .......... .......... .......... .......... 5% 16.5M 31s 26850K .......... .......... .......... .......... .......... 5% 10.7M 31s 26900K .......... .......... .......... .......... .......... 5% 25.0M 31s 26950K .......... .......... .......... .......... .......... 5% 22.1M 31s 27000K .......... .......... .......... .......... .......... 5% 22.6M 31s 27050K .......... .......... .......... .......... .......... 5% 21.9M 31s 27100K .......... .......... .......... .......... .......... 5% 15.9M 31s 27150K .......... .......... .......... .......... .......... 5% 26.4M 31s 27200K .......... .......... .......... .......... .......... 5% 17.4M 31s 27250K .......... .......... .......... .......... .......... 5% 23.9M 31s 27300K .......... .......... .......... .......... .......... 5% 21.0M 31s 27350K .......... .......... .......... .......... .......... 5% 21.2M 31s 27400K .......... .......... .......... .......... .......... 5% 20.9M 31s 27450K .......... .......... .......... .......... .......... 5% 21.3M 31s 27500K .......... .......... .......... .......... .......... 5% 23.7M 31s 27550K .......... .......... .......... .......... .......... 5% 24.1M 31s 27600K .......... .......... .......... .......... .......... 5% 19.7M 31s 27650K .......... .......... .......... .......... .......... 5% 34.5M 31s 27700K .......... .......... .......... .......... .......... 5% 43.8M 31s 27750K .......... .......... .......... .......... .......... 5% 23.7M 31s 27800K .......... .......... .......... .......... .......... 5% 123M 31s 27850K .......... .......... .......... .......... .......... 5% 132M 31s 27900K .......... .......... .......... .......... .......... 5% 34.9M 31s 27950K .......... .......... .......... .......... .......... 5% 39.2M 31s 28000K .......... .......... .......... .......... .......... 5% 34.3M 31s 28050K .......... .......... .......... .......... .......... 5% 26.7M 31s 28100K .......... .......... .......... .......... .......... 5% 19.4M 31s 28150K .......... .......... .......... .......... .......... 5% 21.2M 31s 28200K .......... .......... .......... .......... .......... 5% 23.0M 31s 28250K .......... .......... .......... .......... .......... 5% 25.6M 31s 28300K .......... .......... .......... .......... .......... 5% 37.7M 31s 28350K .......... .......... .......... .......... .......... 5% 20.0M 31s 28400K .......... .......... .......... .......... .......... 5% 29.1M 30s 28450K .......... .......... .......... .......... .......... 5% 19.0M 30s 28500K .......... .......... .......... .......... .......... 5% 23.6M 30s 28550K .......... .......... .......... .......... .......... 5% 18.5M 30s 28600K .......... .......... .......... .......... .......... 5% 14.4M 30s 28650K .......... .......... .......... .......... .......... 5% 22.5M 30s 28700K .......... .......... .......... .......... .......... 5% 16.8M 30s 28750K .......... .......... .......... .......... .......... 5% 18.0M 30s 28800K .......... .......... .......... .......... .......... 5% 16.4M 30s 28850K .......... .......... .......... .......... .......... 5% 15.1M 30s 28900K .......... .......... .......... .......... .......... 5% 19.9M 30s 28950K .......... .......... .......... .......... .......... 5% 13.9M 30s 29000K .......... .......... .......... .......... .......... 5% 14.5M 30s 29050K .......... .......... .......... .......... .......... 5% 12.7M 30s 29100K .......... .......... .......... .......... .......... 5% 17.1M 30s 29150K .......... .......... .......... .......... .......... 5% 16.0M 30s 29200K .......... .......... .......... .......... .......... 5% 16.4M 30s 29250K .......... .......... .......... .......... .......... 5% 15.6M 30s 29300K .......... .......... .......... .......... .......... 5% 15.4M 30s 29350K .......... .......... .......... .......... .......... 5% 15.3M 30s 29400K .......... .......... .......... .......... .......... 5% 16.5M 30s 29450K .......... .......... .......... .......... .......... 5% 17.2M 30s 29500K .......... .......... .......... .......... .......... 5% 15.3M 30s 29550K .......... .......... .......... .......... .......... 5% 23.7M 30s 29600K .......... .......... .......... .......... .......... 5% 10.7M 30s 29650K .......... .......... .......... .......... .......... 5% 16.2M 30s 29700K .......... .......... .......... .......... .......... 5% 12.3M 30s 29750K .......... .......... .......... .......... .......... 5% 10.9M 30s 29800K .......... .......... .......... .......... .......... 5% 15.2M 30s 29850K .......... .......... .......... .......... .......... 5% 13.2M 30s 29900K .......... .......... .......... .......... .......... 5% 15.8M 30s 29950K .......... .......... .......... .......... .......... 5% 18.9M 30s 30000K .......... .......... .......... .......... .......... 5% 15.9M 30s 30050K .......... .......... .......... .......... .......... 5% 15.6M 30s 30100K .......... .......... .......... .......... .......... 5% 15.8M 30s 30150K .......... .......... .......... .......... .......... 5% 18.1M 30s 30200K .......... .......... .......... .......... .......... 5% 15.6M 30s 30250K .......... .......... .......... .......... .......... 5% 14.1M 30s 30300K .......... .......... .......... .......... .......... 5% 19.0M 30s 30350K .......... .......... .......... .......... .......... 5% 12.9M 30s 30400K .......... .......... .......... .......... .......... 5% 19.0M 30s 30450K .......... .......... .......... .......... .......... 5% 12.4M 30s 30500K .......... .......... .......... .......... .......... 5% 22.5M 30s 30550K .......... .......... .......... .......... .......... 6% 16.5M 30s 30600K .......... .......... .......... .......... .......... 6% 12.6M 30s 30650K .......... .......... .......... .......... .......... 6% 16.8M 30s 30700K .......... .......... .......... .......... .......... 6% 14.2M 30s 30750K .......... .......... .......... .......... .......... 6% 18.9M 30s 30800K .......... .......... .......... .......... .......... 6% 15.3M 30s 30850K .......... .......... .......... .......... .......... 6% 15.3M 30s 30900K .......... .......... .......... .......... .......... 6% 18.1M 30s 30950K .......... .......... .......... .......... .......... 6% 14.7M 30s 31000K .......... .......... .......... .......... .......... 6% 16.5M 30s 31050K .......... .......... .......... .......... .......... 6% 18.9M 30s 31100K .......... .......... .......... .......... .......... 6% 13.7M 30s 31150K .......... .......... .......... .......... .......... 6% 12.7M 30s 31200K .......... .......... .......... .......... .......... 6% 27.0M 30s 31250K .......... .......... .......... .......... .......... 6% 27.8M 30s 31300K .......... .......... .......... .......... .......... 6% 25.1M 30s 31350K .......... .......... .......... .......... .......... 6% 22.8M 30s 31400K .......... .......... .......... .......... .......... 6% 22.0M 30s 31450K .......... .......... .......... .......... .......... 6% 8.77M 30s 31500K .......... .......... .......... .......... .......... 6% 7.49M 30s 31550K .......... .......... .......... .......... .......... 6% 6.57M 30s 31600K .......... .......... .......... .......... .......... 6% 6.30M 30s 31650K .......... .......... .......... .......... .......... 6% 5.96M 30s 31700K .......... .......... .......... .......... .......... 6% 10.3M 30s 31750K .......... .......... .......... .......... .......... 6% 31.5M 30s 31800K .......... .......... .......... .......... .......... 6% 27.5M 30s 31850K .......... .......... .......... .......... .......... 6% 30.9M 30s 31900K .......... .......... .......... .......... .......... 6% 35.4M 30s 31950K .......... .......... .......... .......... .......... 6% 19.6M 30s 32000K .......... .......... .......... .......... .......... 6% 33.9M 30s 32050K .......... .......... .......... .......... .......... 6% 25.7M 30s 32100K .......... .......... .......... .......... .......... 6% 23.6M 30s 32150K .......... .......... .......... .......... .......... 6% 23.7M 30s 32200K .......... .......... .......... .......... .......... 6% 23.5M 30s 32250K .......... .......... .......... .......... .......... 6% 31.2M 30s 32300K .......... .......... .......... .......... .......... 6% 20.1M 30s 32350K .......... .......... .......... .......... .......... 6% 16.7M 30s 32400K .......... .......... .......... .......... .......... 6% 17.3M 30s 32450K .......... .......... .......... .......... .......... 6% 18.2M 30s 32500K .......... .......... .......... .......... .......... 6% 20.8M 30s 32550K .......... .......... .......... .......... .......... 6% 19.0M 30s 32600K .......... .......... .......... .......... .......... 6% 16.5M 30s 32650K .......... .......... .......... .......... .......... 6% 22.1M 30s 32700K .......... .......... .......... .......... .......... 6% 16.7M 30s 32750K .......... .......... .......... .......... .......... 6% 14.7M 30s 32800K .......... .......... .......... .......... .......... 6% 13.8M 30s 32850K .......... .......... .......... .......... .......... 6% 10.3M 30s 32900K .......... .......... .......... .......... .......... 6% 15.9M 30s 32950K .......... .......... .......... .......... .......... 6% 9.10M 30s 33000K .......... .......... .......... .......... .......... 6% 11.8M 30s 33050K .......... .......... .......... .......... .......... 6% 15.6M 30s 33100K .......... .......... .......... .......... .......... 6% 11.6M 30s 33150K .......... .......... .......... .......... .......... 6% 13.1M 30s 33200K .......... .......... .......... .......... .......... 6% 9.20M 30s 33250K .......... .......... .......... .......... .......... 6% 13.3M 30s 33300K .......... .......... .......... .......... .......... 6% 16.6M 30s 33350K .......... .......... .......... .......... .......... 6% 5.92M 30s 33400K .......... .......... .......... .......... .......... 6% 8.76M 30s 33450K .......... .......... .......... .......... .......... 6% 8.88M 30s 33500K .......... .......... .......... .......... .......... 6% 8.69M 30s 33550K .......... .......... .......... .......... .......... 6% 8.40M 30s 33600K .......... .......... .......... .......... .......... 6% 4.41M 31s 33650K .......... .......... .......... .......... .......... 6% 9.33M 31s 33700K .......... .......... .......... .......... .......... 6% 8.67M 31s 33750K .......... .......... .......... .......... .......... 6% 10.1M 31s 33800K .......... .......... .......... .......... .......... 6% 10.0M 31s 33850K .......... .......... .......... .......... .......... 6% 8.58M 31s 33900K .......... .......... .......... .......... .......... 6% 9.31M 31s 33950K .......... .......... .......... .......... .......... 6% 13.6M 31s 34000K .......... .......... .......... .......... .......... 6% 26.9M 31s 34050K .......... .......... .......... .......... .......... 6% 21.5M 31s 34100K .......... .......... .......... .......... .......... 6% 16.5M 31s 34150K .......... .......... .......... .......... .......... 6% 25.2M 31s 34200K .......... .......... .......... .......... .......... 6% 13.1M 31s 34250K .......... .......... .......... .......... .......... 6% 17.2M 31s 34300K .......... .......... .......... .......... .......... 6% 11.2M 31s 34350K .......... .......... .......... .......... .......... 6% 13.1M 31s 34400K .......... .......... .......... .......... .......... 6% 13.9M 31s 34450K .......... .......... .......... .......... .......... 6% 11.3M 31s 34500K .......... .......... .......... .......... .......... 6% 12.5M 31s 34550K .......... .......... .......... .......... .......... 6% 12.6M 31s 34600K .......... .......... .......... .......... .......... 6% 10.5M 31s 34650K .......... .......... .......... .......... .......... 6% 7.92M 31s 34700K .......... .......... .......... .......... .......... 6% 4.49M 31s 34750K .......... .......... .......... .......... .......... 6% 4.54M 31s 34800K .......... .......... .......... .......... .......... 6% 5.15M 31s 34850K .......... .......... .......... .......... .......... 6% 8.23M 31s 34900K .......... .......... .......... .......... .......... 6% 9.99M 31s 34950K .......... .......... .......... .......... .......... 6% 8.70M 31s 35000K .......... .......... .......... .......... .......... 6% 12.5M 31s 35050K .......... .......... .......... .......... .......... 6% 10.1M 31s 35100K .......... .......... .......... .......... .......... 6% 8.71M 31s 35150K .......... .......... .......... .......... .......... 6% 10.2M 31s 35200K .......... .......... .......... .......... .......... 6% 10.2M 31s 35250K .......... .......... .......... .......... .......... 6% 18.1M 31s 35300K .......... .......... .......... .......... .......... 6% 30.3M 31s 35350K .......... .......... .......... .......... .......... 6% 24.3M 31s 35400K .......... .......... .......... .......... .......... 6% 17.0M 31s 35450K .......... .......... .......... .......... .......... 6% 20.4M 31s 35500K .......... .......... .......... .......... .......... 6% 18.2M 31s 35550K .......... .......... .......... .......... .......... 6% 22.2M 31s 35600K .......... .......... .......... .......... .......... 6% 18.0M 31s 35650K .......... .......... .......... .......... .......... 7% 23.8M 31s 35700K .......... .......... .......... .......... .......... 7% 20.7M 31s 35750K .......... .......... .......... .......... .......... 7% 19.0M 31s 35800K .......... .......... .......... .......... .......... 7% 23.9M 31s 35850K .......... .......... .......... .......... .......... 7% 15.3M 31s 35900K .......... .......... .......... .......... .......... 7% 20.0M 31s 35950K .......... .......... .......... .......... .......... 7% 13.4M 31s 36000K .......... .......... .......... .......... .......... 7% 17.4M 31s 36050K .......... .......... .......... .......... .......... 7% 15.8M 31s 36100K .......... .......... .......... .......... .......... 7% 10.2M 31s 36150K .......... .......... .......... .......... .......... 7% 15.7M 31s 36200K .......... .......... .......... .......... .......... 7% 12.8M 31s 36250K .......... .......... .......... .......... .......... 7% 15.3M 31s 36300K .......... .......... .......... .......... .......... 7% 14.1M 31s 36350K .......... .......... .......... .......... .......... 7% 11.9M 31s 36400K .......... .......... .......... .......... .......... 7% 41.5M 31s 36450K .......... .......... .......... .......... .......... 7% 16.7M 31s 36500K .......... .......... .......... .......... .......... 7% 498M 31s 36550K .......... .......... .......... .......... .......... 7% 31.5M 31s 36600K .......... .......... .......... .......... .......... 7% 21.7M 31s 36650K .......... .......... .......... .......... .......... 7% 21.5M 31s 36700K .......... .......... .......... .......... .......... 7% 17.4M 31s 36750K .......... .......... .......... .......... .......... 7% 15.9M 31s 36800K .......... .......... .......... .......... .......... 7% 21.3M 31s 36850K .......... .......... .......... .......... .......... 7% 14.1M 31s 36900K .......... .......... .......... .......... .......... 7% 17.1M 31s 36950K .......... .......... .......... .......... .......... 7% 13.6M 31s 37000K .......... .......... .......... .......... .......... 7% 14.1M 31s 37050K .......... .......... .......... .......... .......... 7% 14.6M 31s 37100K .......... .......... .......... .......... .......... 7% 13.1M 31s 37150K .......... .......... .......... .......... .......... 7% 11.2M 31s 37200K .......... .......... .......... .......... .......... 7% 12.6M 31s 37250K .......... .......... .......... .......... .......... 7% 15.9M 31s 37300K .......... .......... .......... .......... .......... 7% 15.9M 31s 37350K .......... .......... .......... .......... .......... 7% 10.5M 31s 37400K .......... .......... .......... .......... .......... 7% 12.7M 31s 37450K .......... .......... .......... .......... .......... 7% 9.09M 31s 37500K .......... .......... .......... .......... .......... 7% 12.3M 31s 37550K .......... .......... .......... .......... .......... 7% 13.2M 31s 37600K .......... .......... .......... .......... .......... 7% 12.2M 31s 37650K .......... .......... .......... .......... .......... 7% 19.3M 31s 37700K .......... .......... .......... .......... .......... 7% 42.5M 31s 37750K .......... .......... .......... .......... .......... 7% 71.0M 31s 37800K .......... .......... .......... .......... .......... 7% 32.3M 31s 37850K .......... .......... .......... .......... .......... 7% 30.3M 31s 37900K .......... .......... .......... .......... .......... 7% 80.0M 31s 37950K .......... .......... .......... .......... .......... 7% 28.9M 31s 38000K .......... .......... .......... .......... .......... 7% 42.6M 31s 38050K .......... .......... .......... .......... .......... 7% 25.2M 31s 38100K .......... .......... .......... .......... .......... 7% 38.8M 31s 38150K .......... .......... .......... .......... .......... 7% 37.9M 31s 38200K .......... .......... .......... .......... .......... 7% 23.4M 31s 38250K .......... .......... .......... .......... .......... 7% 23.8M 30s 38300K .......... .......... .......... .......... .......... 7% 42.6M 30s 38350K .......... .......... .......... .......... .......... 7% 19.9M 30s 38400K .......... .......... .......... .......... .......... 7% 23.2M 30s 38450K .......... .......... .......... .......... .......... 7% 22.7M 30s 38500K .......... .......... .......... .......... .......... 7% 22.4M 30s 38550K .......... .......... .......... .......... .......... 7% 20.1M 30s 38600K .......... .......... .......... .......... .......... 7% 17.7M 30s 38650K .......... .......... .......... .......... .......... 7% 15.1M 30s 38700K .......... .......... .......... .......... .......... 7% 17.3M 30s 38750K .......... .......... .......... .......... .......... 7% 14.6M 30s 38800K .......... .......... .......... .......... .......... 7% 13.5M 30s 38850K .......... .......... .......... .......... .......... 7% 12.6M 30s 38900K .......... .......... .......... .......... .......... 7% 15.3M 30s 38950K .......... .......... .......... .......... .......... 7% 12.7M 30s 39000K .......... .......... .......... .......... .......... 7% 14.2M 30s 39050K .......... .......... .......... .......... .......... 7% 15.8M 30s 39100K .......... .......... .......... .......... .......... 7% 11.1M 30s 39150K .......... .......... .......... .......... .......... 7% 8.87M 30s 39200K .......... .......... .......... .......... .......... 7% 12.2M 30s 39250K .......... .......... .......... .......... .......... 7% 17.5M 30s 39300K .......... .......... .......... .......... .......... 7% 19.5M 30s 39350K .......... .......... .......... .......... .......... 7% 10.4M 30s 39400K .......... .......... .......... .......... .......... 7% 13.9M 30s 39450K .......... .......... .......... .......... .......... 7% 17.2M 30s 39500K .......... .......... .......... .......... .......... 7% 12.7M 30s 39550K .......... .......... .......... .......... .......... 7% 22.0M 30s 39600K .......... .......... .......... .......... .......... 7% 14.0M 30s 39650K .......... .......... .......... .......... .......... 7% 13.6M 30s 39700K .......... .......... .......... .......... .......... 7% 16.8M 30s 39750K .......... .......... .......... .......... .......... 7% 22.2M 30s 39800K .......... .......... .......... .......... .......... 7% 21.4M 30s 39850K .......... .......... .......... .......... .......... 7% 15.6M 30s 39900K .......... .......... .......... .......... .......... 7% 22.4M 30s 39950K .......... .......... .......... .......... .......... 7% 21.0M 30s 40000K .......... .......... .......... .......... .......... 7% 19.8M 30s 40050K .......... .......... .......... .......... .......... 7% 18.8M 30s 40100K .......... .......... .......... .......... .......... 7% 9.46M 30s 40150K .......... .......... .......... .......... .......... 7% 12.0M 30s 40200K .......... .......... .......... .......... .......... 7% 11.9M 30s 40250K .......... .......... .......... .......... .......... 7% 21.9M 30s 40300K .......... .......... .......... .......... .......... 7% 15.0M 30s 40350K .......... .......... .......... .......... .......... 7% 14.3M 30s 40400K .......... .......... .......... .......... .......... 7% 18.1M 30s 40450K .......... .......... .......... .......... .......... 7% 11.5M 30s 40500K .......... .......... .......... .......... .......... 7% 16.5M 30s 40550K .......... .......... .......... .......... .......... 7% 15.8M 30s 40600K .......... .......... .......... .......... .......... 7% 16.4M 30s 40650K .......... .......... .......... .......... .......... 7% 18.1M 30s 40700K .......... .......... .......... .......... .......... 7% 13.7M 30s 40750K .......... .......... .......... .......... .......... 8% 16.7M 30s 40800K .......... .......... .......... .......... .......... 8% 20.1M 30s 40850K .......... .......... .......... .......... .......... 8% 15.0M 30s 40900K .......... .......... .......... .......... .......... 8% 20.9M 30s 40950K .......... .......... .......... .......... .......... 8% 14.2M 30s 41000K .......... .......... .......... .......... .......... 8% 16.6M 30s 41050K .......... .......... .......... .......... .......... 8% 24.4M 30s 41100K .......... .......... .......... .......... .......... 8% 21.2M 30s 41150K .......... .......... .......... .......... .......... 8% 23.7M 30s 41200K .......... .......... .......... .......... .......... 8% 18.1M 30s 41250K .......... .......... .......... .......... .......... 8% 23.5M 30s 41300K .......... .......... .......... .......... .......... 8% 22.5M 30s 41350K .......... .......... .......... .......... .......... 8% 22.1M 30s 41400K .......... .......... .......... .......... .......... 8% 25.3M 30s 41450K .......... .......... .......... .......... .......... 8% 22.0M 30s 41500K .......... .......... .......... .......... .......... 8% 18.0M 30s 41550K .......... .......... .......... .......... .......... 8% 23.9M 30s 41600K .......... .......... .......... .......... .......... 8% 15.3M 30s 41650K .......... .......... .......... .......... .......... 8% 13.2M 30s 41700K .......... .......... .......... .......... .......... 8% 6.89M 30s 41750K .......... .......... .......... .......... .......... 8% 6.25M 30s 41800K .......... .......... .......... .......... .......... 8% 7.78M 30s 41850K .......... .......... .......... .......... .......... 8% 7.01M 30s 41900K .......... .......... .......... .......... .......... 8% 12.3M 30s 41950K .......... .......... .......... .......... .......... 8% 20.2M 30s 42000K .......... .......... .......... .......... .......... 8% 37.2M 30s 42050K .......... .......... .......... .......... .......... 8% 37.2M 30s 42100K .......... .......... .......... .......... .......... 8% 25.1M 30s 42150K .......... .......... .......... .......... .......... 8% 37.1M 30s 42200K .......... .......... .......... .......... .......... 8% 34.4M 30s 42250K .......... .......... .......... .......... .......... 8% 42.5M 30s 42300K .......... .......... .......... .......... .......... 8% 31.5M 30s 42350K .......... .......... .......... .......... .......... 8% 30.1M 30s 42400K .......... .......... .......... .......... .......... 8% 51.3M 30s 42450K .......... .......... .......... .......... .......... 8% 24.7M 30s 42500K .......... .......... .......... .......... .......... 8% 27.8M 30s 42550K .......... .......... .......... .......... .......... 8% 27.3M 30s 42600K .......... .......... .......... .......... .......... 8% 17.0M 30s 42650K .......... .......... .......... .......... .......... 8% 22.5M 30s 42700K .......... .......... .......... .......... .......... 8% 18.8M 30s 42750K .......... .......... .......... .......... .......... 8% 29.3M 30s 42800K .......... .......... .......... .......... .......... 8% 24.0M 30s 42850K .......... .......... .......... .......... .......... 8% 16.5M 30s 42900K .......... .......... .......... .......... .......... 8% 24.0M 30s 42950K .......... .......... .......... .......... .......... 8% 17.4M 30s 43000K .......... .......... .......... .......... .......... 8% 23.4M 30s 43050K .......... .......... .......... .......... .......... 8% 18.0M 30s 43100K .......... .......... .......... .......... .......... 8% 15.7M 30s 43150K .......... .......... .......... .......... .......... 8% 14.7M 30s 43200K .......... .......... .......... .......... .......... 8% 12.7M 30s 43250K .......... .......... .......... .......... .......... 8% 17.0M 30s 43300K .......... .......... .......... .......... .......... 8% 12.8M 30s 43350K .......... .......... .......... .......... .......... 8% 16.5M 30s 43400K .......... .......... .......... .......... .......... 8% 13.4M 30s 43450K .......... .......... .......... .......... .......... 8% 7.62M 30s 43500K .......... .......... .......... .......... .......... 8% 9.22M 30s 43550K .......... .......... .......... .......... .......... 8% 10.5M 30s 43600K .......... .......... .......... .......... .......... 8% 7.30M 30s 43650K .......... .......... .......... .......... .......... 8% 8.27M 30s 43700K .......... .......... .......... .......... .......... 8% 8.70M 30s 43750K .......... .......... .......... .......... .......... 8% 9.92M 30s 43800K .......... .......... .......... .......... .......... 8% 13.9M 30s 43850K .......... .......... .......... .......... .......... 8% 9.77M 30s 43900K .......... .......... .......... .......... .......... 8% 6.46M 30s 43950K .......... .......... .......... .......... .......... 8% 7.42M 30s 44000K .......... .......... .......... .......... .......... 8% 8.50M 30s 44050K .......... .......... .......... .......... .......... 8% 8.06M 30s 44100K .......... .......... .......... .......... .......... 8% 6.13M 30s 44150K .......... .......... .......... .......... .......... 8% 7.92M 30s 44200K .......... .......... .......... .......... .......... 8% 12.4M 30s 44250K .......... .......... .......... .......... .......... 8% 13.2M 30s 44300K .......... .......... .......... .......... .......... 8% 13.6M 30s 44350K .......... .......... .......... .......... .......... 8% 11.9M 30s 44400K .......... .......... .......... .......... .......... 8% 13.3M 30s 44450K .......... .......... .......... .......... .......... 8% 9.47M 30s 44500K .......... .......... .......... .......... .......... 8% 10.3M 30s 44550K .......... .......... .......... .......... .......... 8% 9.69M 30s 44600K .......... .......... .......... .......... .......... 8% 11.4M 30s 44650K .......... .......... .......... .......... .......... 8% 11.6M 30s 44700K .......... .......... .......... .......... .......... 8% 10.6M 30s 44750K .......... .......... .......... .......... .......... 8% 12.6M 30s 44800K .......... .......... .......... .......... .......... 8% 28.9M 30s 44850K .......... .......... .......... .......... .......... 8% 22.4M 30s 44900K .......... .......... .......... .......... .......... 8% 46.2M 30s 44950K .......... .......... .......... .......... .......... 8% 31.5M 30s 45000K .......... .......... .......... .......... .......... 8% 28.4M 30s 45050K .......... .......... .......... .......... .......... 8% 26.5M 30s 45100K .......... .......... .......... .......... .......... 8% 23.7M 30s 45150K .......... .......... .......... .......... .......... 8% 27.3M 30s 45200K .......... .......... .......... .......... .......... 8% 22.5M 30s 45250K .......... .......... .......... .......... .......... 8% 31.5M 30s 45300K .......... .......... .......... .......... .......... 8% 21.4M 30s 45350K .......... .......... .......... .......... .......... 8% 18.4M 30s 45400K .......... .......... .......... .......... .......... 8% 17.3M 30s 45450K .......... .......... .......... .......... .......... 8% 15.9M 30s 45500K .......... .......... .......... .......... .......... 8% 17.2M 30s 45550K .......... .......... .......... .......... .......... 8% 18.9M 30s 45600K .......... .......... .......... .......... .......... 8% 12.6M 30s 45650K .......... .......... .......... .......... .......... 8% 23.5M 30s 45700K .......... .......... .......... .......... .......... 8% 15.1M 30s 45750K .......... .......... .......... .......... .......... 8% 19.4M 30s 45800K .......... .......... .......... .......... .......... 8% 18.9M 30s 45850K .......... .......... .......... .......... .......... 9% 15.7M 30s 45900K .......... .......... .......... .......... .......... 9% 21.7M 30s 45950K .......... .......... .......... .......... .......... 9% 23.5M 30s 46000K .......... .......... .......... .......... .......... 9% 41.2M 30s 46050K .......... .......... .......... .......... .......... 9% 17.9M 30s 46100K .......... .......... .......... .......... .......... 9% 456M 30s 46150K .......... .......... .......... .......... .......... 9% 537M 30s 46200K .......... .......... .......... .......... .......... 9% 23.0M 30s 46250K .......... .......... .......... .......... .......... 9% 47.9M 30s 46300K .......... .......... .......... .......... .......... 9% 344M 30s 46350K .......... .......... .......... .......... .......... 9% 23.6M 30s 46400K .......... .......... .......... .......... .......... 9% 39.8M 30s 46450K .......... .......... .......... .......... .......... 9% 29.1M 30s 46500K .......... .......... .......... .......... .......... 9% 34.2M 30s 46550K .......... .......... .......... .......... .......... 9% 36.8M 30s 46600K .......... .......... .......... .......... .......... 9% 20.3M 30s 46650K .......... .......... .......... .......... .......... 9% 42.5M 30s 46700K .......... .......... .......... .......... .......... 9% 27.4M 30s 46750K .......... .......... .......... .......... .......... 9% 28.9M 30s 46800K .......... .......... .......... .......... .......... 9% 24.2M 30s 46850K .......... .......... .......... .......... .......... 9% 25.5M 30s 46900K .......... .......... .......... .......... .......... 9% 19.9M 30s 46950K .......... .......... .......... .......... .......... 9% 21.2M 30s 47000K .......... .......... .......... .......... .......... 9% 27.3M 30s 47050K .......... .......... .......... .......... .......... 9% 19.5M 30s 47100K .......... .......... .......... .......... .......... 9% 20.5M 30s 47150K .......... .......... .......... .......... .......... 9% 19.1M 30s 47200K .......... .......... .......... .......... .......... 9% 8.49M 30s 47250K .......... .......... .......... .......... .......... 9% 12.7M 30s 47300K .......... .......... .......... .......... .......... 9% 9.95M 30s 47350K .......... .......... .......... .......... .......... 9% 9.35M 30s 47400K .......... .......... .......... .......... .......... 9% 11.3M 30s 47450K .......... .......... .......... .......... .......... 9% 21.4M 30s 47500K .......... .......... .......... .......... .......... 9% 15.2M 30s 47550K .......... .......... .......... .......... .......... 9% 54.9M 30s 47600K .......... .......... .......... .......... .......... 9% 25.6M 30s 47650K .......... .......... .......... .......... .......... 9% 24.9M 30s 47700K .......... .......... .......... .......... .......... 9% 19.8M 30s 47750K .......... .......... .......... .......... .......... 9% 34.5M 29s 47800K .......... .......... .......... .......... .......... 9% 28.6M 29s 47850K .......... .......... .......... .......... .......... 9% 23.8M 29s 47900K .......... .......... .......... .......... .......... 9% 32.3M 29s 47950K .......... .......... .......... .......... .......... 9% 34.2M 29s 48000K .......... .......... .......... .......... .......... 9% 33.8M 29s 48050K .......... .......... .......... .......... .......... 9% 25.3M 29s 48100K .......... .......... .......... .......... .......... 9% 34.9M 29s 48150K .......... .......... .......... .......... .......... 9% 26.5M 29s 48200K .......... .......... .......... .......... .......... 9% 40.5M 29s 48250K .......... .......... .......... .......... .......... 9% 29.2M 29s 48300K .......... .......... .......... .......... .......... 9% 33.1M 29s 48350K .......... .......... .......... .......... .......... 9% 30.3M 29s 48400K .......... .......... .......... .......... .......... 9% 28.7M 29s 48450K .......... .......... .......... .......... .......... 9% 33.4M 29s 48500K .......... .......... .......... .......... .......... 9% 33.4M 29s 48550K .......... .......... .......... .......... .......... 9% 34.9M 29s 48600K .......... .......... .......... .......... .......... 9% 25.2M 29s 48650K .......... .......... .......... .......... .......... 9% 391M 29s 48700K .......... .......... .......... .......... .......... 9% 28.2M 29s 48750K .......... .......... .......... .......... .......... 9% 52.9M 29s 48800K .......... .......... .......... .......... .......... 9% 47.8M 29s 48850K .......... .......... .......... .......... .......... 9% 21.1M 29s 48900K .......... .......... .......... .......... .......... 9% 76.7M 29s 48950K .......... .......... .......... .......... .......... 9% 21.2M 29s 49000K .......... .......... .......... .......... .......... 9% 21.2M 29s 49050K .......... .......... .......... .......... .......... 9% 23.3M 29s 49100K .......... .......... .......... .......... .......... 9% 22.1M 29s 49150K .......... .......... .......... .......... .......... 9% 28.3M 29s 49200K .......... .......... .......... .......... .......... 9% 18.2M 29s 49250K .......... .......... .......... .......... .......... 9% 30.8M 29s 49300K .......... .......... .......... .......... .......... 9% 23.9M 29s 49350K .......... .......... .......... .......... .......... 9% 24.3M 29s 49400K .......... .......... .......... .......... .......... 9% 25.6M 29s 49450K .......... .......... .......... .......... .......... 9% 22.4M 29s 49500K .......... .......... .......... .......... .......... 9% 31.8M 29s 49550K .......... .......... .......... .......... .......... 9% 26.0M 29s 49600K .......... .......... .......... .......... .......... 9% 24.9M 29s 49650K .......... .......... .......... .......... .......... 9% 25.4M 29s 49700K .......... .......... .......... .......... .......... 9% 18.1M 29s 49750K .......... .......... .......... .......... .......... 9% 42.0M 29s 49800K .......... .......... .......... .......... .......... 9% 23.6M 29s 49850K .......... .......... .......... .......... .......... 9% 14.5M 29s 49900K .......... .......... .......... .......... .......... 9% 21.2M 29s 49950K .......... .......... .......... .......... .......... 9% 19.0M 29s 50000K .......... .......... .......... .......... .......... 9% 18.9M 29s 50050K .......... .......... .......... .......... .......... 9% 18.3M 29s 50100K .......... .......... .......... .......... .......... 9% 18.2M 29s 50150K .......... .......... .......... .......... .......... 9% 22.4M 29s 50200K .......... .......... .......... .......... .......... 9% 19.5M 29s 50250K .......... .......... .......... .......... .......... 9% 20.1M 29s 50300K .......... .......... .......... .......... .......... 9% 18.5M 29s 50350K .......... .......... .......... .......... .......... 9% 17.6M 29s 50400K .......... .......... .......... .......... .......... 9% 23.8M 29s 50450K .......... .......... .......... .......... .......... 9% 12.5M 29s 50500K .......... .......... .......... .......... .......... 9% 11.5M 29s 50550K .......... .......... .......... .......... .......... 9% 14.1M 29s 50600K .......... .......... .......... .......... .......... 9% 12.9M 29s 50650K .......... .......... .......... .......... .......... 9% 13.8M 29s 50700K .......... .......... .......... .......... .......... 9% 10.1M 29s 50750K .......... .......... .......... .......... .......... 9% 12.4M 29s 50800K .......... .......... .......... .......... .......... 9% 11.2M 29s 50850K .......... .......... .......... .......... .......... 9% 12.3M 29s 50900K .......... .......... .......... .......... .......... 9% 12.3M 29s 50950K .......... .......... .......... .......... .......... 10% 12.9M 29s 51000K .......... .......... .......... .......... .......... 10% 18.1M 29s 51050K .......... .......... .......... .......... .......... 10% 17.3M 29s 51100K .......... .......... .......... .......... .......... 10% 14.5M 29s 51150K .......... .......... .......... .......... .......... 10% 19.0M 29s 51200K .......... .......... .......... .......... .......... 10% 12.0M 29s 51250K .......... .......... .......... .......... .......... 10% 14.1M 29s 51300K .......... .......... .......... .......... .......... 10% 12.7M 29s 51350K .......... .......... .......... .......... .......... 10% 12.5M 29s 51400K .......... .......... .......... .......... .......... 10% 16.6M 29s 51450K .......... .......... .......... .......... .......... 10% 17.3M 29s 51500K .......... .......... .......... .......... .......... 10% 38.1M 29s 51550K .......... .......... .......... .......... .......... 10% 23.3M 29s 51600K .......... .......... .......... .......... .......... 10% 208M 29s 51650K .......... .......... .......... .......... .......... 10% 22.2M 29s 51700K .......... .......... .......... .......... .......... 10% 78.4M 29s 51750K .......... .......... .......... .......... .......... 10% 29.3M 29s 51800K .......... .......... .......... .......... .......... 10% 23.6M 29s 51850K .......... .......... .......... .......... .......... 10% 18.1M 29s 51900K .......... .......... .......... .......... .......... 10% 22.3M 29s 51950K .......... .......... .......... .......... .......... 10% 18.9M 29s 52000K .......... .......... .......... .......... .......... 10% 19.0M 29s 52050K .......... .......... .......... .......... .......... 10% 16.5M 29s 52100K .......... .......... .......... .......... .......... 10% 15.8M 29s 52150K .......... .......... .......... .......... .......... 10% 20.6M 29s 52200K .......... .......... .......... .......... .......... 10% 11.8M 29s 52250K .......... .......... .......... .......... .......... 10% 22.9M 29s 52300K .......... .......... .......... .......... .......... 10% 19.8M 29s 52350K .......... .......... .......... .......... .......... 10% 13.7M 29s 52400K .......... .......... .......... .......... .......... 10% 16.0M 29s 52450K .......... .......... .......... .......... .......... 10% 13.0M 29s 52500K .......... .......... .......... .......... .......... 10% 14.2M 29s 52550K .......... .......... .......... .......... .......... 10% 15.8M 29s 52600K .......... .......... .......... .......... .......... 10% 15.7M 29s 52650K .......... .......... .......... .......... .......... 10% 17.2M 29s 52700K .......... .......... .......... .......... .......... 10% 12.7M 29s 52750K .......... .......... .......... .......... .......... 10% 10.3M 29s 52800K .......... .......... .......... .......... .......... 10% 25.5M 29s 52850K .......... .......... .......... .......... .......... 10% 13.1M 29s 52900K .......... .......... .......... .......... .......... 10% 11.8M 29s 52950K .......... .......... .......... .......... .......... 10% 25.8M 29s 53000K .......... .......... .......... .......... .......... 10% 16.0M 29s 53050K .......... .......... .......... .......... .......... 10% 16.6M 29s 53100K .......... .......... .......... .......... .......... 10% 16.6M 29s 53150K .......... .......... .......... .......... .......... 10% 16.0M 29s 53200K .......... .......... .......... .......... .......... 10% 14.4M 29s 53250K .......... .......... .......... .......... .......... 10% 22.2M 28s 53300K .......... .......... .......... .......... .......... 10% 20.7M 28s 53350K .......... .......... .......... .......... .......... 10% 13.9M 28s 53400K .......... .......... .......... .......... .......... 10% 15.7M 28s 53450K .......... .......... .......... .......... .......... 10% 13.3M 28s 53500K .......... .......... .......... .......... .......... 10% 15.2M 28s 53550K .......... .......... .......... .......... .......... 10% 13.9M 28s 53600K .......... .......... .......... .......... .......... 10% 11.6M 28s 53650K .......... .......... .......... .......... .......... 10% 15.7M 28s 53700K .......... .......... .......... .......... .......... 10% 11.5M 28s 53750K .......... .......... .......... .......... .......... 10% 17.5M 28s 53800K .......... .......... .......... .......... .......... 10% 13.5M 28s 53850K .......... .......... .......... .......... .......... 10% 14.0M 28s 53900K .......... .......... .......... .......... .......... 10% 22.4M 28s 53950K .......... .......... .......... .......... .......... 10% 19.4M 28s 54000K .......... .......... .......... .......... .......... 10% 479M 28s 54050K .......... .......... .......... .......... .......... 10% 26.0M 28s 54100K .......... .......... .......... .......... .......... 10% 34.6M 28s 54150K .......... .......... .......... .......... .......... 10% 25.5M 28s 54200K .......... .......... .......... .......... .......... 10% 15.1M 28s 54250K .......... .......... .......... .......... .......... 10% 13.8M 28s 54300K .......... .......... .......... .......... .......... 10% 10.6M 28s 54350K .......... .......... .......... .......... .......... 10% 9.04M 28s 54400K .......... .......... .......... .......... .......... 10% 11.1M 28s 54450K .......... .......... .......... .......... .......... 10% 10.6M 28s 54500K .......... .......... .......... .......... .......... 10% 13.1M 28s 54550K .......... .......... .......... .......... .......... 10% 11.0M 28s 54600K .......... .......... .......... .......... .......... 10% 11.9M 28s 54650K .......... .......... .......... .......... .......... 10% 17.3M 28s 54700K .......... .......... .......... .......... .......... 10% 31.2M 28s 54750K .......... .......... .......... .......... .......... 10% 34.6M 28s 54800K .......... .......... .......... .......... .......... 10% 23.0M 28s 54850K .......... .......... .......... .......... .......... 10% 22.8M 28s 54900K .......... .......... .......... .......... .......... 10% 173M 28s 54950K .......... .......... .......... .......... .......... 10% 15.8M 28s 55000K .......... .......... .......... .......... .......... 10% 23.6M 28s 55050K .......... .......... .......... .......... .......... 10% 21.3M 28s 55100K .......... .......... .......... .......... .......... 10% 17.7M 28s 55150K .......... .......... .......... .......... .......... 10% 21.0M 28s 55200K .......... .......... .......... .......... .......... 10% 19.7M 28s 55250K .......... .......... .......... .......... .......... 10% 23.2M 28s 55300K .......... .......... .......... .......... .......... 10% 21.0M 28s 55350K .......... .......... .......... .......... .......... 10% 18.0M 28s 55400K .......... .......... .......... .......... .......... 10% 22.0M 28s 55450K .......... .......... .......... .......... .......... 10% 17.9M 28s 55500K .......... .......... .......... .......... .......... 10% 20.0M 28s 55550K .......... .......... .......... .......... .......... 10% 30.9M 28s 55600K .......... .......... .......... .......... .......... 10% 20.3M 28s 55650K .......... .......... .......... .......... .......... 10% 25.1M 28s 55700K .......... .......... .......... .......... .......... 10% 21.8M 28s 55750K .......... .......... .......... .......... .......... 10% 19.7M 28s 55800K .......... .......... .......... .......... .......... 10% 28.9M 28s 55850K .......... .......... .......... .......... .......... 10% 32.7M 28s 55900K .......... .......... .......... .......... .......... 10% 45.7M 28s 55950K .......... .......... .......... .......... .......... 10% 21.0M 28s 56000K .......... .......... .......... .......... .......... 10% 309M 28s 56050K .......... .......... .......... .......... .......... 11% 568M 28s 56100K .......... .......... .......... .......... .......... 11% 24.5M 28s 56150K .......... .......... .......... .......... .......... 11% 264M 28s 56200K .......... .......... .......... .......... .......... 11% 43.8M 28s 56250K .......... .......... .......... .......... .......... 11% 28.9M 28s 56300K .......... .......... .......... .......... .......... 11% 49.9M 28s 56350K .......... .......... .......... .......... .......... 11% 24.4M 28s 56400K .......... .......... .......... .......... .......... 11% 30.6M 28s 56450K .......... .......... .......... .......... .......... 11% 22.7M 28s 56500K .......... .......... .......... .......... .......... 11% 25.6M 28s 56550K .......... .......... .......... .......... .......... 11% 17.0M 28s 56600K .......... .......... .......... .......... .......... 11% 19.6M 28s 56650K .......... .......... .......... .......... .......... 11% 14.7M 28s 56700K .......... .......... .......... .......... .......... 11% 11.0M 28s 56750K .......... .......... .......... .......... .......... 11% 12.1M 28s 56800K .......... .......... .......... .......... .......... 11% 14.7M 28s 56850K .......... .......... .......... .......... .......... 11% 11.6M 28s 56900K .......... .......... .......... .......... .......... 11% 15.1M 28s 56950K .......... .......... .......... .......... .......... 11% 10.9M 28s 57000K .......... .......... .......... .......... .......... 11% 11.1M 28s 57050K .......... .......... .......... .......... .......... 11% 12.7M 28s 57100K .......... .......... .......... .......... .......... 11% 10.6M 28s 57150K .......... .......... .......... .......... .......... 11% 9.10M 28s 57200K .......... .......... .......... .......... .......... 11% 11.5M 28s 57250K .......... .......... .......... .......... .......... 11% 10.3M 28s 57300K .......... .......... .......... .......... .......... 11% 12.1M 28s 57350K .......... .......... .......... .......... .......... 11% 9.44M 28s 57400K .......... .......... .......... .......... .......... 11% 22.2M 28s 57450K .......... .......... .......... .......... .......... 11% 30.9M 28s 57500K .......... .......... .......... .......... .......... 11% 24.5M 28s 57550K .......... .......... .......... .......... .......... 11% 104M 28s 57600K .......... .......... .......... .......... .......... 11% 31.0M 28s 57650K .......... .......... .......... .......... .......... 11% 42.1M 28s 57700K .......... .......... .......... .......... .......... 11% 41.6M 28s 57750K .......... .......... .......... .......... .......... 11% 27.1M 28s 57800K .......... .......... .......... .......... .......... 11% 25.7M 28s 57850K .......... .......... .......... .......... .......... 11% 31.6M 28s 57900K .......... .......... .......... .......... .......... 11% 25.6M 28s 57950K .......... .......... .......... .......... .......... 11% 17.4M 28s 58000K .......... .......... .......... .......... .......... 11% 25.6M 28s 58050K .......... .......... .......... .......... .......... 11% 21.3M 28s 58100K .......... .......... .......... .......... .......... 11% 17.8M 28s 58150K .......... .......... .......... .......... .......... 11% 24.0M 28s 58200K .......... .......... .......... .......... .......... 11% 20.8M 28s 58250K .......... .......... .......... .......... .......... 11% 14.5M 28s 58300K .......... .......... .......... .......... .......... 11% 17.2M 28s 58350K .......... .......... .......... .......... .......... 11% 19.0M 28s 58400K .......... .......... .......... .......... .......... 11% 16.6M 28s 58450K .......... .......... .......... .......... .......... 11% 11.3M 28s 58500K .......... .......... .......... .......... .......... 11% 11.2M 28s 58550K .......... .......... .......... .......... .......... 11% 12.0M 28s 58600K .......... .......... .......... .......... .......... 11% 11.4M 28s 58650K .......... .......... .......... .......... .......... 11% 14.1M 28s 58700K .......... .......... .......... .......... .......... 11% 11.4M 28s 58750K .......... .......... .......... .......... .......... 11% 15.9M 28s 58800K .......... .......... .......... .......... .......... 11% 17.9M 28s 58850K .......... .......... .......... .......... .......... 11% 12.9M 28s 58900K .......... .......... .......... .......... .......... 11% 17.3M 28s 58950K .......... .......... .......... .......... .......... 11% 13.2M 28s 59000K .......... .......... .......... .......... .......... 11% 13.5M 28s 59050K .......... .......... .......... .......... .......... 11% 17.3M 28s 59100K .......... .......... .......... .......... .......... 11% 13.2M 28s 59150K .......... .......... .......... .......... .......... 11% 15.8M 28s 59200K .......... .......... .......... .......... .......... 11% 18.0M 28s 59250K .......... .......... .......... .......... .......... 11% 34.6M 28s 59300K .......... .......... .......... .......... .......... 11% 60.6M 28s 59350K .......... .......... .......... .......... .......... 11% 16.2M 28s 59400K .......... .......... .......... .......... .......... 11% 22.3M 28s 59450K .......... .......... .......... .......... .......... 11% 14.5M 28s 59500K .......... .......... .......... .......... .......... 11% 14.4M 28s 59550K .......... .......... .......... .......... .......... 11% 11.9M 28s 59600K .......... .......... .......... .......... .......... 11% 10.4M 28s 59650K .......... .......... .......... .......... .......... 11% 13.2M 28s 59700K .......... .......... .......... .......... .......... 11% 10.3M 28s 59750K .......... .......... .......... .......... .......... 11% 11.5M 28s 59800K .......... .......... .......... .......... .......... 11% 12.3M 28s 59850K .......... .......... .......... .......... .......... 11% 10.1M 28s 59900K .......... .......... .......... .......... .......... 11% 10.6M 28s 59950K .......... .......... .......... .......... .......... 11% 8.87M 28s 60000K .......... .......... .......... .......... .......... 11% 7.13M 28s 60050K .......... .......... .......... .......... .......... 11% 6.49M 28s 60100K .......... .......... .......... .......... .......... 11% 6.73M 28s 60150K .......... .......... .......... .......... .......... 11% 7.17M 28s 60200K .......... .......... .......... .......... .......... 11% 6.22M 28s 60250K .......... .......... .......... .......... .......... 11% 13.0M 28s 60300K .......... .......... .......... .......... .......... 11% 26.8M 28s 60350K .......... .......... .......... .......... .......... 11% 24.4M 28s 60400K .......... .......... .......... .......... .......... 11% 30.0M 28s 60450K .......... .......... .......... .......... .......... 11% 20.0M 28s 60500K .......... .......... .......... .......... .......... 11% 19.0M 28s 60550K .......... .......... .......... .......... .......... 11% 15.5M 28s 60600K .......... .......... .......... .......... .......... 11% 12.2M 28s 60650K .......... .......... .......... .......... .......... 11% 22.3M 28s 60700K .......... .......... .......... .......... .......... 11% 16.0M 28s 60750K .......... .......... .......... .......... .......... 11% 16.4M 28s 60800K .......... .......... .......... .......... .......... 11% 18.8M 28s 60850K .......... .......... .......... .......... .......... 11% 15.2M 28s 60900K .......... .......... .......... .......... .......... 11% 21.0M 28s 60950K .......... .......... .......... .......... .......... 11% 15.1M 28s 61000K .......... .......... .......... .......... .......... 11% 18.1M 28s 61050K .......... .......... .......... .......... .......... 11% 22.0M 28s 61100K .......... .......... .......... .......... .......... 11% 15.2M 28s 61150K .......... .......... .......... .......... .......... 12% 15.9M 28s 61200K .......... .......... .......... .......... .......... 12% 13.9M 28s 61250K .......... .......... .......... .......... .......... 12% 15.8M 28s 61300K .......... .......... .......... .......... .......... 12% 14.7M 28s 61350K .......... .......... .......... .......... .......... 12% 8.63M 28s 61400K .......... .......... .......... .......... .......... 12% 13.7M 28s 61450K .......... .......... .......... .......... .......... 12% 9.31M 28s 61500K .......... .......... .......... .......... .......... 12% 6.17M 28s 61550K .......... .......... .......... .......... .......... 12% 8.29M 28s 61600K .......... .......... .......... .......... .......... 12% 6.99M 28s 61650K .......... .......... .......... .......... .......... 12% 6.85M 28s 61700K .......... .......... .......... .......... .......... 12% 6.30M 28s 61750K .......... .......... .......... .......... .......... 12% 10.0M 28s 61800K .......... .......... .......... .......... .......... 12% 26.9M 28s 61850K .......... .......... .......... .......... .......... 12% 11.5M 28s 61900K .......... .......... .......... .......... .......... 12% 47.9M 28s 61950K .......... .......... .......... .......... .......... 12% 15.1M 28s 62000K .......... .......... .......... .......... .......... 12% 14.0M 28s 62050K .......... .......... .......... .......... .......... 12% 13.2M 28s 62100K .......... .......... .......... .......... .......... 12% 12.7M 28s 62150K .......... .......... .......... .......... .......... 12% 8.64M 28s 62200K .......... .......... .......... .......... .......... 12% 6.78M 28s 62250K .......... .......... .......... .......... .......... 12% 8.11M 28s 62300K .......... .......... .......... .......... .......... 12% 6.28M 28s 62350K .......... .......... .......... .......... .......... 12% 5.91M 28s 62400K .......... .......... .......... .......... .......... 12% 7.19M 28s 62450K .......... .......... .......... .......... .......... 12% 13.3M 28s 62500K .......... .......... .......... .......... .......... 12% 41.2M 28s 62550K .......... .......... .......... .......... .......... 12% 23.6M 28s 62600K .......... .......... .......... .......... .......... 12% 16.5M 28s 62650K .......... .......... .......... .......... .......... 12% 20.7M 28s 62700K .......... .......... .......... .......... .......... 12% 12.4M 28s 62750K .......... .......... .......... .......... .......... 12% 22.3M 28s 62800K .......... .......... .......... .......... .......... 12% 17.0M 28s 62850K .......... .......... .......... .......... .......... 12% 17.2M 28s 62900K .......... .......... .......... .......... .......... 12% 17.2M 28s 62950K .......... .......... .......... .......... .......... 12% 15.9M 28s 63000K .......... .......... .......... .......... .......... 12% 15.9M 28s 63050K .......... .......... .......... .......... .......... 12% 15.9M 28s 63100K .......... .......... .......... .......... .......... 12% 12.2M 28s 63150K .......... .......... .......... .......... .......... 12% 15.2M 28s 63200K .......... .......... .......... .......... .......... 12% 17.1M 28s 63250K .......... .......... .......... .......... .......... 12% 18.7M 28s 63300K .......... .......... .......... .......... .......... 12% 21.1M 28s 63350K .......... .......... .......... .......... .......... 12% 31.4M 28s 63400K .......... .......... .......... .......... .......... 12% 34.7M 28s 63450K .......... .......... .......... .......... .......... 12% 33.7M 28s 63500K .......... .......... .......... .......... .......... 12% 62.9M 28s 63550K .......... .......... .......... .......... .......... 12% 32.7M 28s 63600K .......... .......... .......... .......... .......... 12% 30.7M 28s 63650K .......... .......... .......... .......... .......... 12% 23.5M 28s 63700K .......... .......... .......... .......... .......... 12% 17.3M 28s 63750K .......... .......... .......... .......... .......... 12% 31.9M 28s 63800K .......... .......... .......... .......... .......... 12% 13.2M 28s 63850K .......... .......... .......... .......... .......... 12% 19.8M 28s 63900K .......... .......... .......... .......... .......... 12% 18.0M 28s 63950K .......... .......... .......... .......... .......... 12% 17.4M 28s 64000K .......... .......... .......... .......... .......... 12% 19.8M 28s 64050K .......... .......... .......... .......... .......... 12% 18.0M 28s 64100K .......... .......... .......... .......... .......... 12% 16.0M 28s 64150K .......... .......... .......... .......... .......... 12% 17.3M 28s 64200K .......... .......... .......... .......... .......... 12% 10.7M 28s 64250K .......... .......... .......... .......... .......... 12% 14.6M 28s 64300K .......... .......... .......... .......... .......... 12% 13.1M 28s 64350K .......... .......... .......... .......... .......... 12% 10.6M 28s 64400K .......... .......... .......... .......... .......... 12% 10.9M 28s 64450K .......... .......... .......... .......... .......... 12% 14.1M 28s 64500K .......... .......... .......... .......... .......... 12% 10.2M 28s 64550K .......... .......... .......... .......... .......... 12% 9.37M 28s 64600K .......... .......... .......... .......... .......... 12% 7.91M 28s 64650K .......... .......... .......... .......... .......... 12% 10.4M 28s 64700K .......... .......... .......... .......... .......... 12% 9.77M 28s 64750K .......... .......... .......... .......... .......... 12% 10.5M 28s 64800K .......... .......... .......... .......... .......... 12% 10.6M 28s 64850K .......... .......... .......... .......... .......... 12% 8.86M 28s 64900K .......... .......... .......... .......... .......... 12% 10.6M 28s 64950K .......... .......... .......... .......... .......... 12% 21.9M 28s 65000K .......... .......... .......... .......... .......... 12% 36.1M 28s 65050K .......... .......... .......... .......... .......... 12% 36.2M 28s 65100K .......... .......... .......... .......... .......... 12% 23.4M 28s 65150K .......... .......... .......... .......... .......... 12% 35.5M 28s 65200K .......... .......... .......... .......... .......... 12% 27.8M 28s 65250K .......... .......... .......... .......... .......... 12% 27.1M 28s 65300K .......... .......... .......... .......... .......... 12% 23.6M 28s 65350K .......... .......... .......... .......... .......... 12% 22.3M 28s 65400K .......... .......... .......... .......... .......... 12% 31.5M 28s 65450K .......... .......... .......... .......... .......... 12% 22.3M 28s 65500K .......... .......... .......... .......... .......... 12% 19.0M 28s 65550K .......... .......... .......... .......... .......... 12% 29.3M 28s 65600K .......... .......... .......... .......... .......... 12% 19.9M 28s 65650K .......... .......... .......... .......... .......... 12% 17.0M 28s 65700K .......... .......... .......... .......... .......... 12% 14.7M 28s 65750K .......... .......... .......... .......... .......... 12% 12.4M 28s 65800K .......... .......... .......... .......... .......... 12% 15.2M 28s 65850K .......... .......... .......... .......... .......... 12% 11.9M 28s 65900K .......... .......... .......... .......... .......... 12% 17.3M 28s 65950K .......... .......... .......... .......... .......... 12% 12.9M 28s 66000K .......... .......... .......... .......... .......... 12% 17.2M 28s 66050K .......... .......... .......... .......... .......... 12% 13.7M 28s 66100K .......... .......... .......... .......... .......... 12% 13.6M 28s 66150K .......... .......... .......... .......... .......... 12% 16.3M 28s 66200K .......... .......... .......... .......... .......... 12% 12.6M 28s 66250K .......... .......... .......... .......... .......... 13% 40.3M 28s 66300K .......... .......... .......... .......... .......... 13% 36.7M 28s 66350K .......... .......... .......... .......... .......... 13% 22.5M 28s 66400K .......... .......... .......... .......... .......... 13% 40.4M 28s 66450K .......... .......... .......... .......... .......... 13% 70.6M 28s 66500K .......... .......... .......... .......... .......... 13% 103M 28s 66550K .......... .......... .......... .......... .......... 13% 27.5M 28s 66600K .......... .......... .......... .......... .......... 13% 29.2M 28s 66650K .......... .......... .......... .......... .......... 13% 27.4M 28s 66700K .......... .......... .......... .......... .......... 13% 26.0M 28s 66750K .......... .......... .......... .......... .......... 13% 41.8M 28s 66800K .......... .......... .......... .......... .......... 13% 25.7M 28s 66850K .......... .......... .......... .......... .......... 13% 26.7M 28s 66900K .......... .......... .......... .......... .......... 13% 23.4M 28s 66950K .......... .......... .......... .......... .......... 13% 24.6M 28s 67000K .......... .......... .......... .......... .......... 13% 25.3M 28s 67050K .......... .......... .......... .......... .......... 13% 33.4M 28s 67100K .......... .......... .......... .......... .......... 13% 22.3M 28s 67150K .......... .......... .......... .......... .......... 13% 26.8M 28s 67200K .......... .......... .......... .......... .......... 13% 22.5M 28s 67250K .......... .......... .......... .......... .......... 13% 27.0M 28s 67300K .......... .......... .......... .......... .......... 13% 23.5M 28s 67350K .......... .......... .......... .......... .......... 13% 22.1M 28s 67400K .......... .......... .......... .......... .......... 13% 24.0M 28s 67450K .......... .......... .......... .......... .......... 13% 27.2M 27s 67500K .......... .......... .......... .......... .......... 13% 34.1M 27s 67550K .......... .......... .......... .......... .......... 13% 30.1M 27s 67600K .......... .......... .......... .......... .......... 13% 82.3M 27s 67650K .......... .......... .......... .......... .......... 13% 18.1M 27s 67700K .......... .......... .......... .......... .......... 13% 76.1M 27s 67750K .......... .......... .......... .......... .......... 13% 17.5M 27s 67800K .......... .......... .......... .......... .......... 13% 20.9M 27s 67850K .......... .......... .......... .......... .......... 13% 16.9M 27s 67900K .......... .......... .......... .......... .......... 13% 22.8M 27s 67950K .......... .......... .......... .......... .......... 13% 17.9M 27s 68000K .......... .......... .......... .......... .......... 13% 15.7M 27s 68050K .......... .......... .......... .......... .......... 13% 13.6M 27s 68100K .......... .......... .......... .......... .......... 13% 15.3M 27s 68150K .......... .......... .......... .......... .......... 13% 16.7M 27s 68200K .......... .......... .......... .......... .......... 13% 13.7M 27s 68250K .......... .......... .......... .......... .......... 13% 14.8M 27s 68300K .......... .......... .......... .......... .......... 13% 17.4M 27s 68350K .......... .......... .......... .......... .......... 13% 12.2M 27s 68400K .......... .......... .......... .......... .......... 13% 21.2M 27s 68450K .......... .......... .......... .......... .......... 13% 14.4M 27s 68500K .......... .......... .......... .......... .......... 13% 14.0M 27s 68550K .......... .......... .......... .......... .......... 13% 14.6M 27s 68600K .......... .......... .......... .......... .......... 13% 9.46M 27s 68650K .......... .......... .......... .......... .......... 13% 14.0M 27s 68700K .......... .......... .......... .......... .......... 13% 11.4M 27s 68750K .......... .......... .......... .......... .......... 13% 11.9M 27s 68800K .......... .......... .......... .......... .......... 13% 11.9M 27s 68850K .......... .......... .......... .......... .......... 13% 8.25M 27s 68900K .......... .......... .......... .......... .......... 13% 10.3M 27s 68950K .......... .......... .......... .......... .......... 13% 5.60M 27s 69000K .......... .......... .......... .......... .......... 13% 6.23M 27s 69050K .......... .......... .......... .......... .......... 13% 5.71M 27s 69100K .......... .......... .......... .......... .......... 13% 5.71M 28s 69150K .......... .......... .......... .......... .......... 13% 7.92M 28s 69200K .......... .......... .......... .......... .......... 13% 21.0M 28s 69250K .......... .......... .......... .......... .......... 13% 38.1M 28s 69300K .......... .......... .......... .......... .......... 13% 33.7M 28s 69350K .......... .......... .......... .......... .......... 13% 17.8M 27s 69400K .......... .......... .......... .......... .......... 13% 41.7M 27s 69450K .......... .......... .......... .......... .......... 13% 25.2M 27s 69500K .......... .......... .......... .......... .......... 13% 23.5M 27s 69550K .......... .......... .......... .......... .......... 13% 22.2M 27s 69600K .......... .......... .......... .......... .......... 13% 15.7M 27s 69650K .......... .......... .......... .......... .......... 13% 31.8M 27s 69700K .......... .......... .......... .......... .......... 13% 18.6M 27s 69750K .......... .......... .......... .......... .......... 13% 18.0M 27s 69800K .......... .......... .......... .......... .......... 13% 21.0M 27s 69850K .......... .......... .......... .......... .......... 13% 19.8M 27s 69900K .......... .......... .......... .......... .......... 13% 19.0M 27s 69950K .......... .......... .......... .......... .......... 13% 23.3M 27s 70000K .......... .......... .......... .......... .......... 13% 22.4M 27s 70050K .......... .......... .......... .......... .......... 13% 18.9M 27s 70100K .......... .......... .......... .......... .......... 13% 18.9M 27s 70150K .......... .......... .......... .......... .......... 13% 17.0M 27s 70200K .......... .......... .......... .......... .......... 13% 14.1M 27s 70250K .......... .......... .......... .......... .......... 13% 15.3M 27s 70300K .......... .......... .......... .......... .......... 13% 17.4M 27s 70350K .......... .......... .......... .......... .......... 13% 15.3M 27s 70400K .......... .......... .......... .......... .......... 13% 15.2M 27s 70450K .......... .......... .......... .......... .......... 13% 14.6M 27s 70500K .......... .......... .......... .......... .......... 13% 18.0M 27s 70550K .......... .......... .......... .......... .......... 13% 18.1M 27s 70600K .......... .......... .......... .......... .......... 13% 11.7M 27s 70650K .......... .......... .......... .......... .......... 13% 15.4M 27s 70700K .......... .......... .......... .......... .......... 13% 15.9M 27s 70750K .......... .......... .......... .......... .......... 13% 51.0M 27s 70800K .......... .......... .......... .......... .......... 13% 44.1M 27s 70850K .......... .......... .......... .......... .......... 13% 32.5M 27s 70900K .......... .......... .......... .......... .......... 13% 108M 27s 70950K .......... .......... .......... .......... .......... 13% 32.2M 27s 71000K .......... .......... .......... .......... .......... 13% 33.8M 27s 71050K .......... .......... .......... .......... .......... 13% 61.4M 27s 71100K .......... .......... .......... .......... .......... 13% 29.3M 27s 71150K .......... .......... .......... .......... .......... 13% 33.4M 27s 71200K .......... .......... .......... .......... .......... 13% 28.6M 27s 71250K .......... .......... .......... .......... .......... 13% 32.4M 27s 71300K .......... .......... .......... .......... .......... 13% 41.7M 27s 71350K .......... .......... .......... .......... .......... 14% 17.8M 27s 71400K .......... .......... .......... .......... .......... 14% 37.4M 27s 71450K .......... .......... .......... .......... .......... 14% 25.0M 27s 71500K .......... .......... .......... .......... .......... 14% 31.1M 27s 71550K .......... .......... .......... .......... .......... 14% 18.9M 27s 71600K .......... .......... .......... .......... .......... 14% 21.0M 27s 71650K .......... .......... .......... .......... .......... 14% 18.9M 27s 71700K .......... .......... .......... .......... .......... 14% 18.1M 27s 71750K .......... .......... .......... .......... .......... 14% 19.1M 27s 71800K .......... .......... .......... .......... .......... 14% 15.1M 27s 71850K .......... .......... .......... .......... .......... 14% 12.3M 27s 71900K .......... .......... .......... .......... .......... 14% 17.1M 27s 71950K .......... .......... .......... .......... .......... 14% 10.0M 27s 72000K .......... .......... .......... .......... .......... 14% 9.06M 27s 72050K .......... .......... .......... .......... .......... 14% 9.25M 27s 72100K .......... .......... .......... .......... .......... 14% 7.50M 27s 72150K .......... .......... .......... .......... .......... 14% 10.6M 27s 72200K .......... .......... .......... .......... .......... 14% 16.0M 27s 72250K .......... .......... .......... .......... .......... 14% 31.5M 27s 72300K .......... .......... .......... .......... .......... 14% 32.1M 27s 72350K .......... .......... .......... .......... .......... 14% 15.6M 27s 72400K .......... .......... .......... .......... .......... 14% 34.0M 27s 72450K .......... .......... .......... .......... .......... 14% 22.8M 27s 72500K .......... .......... .......... .......... .......... 14% 27.2M 27s 72550K .......... .......... .......... .......... .......... 14% 36.9M 27s 72600K .......... .......... .......... .......... .......... 14% 22.5M 27s 72650K .......... .......... .......... .......... .......... 14% 23.5M 27s 72700K .......... .......... .......... .......... .......... 14% 23.4M 27s 72750K .......... .......... .......... .......... .......... 14% 34.1M 27s 72800K .......... .......... .......... .......... .......... 14% 23.9M 27s 72850K .......... .......... .......... .......... .......... 14% 28.6M 27s 72900K .......... .......... .......... .......... .......... 14% 27.3M 27s 72950K .......... .......... .......... .......... .......... 14% 28.4M 27s 73000K .......... .......... .......... .......... .......... 14% 26.6M 27s 73050K .......... .......... .......... .......... .......... 14% 23.4M 27s 73100K .......... .......... .......... .......... .......... 14% 24.5M 27s 73150K .......... .......... .......... .......... .......... 14% 20.1M 27s 73200K .......... .......... .......... .......... .......... 14% 22.2M 27s 73250K .......... .......... .......... .......... .......... 14% 24.8M 27s 73300K .......... .......... .......... .......... .......... 14% 21.4M 27s 73350K .......... .......... .......... .......... .......... 14% 17.9M 27s 73400K .......... .......... .......... .......... .......... 14% 26.9M 27s 73450K .......... .......... .......... .......... .......... 14% 18.9M 27s 73500K .......... .......... .......... .......... .......... 14% 19.8M 27s 73550K .......... .......... .......... .......... .......... 14% 22.0M 27s 73600K .......... .......... .......... .......... .......... 14% 21.1M 27s 73650K .......... .......... .......... .......... .......... 14% 21.2M 27s 73700K .......... .......... .......... .......... .......... 14% 20.8M 27s 73750K .......... .......... .......... .......... .......... 14% 15.0M 27s 73800K .......... .......... .......... .......... .......... 14% 21.6M 27s 73850K .......... .......... .......... .......... .......... 14% 14.6M 27s 73900K .......... .......... .......... .......... .......... 14% 16.6M 27s 73950K .......... .......... .......... .......... .......... 14% 13.7M 27s 74000K .......... .......... .......... .......... .......... 14% 19.0M 27s 74050K .......... .......... .......... .......... .......... 14% 11.1M 27s 74100K .......... .......... .......... .......... .......... 14% 11.5M 27s 74150K .......... .......... .......... .......... .......... 14% 10.8M 27s 74200K .......... .......... .......... .......... .......... 14% 9.02M 27s 74250K .......... .......... .......... .......... .......... 14% 16.0M 27s 74300K .......... .......... .......... .......... .......... 14% 11.3M 27s 74350K .......... .......... .......... .......... .......... 14% 8.15M 27s 74400K .......... .......... .......... .......... .......... 14% 10.3M 27s 74450K .......... .......... .......... .......... .......... 14% 8.81M 27s 74500K .......... .......... .......... .......... .......... 14% 8.65M 27s 74550K .......... .......... .......... .......... .......... 14% 11.4M 27s 74600K .......... .......... .......... .......... .......... 14% 6.18M 27s 74650K .......... .......... .......... .......... .......... 14% 7.74M 27s 74700K .......... .......... .......... .......... .......... 14% 7.62M 27s 74750K .......... .......... .......... .......... .......... 14% 8.89M 27s 74800K .......... .......... .......... .......... .......... 14% 8.49M 27s 74850K .......... .......... .......... .......... .......... 14% 6.45M 27s 74900K .......... .......... .......... .......... .......... 14% 8.11M 27s 74950K .......... .......... .......... .......... .......... 14% 5.69M 27s 75000K .......... .......... .......... .......... .......... 14% 7.31M 27s 75050K .......... .......... .......... .......... .......... 14% 5.78M 27s 75100K .......... .......... .......... .......... .......... 14% 6.54M 27s 75150K .......... .......... .......... .......... .......... 14% 15.1M 27s 75200K .......... .......... .......... .......... .......... 14% 18.3M 27s 75250K .......... .......... .......... .......... .......... 14% 16.6M 27s 75300K .......... .......... .......... .......... .......... 14% 19.2M 27s 75350K .......... .......... .......... .......... .......... 14% 12.9M 27s 75400K .......... .......... .......... .......... .......... 14% 20.1M 27s 75450K .......... .......... .......... .......... .......... 14% 14.7M 27s 75500K .......... .......... .......... .......... .......... 14% 25.2M 27s 75550K .......... .......... .......... .......... .......... 14% 21.2M 27s 75600K .......... .......... .......... .......... .......... 14% 13.5M 27s 75650K .......... .......... .......... .......... .......... 14% 20.2M 27s 75700K .......... .......... .......... .......... .......... 14% 17.2M 27s 75750K .......... .......... .......... .......... .......... 14% 21.9M 27s 75800K .......... .......... .......... .......... .......... 14% 19.1M 27s 75850K .......... .......... .......... .......... .......... 14% 17.2M 27s 75900K .......... .......... .......... .......... .......... 14% 20.0M 27s 75950K .......... .......... .......... .......... .......... 14% 16.4M 27s 76000K .......... .......... .......... .......... .......... 14% 14.1M 27s 76050K .......... .......... .......... .......... .......... 14% 17.2M 27s 76100K .......... .......... .......... .......... .......... 14% 8.60M 27s 76150K .......... .......... .......... .......... .......... 14% 11.4M 27s 76200K .......... .......... .......... .......... .......... 14% 6.95M 27s 76250K .......... .......... .......... .......... .......... 14% 7.47M 27s 76300K .......... .......... .......... .......... .......... 14% 9.77M 27s 76350K .......... .......... .......... .......... .......... 14% 6.56M 27s 76400K .......... .......... .......... .......... .......... 14% 10.5M 27s 76450K .......... .......... .......... .......... .......... 15% 11.2M 27s 76500K .......... .......... .......... .......... .......... 15% 23.5M 27s 76550K .......... .......... .......... .......... .......... 15% 10.7M 27s 76600K .......... .......... .......... .......... .......... 15% 11.5M 27s 76650K .......... .......... .......... .......... .......... 15% 17.1M 27s 76700K .......... .......... .......... .......... .......... 15% 10.6M 27s 76750K .......... .......... .......... .......... .......... 15% 14.5M 27s 76800K .......... .......... .......... .......... .......... 15% 16.8M 27s 76850K .......... .......... .......... .......... .......... 15% 13.0M 27s 76900K .......... .......... .......... .......... .......... 15% 13.6M 27s 76950K .......... .......... .......... .......... .......... 15% 8.20M 27s 77000K .......... .......... .......... .......... .......... 15% 8.63M 27s 77050K .......... .......... .......... .......... .......... 15% 7.29M 27s 77100K .......... .......... .......... .......... .......... 15% 6.48M 27s 77150K .......... .......... .......... .......... .......... 15% 7.20M 27s 77200K .......... .......... .......... .......... .......... 15% 5.96M 27s 77250K .......... .......... .......... .......... .......... 15% 5.73M 27s 77300K .......... .......... .......... .......... .......... 15% 13.1M 27s 77350K .......... .......... .......... .......... .......... 15% 14.6M 27s 77400K .......... .......... .......... .......... .......... 15% 12.3M 27s 77450K .......... .......... .......... .......... .......... 15% 7.93M 27s 77500K .......... .......... .......... .......... .......... 15% 10.6M 27s 77550K .......... .......... .......... .......... .......... 15% 8.87M 27s 77600K .......... .......... .......... .......... .......... 15% 10.1M 27s 77650K .......... .......... .......... .......... .......... 15% 18.8M 27s 77700K .......... .......... .......... .......... .......... 15% 14.0M 27s 77750K .......... .......... .......... .......... .......... 15% 20.8M 27s 77800K .......... .......... .......... .......... .......... 15% 20.0M 27s 77850K .......... .......... .......... .......... .......... 15% 18.8M 27s 77900K .......... .......... .......... .......... .......... 15% 16.3M 27s 77950K .......... .......... .......... .......... .......... 15% 17.2M 27s 78000K .......... .......... .......... .......... .......... 15% 17.9M 27s 78050K .......... .......... .......... .......... .......... 15% 19.8M 27s 78100K .......... .......... .......... .......... .......... 15% 8.98M 27s 78150K .......... .......... .......... .......... .......... 15% 6.91M 27s 78200K .......... .......... .......... .......... .......... 15% 13.2M 27s 78250K .......... .......... .......... .......... .......... 15% 22.5M 27s 78300K .......... .......... .......... .......... .......... 15% 17.3M 27s 78350K .......... .......... .......... .......... .......... 15% 17.4M 27s 78400K .......... .......... .......... .......... .......... 15% 19.9M 27s 78450K .......... .......... .......... .......... .......... 15% 22.2M 27s 78500K .......... .......... .......... .......... .......... 15% 27.3M 27s 78550K .......... .......... .......... .......... .......... 15% 26.5M 27s 78600K .......... .......... .......... .......... .......... 15% 19.0M 27s 78650K .......... .......... .......... .......... .......... 15% 25.0M 27s 78700K .......... .......... .......... .......... .......... 15% 16.0M 27s 78750K .......... .......... .......... .......... .......... 15% 22.3M 27s 78800K .......... .......... .......... .......... .......... 15% 16.0M 27s 78850K .......... .......... .......... .......... .......... 15% 15.1M 27s 78900K .......... .......... .......... .......... .......... 15% 12.8M 27s 78950K .......... .......... .......... .......... .......... 15% 12.8M 27s 79000K .......... .......... .......... .......... .......... 15% 18.2M 27s 79050K .......... .......... .......... .......... .......... 15% 17.3M 27s 79100K .......... .......... .......... .......... .......... 15% 13.1M 27s 79150K .......... .......... .......... .......... .......... 15% 18.7M 27s 79200K .......... .......... .......... .......... .......... 15% 13.4M 27s 79250K .......... .......... .......... .......... .......... 15% 16.3M 27s 79300K .......... .......... .......... .......... .......... 15% 23.8M 27s 79350K .......... .......... .......... .......... .......... 15% 37.6M 27s 79400K .......... .......... .......... .......... .......... 15% 23.2M 27s 79450K .......... .......... .......... .......... .......... 15% 40.5M 27s 79500K .......... .......... .......... .......... .......... 15% 456M 27s 79550K .......... .......... .......... .......... .......... 15% 34.1M 27s 79600K .......... .......... .......... .......... .......... 15% 23.6M 27s 79650K .......... .......... .......... .......... .......... 15% 31.7M 27s 79700K .......... .......... .......... .......... .......... 15% 17.8M 27s 79750K .......... .......... .......... .......... .......... 15% 20.0M 27s 79800K .......... .......... .......... .......... .......... 15% 16.5M 27s 79850K .......... .......... .......... .......... .......... 15% 11.2M 27s 79900K .......... .......... .......... .......... .......... 15% 15.2M 27s 79950K .......... .......... .......... .......... .......... 15% 11.1M 27s 80000K .......... .......... .......... .......... .......... 15% 19.0M 27s 80050K .......... .......... .......... .......... .......... 15% 13.6M 27s 80100K .......... .......... .......... .......... .......... 15% 15.3M 27s 80150K .......... .......... .......... .......... .......... 15% 15.3M 27s 80200K .......... .......... .......... .......... .......... 15% 15.6M 27s 80250K .......... .......... .......... .......... .......... 15% 12.1M 27s 80300K .......... .......... .......... .......... .......... 15% 15.4M 27s 80350K .......... .......... .......... .......... .......... 15% 10.6M 27s 80400K .......... .......... .......... .......... .......... 15% 12.8M 27s 80450K .......... .......... .......... .......... .......... 15% 12.3M 27s 80500K .......... .......... .......... .......... .......... 15% 12.4M 27s 80550K .......... .......... .......... .......... .......... 15% 13.0M 27s 80600K .......... .......... .......... .......... .......... 15% 8.47M 27s 80650K .......... .......... .......... .......... .......... 15% 15.3M 27s 80700K .......... .......... .......... .......... .......... 15% 11.9M 27s 80750K .......... .......... .......... .......... .......... 15% 25.2M 27s 80800K .......... .......... .......... .......... .......... 15% 37.1M 27s 80850K .......... .......... .......... .......... .......... 15% 22.9M 27s 80900K .......... .......... .......... .......... .......... 15% 19.1M 27s 80950K .......... .......... .......... .......... .......... 15% 13.0M 27s 81000K .......... .......... .......... .......... .......... 15% 29.2M 27s 81050K .......... .......... .......... .......... .......... 15% 17.1M 27s 81100K .......... .......... .......... .......... .......... 15% 18.2M 27s 81150K .......... .......... .......... .......... .......... 15% 20.8M 27s 81200K .......... .......... .......... .......... .......... 15% 14.1M 27s 81250K .......... .......... .......... .......... .......... 15% 23.5M 27s 81300K .......... .......... .......... .......... .......... 15% 14.8M 27s 81350K .......... .......... .......... .......... .......... 15% 20.6M 27s 81400K .......... .......... .......... .......... .......... 15% 17.5M 27s 81450K .......... .......... .......... .......... .......... 15% 16.6M 27s 81500K .......... .......... .......... .......... .......... 15% 23.7M 27s 81550K .......... .......... .......... .......... .......... 16% 18.3M 27s 81600K .......... .......... .......... .......... .......... 16% 14.5M 27s 81650K .......... .......... .......... .......... .......... 16% 20.9M 27s 81700K .......... .......... .......... .......... .......... 16% 21.5M 27s 81750K .......... .......... .......... .......... .......... 16% 45.8M 27s 81800K .......... .......... .......... .......... .......... 16% 88.6M 27s 81850K .......... .......... .......... .......... .......... 16% 26.4M 27s 81900K .......... .......... .......... .......... .......... 16% 112M 27s 81950K .......... .......... .......... .......... .......... 16% 29.6M 27s 82000K .......... .......... .......... .......... .......... 16% 32.6M 27s 82050K .......... .......... .......... .......... .......... 16% 24.2M 27s 82100K .......... .......... .......... .......... .......... 16% 16.3M 27s 82150K .......... .......... .......... .......... .......... 16% 21.0M 27s 82200K .......... .......... .......... .......... .......... 16% 18.7M 27s 82250K .......... .......... .......... .......... .......... 16% 15.5M 27s 82300K .......... .......... .......... .......... .......... 16% 20.9M 27s 82350K .......... .......... .......... .......... .......... 16% 15.9M 27s 82400K .......... .......... .......... .......... .......... 16% 15.8M 27s 82450K .......... .......... .......... .......... .......... 16% 18.2M 27s 82500K .......... .......... .......... .......... .......... 16% 16.5M 27s 82550K .......... .......... .......... .......... .......... 16% 19.6M 27s 82600K .......... .......... .......... .......... .......... 16% 13.9M 27s 82650K .......... .......... .......... .......... .......... 16% 25.7M 27s 82700K .......... .......... .......... .......... .......... 16% 13.6M 27s 82750K .......... .......... .......... .......... .......... 16% 42.1M 27s 82800K .......... .......... .......... .......... .......... 16% 46.6M 27s 82850K .......... .......... .......... .......... .......... 16% 23.1M 27s 82900K .......... .......... .......... .......... .......... 16% 71.7M 27s 82950K .......... .......... .......... .......... .......... 16% 42.0M 27s 83000K .......... .......... .......... .......... .......... 16% 88.1M 27s 83050K .......... .......... .......... .......... .......... 16% 42.2M 27s 83100K .......... .......... .......... .......... .......... 16% 44.2M 27s 83150K .......... .......... .......... .......... .......... 16% 26.5M 27s 83200K .......... .......... .......... .......... .......... 16% 22.6M 27s 83250K .......... .......... .......... .......... .......... 16% 23.8M 27s 83300K .......... .......... .......... .......... .......... 16% 19.0M 27s 83350K .......... .......... .......... .......... .......... 16% 19.8M 27s 83400K .......... .......... .......... .......... .......... 16% 26.6M 27s 83450K .......... .......... .......... .......... .......... 16% 11.1M 27s 83500K .......... .......... .......... .......... .......... 16% 25.5M 27s 83550K .......... .......... .......... .......... .......... 16% 23.7M 27s 83600K .......... .......... .......... .......... .......... 16% 21.3M 27s 83650K .......... .......... .......... .......... .......... 16% 25.8M 27s 83700K .......... .......... .......... .......... .......... 16% 25.5M 27s 83750K .......... .......... .......... .......... .......... 16% 24.5M 27s 83800K .......... .......... .......... .......... .......... 16% 28.3M 27s 83850K .......... .......... .......... .......... .......... 16% 19.9M 27s 83900K .......... .......... .......... .......... .......... 16% 34.1M 27s 83950K .......... .......... .......... .......... .......... 16% 26.4M 27s 84000K .......... .......... .......... .......... .......... 16% 72.2M 26s 84050K .......... .......... .......... .......... .......... 16% 50.8M 26s 84100K .......... .......... .......... .......... .......... 16% 23.4M 26s 84150K .......... .......... .......... .......... .......... 16% 120M 26s 84200K .......... .......... .......... .......... .......... 16% 503M 26s 84250K .......... .......... .......... .......... .......... 16% 62.0M 26s 84300K .......... .......... .......... .......... .......... 16% 28.0M 26s 84350K .......... .......... .......... .......... .......... 16% 448M 26s 84400K .......... .......... .......... .......... .......... 16% 23.1M 26s 84450K .......... .......... .......... .......... .......... 16% 91.3M 26s 84500K .......... .......... .......... .......... .......... 16% 27.9M 26s 84550K .......... .......... .......... .......... .......... 16% 16.5M 26s 84600K .......... .......... .......... .......... .......... 16% 21.4M 26s 84650K .......... .......... .......... .......... .......... 16% 29.1M 26s 84700K .......... .......... .......... .......... .......... 16% 19.4M 26s 84750K .......... .......... .......... .......... .......... 16% 14.0M 26s 84800K .......... .......... .......... .......... .......... 16% 17.9M 26s 84850K .......... .......... .......... .......... .......... 16% 13.9M 26s 84900K .......... .......... .......... .......... .......... 16% 12.3M 26s 84950K .......... .......... .......... .......... .......... 16% 13.4M 26s 85000K .......... .......... .......... .......... .......... 16% 13.4M 26s 85050K .......... .......... .......... .......... .......... 16% 13.9M 26s 85100K .......... .......... .......... .......... .......... 16% 9.70M 26s 85150K .......... .......... .......... .......... .......... 16% 12.3M 26s 85200K .......... .......... .......... .......... .......... 16% 10.1M 26s 85250K .......... .......... .......... .......... .......... 16% 7.47M 26s 85300K .......... .......... .......... .......... .......... 16% 12.4M 26s 85350K .......... .......... .......... .......... .......... 16% 11.5M 26s 85400K .......... .......... .......... .......... .......... 16% 15.8M 26s 85450K .......... .......... .......... .......... .......... 16% 9.71M 26s 85500K .......... .......... .......... .......... .......... 16% 12.7M 26s 85550K .......... .......... .......... .......... .......... 16% 12.7M 26s 85600K .......... .......... .......... .......... .......... 16% 9.44M 26s 85650K .......... .......... .......... .......... .......... 16% 11.4M 26s 85700K .......... .......... .......... .......... .......... 16% 9.79M 26s 85750K .......... .......... .......... .......... .......... 16% 9.52M 26s 85800K .......... .......... .......... .......... .......... 16% 8.41M 26s 85850K .......... .......... .......... .......... .......... 16% 8.25M 26s 85900K .......... .......... .......... .......... .......... 16% 12.3M 26s 85950K .......... .......... .......... .......... .......... 16% 9.23M 26s 86000K .......... .......... .......... .......... .......... 16% 11.4M 26s 86050K .......... .......... .......... .......... .......... 16% 10.3M 26s 86100K .......... .......... .......... .......... .......... 16% 10.4M 26s 86150K .......... .......... .......... .......... .......... 16% 15.8M 26s 86200K .......... .......... .......... .......... .......... 16% 11.5M 26s 86250K .......... .......... .......... .......... .......... 16% 10.6M 26s 86300K .......... .......... .......... .......... .......... 16% 13.7M 26s 86350K .......... .......... .......... .......... .......... 16% 10.8M 26s 86400K .......... .......... .......... .......... .......... 16% 13.7M 26s 86450K .......... .......... .......... .......... .......... 16% 10.0M 26s 86500K .......... .......... .......... .......... .......... 16% 9.28M 26s 86550K .......... .......... .......... .......... .......... 16% 7.35M 26s 86600K .......... .......... .......... .......... .......... 16% 5.62M 26s 86650K .......... .......... .......... .......... .......... 17% 4.17M 27s 86700K .......... .......... .......... .......... .......... 17% 5.39M 27s 86750K .......... .......... .......... .......... .......... 17% 8.23M 27s 86800K .......... .......... .......... .......... .......... 17% 10.5M 27s 86850K .......... .......... .......... .......... .......... 17% 8.24M 27s 86900K .......... .......... .......... .......... .......... 17% 9.51M 27s 86950K .......... .......... .......... .......... .......... 17% 10.8M 27s 87000K .......... .......... .......... .......... .......... 17% 8.85M 27s 87050K .......... .......... .......... .......... .......... 17% 12.0M 27s 87100K .......... .......... .......... .......... .......... 17% 13.2M 27s 87150K .......... .......... .......... .......... .......... 17% 14.1M 27s 87200K .......... .......... .......... .......... .......... 17% 9.97M 27s 87250K .......... .......... .......... .......... .......... 17% 14.2M 27s 87300K .......... .......... .......... .......... .......... 17% 15.0M 27s 87350K .......... .......... .......... .......... .......... 17% 9.48M 27s 87400K .......... .......... .......... .......... .......... 17% 16.4M 27s 87450K .......... .......... .......... .......... .......... 17% 12.5M 27s 87500K .......... .......... .......... .......... .......... 17% 17.2M 27s 87550K .......... .......... .......... .......... .......... 17% 13.4M 27s 87600K .......... .......... .......... .......... .......... 17% 12.6M 27s 87650K .......... .......... .......... .......... .......... 17% 15.0M 27s 87700K .......... .......... .......... .......... .......... 17% 12.0M 27s 87750K .......... .......... .......... .......... .......... 17% 14.2M 27s 87800K .......... .......... .......... .......... .......... 17% 11.2M 27s 87850K .......... .......... .......... .......... .......... 17% 21.1M 27s 87900K .......... .......... .......... .......... .......... 17% 23.4M 27s 87950K .......... .......... .......... .......... .......... 17% 22.9M 27s 88000K .......... .......... .......... .......... .......... 17% 27.3M 27s 88050K .......... .......... .......... .......... .......... 17% 22.5M 27s 88100K .......... .......... .......... .......... .......... 17% 17.2M 27s 88150K .......... .......... .......... .......... .......... 17% 16.3M 27s 88200K .......... .......... .......... .......... .......... 17% 19.2M 27s 88250K .......... .......... .......... .......... .......... 17% 21.1M 27s 88300K .......... .......... .......... .......... .......... 17% 20.5M 27s 88350K .......... .......... .......... .......... .......... 17% 19.9M 27s 88400K .......... .......... .......... .......... .......... 17% 20.1M 27s 88450K .......... .......... .......... .......... .......... 17% 14.0M 27s 88500K .......... .......... .......... .......... .......... 17% 13.6M 27s 88550K .......... .......... .......... .......... .......... 17% 11.4M 27s 88600K .......... .......... .......... .......... .......... 17% 9.95M 27s 88650K .......... .......... .......... .......... .......... 17% 12.5M 27s 88700K .......... .......... .......... .......... .......... 17% 10.9M 27s 88750K .......... .......... .......... .......... .......... 17% 14.0M 27s 88800K .......... .......... .......... .......... .......... 17% 12.2M 27s 88850K .......... .......... .......... .......... .......... 17% 11.2M 27s 88900K .......... .......... .......... .......... .......... 17% 13.1M 27s 88950K .......... .......... .......... .......... .......... 17% 25.4M 27s 89000K .......... .......... .......... .......... .......... 17% 24.7M 26s 89050K .......... .......... .......... .......... .......... 17% 574M 26s 89100K .......... .......... .......... .......... .......... 17% 37.5M 26s 89150K .......... .......... .......... .......... .......... 17% 37.8M 26s 89200K .......... .......... .......... .......... .......... 17% 27.2M 26s 89250K .......... .......... .......... .......... .......... 17% 30.7M 26s 89300K .......... .......... .......... .......... .......... 17% 36.2M 26s 89350K .......... .......... .......... .......... .......... 17% 25.5M 26s 89400K .......... .......... .......... .......... .......... 17% 30.4M 26s 89450K .......... .......... .......... .......... .......... 17% 22.0M 26s 89500K .......... .......... .......... .......... .......... 17% 18.1M 26s 89550K .......... .......... .......... .......... .......... 17% 27.1M 26s 89600K .......... .......... .......... .......... .......... 17% 14.1M 26s 89650K .......... .......... .......... .......... .......... 17% 19.2M 26s 89700K .......... .......... .......... .......... .......... 17% 15.8M 26s 89750K .......... .......... .......... .......... .......... 17% 20.8M 26s 89800K .......... .......... .......... .......... .......... 17% 21.0M 26s 89850K .......... .......... .......... .......... .......... 17% 17.6M 26s 89900K .......... .......... .......... .......... .......... 17% 15.3M 26s 89950K .......... .......... .......... .......... .......... 17% 14.2M 26s 90000K .......... .......... .......... .......... .......... 17% 14.5M 26s 90050K .......... .......... .......... .......... .......... 17% 10.8M 26s 90100K .......... .......... .......... .......... .......... 17% 10.0M 26s 90150K .......... .......... .......... .......... .......... 17% 17.3M 26s 90200K .......... .......... .......... .......... .......... 17% 13.9M 26s 90250K .......... .......... .......... .......... .......... 17% 18.0M 26s 90300K .......... .......... .......... .......... .......... 17% 14.7M 26s 90350K .......... .......... .......... .......... .......... 17% 14.7M 26s 90400K .......... .......... .......... .......... .......... 17% 17.2M 26s 90450K .......... .......... .......... .......... .......... 17% 10.9M 26s 90500K .......... .......... .......... .......... .......... 17% 9.40M 26s 90550K .......... .......... .......... .......... .......... 17% 8.76M 26s 90600K .......... .......... .......... .......... .......... 17% 7.41M 26s 90650K .......... .......... .......... .......... .......... 17% 8.87M 26s 90700K .......... .......... .......... .......... .......... 17% 7.07M 26s 90750K .......... .......... .......... .......... .......... 17% 9.05M 26s 90800K .......... .......... .......... .......... .......... 17% 7.42M 26s 90850K .......... .......... .......... .......... .......... 17% 6.12M 26s 90900K .......... .......... .......... .......... .......... 17% 6.55M 26s 90950K .......... .......... .......... .......... .......... 17% 6.07M 26s 91000K .......... .......... .......... .......... .......... 17% 5.60M 26s 91050K .......... .......... .......... .......... .......... 17% 8.66M 26s 91100K .......... .......... .......... .......... .......... 17% 6.44M 27s 91150K .......... .......... .......... .......... .......... 17% 5.91M 27s 91200K .......... .......... .......... .......... .......... 17% 6.73M 27s 91250K .......... .......... .......... .......... .......... 17% 7.18M 27s 91300K .......... .......... .......... .......... .......... 17% 6.44M 27s 91350K .......... .......... .......... .......... .......... 17% 5.43M 27s 91400K .......... .......... .......... .......... .......... 17% 6.88M 27s 91450K .......... .......... .......... .......... .......... 17% 10.9M 27s 91500K .......... .......... .......... .......... .......... 17% 14.2M 27s 91550K .......... .......... .......... .......... .......... 17% 12.6M 27s 91600K .......... .......... .......... .......... .......... 17% 12.8M 27s 91650K .......... .......... .......... .......... .......... 17% 15.6M 27s 91700K .......... .......... .......... .......... .......... 17% 12.7M 27s 91750K .......... .......... .......... .......... .......... 18% 14.8M 27s 91800K .......... .......... .......... .......... .......... 18% 18.1M 27s 91850K .......... .......... .......... .......... .......... 18% 11.1M 27s 91900K .......... .......... .......... .......... .......... 18% 13.9M 27s 91950K .......... .......... .......... .......... .......... 18% 8.62M 27s 92000K .......... .......... .......... .......... .......... 18% 13.6M 27s 92050K .......... .......... .......... .......... .......... 18% 7.35M 27s 92100K .......... .......... .......... .......... .......... 18% 7.25M 27s 92150K .......... .......... .......... .......... .......... 18% 10.1M 27s 92200K .......... .......... .......... .......... .......... 18% 12.8M 27s 92250K .......... .......... .......... .......... .......... 18% 25.4M 27s 92300K .......... .......... .......... .......... .......... 18% 35.9M 27s 92350K .......... .......... .......... .......... .......... 18% 22.9M 27s 92400K .......... .......... .......... .......... .......... 18% 54.4M 27s 92450K .......... .......... .......... .......... .......... 18% 18.3M 27s 92500K .......... .......... .......... .......... .......... 18% 25.2M 27s 92550K .......... .......... .......... .......... .......... 18% 25.0M 27s 92600K .......... .......... .......... .......... .......... 18% 22.9M 27s 92650K .......... .......... .......... .......... .......... 18% 22.8M 27s 92700K .......... .......... .......... .......... .......... 18% 17.2M 27s 92750K .......... .......... .......... .......... .......... 18% 25.0M 27s 92800K .......... .......... .......... .......... .......... 18% 19.0M 27s 92850K .......... .......... .......... .......... .......... 18% 15.1M 27s 92900K .......... .......... .......... .......... .......... 18% 15.7M 27s 92950K .......... .......... .......... .......... .......... 18% 9.52M 27s 93000K .......... .......... .......... .......... .......... 18% 11.2M 27s 93050K .......... .......... .......... .......... .......... 18% 15.9M 27s 93100K .......... .......... .......... .......... .......... 18% 9.50M 27s 93150K .......... .......... .......... .......... .......... 18% 15.7M 27s 93200K .......... .......... .......... .......... .......... 18% 14.0M 27s 93250K .......... .......... .......... .......... .......... 18% 16.7M 27s 93300K .......... .......... .......... .......... .......... 18% 15.9M 27s 93350K .......... .......... .......... .......... .......... 18% 12.7M 27s 93400K .......... .......... .......... .......... .......... 18% 18.0M 27s 93450K .......... .......... .......... .......... .......... 18% 12.3M 27s 93500K .......... .......... .......... .......... .......... 18% 18.4M 27s 93550K .......... .......... .......... .......... .......... 18% 24.0M 27s 93600K .......... .......... .......... .......... .......... 18% 9.16M 27s 93650K .......... .......... .......... .......... .......... 18% 13.5M 27s 93700K .......... .......... .......... .......... .......... 18% 9.83M 27s 93750K .......... .......... .......... .......... .......... 18% 13.2M 27s 93800K .......... .......... .......... .......... .......... 18% 11.6M 27s 93850K .......... .......... .......... .......... .......... 18% 10.1M 27s 93900K .......... .......... .......... .......... .......... 18% 13.6M 27s 93950K .......... .......... .......... .......... .......... 18% 9.89M 27s 94000K .......... .......... .......... .......... .......... 18% 11.3M 27s 94050K .......... .......... .......... .......... .......... 18% 12.2M 27s 94100K .......... .......... .......... .......... .......... 18% 9.73M 27s 94150K .......... .......... .......... .......... .......... 18% 11.0M 27s 94200K .......... .......... .......... .......... .......... 18% 9.96M 27s 94250K .......... .......... .......... .......... .......... 18% 8.99M 27s 94300K .......... .......... .......... .......... .......... 18% 9.30M 27s 94350K .......... .......... .......... .......... .......... 18% 7.68M 27s 94400K .......... .......... .......... .......... .......... 18% 9.97M 27s 94450K .......... .......... .......... .......... .......... 18% 8.19M 27s 94500K .......... .......... .......... .......... .......... 18% 8.30M 27s 94550K .......... .......... .......... .......... .......... 18% 9.15M 27s 94600K .......... .......... .......... .......... .......... 18% 9.32M 27s 94650K .......... .......... .......... .......... .......... 18% 12.6M 27s 94700K .......... .......... .......... .......... .......... 18% 9.06M 27s 94750K .......... .......... .......... .......... .......... 18% 11.8M 27s 94800K .......... .......... .......... .......... .......... 18% 14.7M 27s 94850K .......... .......... .......... .......... .......... 18% 11.4M 27s 94900K .......... .......... .......... .......... .......... 18% 13.4M 27s 94950K .......... .......... .......... .......... .......... 18% 13.5M 27s 95000K .......... .......... .......... .......... .......... 18% 18.1M 27s 95050K .......... .......... .......... .......... .......... 18% 31.4M 27s 95100K .......... .......... .......... .......... .......... 18% 15.1M 27s 95150K .......... .......... .......... .......... .......... 18% 23.7M 27s 95200K .......... .......... .......... .......... .......... 18% 18.0M 27s 95250K .......... .......... .......... .......... .......... 18% 19.1M 27s 95300K .......... .......... .......... .......... .......... 18% 20.1M 27s 95350K .......... .......... .......... .......... .......... 18% 14.0M 27s 95400K .......... .......... .......... .......... .......... 18% 11.4M 27s 95450K .......... .......... .......... .......... .......... 18% 15.8M 27s 95500K .......... .......... .......... .......... .......... 18% 16.1M 27s 95550K .......... .......... .......... .......... .......... 18% 13.1M 27s 95600K .......... .......... .......... .......... .......... 18% 12.0M 27s 95650K .......... .......... .......... .......... .......... 18% 14.0M 27s 95700K .......... .......... .......... .......... .......... 18% 13.2M 27s 95750K .......... .......... .......... .......... .......... 18% 15.9M 27s 95800K .......... .......... .......... .......... .......... 18% 13.6M 27s 95850K .......... .......... .......... .......... .......... 18% 14.5M 27s 95900K .......... .......... .......... .......... .......... 18% 14.7M 27s 95950K .......... .......... .......... .......... .......... 18% 18.9M 27s 96000K .......... .......... .......... .......... .......... 18% 33.6M 27s 96050K .......... .......... .......... .......... .......... 18% 24.8M 27s 96100K .......... .......... .......... .......... .......... 18% 77.6M 26s 96150K .......... .......... .......... .......... .......... 18% 26.7M 26s 96200K .......... .......... .......... .......... .......... 18% 22.3M 26s 96250K .......... .......... .......... .......... .......... 18% 37.4M 26s 96300K .......... .......... .......... .......... .......... 18% 18.4M 26s 96350K .......... .......... .......... .......... .......... 18% 26.9M 26s 96400K .......... .......... .......... .......... .......... 18% 25.0M 26s 96450K .......... .......... .......... .......... .......... 18% 20.0M 26s 96500K .......... .......... .......... .......... .......... 18% 18.8M 26s 96550K .......... .......... .......... .......... .......... 18% 20.6M 26s 96600K .......... .......... .......... .......... .......... 18% 17.6M 26s 96650K .......... .......... .......... .......... .......... 18% 20.4M 26s 96700K .......... .......... .......... .......... .......... 18% 19.9M 26s 96750K .......... .......... .......... .......... .......... 18% 20.5M 26s 96800K .......... .......... .......... .......... .......... 18% 20.8M 26s 96850K .......... .......... .......... .......... .......... 19% 19.8M 26s 96900K .......... .......... .......... .......... .......... 19% 14.4M 26s 96950K .......... .......... .......... .......... .......... 19% 17.4M 26s 97000K .......... .......... .......... .......... .......... 19% 18.8M 26s 97050K .......... .......... .......... .......... .......... 19% 18.1M 26s 97100K .......... .......... .......... .......... .......... 19% 17.3M 26s 97150K .......... .......... .......... .......... .......... 19% 17.2M 26s 97200K .......... .......... .......... .......... .......... 19% 16.5M 26s 97250K .......... .......... .......... .......... .......... 19% 25.1M 26s 97300K .......... .......... .......... .......... .......... 19% 15.9M 26s 97350K .......... .......... .......... .......... .......... 19% 14.6M 26s 97400K .......... .......... .......... .......... .......... 19% 17.1M 26s 97450K .......... .......... .......... .......... .......... 19% 13.2M 26s 97500K .......... .......... .......... .......... .......... 19% 13.2M 26s 97550K .......... .......... .......... .......... .......... 19% 20.0M 26s 97600K .......... .......... .......... .......... .......... 19% 39.6M 26s 97650K .......... .......... .......... .......... .......... 19% 39.3M 26s 97700K .......... .......... .......... .......... .......... 19% 28.6M 26s 97750K .......... .......... .......... .......... .......... 19% 53.8M 26s 97800K .......... .......... .......... .......... .......... 19% 52.9M 26s 97850K .......... .......... .......... .......... .......... 19% 28.6M 26s 97900K .......... .......... .......... .......... .......... 19% 28.5M 26s 97950K .......... .......... .......... .......... .......... 19% 28.9M 26s 98000K .......... .......... .......... .......... .......... 19% 25.1M 26s 98050K .......... .......... .......... .......... .......... 19% 25.7M 26s 98100K .......... .......... .......... .......... .......... 19% 20.3M 26s 98150K .......... .......... .......... .......... .......... 19% 22.2M 26s 98200K .......... .......... .......... .......... .......... 19% 17.2M 26s 98250K .......... .......... .......... .......... .......... 19% 23.9M 26s 98300K .......... .......... .......... .......... .......... 19% 21.1M 26s 98350K .......... .......... .......... .......... .......... 19% 16.3M 26s 98400K .......... .......... .......... .......... .......... 19% 12.7M 26s 98450K .......... .......... .......... .......... .......... 19% 12.7M 26s 98500K .......... .......... .......... .......... .......... 19% 18.1M 26s 98550K .......... .......... .......... .......... .......... 19% 11.3M 26s 98600K .......... .......... .......... .......... .......... 19% 7.19M 26s 98650K .......... .......... .......... .......... .......... 19% 9.57M 26s 98700K .......... .......... .......... .......... .......... 19% 7.98M 26s 98750K .......... .......... .......... .......... .......... 19% 10.6M 26s 98800K .......... .......... .......... .......... .......... 19% 12.0M 26s 98850K .......... .......... .......... .......... .......... 19% 13.0M 26s 98900K .......... .......... .......... .......... .......... 19% 12.2M 26s 98950K .......... .......... .......... .......... .......... 19% 10.2M 26s 99000K .......... .......... .......... .......... .......... 19% 11.2M 26s 99050K .......... .......... .......... .......... .......... 19% 9.33M 26s 99100K .......... .......... .......... .......... .......... 19% 10.1M 26s 99150K .......... .......... .......... .......... .......... 19% 8.64M 26s 99200K .......... .......... .......... .......... .......... 19% 8.08M 26s 99250K .......... .......... .......... .......... .......... 19% 11.9M 26s 99300K .......... .......... .......... .......... .......... 19% 19.0M 26s 99350K .......... .......... .......... .......... .......... 19% 17.4M 26s 99400K .......... .......... .......... .......... .......... 19% 20.9M 26s 99450K .......... .......... .......... .......... .......... 19% 13.9M 26s 99500K .......... .......... .......... .......... .......... 19% 24.2M 26s 99550K .......... .......... .......... .......... .......... 19% 19.8M 26s 99600K .......... .......... .......... .......... .......... 19% 12.9M 26s 99650K .......... .......... .......... .......... .......... 19% 11.0M 26s 99700K .......... .......... .......... .......... .......... 19% 8.31M 26s 99750K .......... .......... .......... .......... .......... 19% 10.3M 26s 99800K .......... .......... .......... .......... .......... 19% 11.2M 26s 99850K .......... .......... .......... .......... .......... 19% 7.90M 26s 99900K .......... .......... .......... .......... .......... 19% 9.06M 26s 99950K .......... .......... .......... .......... .......... 19% 8.28M 26s 100000K .......... .......... .......... .......... .......... 19% 11.7M 26s 100050K .......... .......... .......... .......... .......... 19% 22.1M 26s 100100K .......... .......... .......... .......... .......... 19% 29.8M 26s 100150K .......... .......... .......... .......... .......... 19% 37.4M 26s 100200K .......... .......... .......... .......... .......... 19% 43.4M 26s 100250K .......... .......... .......... .......... .......... 19% 16.9M 26s 100300K .......... .......... .......... .......... .......... 19% 30.4M 26s 100350K .......... .......... .......... .......... .......... 19% 10.9M 26s 100400K .......... .......... .......... .......... .......... 19% 11.8M 26s 100450K .......... .......... .......... .......... .......... 19% 11.1M 26s 100500K .......... .......... .......... .......... .......... 19% 13.6M 26s 100550K .......... .......... .......... .......... .......... 19% 11.9M 26s 100600K .......... .......... .......... .......... .......... 19% 10.0M 26s 100650K .......... .......... .......... .......... .......... 19% 11.4M 26s 100700K .......... .......... .......... .......... .......... 19% 8.72M 26s 100750K .......... .......... .......... .......... .......... 19% 19.9M 26s 100800K .......... .......... .......... .......... .......... 19% 20.3M 26s 100850K .......... .......... .......... .......... .......... 19% 23.2M 26s 100900K .......... .......... .......... .......... .......... 19% 17.3M 26s 100950K .......... .......... .......... .......... .......... 19% 26.7M 26s 101000K .......... .......... .......... .......... .......... 19% 19.1M 26s 101050K .......... .......... .......... .......... .......... 19% 19.7M 26s 101100K .......... .......... .......... .......... .......... 19% 10.5M 26s 101150K .......... .......... .......... .......... .......... 19% 12.6M 26s 101200K .......... .......... .......... .......... .......... 19% 11.2M 26s 101250K .......... .......... .......... .......... .......... 19% 11.2M 26s 101300K .......... .......... .......... .......... .......... 19% 12.2M 26s 101350K .......... .......... .......... .......... .......... 19% 9.56M 26s 101400K .......... .......... .......... .......... .......... 19% 12.6M 26s 101450K .......... .......... .......... .......... .......... 19% 8.30M 26s 101500K .......... .......... .......... .......... .......... 19% 11.1M 26s 101550K .......... .......... .......... .......... .......... 19% 13.3M 26s 101600K .......... .......... .......... .......... .......... 19% 18.0M 26s 101650K .......... .......... .......... .......... .......... 19% 19.3M 26s 101700K .......... .......... .......... .......... .......... 19% 19.4M 26s 101750K .......... .......... .......... .......... .......... 19% 16.8M 26s 101800K .......... .......... .......... .......... .......... 19% 19.0M 26s 101850K .......... .......... .......... .......... .......... 19% 21.1M 26s 101900K .......... .......... .......... .......... .......... 19% 20.9M 26s 101950K .......... .......... .......... .......... .......... 20% 19.8M 26s 102000K .......... .......... .......... .......... .......... 20% 22.5M 26s 102050K .......... .......... .......... .......... .......... 20% 22.1M 26s 102100K .......... .......... .......... .......... .......... 20% 25.9M 26s 102150K .......... .......... .......... .......... .......... 20% 20.2M 26s 102200K .......... .......... .......... .......... .......... 20% 24.5M 26s 102250K .......... .......... .......... .......... .......... 20% 19.1M 26s 102300K .......... .......... .......... .......... .......... 20% 25.2M 26s 102350K .......... .......... .......... .......... .......... 20% 17.0M 26s 102400K .......... .......... .......... .......... .......... 20% 19.3M 26s 102450K .......... .......... .......... .......... .......... 20% 10.4M 26s 102500K .......... .......... .......... .......... .......... 20% 19.8M 26s 102550K .......... .......... .......... .......... .......... 20% 12.9M 26s 102600K .......... .......... .......... .......... .......... 20% 15.8M 26s 102650K .......... .......... .......... .......... .......... 20% 12.0M 26s 102700K .......... .......... .......... .......... .......... 20% 12.3M 26s 102750K .......... .......... .......... .......... .......... 20% 17.2M 26s 102800K .......... .......... .......... .......... .......... 20% 15.3M 26s 102850K .......... .......... .......... .......... .......... 20% 11.1M 26s 102900K .......... .......... .......... .......... .......... 20% 11.9M 26s 102950K .......... .......... .......... .......... .......... 20% 8.13M 26s 103000K .......... .......... .......... .......... .......... 20% 10.9M 26s 103050K .......... .......... .......... .......... .......... 20% 7.93M 26s 103100K .......... .......... .......... .......... .......... 20% 7.35M 26s 103150K .......... .......... .......... .......... .......... 20% 11.6M 26s 103200K .......... .......... .......... .......... .......... 20% 9.93M 26s 103250K .......... .......... .......... .......... .......... 20% 11.9M 26s 103300K .......... .......... .......... .......... .......... 20% 14.1M 26s 103350K .......... .......... .......... .......... .......... 20% 10.9M 26s 103400K .......... .......... .......... .......... .......... 20% 13.0M 26s 103450K .......... .......... .......... .......... .......... 20% 13.1M 26s 103500K .......... .......... .......... .......... .......... 20% 12.4M 26s 103550K .......... .......... .......... .......... .......... 20% 11.8M 26s 103600K .......... .......... .......... .......... .......... 20% 24.9M 26s 103650K .......... .......... .......... .......... .......... 20% 34.8M 26s 103700K .......... .......... .......... .......... .......... 20% 38.0M 26s 103750K .......... .......... .......... .......... .......... 20% 37.8M 26s 103800K .......... .......... .......... .......... .......... 20% 44.4M 26s 103850K .......... .......... .......... .......... .......... 20% 29.7M 26s 103900K .......... .......... .......... .......... .......... 20% 43.2M 26s 103950K .......... .......... .......... .......... .......... 20% 37.8M 26s 104000K .......... .......... .......... .......... .......... 20% 23.3M 26s 104050K .......... .......... .......... .......... .......... 20% 479M 26s 104100K .......... .......... .......... .......... .......... 20% 27.4M 26s 104150K .......... .......... .......... .......... .......... 20% 29.1M 26s 104200K .......... .......... .......... .......... .......... 20% 16.6M 26s 104250K .......... .......... .......... .......... .......... 20% 21.2M 26s 104300K .......... .......... .......... .......... .......... 20% 18.0M 26s 104350K .......... .......... .......... .......... .......... 20% 15.8M 26s 104400K .......... .......... .......... .......... .......... 20% 19.1M 26s 104450K .......... .......... .......... .......... .......... 20% 19.9M 26s 104500K .......... .......... .......... .......... .......... 20% 16.5M 26s 104550K .......... .......... .......... .......... .......... 20% 22.6M 26s 104600K .......... .......... .......... .......... .......... 20% 15.3M 26s 104650K .......... .......... .......... .......... .......... 20% 17.3M 26s 104700K .......... .......... .......... .......... .......... 20% 18.1M 26s 104750K .......... .......... .......... .......... .......... 20% 18.7M 26s 104800K .......... .......... .......... .......... .......... 20% 15.7M 26s 104850K .......... .......... .......... .......... .......... 20% 11.4M 26s 104900K .......... .......... .......... .......... .......... 20% 12.6M 26s 104950K .......... .......... .......... .......... .......... 20% 14.1M 26s 105000K .......... .......... .......... .......... .......... 20% 17.8M 26s 105050K .......... .......... .......... .......... .......... 20% 13.9M 26s 105100K .......... .......... .......... .......... .......... 20% 10.8M 26s 105150K .......... .......... .......... .......... .......... 20% 14.0M 26s 105200K .......... .......... .......... .......... .......... 20% 10.8M 26s 105250K .......... .......... .......... .......... .......... 20% 16.3M 26s 105300K .......... .......... .......... .......... .......... 20% 17.3M 26s 105350K .......... .......... .......... .......... .......... 20% 15.2M 26s 105400K .......... .......... .......... .......... .......... 20% 15.2M 26s 105450K .......... .......... .......... .......... .......... 20% 21.3M 26s 105500K .......... .......... .......... .......... .......... 20% 23.4M 26s 105550K .......... .......... .......... .......... .......... 20% 17.2M 26s 105600K .......... .......... .......... .......... .......... 20% 15.2M 26s 105650K .......... .......... .......... .......... .......... 20% 10.1M 26s 105700K .......... .......... .......... .......... .......... 20% 11.1M 26s 105750K .......... .......... .......... .......... .......... 20% 13.8M 26s 105800K .......... .......... .......... .......... .......... 20% 12.4M 26s 105850K .......... .......... .......... .......... .......... 20% 10.5M 26s 105900K .......... .......... .......... .......... .......... 20% 13.6M 26s 105950K .......... .......... .......... .......... .......... 20% 11.2M 26s 106000K .......... .......... .......... .......... .......... 20% 12.6M 26s 106050K .......... .......... .......... .......... .......... 20% 12.8M 26s 106100K .......... .......... .......... .......... .......... 20% 14.1M 26s 106150K .......... .......... .......... .......... .......... 20% 24.1M 26s 106200K .......... .......... .......... .......... .......... 20% 13.1M 26s 106250K .......... .......... .......... .......... .......... 20% 38.5M 26s 106300K .......... .......... .......... .......... .......... 20% 21.3M 26s 106350K .......... .......... .......... .......... .......... 20% 18.1M 26s 106400K .......... .......... .......... .......... .......... 20% 18.8M 26s 106450K .......... .......... .......... .......... .......... 20% 20.0M 26s 106500K .......... .......... .......... .......... .......... 20% 24.9M 26s 106550K .......... .......... .......... .......... .......... 20% 19.8M 26s 106600K .......... .......... .......... .......... .......... 20% 14.4M 26s 106650K .......... .......... .......... .......... .......... 20% 19.7M 26s 106700K .......... .......... .......... .......... .......... 20% 11.9M 26s 106750K .......... .......... .......... .......... .......... 20% 19.0M 26s 106800K .......... .......... .......... .......... .......... 20% 18.1M 26s 106850K .......... .......... .......... .......... .......... 20% 7.96M 26s 106900K .......... .......... .......... .......... .......... 20% 17.3M 26s 106950K .......... .......... .......... .......... .......... 20% 10.9M 26s 107000K .......... .......... .......... .......... .......... 20% 14.0M 26s 107050K .......... .......... .......... .......... .......... 21% 11.9M 26s 107100K .......... .......... .......... .......... .......... 21% 11.7M 26s 107150K .......... .......... .......... .......... .......... 21% 15.3M 26s 107200K .......... .......... .......... .......... .......... 21% 12.0M 26s 107250K .......... .......... .......... .......... .......... 21% 15.2M 26s 107300K .......... .......... .......... .......... .......... 21% 15.4M 26s 107350K .......... .......... .......... .......... .......... 21% 15.8M 26s 107400K .......... .......... .......... .......... .......... 21% 41.2M 26s 107450K .......... .......... .......... .......... .......... 21% 25.7M 26s 107500K .......... .......... .......... .......... .......... 21% 39.1M 26s 107550K .......... .......... .......... .......... .......... 21% 25.7M 26s 107600K .......... .......... .......... .......... .......... 21% 25.8M 26s 107650K .......... .......... .......... .......... .......... 21% 19.8M 26s 107700K .......... .......... .......... .......... .......... 21% 14.5M 26s 107750K .......... .......... .......... .......... .......... 21% 18.0M 26s 107800K .......... .......... .......... .......... .......... 21% 12.6M 26s 107850K .......... .......... .......... .......... .......... 21% 8.88M 26s 107900K .......... .......... .......... .......... .......... 21% 13.7M 26s 107950K .......... .......... .......... .......... .......... 21% 12.7M 26s 108000K .......... .......... .......... .......... .......... 21% 17.2M 26s 108050K .......... .......... .......... .......... .......... 21% 15.1M 26s 108100K .......... .......... .......... .......... .......... 21% 15.7M 26s 108150K .......... .......... .......... .......... .......... 21% 17.5M 26s 108200K .......... .......... .......... .......... .......... 21% 13.1M 26s 108250K .......... .......... .......... .......... .......... 21% 10.3M 26s 108300K .......... .......... .......... .......... .......... 21% 9.59M 26s 108350K .......... .......... .......... .......... .......... 21% 7.46M 26s 108400K .......... .......... .......... .......... .......... 21% 6.17M 26s 108450K .......... .......... .......... .......... .......... 21% 6.37M 26s 108500K .......... .......... .......... .......... .......... 21% 6.70M 26s 108550K .......... .......... .......... .......... .......... 21% 3.37M 26s 108600K .......... .......... .......... .......... .......... 21% 6.30M 26s 108650K .......... .......... .......... .......... .......... 21% 11.5M 26s 108700K .......... .......... .......... .......... .......... 21% 9.12M 26s 108750K .......... .......... .......... .......... .......... 21% 18.3M 26s 108800K .......... .......... .......... .......... .......... 21% 8.45M 26s 108850K .......... .......... .......... .......... .......... 21% 14.6M 26s 108900K .......... .......... .......... .......... .......... 21% 18.9M 26s 108950K .......... .......... .......... .......... .......... 21% 17.1M 26s 109000K .......... .......... .......... .......... .......... 21% 20.5M 26s 109050K .......... .......... .......... .......... .......... 21% 13.0M 26s 109100K .......... .......... .......... .......... .......... 21% 11.9M 26s 109150K .......... .......... .......... .......... .......... 21% 15.1M 26s 109200K .......... .......... .......... .......... .......... 21% 14.2M 26s 109250K .......... .......... .......... .......... .......... 21% 16.6M 26s 109300K .......... .......... .......... .......... .......... 21% 19.1M 26s 109350K .......... .......... .......... .......... .......... 21% 14.1M 26s 109400K .......... .......... .......... .......... .......... 21% 17.6M 26s 109450K .......... .......... .......... .......... .......... 21% 14.7M 26s 109500K .......... .......... .......... .......... .......... 21% 15.1M 26s 109550K .......... .......... .......... .......... .......... 21% 18.1M 26s 109600K .......... .......... .......... .......... .......... 21% 15.0M 26s 109650K .......... .......... .......... .......... .......... 21% 33.7M 26s 109700K .......... .......... .......... .......... .......... 21% 31.0M 26s 109750K .......... .......... .......... .......... .......... 21% 27.0M 26s 109800K .......... .......... .......... .......... .......... 21% 381M 26s 109850K .......... .......... .......... .......... .......... 21% 28.7M 26s 109900K .......... .......... .......... .......... .......... 21% 384M 26s 109950K .......... .......... .......... .......... .......... 21% 18.8M 26s 110000K .......... .......... .......... .......... .......... 21% 22.0M 26s 110050K .......... .......... .......... .......... .......... 21% 19.2M 26s 110100K .......... .......... .......... .......... .......... 21% 12.8M 26s 110150K .......... .......... .......... .......... .......... 21% 18.7M 26s 110200K .......... .......... .......... .......... .......... 21% 14.2M 26s 110250K .......... .......... .......... .......... .......... 21% 20.0M 26s 110300K .......... .......... .......... .......... .......... 21% 25.6M 26s 110350K .......... .......... .......... .......... .......... 21% 16.0M 26s 110400K .......... .......... .......... .......... .......... 21% 22.4M 26s 110450K .......... .......... .......... .......... .......... 21% 13.5M 26s 110500K .......... .......... .......... .......... .......... 21% 18.9M 26s 110550K .......... .......... .......... .......... .......... 21% 17.9M 26s 110600K .......... .......... .......... .......... .......... 21% 15.9M 26s 110650K .......... .......... .......... .......... .......... 21% 17.2M 26s 110700K .......... .......... .......... .......... .......... 21% 12.5M 26s 110750K .......... .......... .......... .......... .......... 21% 19.1M 26s 110800K .......... .......... .......... .......... .......... 21% 15.7M 26s 110850K .......... .......... .......... .......... .......... 21% 10.3M 26s 110900K .......... .......... .......... .......... .......... 21% 13.1M 26s 110950K .......... .......... .......... .......... .......... 21% 8.05M 26s 111000K .......... .......... .......... .......... .......... 21% 9.52M 26s 111050K .......... .......... .......... .......... .......... 21% 8.68M 26s 111100K .......... .......... .......... .......... .......... 21% 8.15M 26s 111150K .......... .......... .......... .......... .......... 21% 9.84M 26s 111200K .......... .......... .......... .......... .......... 21% 8.26M 26s 111250K .......... .......... .......... .......... .......... 21% 9.71M 26s 111300K .......... .......... .......... .......... .......... 21% 23.3M 26s 111350K .......... .......... .......... .......... .......... 21% 37.3M 26s 111400K .......... .......... .......... .......... .......... 21% 38.8M 26s 111450K .......... .......... .......... .......... .......... 21% 26.2M 26s 111500K .......... .......... .......... .......... .......... 21% 56.5M 26s 111550K .......... .......... .......... .......... .......... 21% 29.2M 26s 111600K .......... .......... .......... .......... .......... 21% 34.2M 26s 111650K .......... .......... .......... .......... .......... 21% 25.3M 26s 111700K .......... .......... .......... .......... .......... 21% 33.7M 26s 111750K .......... .......... .......... .......... .......... 21% 31.0M 26s 111800K .......... .......... .......... .......... .......... 21% 34.7M 26s 111850K .......... .......... .......... .......... .......... 21% 16.0M 26s 111900K .......... .......... .......... .......... .......... 21% 94.8M 26s 111950K .......... .......... .......... .......... .......... 21% 21.0M 26s 112000K .......... .......... .......... .......... .......... 21% 25.5M 26s 112050K .......... .......... .......... .......... .......... 21% 25.9M 26s 112100K .......... .......... .......... .......... .......... 21% 26.4M 25s 112150K .......... .......... .......... .......... .......... 22% 26.5M 25s 112200K .......... .......... .......... .......... .......... 22% 20.7M 25s 112250K .......... .......... .......... .......... .......... 22% 26.8M 25s 112300K .......... .......... .......... .......... .......... 22% 27.3M 25s 112350K .......... .......... .......... .......... .......... 22% 24.5M 25s 112400K .......... .......... .......... .......... .......... 22% 28.7M 25s 112450K .......... .......... .......... .......... .......... 22% 27.3M 25s 112500K .......... .......... .......... .......... .......... 22% 25.3M 25s 112550K .......... .......... .......... .......... .......... 22% 21.0M 25s 112600K .......... .......... .......... .......... .......... 22% 18.8M 25s 112650K .......... .......... .......... .......... .......... 22% 24.7M 25s 112700K .......... .......... .......... .......... .......... 22% 16.6M 25s 112750K .......... .......... .......... .......... .......... 22% 20.2M 25s 112800K .......... .......... .......... .......... .......... 22% 16.0M 25s 112850K .......... .......... .......... .......... .......... 22% 15.2M 25s 112900K .......... .......... .......... .......... .......... 22% 10.9M 25s 112950K .......... .......... .......... .......... .......... 22% 11.1M 25s 113000K .......... .......... .......... .......... .......... 22% 13.6M 25s 113050K .......... .......... .......... .......... .......... 22% 12.3M 25s 113100K .......... .......... .......... .......... .......... 22% 15.3M 25s 113150K .......... .......... .......... .......... .......... 22% 15.8M 25s 113200K .......... .......... .......... .......... .......... 22% 174M 25s 113250K .......... .......... .......... .......... .......... 22% 21.0M 25s 113300K .......... .......... .......... .......... .......... 22% 15.0M 25s 113350K .......... .......... .......... .......... .......... 22% 11.7M 25s 113400K .......... .......... .......... .......... .......... 22% 15.8M 25s 113450K .......... .......... .......... .......... .......... 22% 14.6M 25s 113500K .......... .......... .......... .......... .......... 22% 12.6M 25s 113550K .......... .......... .......... .......... .......... 22% 15.8M 25s 113600K .......... .......... .......... .......... .......... 22% 14.1M 25s 113650K .......... .......... .......... .......... .......... 22% 15.1M 25s 113700K .......... .......... .......... .......... .......... 22% 12.0M 25s 113750K .......... .......... .......... .......... .......... 22% 15.8M 25s 113800K .......... .......... .......... .......... .......... 22% 16.6M 25s 113850K .......... .......... .......... .......... .......... 22% 15.5M 25s 113900K .......... .......... .......... .......... .......... 22% 15.8M 25s 113950K .......... .......... .......... .......... .......... 22% 28.7M 25s 114000K .......... .......... .......... .......... .......... 22% 41.9M 25s 114050K .......... .......... .......... .......... .......... 22% 26.6M 25s 114100K .......... .......... .......... .......... .......... 22% 109M 25s 114150K .......... .......... .......... .......... .......... 22% 147M 25s 114200K .......... .......... .......... .......... .......... 22% 43.5M 25s 114250K .......... .......... .......... .......... .......... 22% 26.2M 25s 114300K .......... .......... .......... .......... .......... 22% 30.2M 25s 114350K .......... .......... .......... .......... .......... 22% 38.9M 25s 114400K .......... .......... .......... .......... .......... 22% 31.5M 25s 114450K .......... .......... .......... .......... .......... 22% 23.7M 25s 114500K .......... .......... .......... .......... .......... 22% 37.5M 25s 114550K .......... .......... .......... .......... .......... 22% 24.9M 25s 114600K .......... .......... .......... .......... .......... 22% 29.4M 25s 114650K .......... .......... .......... .......... .......... 22% 33.0M 25s 114700K .......... .......... .......... .......... .......... 22% 26.7M 25s 114750K .......... .......... .......... .......... .......... 22% 27.2M 25s 114800K .......... .......... .......... .......... .......... 22% 37.6M 25s 114850K .......... .......... .......... .......... .......... 22% 26.1M 25s 114900K .......... .......... .......... .......... .......... 22% 29.5M 25s 114950K .......... .......... .......... .......... .......... 22% 26.8M 25s 115000K .......... .......... .......... .......... .......... 22% 27.4M 25s 115050K .......... .......... .......... .......... .......... 22% 41.6M 25s 115100K .......... .......... .......... .......... .......... 22% 25.4M 25s 115150K .......... .......... .......... .......... .......... 22% 36.3M 25s 115200K .......... .......... .......... .......... .......... 22% 19.8M 25s 115250K .......... .......... .......... .......... .......... 22% 22.3M 25s 115300K .......... .......... .......... .......... .......... 22% 21.2M 25s 115350K .......... .......... .......... .......... .......... 22% 25.2M 25s 115400K .......... .......... .......... .......... .......... 22% 18.9M 25s 115450K .......... .......... .......... .......... .......... 22% 20.1M 25s 115500K .......... .......... .......... .......... .......... 22% 47.5M 25s 115550K .......... .......... .......... .......... .......... 22% 19.0M 25s 115600K .......... .......... .......... .......... .......... 22% 34.7M 25s 115650K .......... .......... .......... .......... .......... 22% 21.8M 25s 115700K .......... .......... .......... .......... .......... 22% 13.0M 25s 115750K .......... .......... .......... .......... .......... 22% 555M 25s 115800K .......... .......... .......... .......... .......... 22% 28.8M 25s 115850K .......... .......... .......... .......... .......... 22% 20.0M 25s 115900K .......... .......... .......... .......... .......... 22% 13.2M 25s 115950K .......... .......... .......... .......... .......... 22% 48.0M 25s 116000K .......... .......... .......... .......... .......... 22% 29.0M 25s 116050K .......... .......... .......... .......... .......... 22% 18.0M 25s 116100K .......... .......... .......... .......... .......... 22% 16.0M 25s 116150K .......... .......... .......... .......... .......... 22% 19.4M 25s 116200K .......... .......... .......... .......... .......... 22% 13.0M 25s 116250K .......... .......... .......... .......... .......... 22% 16.6M 25s 116300K .......... .......... .......... .......... .......... 22% 14.1M 25s 116350K .......... .......... .......... .......... .......... 22% 16.5M 25s 116400K .......... .......... .......... .......... .......... 22% 19.9M 25s 116450K .......... .......... .......... .......... .......... 22% 16.5M 25s 116500K .......... .......... .......... .......... .......... 22% 19.0M 25s 116550K .......... .......... .......... .......... .......... 22% 17.0M 25s 116600K .......... .......... .......... .......... .......... 22% 16.6M 25s 116650K .......... .......... .......... .......... .......... 22% 13.9M 25s 116700K .......... .......... .......... .......... .......... 22% 16.6M 25s 116750K .......... .......... .......... .......... .......... 22% 19.0M 25s 116800K .......... .......... .......... .......... .......... 22% 18.9M 25s 116850K .......... .......... .......... .......... .......... 22% 13.5M 25s 116900K .......... .......... .......... .......... .......... 22% 20.0M 25s 116950K .......... .......... .......... .......... .......... 22% 14.6M 25s 117000K .......... .......... .......... .......... .......... 22% 17.3M 25s 117050K .......... .......... .......... .......... .......... 22% 16.8M 25s 117100K .......... .......... .......... .......... .......... 22% 16.6M 25s 117150K .......... .......... .......... .......... .......... 22% 16.5M 25s 117200K .......... .......... .......... .......... .......... 22% 19.2M 25s 117250K .......... .......... .......... .......... .......... 23% 18.1M 25s 117300K .......... .......... .......... .......... .......... 23% 22.4M 25s 117350K .......... .......... .......... .......... .......... 23% 23.5M 25s 117400K .......... .......... .......... .......... .......... 23% 25.1M 25s 117450K .......... .......... .......... .......... .......... 23% 16.7M 25s 117500K .......... .......... .......... .......... .......... 23% 31.2M 25s 117550K .......... .......... .......... .......... .......... 23% 21.7M 25s 117600K .......... .......... .......... .......... .......... 23% 14.8M 25s 117650K .......... .......... .......... .......... .......... 23% 35.2M 25s 117700K .......... .......... .......... .......... .......... 23% 15.6M 25s 117750K .......... .......... .......... .......... .......... 23% 22.3M 25s 117800K .......... .......... .......... .......... .......... 23% 21.2M 25s 117850K .......... .......... .......... .......... .......... 23% 17.7M 25s 117900K .......... .......... .......... .......... .......... 23% 24.8M 25s 117950K .......... .......... .......... .......... .......... 23% 20.8M 25s 118000K .......... .......... .......... .......... .......... 23% 23.5M 25s 118050K .......... .......... .......... .......... .......... 23% 18.7M 25s 118100K .......... .......... .......... .......... .......... 23% 16.4M 25s 118150K .......... .......... .......... .......... .......... 23% 17.4M 25s 118200K .......... .......... .......... .......... .......... 23% 17.7M 25s 118250K .......... .......... .......... .......... .......... 23% 14.5M 25s 118300K .......... .......... .......... .......... .......... 23% 14.7M 25s 118350K .......... .......... .......... .......... .......... 23% 13.5M 25s 118400K .......... .......... .......... .......... .......... 23% 12.3M 25s 118450K .......... .......... .......... .......... .......... 23% 7.93M 25s 118500K .......... .......... .......... .......... .......... 23% 4.56M 25s 118550K .......... .......... .......... .......... .......... 23% 6.66M 25s 118600K .......... .......... .......... .......... .......... 23% 9.58M 25s 118650K .......... .......... .......... .......... .......... 23% 13.2M 25s 118700K .......... .......... .......... .......... .......... 23% 20.9M 25s 118750K .......... .......... .......... .......... .......... 23% 14.2M 25s 118800K .......... .......... .......... .......... .......... 23% 17.4M 25s 118850K .......... .......... .......... .......... .......... 23% 11.2M 25s 118900K .......... .......... .......... .......... .......... 23% 15.2M 25s 118950K .......... .......... .......... .......... .......... 23% 15.6M 25s 119000K .......... .......... .......... .......... .......... 23% 16.5M 25s 119050K .......... .......... .......... .......... .......... 23% 13.5M 25s 119100K .......... .......... .......... .......... .......... 23% 15.8M 25s 119150K .......... .......... .......... .......... .......... 23% 19.8M 25s 119200K .......... .......... .......... .......... .......... 23% 15.3M 25s 119250K .......... .......... .......... .......... .......... 23% 17.1M 25s 119300K .......... .......... .......... .......... .......... 23% 16.6M 25s 119350K .......... .......... .......... .......... .......... 23% 13.9M 25s 119400K .......... .......... .......... .......... .......... 23% 17.1M 25s 119450K .......... .......... .......... .......... .......... 23% 15.6M 25s 119500K .......... .......... .......... .......... .......... 23% 16.4M 25s 119550K .......... .......... .......... .......... .......... 23% 13.5M 25s 119600K .......... .......... .......... .......... .......... 23% 13.3M 25s 119650K .......... .......... .......... .......... .......... 23% 16.5M 25s 119700K .......... .......... .......... .......... .......... 23% 12.3M 25s 119750K .......... .......... .......... .......... .......... 23% 14.6M 25s 119800K .......... .......... .......... .......... .......... 23% 17.1M 25s 119850K .......... .......... .......... .......... .......... 23% 13.9M 25s 119900K .......... .......... .......... .......... .......... 23% 22.1M 25s 119950K .......... .......... .......... .......... .......... 23% 8.02M 25s 120000K .......... .......... .......... .......... .......... 23% 42.8M 25s 120050K .......... .......... .......... .......... .......... 23% 12.6M 25s 120100K .......... .......... .......... .......... .......... 23% 9.17M 25s 120150K .......... .......... .......... .......... .......... 23% 11.8M 25s 120200K .......... .......... .......... .......... .......... 23% 6.84M 25s 120250K .......... .......... .......... .......... .......... 23% 7.07M 25s 120300K .......... .......... .......... .......... .......... 23% 8.68M 25s 120350K .......... .......... .......... .......... .......... 23% 6.67M 25s 120400K .......... .......... .......... .......... .......... 23% 7.83M 25s 120450K .......... .......... .......... .......... .......... 23% 8.99M 25s 120500K .......... .......... .......... .......... .......... 23% 29.3M 25s 120550K .......... .......... .......... .......... .......... 23% 34.0M 25s 120600K .......... .......... .......... .......... .......... 23% 27.5M 25s 120650K .......... .......... .......... .......... .......... 23% 25.3M 25s 120700K .......... .......... .......... .......... .......... 23% 15.6M 25s 120750K .......... .......... .......... .......... .......... 23% 19.6M 25s 120800K .......... .......... .......... .......... .......... 23% 23.8M 25s 120850K .......... .......... .......... .......... .......... 23% 16.5M 25s 120900K .......... .......... .......... .......... .......... 23% 16.5M 25s 120950K .......... .......... .......... .......... .......... 23% 14.5M 25s 121000K .......... .......... .......... .......... .......... 23% 15.3M 25s 121050K .......... .......... .......... .......... .......... 23% 14.2M 25s 121100K .......... .......... .......... .......... .......... 23% 13.1M 25s 121150K .......... .......... .......... .......... .......... 23% 16.4M 25s 121200K .......... .......... .......... .......... .......... 23% 12.7M 25s 121250K .......... .......... .......... .......... .......... 23% 13.2M 25s 121300K .......... .......... .......... .......... .......... 23% 16.6M 25s 121350K .......... .......... .......... .......... .......... 23% 11.8M 25s 121400K .......... .......... .......... .......... .......... 23% 8.88M 25s 121450K .......... .......... .......... .......... .......... 23% 14.5M 25s 121500K .......... .......... .......... .......... .......... 23% 34.1M 25s 121550K .......... .......... .......... .......... .......... 23% 27.6M 25s 121600K .......... .......... .......... .......... .......... 23% 14.9M 25s 121650K .......... .......... .......... .......... .......... 23% 483M 25s 121700K .......... .......... .......... .......... .......... 23% 20.9M 25s 121750K .......... .......... .......... .......... .......... 23% 18.7M 25s 121800K .......... .......... .......... .......... .......... 23% 22.5M 25s 121850K .......... .......... .......... .......... .......... 23% 19.5M 25s 121900K .......... .......... .......... .......... .......... 23% 23.7M 25s 121950K .......... .......... .......... .......... .......... 23% 18.0M 25s 122000K .......... .......... .......... .......... .......... 23% 19.0M 25s 122050K .......... .......... .......... .......... .......... 23% 22.1M 25s 122100K .......... .......... .......... .......... .......... 23% 15.7M 25s 122150K .......... .......... .......... .......... .......... 23% 23.6M 25s 122200K .......... .......... .......... .......... .......... 23% 11.9M 25s 122250K .......... .......... .......... .......... .......... 23% 12.7M 25s 122300K .......... .......... .......... .......... .......... 23% 15.9M 25s 122350K .......... .......... .......... .......... .......... 24% 14.5M 25s 122400K .......... .......... .......... .......... .......... 24% 19.0M 25s 122450K .......... .......... .......... .......... .......... 24% 13.0M 25s 122500K .......... .......... .......... .......... .......... 24% 17.3M 25s 122550K .......... .......... .......... .......... .......... 24% 17.7M 25s 122600K .......... .......... .......... .......... .......... 24% 9.73M 25s 122650K .......... .......... .......... .......... .......... 24% 14.2M 25s 122700K .......... .......... .......... .......... .......... 24% 10.8M 25s 122750K .......... .......... .......... .......... .......... 24% 13.6M 25s 122800K .......... .......... .......... .......... .......... 24% 13.5M 25s 122850K .......... .......... .......... .......... .......... 24% 8.82M 25s 122900K .......... .......... .......... .......... .......... 24% 8.96M 25s 122950K .......... .......... .......... .......... .......... 24% 5.42M 25s 123000K .......... .......... .......... .......... .......... 24% 7.41M 25s 123050K .......... .......... .......... .......... .......... 24% 7.35M 25s 123100K .......... .......... .......... .......... .......... 24% 7.60M 25s 123150K .......... .......... .......... .......... .......... 24% 10.5M 25s 123200K .......... .......... .......... .......... .......... 24% 18.6M 25s 123250K .......... .......... .......... .......... .......... 24% 36.9M 25s 123300K .......... .......... .......... .......... .......... 24% 22.5M 25s 123350K .......... .......... .......... .......... .......... 24% 26.0M 25s 123400K .......... .......... .......... .......... .......... 24% 23.7M 25s 123450K .......... .......... .......... .......... .......... 24% 23.5M 25s 123500K .......... .......... .......... .......... .......... 24% 24.9M 25s 123550K .......... .......... .......... .......... .......... 24% 27.1M 25s 123600K .......... .......... .......... .......... .......... 24% 17.9M 25s 123650K .......... .......... .......... .......... .......... 24% 31.9M 25s 123700K .......... .......... .......... .......... .......... 24% 23.1M 25s 123750K .......... .......... .......... .......... .......... 24% 27.2M 25s 123800K .......... .......... .......... .......... .......... 24% 26.2M 25s 123850K .......... .......... .......... .......... .......... 24% 21.1M 25s 123900K .......... .......... .......... .......... .......... 24% 25.2M 25s 123950K .......... .......... .......... .......... .......... 24% 19.9M 25s 124000K .......... .......... .......... .......... .......... 24% 20.1M 25s 124050K .......... .......... .......... .......... .......... 24% 17.7M 25s 124100K .......... .......... .......... .......... .......... 24% 19.8M 25s 124150K .......... .......... .......... .......... .......... 24% 21.1M 25s 124200K .......... .......... .......... .......... .......... 24% 26.1M 25s 124250K .......... .......... .......... .......... .......... 24% 47.6M 24s 124300K .......... .......... .......... .......... .......... 24% 19.7M 24s 124350K .......... .......... .......... .......... .......... 24% 106M 24s 124400K .......... .......... .......... .......... .......... 24% 503M 24s 124450K .......... .......... .......... .......... .......... 24% 34.7M 24s 124500K .......... .......... .......... .......... .......... 24% 95.0M 24s 124550K .......... .......... .......... .......... .......... 24% 28.1M 24s 124600K .......... .......... .......... .......... .......... 24% 48.2M 24s 124650K .......... .......... .......... .......... .......... 24% 29.4M 24s 124700K .......... .......... .......... .......... .......... 24% 21.7M 24s 124750K .......... .......... .......... .......... .......... 24% 27.4M 24s 124800K .......... .......... .......... .......... .......... 24% 29.0M 24s 124850K .......... .......... .......... .......... .......... 24% 19.8M 24s 124900K .......... .......... .......... .......... .......... 24% 25.3M 24s 124950K .......... .......... .......... .......... .......... 24% 23.3M 24s 125000K .......... .......... .......... .......... .......... 24% 23.7M 24s 125050K .......... .......... .......... .......... .......... 24% 31.0M 24s 125100K .......... .......... .......... .......... .......... 24% 16.3M 24s 125150K .......... .......... .......... .......... .......... 24% 16.2M 24s 125200K .......... .......... .......... .......... .......... 24% 13.8M 24s 125250K .......... .......... .......... .......... .......... 24% 13.7M 24s 125300K .......... .......... .......... .......... .......... 24% 17.8M 24s 125350K .......... .......... .......... .......... .......... 24% 14.7M 24s 125400K .......... .......... .......... .......... .......... 24% 19.4M 24s 125450K .......... .......... .......... .......... .......... 24% 11.8M 24s 125500K .......... .......... .......... .......... .......... 24% 21.1M 24s 125550K .......... .......... .......... .......... .......... 24% 13.6M 24s 125600K .......... .......... .......... .......... .......... 24% 15.3M 24s 125650K .......... .......... .......... .......... .......... 24% 23.3M 24s 125700K .......... .......... .......... .......... .......... 24% 16.5M 24s 125750K .......... .......... .......... .......... .......... 24% 23.5M 24s 125800K .......... .......... .......... .......... .......... 24% 32.6M 24s 125850K .......... .......... .......... .......... .......... 24% 25.8M 24s 125900K .......... .......... .......... .......... .......... 24% 89.6M 24s 125950K .......... .......... .......... .......... .......... 24% 36.4M 24s 126000K .......... .......... .......... .......... .......... 24% 62.2M 24s 126050K .......... .......... .......... .......... .......... 24% 48.1M 24s 126100K .......... .......... .......... .......... .......... 24% 41.6M 24s 126150K .......... .......... .......... .......... .......... 24% 35.1M 24s 126200K .......... .......... .......... .......... .......... 24% 33.9M 24s 126250K .......... .......... .......... .......... .......... 24% 46.8M 24s 126300K .......... .......... .......... .......... .......... 24% 40.7M 24s 126350K .......... .......... .......... .......... .......... 24% 23.7M 24s 126400K .......... .......... .......... .......... .......... 24% 37.8M 24s 126450K .......... .......... .......... .......... .......... 24% 20.3M 24s 126500K .......... .......... .......... .......... .......... 24% 34.4M 24s 126550K .......... .......... .......... .......... .......... 24% 29.6M 24s 126600K .......... .......... .......... .......... .......... 24% 22.2M 24s 126650K .......... .......... .......... .......... .......... 24% 23.8M 24s 126700K .......... .......... .......... .......... .......... 24% 18.0M 24s 126750K .......... .......... .......... .......... .......... 24% 27.4M 24s 126800K .......... .......... .......... .......... .......... 24% 23.6M 24s 126850K .......... .......... .......... .......... .......... 24% 16.5M 24s 126900K .......... .......... .......... .......... .......... 24% 22.4M 24s 126950K .......... .......... .......... .......... .......... 24% 23.9M 24s 127000K .......... .......... .......... .......... .......... 24% 18.7M 24s 127050K .......... .......... .......... .......... .......... 24% 23.6M 24s 127100K .......... .......... .......... .......... .......... 24% 23.3M 24s 127150K .......... .......... .......... .......... .......... 24% 21.1M 24s 127200K .......... .......... .......... .......... .......... 24% 18.3M 24s 127250K .......... .......... .......... .......... .......... 24% 22.2M 24s 127300K .......... .......... .......... .......... .......... 24% 22.8M 24s 127350K .......... .......... .......... .......... .......... 24% 11.3M 24s 127400K .......... .......... .......... .......... .......... 25% 9.75M 24s 127450K .......... .......... .......... .......... .......... 25% 10.5M 24s 127500K .......... .......... .......... .......... .......... 25% 10.9M 24s 127550K .......... .......... .......... .......... .......... 25% 9.35M 24s 127600K .......... .......... .......... .......... .......... 25% 9.34M 24s 127650K .......... .......... .......... .......... .......... 25% 6.68M 24s 127700K .......... .......... .......... .......... .......... 25% 9.79M 24s 127750K .......... .......... .......... .......... .......... 25% 10.9M 24s 127800K .......... .......... .......... .......... .......... 25% 10.5M 24s 127850K .......... .......... .......... .......... .......... 25% 8.35M 24s 127900K .......... .......... .......... .......... .......... 25% 22.4M 24s 127950K .......... .......... .......... .......... .......... 25% 18.4M 24s 128000K .......... .......... .......... .......... .......... 25% 37.4M 24s 128050K .......... .......... .......... .......... .......... 25% 22.3M 24s 128100K .......... .......... .......... .......... .......... 25% 23.2M 24s 128150K .......... .......... .......... .......... .......... 25% 17.6M 24s 128200K .......... .......... .......... .......... .......... 25% 23.8M 24s 128250K .......... .......... .......... .......... .......... 25% 32.1M 24s 128300K .......... .......... .......... .......... .......... 25% 17.6M 24s 128350K .......... .......... .......... .......... .......... 25% 24.2M 24s 128400K .......... .......... .......... .......... .......... 25% 16.7M 24s 128450K .......... .......... .......... .......... .......... 25% 13.0M 24s 128500K .......... .......... .......... .......... .......... 25% 39.9M 24s 128550K .......... .......... .......... .......... .......... 25% 16.7M 24s 128600K .......... .......... .......... .......... .......... 25% 10.8M 24s 128650K .......... .......... .......... .......... .......... 25% 31.3M 24s 128700K .......... .......... .......... .......... .......... 25% 11.7M 24s 128750K .......... .......... .......... .......... .......... 25% 8.28M 24s 128800K .......... .......... .......... .......... .......... 25% 15.2M 24s 128850K .......... .......... .......... .......... .......... 25% 9.23M 24s 128900K .......... .......... .......... .......... .......... 25% 12.2M 24s 128950K .......... .......... .......... .......... .......... 25% 10.9M 24s 129000K .......... .......... .......... .......... .......... 25% 10.8M 24s 129050K .......... .......... .......... .......... .......... 25% 8.30M 24s 129100K .......... .......... .......... .......... .......... 25% 6.92M 24s 129150K .......... .......... .......... .......... .......... 25% 23.6M 24s 129200K .......... .......... .......... .......... .......... 25% 16.2M 24s 129250K .......... .......... .......... .......... .......... 25% 35.2M 24s 129300K .......... .......... .......... .......... .......... 25% 37.3M 24s 129350K .......... .......... .......... .......... .......... 25% 23.9M 24s 129400K .......... .......... .......... .......... .......... 25% 23.9M 24s 129450K .......... .......... .......... .......... .......... 25% 18.6M 24s 129500K .......... .......... .......... .......... .......... 25% 22.2M 24s 129550K .......... .......... .......... .......... .......... 25% 21.8M 24s 129600K .......... .......... .......... .......... .......... 25% 16.5M 24s 129650K .......... .......... .......... .......... .......... 25% 23.5M 24s 129700K .......... .......... .......... .......... .......... 25% 20.6M 24s 129750K .......... .......... .......... .......... .......... 25% 23.7M 24s 129800K .......... .......... .......... .......... .......... 25% 24.9M 24s 129850K .......... .......... .......... .......... .......... 25% 22.1M 24s 129900K .......... .......... .......... .......... .......... 25% 25.2M 24s 129950K .......... .......... .......... .......... .......... 25% 19.6M 24s 130000K .......... .......... .......... .......... .......... 25% 25.3M 24s 130050K .......... .......... .......... .......... .......... 25% 22.4M 24s 130100K .......... .......... .......... .......... .......... 25% 23.1M 24s 130150K .......... .......... .......... .......... .......... 25% 19.2M 24s 130200K .......... .......... .......... .......... .......... 25% 21.1M 24s 130250K .......... .......... .......... .......... .......... 25% 25.2M 24s 130300K .......... .......... .......... .......... .......... 25% 23.6M 24s 130350K .......... .......... .......... .......... .......... 25% 24.1M 24s 130400K .......... .......... .......... .......... .......... 25% 493M 24s 130450K .......... .......... .......... .......... .......... 25% 25.3M 24s 130500K .......... .......... .......... .......... .......... 25% 35.9M 24s 130550K .......... .......... .......... .......... .......... 25% 29.9M 24s 130600K .......... .......... .......... .......... .......... 25% 23.1M 24s 130650K .......... .......... .......... .......... .......... 25% 28.8M 24s 130700K .......... .......... .......... .......... .......... 25% 27.9M 24s 130750K .......... .......... .......... .......... .......... 25% 18.0M 24s 130800K .......... .......... .......... .......... .......... 25% 27.9M 24s 130850K .......... .......... .......... .......... .......... 25% 17.1M 24s 130900K .......... .......... .......... .......... .......... 25% 20.8M 24s 130950K .......... .......... .......... .......... .......... 25% 20.9M 24s 131000K .......... .......... .......... .......... .......... 25% 22.2M 24s 131050K .......... .......... .......... .......... .......... 25% 13.5M 24s 131100K .......... .......... .......... .......... .......... 25% 18.6M 24s 131150K .......... .......... .......... .......... .......... 25% 13.6M 24s 131200K .......... .......... .......... .......... .......... 25% 16.6M 24s 131250K .......... .......... .......... .......... .......... 25% 17.9M 24s 131300K .......... .......... .......... .......... .......... 25% 13.1M 24s 131350K .......... .......... .......... .......... .......... 25% 10.0M 24s 131400K .......... .......... .......... .......... .......... 25% 13.7M 24s 131450K .......... .......... .......... .......... .......... 25% 13.0M 24s 131500K .......... .......... .......... .......... .......... 25% 16.7M 24s 131550K .......... .......... .......... .......... .......... 25% 14.0M 24s 131600K .......... .......... .......... .......... .......... 25% 11.9M 24s 131650K .......... .......... .......... .......... .......... 25% 16.5M 24s 131700K .......... .......... .......... .......... .......... 25% 13.5M 24s 131750K .......... .......... .......... .......... .......... 25% 14.7M 24s 131800K .......... .......... .......... .......... .......... 25% 16.4M 24s 131850K .......... .......... .......... .......... .......... 25% 13.5M 24s 131900K .......... .......... .......... .......... .......... 25% 16.5M 24s 131950K .......... .......... .......... .......... .......... 25% 22.1M 24s 132000K .......... .......... .......... .......... .......... 25% 63.8M 24s 132050K .......... .......... .......... .......... .......... 25% 21.2M 24s 132100K .......... .......... .......... .......... .......... 25% 92.1M 24s 132150K .......... .......... .......... .......... .......... 25% 27.5M 24s 132200K .......... .......... .......... .......... .......... 25% 21.9M 24s 132250K .......... .......... .......... .......... .......... 25% 20.7M 24s 132300K .......... .......... .......... .......... .......... 25% 19.1M 24s 132350K .......... .......... .......... .......... .......... 25% 21.1M 24s 132400K .......... .......... .......... .......... .......... 25% 25.2M 24s 132450K .......... .......... .......... .......... .......... 25% 19.0M 24s 132500K .......... .......... .......... .......... .......... 26% 18.7M 24s 132550K .......... .......... .......... .......... .......... 26% 27.3M 24s 132600K .......... .......... .......... .......... .......... 26% 21.9M 24s 132650K .......... .......... .......... .......... .......... 26% 19.1M 24s 132700K .......... .......... .......... .......... .......... 26% 15.2M 24s 132750K .......... .......... .......... .......... .......... 26% 14.1M 24s 132800K .......... .......... .......... .......... .......... 26% 18.2M 24s 132850K .......... .......... .......... .......... .......... 26% 11.2M 24s 132900K .......... .......... .......... .......... .......... 26% 14.1M 24s 132950K .......... .......... .......... .......... .......... 26% 9.07M 24s 133000K .......... .......... .......... .......... .......... 26% 11.1M 24s 133050K .......... .......... .......... .......... .......... 26% 8.26M 24s 133100K .......... .......... .......... .......... .......... 26% 4.74M 24s 133150K .......... .......... .......... .......... .......... 26% 18.8M 24s 133200K .......... .......... .......... .......... .......... 26% 14.2M 24s 133250K .......... .......... .......... .......... .......... 26% 22.1M 24s 133300K .......... .......... .......... .......... .......... 26% 19.9M 24s 133350K .......... .......... .......... .......... .......... 26% 22.3M 24s 133400K .......... .......... .......... .......... .......... 26% 19.8M 24s 133450K .......... .......... .......... .......... .......... 26% 25.1M 24s 133500K .......... .......... .......... .......... .......... 26% 22.3M 24s 133550K .......... .......... .......... .......... .......... 26% 20.9M 24s 133600K .......... .......... .......... .......... .......... 26% 15.8M 24s 133650K .......... .......... .......... .......... .......... 26% 20.9M 24s 133700K .......... .......... .......... .......... .......... 26% 13.6M 24s 133750K .......... .......... .......... .......... .......... 26% 18.1M 24s 133800K .......... .......... .......... .......... .......... 26% 18.0M 24s 133850K .......... .......... .......... .......... .......... 26% 14.0M 24s 133900K .......... .......... .......... .......... .......... 26% 16.5M 24s 133950K .......... .......... .......... .......... .......... 26% 17.2M 24s 134000K .......... .......... .......... .......... .......... 26% 16.6M 24s 134050K .......... .......... .......... .......... .......... 26% 20.4M 24s 134100K .......... .......... .......... .......... .......... 26% 12.7M 24s 134150K .......... .......... .......... .......... .......... 26% 16.0M 24s 134200K .......... .......... .......... .......... .......... 26% 9.32M 24s 134250K .......... .......... .......... .......... .......... 26% 12.5M 24s 134300K .......... .......... .......... .......... .......... 26% 11.2M 24s 134350K .......... .......... .......... .......... .......... 26% 11.2M 24s 134400K .......... .......... .......... .......... .......... 26% 10.2M 24s 134450K .......... .......... .......... .......... .......... 26% 9.74M 24s 134500K .......... .......... .......... .......... .......... 26% 7.94M 24s 134550K .......... .......... .......... .......... .......... 26% 7.96M 24s 134600K .......... .......... .......... .......... .......... 26% 7.77M 24s 134650K .......... .......... .......... .......... .......... 26% 8.86M 24s 134700K .......... .......... .......... .......... .......... 26% 9.55M 24s 134750K .......... .......... .......... .......... .......... 26% 10.2M 24s 134800K .......... .......... .......... .......... .......... 26% 9.06M 24s 134850K .......... .......... .......... .......... .......... 26% 5.59M 24s 134900K .......... .......... .......... .......... .......... 26% 8.13M 24s 134950K .......... .......... .......... .......... .......... 26% 5.37M 24s 135000K .......... .......... .......... .......... .......... 26% 7.50M 24s 135050K .......... .......... .......... .......... .......... 26% 6.66M 24s 135100K .......... .......... .......... .......... .......... 26% 5.69M 24s 135150K .......... .......... .......... .......... .......... 26% 7.13M 24s 135200K .......... .......... .......... .......... .......... 26% 5.86M 24s 135250K .......... .......... .......... .......... .......... 26% 7.52M 24s 135300K .......... .......... .......... .......... .......... 26% 11.1M 24s 135350K .......... .......... .......... .......... .......... 26% 24.6M 24s 135400K .......... .......... .......... .......... .......... 26% 14.5M 24s 135450K .......... .......... .......... .......... .......... 26% 15.7M 24s 135500K .......... .......... .......... .......... .......... 26% 16.4M 24s 135550K .......... .......... .......... .......... .......... 26% 13.5M 24s 135600K .......... .......... .......... .......... .......... 26% 10.3M 24s 135650K .......... .......... .......... .......... .......... 26% 12.7M 24s 135700K .......... .......... .......... .......... .......... 26% 11.5M 24s 135750K .......... .......... .......... .......... .......... 26% 13.1M 24s 135800K .......... .......... .......... .......... .......... 26% 13.2M 24s 135850K .......... .......... .......... .......... .......... 26% 10.9M 24s 135900K .......... .......... .......... .......... .......... 26% 13.1M 24s 135950K .......... .......... .......... .......... .......... 26% 9.67M 24s 136000K .......... .......... .......... .......... .......... 26% 19.8M 24s 136050K .......... .......... .......... .......... .......... 26% 38.0M 24s 136100K .......... .......... .......... .......... .......... 26% 27.7M 24s 136150K .......... .......... .......... .......... .......... 26% 38.2M 24s 136200K .......... .......... .......... .......... .......... 26% 24.7M 24s 136250K .......... .......... .......... .......... .......... 26% 26.7M 24s 136300K .......... .......... .......... .......... .......... 26% 25.6M 24s 136350K .......... .......... .......... .......... .......... 26% 27.3M 24s 136400K .......... .......... .......... .......... .......... 26% 22.0M 24s 136450K .......... .......... .......... .......... .......... 26% 22.9M 24s 136500K .......... .......... .......... .......... .......... 26% 19.1M 24s 136550K .......... .......... .......... .......... .......... 26% 23.9M 24s 136600K .......... .......... .......... .......... .......... 26% 20.8M 24s 136650K .......... .......... .......... .......... .......... 26% 16.6M 24s 136700K .......... .......... .......... .......... .......... 26% 23.4M 24s 136750K .......... .......... .......... .......... .......... 26% 26.8M 24s 136800K .......... .......... .......... .......... .......... 26% 24.9M 24s 136850K .......... .......... .......... .......... .......... 26% 21.2M 24s 136900K .......... .......... .......... .......... .......... 26% 25.4M 24s 136950K .......... .......... .......... .......... .......... 26% 23.3M 24s 137000K .......... .......... .......... .......... .......... 26% 26.4M 24s 137050K .......... .......... .......... .......... .......... 26% 24.5M 24s 137100K .......... .......... .......... .......... .......... 26% 21.8M 24s 137150K .......... .......... .......... .......... .......... 26% 23.7M 24s 137200K .......... .......... .......... .......... .......... 26% 18.0M 24s 137250K .......... .......... .......... .......... .......... 26% 25.0M 24s 137300K .......... .......... .......... .......... .......... 26% 24.9M 24s 137350K .......... .......... .......... .......... .......... 26% 31.6M 24s 137400K .......... .......... .......... .......... .......... 26% 62.3M 24s 137450K .......... .......... .......... .......... .......... 26% 21.7M 24s 137500K .......... .......... .......... .......... .......... 26% 307M 23s 137550K .......... .......... .......... .......... .......... 26% 40.7M 23s 137600K .......... .......... .......... .......... .......... 27% 92.7M 23s 137650K .......... .......... .......... .......... .......... 27% 60.1M 23s 137700K .......... .......... .......... .......... .......... 27% 86.3M 23s 137750K .......... .......... .......... .......... .......... 27% 30.2M 23s 137800K .......... .......... .......... .......... .......... 27% 82.2M 23s 137850K .......... .......... .......... .......... .......... 27% 22.2M 23s 137900K .......... .......... .......... .......... .......... 27% 34.5M 23s 137950K .......... .......... .......... .......... .......... 27% 23.4M 23s 138000K .......... .......... .......... .......... .......... 27% 38.0M 23s 138050K .......... .......... .......... .......... .......... 27% 31.6M 23s 138100K .......... .......... .......... .......... .......... 27% 23.5M 23s 138150K .......... .......... .......... .......... .......... 27% 29.3M 23s 138200K .......... .......... .......... .......... .......... 27% 22.4M 23s 138250K .......... .......... .......... .......... .......... 27% 23.6M 23s 138300K .......... .......... .......... .......... .......... 27% 25.2M 23s 138350K .......... .......... .......... .......... .......... 27% 21.0M 23s 138400K .......... .......... .......... .......... .......... 27% 23.8M 23s 138450K .......... .......... .......... .......... .......... 27% 23.3M 23s 138500K .......... .......... .......... .......... .......... 27% 22.3M 23s 138550K .......... .......... .......... .......... .......... 27% 24.9M 23s 138600K .......... .......... .......... .......... .......... 27% 18.8M 23s 138650K .......... .......... .......... .......... .......... 27% 26.7M 23s 138700K .......... .......... .......... .......... .......... 27% 22.2M 23s 138750K .......... .......... .......... .......... .......... 27% 24.7M 23s 138800K .......... .......... .......... .......... .......... 27% 27.2M 23s 138850K .......... .......... .......... .......... .......... 27% 20.6M 23s 138900K .......... .......... .......... .......... .......... 27% 20.9M 23s 138950K .......... .......... .......... .......... .......... 27% 21.1M 23s 139000K .......... .......... .......... .......... .......... 27% 25.4M 23s 139050K .......... .......... .......... .......... .......... 27% 23.7M 23s 139100K .......... .......... .......... .......... .......... 27% 359M 23s 139150K .......... .......... .......... .......... .......... 27% 29.1M 23s 139200K .......... .......... .......... .......... .......... 27% 53.8M 23s 139250K .......... .......... .......... .......... .......... 27% 26.5M 23s 139300K .......... .......... .......... .......... .......... 27% 56.5M 23s 139350K .......... .......... .......... .......... .......... 27% 20.7M 23s 139400K .......... .......... .......... .......... .......... 27% 37.7M 23s 139450K .......... .......... .......... .......... .......... 27% 22.2M 23s 139500K .......... .......... .......... .......... .......... 27% 27.0M 23s 139550K .......... .......... .......... .......... .......... 27% 28.6M 23s 139600K .......... .......... .......... .......... .......... 27% 17.8M 23s 139650K .......... .......... .......... .......... .......... 27% 15.1M 23s 139700K .......... .......... .......... .......... .......... 27% 11.9M 23s 139750K .......... .......... .......... .......... .......... 27% 15.2M 23s 139800K .......... .......... .......... .......... .......... 27% 14.2M 23s 139850K .......... .......... .......... .......... .......... 27% 14.1M 23s 139900K .......... .......... .......... .......... .......... 27% 17.1M 23s 139950K .......... .......... .......... .......... .......... 27% 14.4M 23s 140000K .......... .......... .......... .......... .......... 27% 13.8M 23s 140050K .......... .......... .......... .......... .......... 27% 19.7M 23s 140100K .......... .......... .......... .......... .......... 27% 14.4M 23s 140150K .......... .......... .......... .......... .......... 27% 17.0M 23s 140200K .......... .......... .......... .......... .......... 27% 15.1M 23s 140250K .......... .......... .......... .......... .......... 27% 17.2M 23s 140300K .......... .......... .......... .......... .......... 27% 27.4M 23s 140350K .......... .......... .......... .......... .......... 27% 32.1M 23s 140400K .......... .......... .......... .......... .......... 27% 68.8M 23s 140450K .......... .......... .......... .......... .......... 27% 31.3M 23s 140500K .......... .......... .......... .......... .......... 27% 27.2M 23s 140550K .......... .......... .......... .......... .......... 27% 34.2M 23s 140600K .......... .......... .......... .......... .......... 27% 20.1M 23s 140650K .......... .......... .......... .......... .......... 27% 20.8M 23s 140700K .......... .......... .......... .......... .......... 27% 26.4M 23s 140750K .......... .......... .......... .......... .......... 27% 25.1M 23s 140800K .......... .......... .......... .......... .......... 27% 27.4M 23s 140850K .......... .......... .......... .......... .......... 27% 22.6M 23s 140900K .......... .......... .......... .......... .......... 27% 28.6M 23s 140950K .......... .......... .......... .......... .......... 27% 19.2M 23s 141000K .......... .......... .......... .......... .......... 27% 25.2M 23s 141050K .......... .......... .......... .......... .......... 27% 24.9M 23s 141100K .......... .......... .......... .......... .......... 27% 15.8M 23s 141150K .......... .......... .......... .......... .......... 27% 21.1M 23s 141200K .......... .......... .......... .......... .......... 27% 12.3M 23s 141250K .......... .......... .......... .......... .......... 27% 11.8M 23s 141300K .......... .......... .......... .......... .......... 27% 12.6M 23s 141350K .......... .......... .......... .......... .......... 27% 9.26M 23s 141400K .......... .......... .......... .......... .......... 27% 14.5M 23s 141450K .......... .......... .......... .......... .......... 27% 8.66M 23s 141500K .......... .......... .......... .......... .......... 27% 14.8M 23s 141550K .......... .......... .......... .......... .......... 27% 11.6M 23s 141600K .......... .......... .......... .......... .......... 27% 11.8M 23s 141650K .......... .......... .......... .......... .......... 27% 23.6M 23s 141700K .......... .......... .......... .......... .......... 27% 31.4M 23s 141750K .......... .......... .......... .......... .......... 27% 22.1M 23s 141800K .......... .......... .......... .......... .......... 27% 130M 23s 141850K .......... .......... .......... .......... .......... 27% 18.6M 23s 141900K .......... .......... .......... .......... .......... 27% 38.1M 23s 141950K .......... .......... .......... .......... .......... 27% 18.0M 23s 142000K .......... .......... .......... .......... .......... 27% 16.3M 23s 142050K .......... .......... .......... .......... .......... 27% 17.4M 23s 142100K .......... .......... .......... .......... .......... 27% 11.1M 23s 142150K .......... .......... .......... .......... .......... 27% 25.2M 23s 142200K .......... .......... .......... .......... .......... 27% 13.4M 23s 142250K .......... .......... .......... .......... .......... 27% 23.5M 23s 142300K .......... .......... .......... .......... .......... 27% 18.2M 23s 142350K .......... .......... .......... .......... .......... 27% 12.4M 23s 142400K .......... .......... .......... .......... .......... 27% 12.2M 23s 142450K .......... .......... .......... .......... .......... 27% 11.8M 23s 142500K .......... .......... .......... .......... .......... 27% 12.3M 23s 142550K .......... .......... .......... .......... .......... 27% 13.0M 23s 142600K .......... .......... .......... .......... .......... 27% 8.40M 23s 142650K .......... .......... .......... .......... .......... 27% 17.4M 23s 142700K .......... .......... .......... .......... .......... 28% 13.1M 23s 142750K .......... .......... .......... .......... .......... 28% 14.1M 23s 142800K .......... .......... .......... .......... .......... 28% 16.5M 23s 142850K .......... .......... .......... .......... .......... 28% 14.1M 23s 142900K .......... .......... .......... .......... .......... 28% 15.1M 23s 142950K .......... .......... .......... .......... .......... 28% 10.9M 23s 143000K .......... .......... .......... .......... .......... 28% 15.0M 23s 143050K .......... .......... .......... .......... .......... 28% 12.2M 23s 143100K .......... .......... .......... .......... .......... 28% 11.8M 23s 143150K .......... .......... .......... .......... .......... 28% 15.5M 23s 143200K .......... .......... .......... .......... .......... 28% 12.0M 23s 143250K .......... .......... .......... .......... .......... 28% 13.4M 23s 143300K .......... .......... .......... .......... .......... 28% 13.5M 23s 143350K .......... .......... .......... .......... .......... 28% 11.6M 23s 143400K .......... .......... .......... .......... .......... 28% 10.6M 23s 143450K .......... .......... .......... .......... .......... 28% 13.0M 23s 143500K .......... .......... .......... .......... .......... 28% 18.7M 23s 143550K .......... .......... .......... .......... .......... 28% 8.83M 23s 143600K .......... .......... .......... .......... .......... 28% 11.7M 23s 143650K .......... .......... .......... .......... .......... 28% 11.8M 23s 143700K .......... .......... .......... .......... .......... 28% 9.78M 23s 143750K .......... .......... .......... .......... .......... 28% 10.9M 23s 143800K .......... .......... .......... .......... .......... 28% 11.9M 23s 143850K .......... .......... .......... .......... .......... 28% 7.57M 23s 143900K .......... .......... .......... .......... .......... 28% 7.61M 23s 143950K .......... .......... .......... .......... .......... 28% 15.1M 23s 144000K .......... .......... .......... .......... .......... 28% 22.2M 23s 144050K .......... .......... .......... .......... .......... 28% 24.5M 23s 144100K .......... .......... .......... .......... .......... 28% 19.5M 23s 144150K .......... .......... .......... .......... .......... 28% 18.7M 23s 144200K .......... .......... .......... .......... .......... 28% 23.8M 23s 144250K .......... .......... .......... .......... .......... 28% 15.9M 23s 144300K .......... .......... .......... .......... .......... 28% 21.3M 23s 144350K .......... .......... .......... .......... .......... 28% 14.6M 23s 144400K .......... .......... .......... .......... .......... 28% 15.2M 23s 144450K .......... .......... .......... .......... .......... 28% 18.9M 23s 144500K .......... .......... .......... .......... .......... 28% 16.6M 23s 144550K .......... .......... .......... .......... .......... 28% 20.0M 23s 144600K .......... .......... .......... .......... .......... 28% 16.6M 23s 144650K .......... .......... .......... .......... .......... 28% 25.2M 23s 144700K .......... .......... .......... .......... .......... 28% 18.1M 23s 144750K .......... .......... .......... .......... .......... 28% 19.2M 23s 144800K .......... .......... .......... .......... .......... 28% 19.8M 23s 144850K .......... .......... .......... .......... .......... 28% 29.0M 23s 144900K .......... .......... .......... .......... .......... 28% 42.1M 23s 144950K .......... .......... .......... .......... .......... 28% 26.9M 23s 145000K .......... .......... .......... .......... .......... 28% 235M 23s 145050K .......... .......... .......... .......... .......... 28% 52.7M 23s 145100K .......... .......... .......... .......... .......... 28% 28.7M 23s 145150K .......... .......... .......... .......... .......... 28% 116M 23s 145200K .......... .......... .......... .......... .......... 28% 28.2M 23s 145250K .......... .......... .......... .......... .......... 28% 36.5M 23s 145300K .......... .......... .......... .......... .......... 28% 27.3M 23s 145350K .......... .......... .......... .......... .......... 28% 21.2M 23s 145400K .......... .......... .......... .......... .......... 28% 31.7M 23s 145450K .......... .......... .......... .......... .......... 28% 20.9M 23s 145500K .......... .......... .......... .......... .......... 28% 21.1M 23s 145550K .......... .......... .......... .......... .......... 28% 21.8M 23s 145600K .......... .......... .......... .......... .......... 28% 23.8M 23s 145650K .......... .......... .......... .......... .......... 28% 17.8M 23s 145700K .......... .......... .......... .......... .......... 28% 18.1M 23s 145750K .......... .......... .......... .......... .......... 28% 17.0M 23s 145800K .......... .......... .......... .......... .......... 28% 17.7M 23s 145850K .......... .......... .......... .......... .......... 28% 13.1M 23s 145900K .......... .......... .......... .......... .......... 28% 19.9M 23s 145950K .......... .......... .......... .......... .......... 28% 14.6M 23s 146000K .......... .......... .......... .......... .......... 28% 19.9M 23s 146050K .......... .......... .......... .......... .......... 28% 11.5M 23s 146100K .......... .......... .......... .......... .......... 28% 11.4M 23s 146150K .......... .......... .......... .......... .......... 28% 10.7M 23s 146200K .......... .......... .......... .......... .......... 28% 10.0M 23s 146250K .......... .......... .......... .......... .......... 28% 11.6M 23s 146300K .......... .......... .......... .......... .......... 28% 13.1M 23s 146350K .......... .......... .......... .......... .......... 28% 8.05M 23s 146400K .......... .......... .......... .......... .......... 28% 9.91M 23s 146450K .......... .......... .......... .......... .......... 28% 10.2M 23s 146500K .......... .......... .......... .......... .......... 28% 9.47M 23s 146550K .......... .......... .......... .......... .......... 28% 10.1M 23s 146600K .......... .......... .......... .......... .......... 28% 7.95M 23s 146650K .......... .......... .......... .......... .......... 28% 8.99M 23s 146700K .......... .......... .......... .......... .......... 28% 22.0M 23s 146750K .......... .......... .......... .......... .......... 28% 41.2M 23s 146800K .......... .......... .......... .......... .......... 28% 23.3M 23s 146850K .......... .......... .......... .......... .......... 28% 80.3M 23s 146900K .......... .......... .......... .......... .......... 28% 17.2M 23s 146950K .......... .......... .......... .......... .......... 28% 34.1M 23s 147000K .......... .......... .......... .......... .......... 28% 20.6M 23s 147050K .......... .......... .......... .......... .......... 28% 20.1M 23s 147100K .......... .......... .......... .......... .......... 28% 15.6M 23s 147150K .......... .......... .......... .......... .......... 28% 17.5M 23s 147200K .......... .......... .......... .......... .......... 28% 15.1M 23s 147250K .......... .......... .......... .......... .......... 28% 12.2M 23s 147300K .......... .......... .......... .......... .......... 28% 8.25M 23s 147350K .......... .......... .......... .......... .......... 28% 9.38M 23s 147400K .......... .......... .......... .......... .......... 28% 9.99M 23s 147450K .......... .......... .......... .......... .......... 28% 7.32M 23s 147500K .......... .......... .......... .......... .......... 28% 9.32M 23s 147550K .......... .......... .......... .......... .......... 28% 4.66M 23s 147600K .......... .......... .......... .......... .......... 28% 7.40M 23s 147650K .......... .......... .......... .......... .......... 28% 16.3M 23s 147700K .......... .......... .......... .......... .......... 28% 17.4M 23s 147750K .......... .......... .......... .......... .......... 28% 17.8M 23s 147800K .......... .......... .......... .......... .......... 29% 14.8M 23s 147850K .......... .......... .......... .......... .......... 29% 17.3M 23s 147900K .......... .......... .......... .......... .......... 29% 13.5M 23s 147950K .......... .......... .......... .......... .......... 29% 18.0M 23s 148000K .......... .......... .......... .......... .......... 29% 16.5M 23s 148050K .......... .......... .......... .......... .......... 29% 19.1M 23s 148100K .......... .......... .......... .......... .......... 29% 14.1M 23s 148150K .......... .......... .......... .......... .......... 29% 12.7M 23s 148200K .......... .......... .......... .......... .......... 29% 11.4M 23s 148250K .......... .......... .......... .......... .......... 29% 15.9M 23s 148300K .......... .......... .......... .......... .......... 29% 22.2M 23s 148350K .......... .......... .......... .......... .......... 29% 15.9M 23s 148400K .......... .......... .......... .......... .......... 29% 15.3M 23s 148450K .......... .......... .......... .......... .......... 29% 16.7M 23s 148500K .......... .......... .......... .......... .......... 29% 21.2M 23s 148550K .......... .......... .......... .......... .......... 29% 21.0M 23s 148600K .......... .......... .......... .......... .......... 29% 15.8M 23s 148650K .......... .......... .......... .......... .......... 29% 22.1M 23s 148700K .......... .......... .......... .......... .......... 29% 14.7M 23s 148750K .......... .......... .......... .......... .......... 29% 18.8M 23s 148800K .......... .......... .......... .......... .......... 29% 22.0M 23s 148850K .......... .......... .......... .......... .......... 29% 23.8M 23s 148900K .......... .......... .......... .......... .......... 29% 72.1M 23s 148950K .......... .......... .......... .......... .......... 29% 47.2M 23s 149000K .......... .......... .......... .......... .......... 29% 46.9M 23s 149050K .......... .......... .......... .......... .......... 29% 60.7M 23s 149100K .......... .......... .......... .......... .......... 29% 25.1M 23s 149150K .......... .......... .......... .......... .......... 29% 417M 23s 149200K .......... .......... .......... .......... .......... 29% 24.5M 23s 149250K .......... .......... .......... .......... .......... 29% 448M 23s 149300K .......... .......... .......... .......... .......... 29% 37.4M 23s 149350K .......... .......... .......... .......... .......... 29% 42.9M 23s 149400K .......... .......... .......... .......... .......... 29% 45.3M 23s 149450K .......... .......... .......... .......... .......... 29% 25.1M 23s 149500K .......... .......... .......... .......... .......... 29% 48.4M 23s 149550K .......... .......... .......... .......... .......... 29% 31.2M 23s 149600K .......... .......... .......... .......... .......... 29% 38.1M 23s 149650K .......... .......... .......... .......... .......... 29% 32.9M 23s 149700K .......... .......... .......... .......... .......... 29% 25.3M 23s 149750K .......... .......... .......... .......... .......... 29% 21.1M 22s 149800K .......... .......... .......... .......... .......... 29% 22.4M 22s 149850K .......... .......... .......... .......... .......... 29% 16.5M 22s 149900K .......... .......... .......... .......... .......... 29% 23.8M 22s 149950K .......... .......... .......... .......... .......... 29% 16.5M 22s 150000K .......... .......... .......... .......... .......... 29% 23.6M 22s 150050K .......... .......... .......... .......... .......... 29% 18.2M 22s 150100K .......... .......... .......... .......... .......... 29% 15.8M 22s 150150K .......... .......... .......... .......... .......... 29% 17.6M 22s 150200K .......... .......... .......... .......... .......... 29% 13.2M 22s 150250K .......... .......... .......... .......... .......... 29% 13.3M 22s 150300K .......... .......... .......... .......... .......... 29% 16.5M 22s 150350K .......... .......... .......... .......... .......... 29% 10.9M 22s 150400K .......... .......... .......... .......... .......... 29% 13.6M 22s 150450K .......... .......... .......... .......... .......... 29% 10.6M 22s 150500K .......... .......... .......... .......... .......... 29% 11.2M 22s 150550K .......... .......... .......... .......... .......... 29% 11.9M 22s 150600K .......... .......... .......... .......... .......... 29% 10.0M 22s 150650K .......... .......... .......... .......... .......... 29% 10.1M 22s 150700K .......... .......... .......... .......... .......... 29% 9.42M 22s 150750K .......... .......... .......... .......... .......... 29% 26.4M 22s 150800K .......... .......... .......... .......... .......... 29% 25.2M 22s 150850K .......... .......... .......... .......... .......... 29% 16.0M 22s 150900K .......... .......... .......... .......... .......... 29% 31.2M 22s 150950K .......... .......... .......... .......... .......... 29% 29.2M 22s 151000K .......... .......... .......... .......... .......... 29% 22.2M 22s 151050K .......... .......... .......... .......... .......... 29% 18.8M 22s 151100K .......... .......... .......... .......... .......... 29% 21.1M 22s 151150K .......... .......... .......... .......... .......... 29% 19.0M 22s 151200K .......... .......... .......... .......... .......... 29% 18.0M 22s 151250K .......... .......... .......... .......... .......... 29% 19.8M 22s 151300K .......... .......... .......... .......... .......... 29% 18.1M 22s 151350K .......... .......... .......... .......... .......... 29% 15.1M 22s 151400K .......... .......... .......... .......... .......... 29% 20.1M 22s 151450K .......... .......... .......... .......... .......... 29% 14.2M 22s 151500K .......... .......... .......... .......... .......... 29% 15.2M 22s 151550K .......... .......... .......... .......... .......... 29% 17.9M 22s 151600K .......... .......... .......... .......... .......... 29% 15.0M 22s 151650K .......... .......... .......... .......... .......... 29% 14.6M 22s 151700K .......... .......... .......... .......... .......... 29% 12.6M 22s 151750K .......... .......... .......... .......... .......... 29% 18.0M 22s 151800K .......... .......... .......... .......... .......... 29% 20.1M 22s 151850K .......... .......... .......... .......... .......... 29% 9.03M 22s 151900K .......... .......... .......... .......... .......... 29% 12.2M 22s 151950K .......... .......... .......... .......... .......... 29% 12.7M 22s 152000K .......... .......... .......... .......... .......... 29% 12.7M 22s 152050K .......... .......... .......... .......... .......... 29% 12.5M 22s 152100K .......... .......... .......... .......... .......... 29% 9.08M 22s 152150K .......... .......... .......... .......... .......... 29% 12.1M 22s 152200K .......... .......... .......... .......... .......... 29% 10.9M 22s 152250K .......... .......... .......... .......... .......... 29% 14.0M 22s 152300K .......... .......... .......... .......... .......... 29% 12.3M 22s 152350K .......... .......... .......... .......... .......... 29% 10.6M 22s 152400K .......... .......... .......... .......... .......... 29% 10.0M 22s 152450K .......... .......... .......... .......... .......... 29% 9.99M 22s 152500K .......... .......... .......... .......... .......... 29% 16.0M 22s 152550K .......... .......... .......... .......... .......... 29% 14.3M 22s 152600K .......... .......... .......... .......... .......... 29% 9.79M 22s 152650K .......... .......... .......... .......... .......... 29% 8.86M 22s 152700K .......... .......... .......... .......... .......... 29% 9.51M 22s 152750K .......... .......... .......... .......... .......... 29% 12.4M 22s 152800K .......... .......... .......... .......... .......... 29% 11.6M 22s 152850K .......... .......... .......... .......... .......... 29% 11.4M 22s 152900K .......... .......... .......... .......... .......... 30% 15.0M 22s 152950K .......... .......... .......... .......... .......... 30% 13.7M 22s 153000K .......... .......... .......... .......... .......... 30% 35.2M 22s 153050K .......... .......... .......... .......... .......... 30% 36.1M 22s 153100K .......... .......... .......... .......... .......... 30% 22.9M 22s 153150K .......... .......... .......... .......... .......... 30% 581M 22s 153200K .......... .......... .......... .......... .......... 30% 43.4M 22s 153250K .......... .......... .......... .......... .......... 30% 48.2M 22s 153300K .......... .......... .......... .......... .......... 30% 37.3M 22s 153350K .......... .......... .......... .......... .......... 30% 47.2M 22s 153400K .......... .......... .......... .......... .......... 30% 42.3M 22s 153450K .......... .......... .......... .......... .......... 30% 30.9M 22s 153500K .......... .......... .......... .......... .......... 30% 37.5M 22s 153550K .......... .......... .......... .......... .......... 30% 54.3M 22s 153600K .......... .......... .......... .......... .......... 30% 45.3M 22s 153650K .......... .......... .......... .......... .......... 30% 46.2M 22s 153700K .......... .......... .......... .......... .......... 30% 33.5M 22s 153750K .......... .......... .......... .......... .......... 30% 52.0M 22s 153800K .......... .......... .......... .......... .......... 30% 37.8M 22s 153850K .......... .......... .......... .......... .......... 30% 30.6M 22s 153900K .......... .......... .......... .......... .......... 30% 47.6M 22s 153950K .......... .......... .......... .......... .......... 30% 33.4M 22s 154000K .......... .......... .......... .......... .......... 30% 40.9M 22s 154050K .......... .......... .......... .......... .......... 30% 34.7M 22s 154100K .......... .......... .......... .......... .......... 30% 26.8M 22s 154150K .......... .......... .......... .......... .......... 30% 41.4M 22s 154200K .......... .......... .......... .......... .......... 30% 22.5M 22s 154250K .......... .......... .......... .......... .......... 30% 26.8M 22s 154300K .......... .......... .......... .......... .......... 30% 37.2M 22s 154350K .......... .......... .......... .......... .......... 30% 28.1M 22s 154400K .......... .......... .......... .......... .......... 30% 28.3M 22s 154450K .......... .......... .......... .......... .......... 30% 17.9M 22s 154500K .......... .......... .......... .......... .......... 30% 25.4M 22s 154550K .......... .......... .......... .......... .......... 30% 7.60M 22s 154600K .......... .......... .......... .......... .......... 30% 9.97M 22s 154650K .......... .......... .......... .......... .......... 30% 10.8M 22s 154700K .......... .......... .......... .......... .......... 30% 8.87M 22s 154750K .......... .......... .......... .......... .......... 30% 10.9M 22s 154800K .......... .......... .......... .......... .......... 30% 10.6M 22s 154850K .......... .......... .......... .......... .......... 30% 7.49M 22s 154900K .......... .......... .......... .......... .......... 30% 8.51M 22s 154950K .......... .......... .......... .......... .......... 30% 13.5M 22s 155000K .......... .......... .......... .......... .......... 30% 15.7M 22s 155050K .......... .......... .......... .......... .......... 30% 23.8M 22s 155100K .......... .......... .......... .......... .......... 30% 17.3M 22s 155150K .......... .......... .......... .......... .......... 30% 17.8M 22s 155200K .......... .......... .......... .......... .......... 30% 14.1M 22s 155250K .......... .......... .......... .......... .......... 30% 17.8M 22s 155300K .......... .......... .......... .......... .......... 30% 12.7M 22s 155350K .......... .......... .......... .......... .......... 30% 9.67M 22s 155400K .......... .......... .......... .......... .......... 30% 12.3M 22s 155450K .......... .......... .......... .......... .......... 30% 9.48M 22s 155500K .......... .......... .......... .......... .......... 30% 10.6M 22s 155550K .......... .......... .......... .......... .......... 30% 8.50M 22s 155600K .......... .......... .......... .......... .......... 30% 7.93M 22s 155650K .......... .......... .......... .......... .......... 30% 10.3M 22s 155700K .......... .......... .......... .......... .......... 30% 29.8M 22s 155750K .......... .......... .......... .......... .......... 30% 32.1M 22s 155800K .......... .......... .......... .......... .......... 30% 25.1M 22s 155850K .......... .......... .......... .......... .......... 30% 26.2M 22s 155900K .......... .......... .......... .......... .......... 30% 31.6M 22s 155950K .......... .......... .......... .......... .......... 30% 17.2M 22s 156000K .......... .......... .......... .......... .......... 30% 22.0M 22s 156050K .......... .......... .......... .......... .......... 30% 15.2M 22s 156100K .......... .......... .......... .......... .......... 30% 9.92M 22s 156150K .......... .......... .......... .......... .......... 30% 12.8M 22s 156200K .......... .......... .......... .......... .......... 30% 8.27M 22s 156250K .......... .......... .......... .......... .......... 30% 7.86M 22s 156300K .......... .......... .......... .......... .......... 30% 8.22M 22s 156350K .......... .......... .......... .......... .......... 30% 4.14M 22s 156400K .......... .......... .......... .......... .......... 30% 3.68M 22s 156450K .......... .......... .......... .......... .......... 30% 4.98M 22s 156500K .......... .......... .......... .......... .......... 30% 16.6M 22s 156550K .......... .......... .......... .......... .......... 30% 23.1M 22s 156600K .......... .......... .......... .......... .......... 30% 21.6M 22s 156650K .......... .......... .......... .......... .......... 30% 27.3M 22s 156700K .......... .......... .......... .......... .......... 30% 15.4M 22s 156750K .......... .......... .......... .......... .......... 30% 20.2M 22s 156800K .......... .......... .......... .......... .......... 30% 15.9M 22s 156850K .......... .......... .......... .......... .......... 30% 13.4M 22s 156900K .......... .......... .......... .......... .......... 30% 17.8M 22s 156950K .......... .......... .......... .......... .......... 30% 13.0M 22s 157000K .......... .......... .......... .......... .......... 30% 12.9M 22s 157050K .......... .......... .......... .......... .......... 30% 17.2M 22s 157100K .......... .......... .......... .......... .......... 30% 12.7M 22s 157150K .......... .......... .......... .......... .......... 30% 17.0M 22s 157200K .......... .......... .......... .......... .......... 30% 13.1M 22s 157250K .......... .......... .......... .......... .......... 30% 15.8M 22s 157300K .......... .......... .......... .......... .......... 30% 15.7M 22s 157350K .......... .......... .......... .......... .......... 30% 26.7M 22s 157400K .......... .......... .......... .......... .......... 30% 30.2M 22s 157450K .......... .......... .......... .......... .......... 30% 26.8M 22s 157500K .......... .......... .......... .......... .......... 30% 11.7M 22s 157550K .......... .......... .......... .......... .......... 30% 421M 22s 157600K .......... .......... .......... .......... .......... 30% 11.9M 22s 157650K .......... .......... .......... .......... .......... 30% 18.6M 22s 157700K .......... .......... .......... .......... .......... 30% 19.6M 22s 157750K .......... .......... .......... .......... .......... 30% 12.9M 22s 157800K .......... .......... .......... .......... .......... 30% 18.8M 22s 157850K .......... .......... .......... .......... .......... 30% 13.6M 22s 157900K .......... .......... .......... .......... .......... 30% 10.1M 22s 157950K .......... .......... .......... .......... .......... 30% 12.5M 22s 158000K .......... .......... .......... .......... .......... 31% 14.6M 22s 158050K .......... .......... .......... .......... .......... 31% 14.6M 22s 158100K .......... .......... .......... .......... .......... 31% 9.64M 22s 158150K .......... .......... .......... .......... .......... 31% 11.4M 22s 158200K .......... .......... .......... .......... .......... 31% 9.03M 22s 158250K .......... .......... .......... .......... .......... 31% 10.4M 22s 158300K .......... .......... .......... .......... .......... 31% 10.6M 22s 158350K .......... .......... .......... .......... .......... 31% 7.87M 22s 158400K .......... .......... .......... .......... .......... 31% 10.2M 22s 158450K .......... .......... .......... .......... .......... 31% 8.00M 22s 158500K .......... .......... .......... .......... .......... 31% 8.90M 22s 158550K .......... .......... .......... .......... .......... 31% 7.96M 22s 158600K .......... .......... .......... .......... .......... 31% 7.95M 22s 158650K .......... .......... .......... .......... .......... 31% 9.73M 22s 158700K .......... .......... .......... .......... .......... 31% 19.2M 22s 158750K .......... .......... .......... .......... .......... 31% 37.6M 22s 158800K .......... .......... .......... .......... .......... 31% 34.5M 22s 158850K .......... .......... .......... .......... .......... 31% 21.2M 22s 158900K .......... .......... .......... .......... .......... 31% 34.2M 22s 158950K .......... .......... .......... .......... .......... 31% 14.0M 22s 159000K .......... .......... .......... .......... .......... 31% 186M 22s 159050K .......... .......... .......... .......... .......... 31% 20.4M 22s 159100K .......... .......... .......... .......... .......... 31% 20.9M 22s 159150K .......... .......... .......... .......... .......... 31% 28.7M 22s 159200K .......... .......... .......... .......... .......... 31% 18.9M 22s 159250K .......... .......... .......... .......... .......... 31% 37.8M 22s 159300K .......... .......... .......... .......... .......... 31% 17.4M 22s 159350K .......... .......... .......... .......... .......... 31% 15.2M 22s 159400K .......... .......... .......... .......... .......... 31% 25.0M 22s 159450K .......... .......... .......... .......... .......... 31% 10.9M 22s 159500K .......... .......... .......... .......... .......... 31% 13.9M 22s 159550K .......... .......... .......... .......... .......... 31% 16.5M 22s 159600K .......... .......... .......... .......... .......... 31% 13.0M 22s 159650K .......... .......... .......... .......... .......... 31% 19.0M 22s 159700K .......... .......... .......... .......... .......... 31% 10.3M 22s 159750K .......... .......... .......... .......... .......... 31% 13.6M 22s 159800K .......... .......... .......... .......... .......... 31% 12.6M 22s 159850K .......... .......... .......... .......... .......... 31% 10.2M 22s 159900K .......... .......... .......... .......... .......... 31% 12.2M 22s 159950K .......... .......... .......... .......... .......... 31% 10.2M 22s 160000K .......... .......... .......... .......... .......... 31% 14.1M 22s 160050K .......... .......... .......... .......... .......... 31% 12.7M 22s 160100K .......... .......... .......... .......... .......... 31% 11.5M 22s 160150K .......... .......... .......... .......... .......... 31% 37.7M 22s 160200K .......... .......... .......... .......... .......... 31% 22.6M 22s 160250K .......... .......... .......... .......... .......... 31% 36.0M 22s 160300K .......... .......... .......... .......... .......... 31% 38.1M 22s 160350K .......... .......... .......... .......... .......... 31% 18.7M 22s 160400K .......... .......... .......... .......... .......... 31% 24.4M 22s 160450K .......... .......... .......... .......... .......... 31% 26.7M 22s 160500K .......... .......... .......... .......... .......... 31% 31.2M 22s 160550K .......... .......... .......... .......... .......... 31% 31.4M 22s 160600K .......... .......... .......... .......... .......... 31% 27.0M 22s 160650K .......... .......... .......... .......... .......... 31% 37.7M 22s 160700K .......... .......... .......... .......... .......... 31% 22.1M 22s 160750K .......... .......... .......... .......... .......... 31% 31.6M 22s 160800K .......... .......... .......... .......... .......... 31% 19.6M 22s 160850K .......... .......... .......... .......... .......... 31% 38.1M 22s 160900K .......... .......... .......... .......... .......... 31% 17.6M 22s 160950K .......... .......... .......... .......... .......... 31% 13.5M 22s 161000K .......... .......... .......... .......... .......... 31% 18.7M 22s 161050K .......... .......... .......... .......... .......... 31% 25.0M 22s 161100K .......... .......... .......... .......... .......... 31% 13.9M 22s 161150K .......... .......... .......... .......... .......... 31% 14.1M 22s 161200K .......... .......... .......... .......... .......... 31% 9.55M 22s 161250K .......... .......... .......... .......... .......... 31% 10.6M 22s 161300K .......... .......... .......... .......... .......... 31% 14.8M 22s 161350K .......... .......... .......... .......... .......... 31% 6.50M 22s 161400K .......... .......... .......... .......... .......... 31% 6.42M 22s 161450K .......... .......... .......... .......... .......... 31% 5.86M 22s 161500K .......... .......... .......... .......... .......... 31% 6.38M 22s 161550K .......... .......... .......... .......... .......... 31% 6.35M 22s 161600K .......... .......... .......... .......... .......... 31% 3.72M 22s 161650K .......... .......... .......... .......... .......... 31% 4.68M 22s 161700K .......... .......... .......... .......... .......... 31% 7.03M 22s 161750K .......... .......... .......... .......... .......... 31% 14.7M 22s 161800K .......... .......... .......... .......... .......... 31% 28.8M 22s 161850K .......... .......... .......... .......... .......... 31% 37.0M 22s 161900K .......... .......... .......... .......... .......... 31% 24.2M 22s 161950K .......... .......... .......... .......... .......... 31% 28.3M 22s 162000K .......... .......... .......... .......... .......... 31% 20.8M 22s 162050K .......... .......... .......... .......... .......... 31% 34.0M 22s 162100K .......... .......... .......... .......... .......... 31% 22.3M 22s 162150K .......... .......... .......... .......... .......... 31% 23.8M 22s 162200K .......... .......... .......... .......... .......... 31% 18.1M 22s 162250K .......... .......... .......... .......... .......... 31% 12.2M 22s 162300K .......... .......... .......... .......... .......... 31% 11.6M 22s 162350K .......... .......... .......... .......... .......... 31% 9.08M 22s 162400K .......... .......... .......... .......... .......... 31% 12.2M 22s 162450K .......... .......... .......... .......... .......... 31% 12.6M 22s 162500K .......... .......... .......... .......... .......... 31% 13.5M 22s 162550K .......... .......... .......... .......... .......... 31% 16.7M 22s 162600K .......... .......... .......... .......... .......... 31% 14.0M 22s 162650K .......... .......... .......... .......... .......... 31% 16.4M 22s 162700K .......... .......... .......... .......... .......... 31% 13.1M 22s 162750K .......... .......... .......... .......... .......... 31% 14.4M 22s 162800K .......... .......... .......... .......... .......... 31% 12.0M 22s 162850K .......... .......... .......... .......... .......... 31% 9.16M 22s 162900K .......... .......... .......... .......... .......... 31% 12.5M 22s 162950K .......... .......... .......... .......... .......... 31% 9.85M 22s 163000K .......... .......... .......... .......... .......... 31% 13.1M 22s 163050K .......... .......... .......... .......... .......... 31% 8.01M 22s 163100K .......... .......... .......... .......... .......... 32% 7.44M 22s 163150K .......... .......... .......... .......... .......... 32% 6.83M 22s 163200K .......... .......... .......... .......... .......... 32% 6.26M 22s 163250K .......... .......... .......... .......... .......... 32% 7.91M 22s 163300K .......... .......... .......... .......... .......... 32% 8.06M 22s 163350K .......... .......... .......... .......... .......... 32% 12.9M 22s 163400K .......... .......... .......... .......... .......... 32% 31.4M 22s 163450K .......... .......... .......... .......... .......... 32% 19.5M 22s 163500K .......... .......... .......... .......... .......... 32% 29.2M 22s 163550K .......... .......... .......... .......... .......... 32% 23.1M 22s 163600K .......... .......... .......... .......... .......... 32% 13.1M 22s 163650K .......... .......... .......... .......... .......... 32% 15.1M 22s 163700K .......... .......... .......... .......... .......... 32% 14.7M 22s 163750K .......... .......... .......... .......... .......... 32% 17.8M 22s 163800K .......... .......... .......... .......... .......... 32% 17.2M 22s 163850K .......... .......... .......... .......... .......... 32% 18.8M 22s 163900K .......... .......... .......... .......... .......... 32% 11.8M 22s 163950K .......... .......... .......... .......... .......... 32% 12.1M 22s 164000K .......... .......... .......... .......... .......... 32% 11.6M 22s 164050K .......... .......... .......... .......... .......... 32% 14.7M 22s 164100K .......... .......... .......... .......... .......... 32% 11.1M 22s 164150K .......... .......... .......... .......... .......... 32% 11.2M 22s 164200K .......... .......... .......... .......... .......... 32% 9.75M 22s 164250K .......... .......... .......... .......... .......... 32% 11.1M 22s 164300K .......... .......... .......... .......... .......... 32% 13.1M 22s 164350K .......... .......... .......... .......... .......... 32% 22.2M 22s 164400K .......... .......... .......... .......... .......... 32% 37.6M 22s 164450K .......... .......... .......... .......... .......... 32% 20.6M 22s 164500K .......... .......... .......... .......... .......... 32% 26.3M 22s 164550K .......... .......... .......... .......... .......... 32% 128M 22s 164600K .......... .......... .......... .......... .......... 32% 21.0M 22s 164650K .......... .......... .......... .......... .......... 32% 15.3M 22s 164700K .......... .......... .......... .......... .......... 32% 28.7M 22s 164750K .......... .......... .......... .......... .......... 32% 14.2M 22s 164800K .......... .......... .......... .......... .......... 32% 18.6M 22s 164850K .......... .......... .......... .......... .......... 32% 16.3M 22s 164900K .......... .......... .......... .......... .......... 32% 12.2M 22s 164950K .......... .......... .......... .......... .......... 32% 17.2M 22s 165000K .......... .......... .......... .......... .......... 32% 19.0M 22s 165050K .......... .......... .......... .......... .......... 32% 13.5M 22s 165100K .......... .......... .......... .......... .......... 32% 17.3M 22s 165150K .......... .......... .......... .......... .......... 32% 16.5M 22s 165200K .......... .......... .......... .......... .......... 32% 10.7M 22s 165250K .......... .......... .......... .......... .......... 32% 12.2M 22s 165300K .......... .......... .......... .......... .......... 32% 15.2M 22s 165350K .......... .......... .......... .......... .......... 32% 11.9M 22s 165400K .......... .......... .......... .......... .......... 32% 15.8M 22s 165450K .......... .......... .......... .......... .......... 32% 9.95M 22s 165500K .......... .......... .......... .......... .......... 32% 6.51M 22s 165550K .......... .......... .......... .......... .......... 32% 9.51M 22s 165600K .......... .......... .......... .......... .......... 32% 8.14M 22s 165650K .......... .......... .......... .......... .......... 32% 13.1M 22s 165700K .......... .......... .......... .......... .......... 32% 29.1M 22s 165750K .......... .......... .......... .......... .......... 32% 45.8M 22s 165800K .......... .......... .......... .......... .......... 32% 19.8M 22s 165850K .......... .......... .......... .......... .......... 32% 32.9M 22s 165900K .......... .......... .......... .......... .......... 32% 39.7M 22s 165950K .......... .......... .......... .......... .......... 32% 26.7M 22s 166000K .......... .......... .......... .......... .......... 32% 17.2M 22s 166050K .......... .......... .......... .......... .......... 32% 38.7M 22s 166100K .......... .......... .......... .......... .......... 32% 16.4M 22s 166150K .......... .......... .......... .......... .......... 32% 17.1M 22s 166200K .......... .......... .......... .......... .......... 32% 12.3M 22s 166250K .......... .......... .......... .......... .......... 32% 14.8M 22s 166300K .......... .......... .......... .......... .......... 32% 13.6M 22s 166350K .......... .......... .......... .......... .......... 32% 13.1M 22s 166400K .......... .......... .......... .......... .......... 32% 14.6M 22s 166450K .......... .......... .......... .......... .......... 32% 14.7M 22s 166500K .......... .......... .......... .......... .......... 32% 10.3M 22s 166550K .......... .......... .......... .......... .......... 32% 11.0M 22s 166600K .......... .......... .......... .......... .......... 32% 7.24M 22s 166650K .......... .......... .......... .......... .......... 32% 8.85M 22s 166700K .......... .......... .......... .......... .......... 32% 7.57M 22s 166750K .......... .......... .......... .......... .......... 32% 8.62M 22s 166800K .......... .......... .......... .......... .......... 32% 8.90M 22s 166850K .......... .......... .......... .......... .......... 32% 6.36M 22s 166900K .......... .......... .......... .......... .......... 32% 7.92M 22s 166950K .......... .......... .......... .......... .......... 32% 6.01M 22s 167000K .......... .......... .......... .......... .......... 32% 6.92M 22s 167050K .......... .......... .......... .......... .......... 32% 6.25M 22s 167100K .......... .......... .......... .......... .......... 32% 6.31M 22s 167150K .......... .......... .......... .......... .......... 32% 25.3M 22s 167200K .......... .......... .......... .......... .......... 32% 23.1M 22s 167250K .......... .......... .......... .......... .......... 32% 11.1M 22s 167300K .......... .......... .......... .......... .......... 32% 531M 22s 167350K .......... .......... .......... .......... .......... 32% 10.7M 22s 167400K .......... .......... .......... .......... .......... 32% 8.76M 22s 167450K .......... .......... .......... .......... .......... 32% 3.94M 22s 167500K .......... .......... .......... .......... .......... 32% 3.23M 22s 167550K .......... .......... .......... .......... .......... 32% 3.89M 22s 167600K .......... .......... .......... .......... .......... 32% 7.62M 22s 167650K .......... .......... .......... .......... .......... 32% 23.7M 22s 167700K .......... .......... .......... .......... .......... 32% 19.0M 22s 167750K .......... .......... .......... .......... .......... 32% 14.5M 22s 167800K .......... .......... .......... .......... .......... 32% 18.4M 22s 167850K .......... .......... .......... .......... .......... 32% 17.9M 22s 167900K .......... .......... .......... .......... .......... 32% 29.0M 22s 167950K .......... .......... .......... .......... .......... 32% 21.3M 22s 168000K .......... .......... .......... .......... .......... 32% 22.4M 22s 168050K .......... .......... .......... .......... .......... 32% 21.8M 22s 168100K .......... .......... .......... .......... .......... 32% 21.7M 22s 168150K .......... .......... .......... .......... .......... 32% 24.6M 22s 168200K .......... .......... .......... .......... .......... 33% 14.9M 22s 168250K .......... .......... .......... .......... .......... 33% 16.1M 22s 168300K .......... .......... .......... .......... .......... 33% 17.3M 22s 168350K .......... .......... .......... .......... .......... 33% 14.1M 22s 168400K .......... .......... .......... .......... .......... 33% 16.5M 22s 168450K .......... .......... .......... .......... .......... 33% 12.5M 22s 168500K .......... .......... .......... .......... .......... 33% 22.4M 22s 168550K .......... .......... .......... .......... .......... 33% 13.0M 22s 168600K .......... .......... .......... .......... .......... 33% 13.5M 22s 168650K .......... .......... .......... .......... .......... 33% 16.5M 22s 168700K .......... .......... .......... .......... .......... 33% 11.9M 22s 168750K .......... .......... .......... .......... .......... 33% 16.3M 22s 168800K .......... .......... .......... .......... .......... 33% 16.7M 22s 168850K .......... .......... .......... .......... .......... 33% 12.0M 22s 168900K .......... .......... .......... .......... .......... 33% 12.3M 22s 168950K .......... .......... .......... .......... .......... 33% 9.23M 22s 169000K .......... .......... .......... .......... .......... 33% 29.2M 22s 169050K .......... .......... .......... .......... .......... 33% 27.7M 22s 169100K .......... .......... .......... .......... .......... 33% 33.9M 22s 169150K .......... .......... .......... .......... .......... 33% 27.2M 22s 169200K .......... .......... .......... .......... .......... 33% 20.9M 22s 169250K .......... .......... .......... .......... .......... 33% 17.1M 22s 169300K .......... .......... .......... .......... .......... 33% 49.0M 22s 169350K .......... .......... .......... .......... .......... 33% 11.8M 22s 169400K .......... .......... .......... .......... .......... 33% 42.4M 22s 169450K .......... .......... .......... .......... .......... 33% 17.1M 22s 169500K .......... .......... .......... .......... .......... 33% 19.9M 22s 169550K .......... .......... .......... .......... .......... 33% 17.3M 22s 169600K .......... .......... .......... .......... .......... 33% 21.2M 22s 169650K .......... .......... .......... .......... .......... 33% 15.7M 22s 169700K .......... .......... .......... .......... .......... 33% 15.2M 22s 169750K .......... .......... .......... .......... .......... 33% 19.6M 22s 169800K .......... .......... .......... .......... .......... 33% 23.4M 22s 169850K .......... .......... .......... .......... .......... 33% 13.2M 22s 169900K .......... .......... .......... .......... .......... 33% 16.5M 22s 169950K .......... .......... .......... .......... .......... 33% 12.9M 22s 170000K .......... .......... .......... .......... .......... 33% 14.3M 22s 170050K .......... .......... .......... .......... .......... 33% 12.8M 22s 170100K .......... .......... .......... .......... .......... 33% 15.2M 22s 170150K .......... .......... .......... .......... .......... 33% 12.0M 22s 170200K .......... .......... .......... .......... .......... 33% 12.4M 22s 170250K .......... .......... .......... .......... .......... 33% 13.3M 22s 170300K .......... .......... .......... .......... .......... 33% 11.3M 22s 170350K .......... .......... .......... .......... .......... 33% 25.3M 22s 170400K .......... .......... .......... .......... .......... 33% 18.6M 22s 170450K .......... .......... .......... .......... .......... 33% 13.3M 22s 170500K .......... .......... .......... .......... .......... 33% 9.06M 22s 170550K .......... .......... .......... .......... .......... 33% 14.5M 22s 170600K .......... .......... .......... .......... .......... 33% 10.5M 22s 170650K .......... .......... .......... .......... .......... 33% 15.4M 22s 170700K .......... .......... .......... .......... .......... 33% 10.2M 22s 170750K .......... .......... .......... .......... .......... 33% 15.7M 22s 170800K .......... .......... .......... .......... .......... 33% 14.5M 22s 170850K .......... .......... .......... .......... .......... 33% 11.2M 22s 170900K .......... .......... .......... .......... .......... 33% 15.0M 22s 170950K .......... .......... .......... .......... .......... 33% 11.3M 22s 171000K .......... .......... .......... .......... .......... 33% 14.1M 22s 171050K .......... .......... .......... .......... .......... 33% 18.0M 22s 171100K .......... .......... .......... .......... .......... 33% 13.1M 22s 171150K .......... .......... .......... .......... .......... 33% 10.2M 22s 171200K .......... .......... .......... .......... .......... 33% 9.69M 22s 171250K .......... .......... .......... .......... .......... 33% 14.0M 22s 171300K .......... .......... .......... .......... .......... 33% 15.3M 21s 171350K .......... .......... .......... .......... .......... 33% 11.9M 21s 171400K .......... .......... .......... .......... .......... 33% 15.1M 21s 171450K .......... .......... .......... .......... .......... 33% 14.1M 21s 171500K .......... .......... .......... .......... .......... 33% 16.7M 21s 171550K .......... .......... .......... .......... .......... 33% 8.82M 21s 171600K .......... .......... .......... .......... .......... 33% 8.42M 21s 171650K .......... .......... .......... .......... .......... 33% 12.6M 21s 171700K .......... .......... .......... .......... .......... 33% 9.65M 21s 171750K .......... .......... .......... .......... .......... 33% 10.9M 21s 171800K .......... .......... .......... .......... .......... 33% 8.37M 21s 171850K .......... .......... .......... .......... .......... 33% 5.63M 21s 171900K .......... .......... .......... .......... .......... 33% 17.0M 21s 171950K .......... .......... .......... .......... .......... 33% 23.3M 21s 172000K .......... .......... .......... .......... .......... 33% 18.5M 21s 172050K .......... .......... .......... .......... .......... 33% 20.9M 21s 172100K .......... .......... .......... .......... .......... 33% 29.5M 21s 172150K .......... .......... .......... .......... .......... 33% 20.0M 21s 172200K .......... .......... .......... .......... .......... 33% 23.3M 21s 172250K .......... .......... .......... .......... .......... 33% 21.4M 21s 172300K .......... .......... .......... .......... .......... 33% 26.8M 21s 172350K .......... .......... .......... .......... .......... 33% 21.2M 21s 172400K .......... .......... .......... .......... .......... 33% 20.7M 21s 172450K .......... .......... .......... .......... .......... 33% 16.7M 21s 172500K .......... .......... .......... .......... .......... 33% 17.3M 21s 172550K .......... .......... .......... .......... .......... 33% 15.4M 21s 172600K .......... .......... .......... .......... .......... 33% 15.8M 21s 172650K .......... .......... .......... .......... .......... 33% 16.0M 21s 172700K .......... .......... .......... .......... .......... 33% 14.0M 21s 172750K .......... .......... .......... .......... .......... 33% 22.2M 21s 172800K .......... .......... .......... .......... .......... 33% 15.1M 21s 172850K .......... .......... .......... .......... .......... 33% 15.8M 21s 172900K .......... .......... .......... .......... .......... 33% 22.1M 21s 172950K .......... .......... .......... .......... .......... 33% 17.4M 21s 173000K .......... .......... .......... .......... .......... 33% 16.5M 21s 173050K .......... .......... .......... .......... .......... 33% 16.0M 21s 173100K .......... .......... .......... .......... .......... 33% 16.5M 21s 173150K .......... .......... .......... .......... .......... 33% 24.1M 21s 173200K .......... .......... .......... .......... .......... 33% 24.9M 21s 173250K .......... .......... .......... .......... .......... 33% 32.4M 21s 173300K .......... .......... .......... .......... .......... 34% 271M 21s 173350K .......... .......... .......... .......... .......... 34% 23.3M 21s 173400K .......... .......... .......... .......... .......... 34% 294M 21s 173450K .......... .......... .......... .......... .......... 34% 29.7M 21s 173500K .......... .......... .......... .......... .......... 34% 25.7M 21s 173550K .......... .......... .......... .......... .......... 34% 23.4M 21s 173600K .......... .......... .......... .......... .......... 34% 20.1M 21s 173650K .......... .......... .......... .......... .......... 34% 15.9M 21s 173700K .......... .......... .......... .......... .......... 34% 14.6M 21s 173750K .......... .......... .......... .......... .......... 34% 11.0M 21s 173800K .......... .......... .......... .......... .......... 34% 19.8M 21s 173850K .......... .......... .......... .......... .......... 34% 9.34M 21s 173900K .......... .......... .......... .......... .......... 34% 11.2M 21s 173950K .......... .......... .......... .......... .......... 34% 10.4M 21s 174000K .......... .......... .......... .......... .......... 34% 11.0M 21s 174050K .......... .......... .......... .......... .......... 34% 9.76M 21s 174100K .......... .......... .......... .......... .......... 34% 8.00M 21s 174150K .......... .......... .......... .......... .......... 34% 7.05M 21s 174200K .......... .......... .......... .......... .......... 34% 6.46M 21s 174250K .......... .......... .......... .......... .......... 34% 11.4M 21s 174300K .......... .......... .......... .......... .......... 34% 25.4M 21s 174350K .......... .......... .......... .......... .......... 34% 17.9M 21s 174400K .......... .......... .......... .......... .......... 34% 14.5M 21s 174450K .......... .......... .......... .......... .......... 34% 19.1M 21s 174500K .......... .......... .......... .......... .......... 34% 31.5M 21s 174550K .......... .......... .......... .......... .......... 34% 18.8M 21s 174600K .......... .......... .......... .......... .......... 34% 18.7M 21s 174650K .......... .......... .......... .......... .......... 34% 11.1M 21s 174700K .......... .......... .......... .......... .......... 34% 16.7M 21s 174750K .......... .......... .......... .......... .......... 34% 13.9M 21s 174800K .......... .......... .......... .......... .......... 34% 14.6M 21s 174850K .......... .......... .......... .......... .......... 34% 9.84M 21s 174900K .......... .......... .......... .......... .......... 34% 12.4M 21s 174950K .......... .......... .......... .......... .......... 34% 8.82M 21s 175000K .......... .......... .......... .......... .......... 34% 14.0M 21s 175050K .......... .......... .......... .......... .......... 34% 10.3M 21s 175100K .......... .......... .......... .......... .......... 34% 8.71M 21s 175150K .......... .......... .......... .......... .......... 34% 10.8M 21s 175200K .......... .......... .......... .......... .......... 34% 20.3M 21s 175250K .......... .......... .......... .......... .......... 34% 40.3M 21s 175300K .......... .......... .......... .......... .......... 34% 23.9M 21s 175350K .......... .......... .......... .......... .......... 34% 19.9M 21s 175400K .......... .......... .......... .......... .......... 34% 24.2M 21s 175450K .......... .......... .......... .......... .......... 34% 16.3M 21s 175500K .......... .......... .......... .......... .......... 34% 21.1M 21s 175550K .......... .......... .......... .......... .......... 34% 19.6M 21s 175600K .......... .......... .......... .......... .......... 34% 15.7M 21s 175650K .......... .......... .......... .......... .......... 34% 13.5M 21s 175700K .......... .......... .......... .......... .......... 34% 14.8M 21s 175750K .......... .......... .......... .......... .......... 34% 18.0M 21s 175800K .......... .......... .......... .......... .......... 34% 15.8M 21s 175850K .......... .......... .......... .......... .......... 34% 12.2M 21s 175900K .......... .......... .......... .......... .......... 34% 16.2M 21s 175950K .......... .......... .......... .......... .......... 34% 11.4M 21s 176000K .......... .......... .......... .......... .......... 34% 14.5M 21s 176050K .......... .......... .......... .......... .......... 34% 17.1M 21s 176100K .......... .......... .......... .......... .......... 34% 13.5M 21s 176150K .......... .......... .......... .......... .......... 34% 15.7M 21s 176200K .......... .......... .......... .......... .......... 34% 15.7M 21s 176250K .......... .......... .......... .......... .......... 34% 30.4M 21s 176300K .......... .......... .......... .......... .......... 34% 27.8M 21s 176350K .......... .......... .......... .......... .......... 34% 28.7M 21s 176400K .......... .......... .......... .......... .......... 34% 42.4M 21s 176450K .......... .......... .......... .......... .......... 34% 20.6M 21s 176500K .......... .......... .......... .......... .......... 34% 29.5M 21s 176550K .......... .......... .......... .......... .......... 34% 21.9M 21s 176600K .......... .......... .......... .......... .......... 34% 19.6M 21s 176650K .......... .......... .......... .......... .......... 34% 20.2M 21s 176700K .......... .......... .......... .......... .......... 34% 15.2M 21s 176750K .......... .......... .......... .......... .......... 34% 17.8M 21s 176800K .......... .......... .......... .......... .......... 34% 15.0M 21s 176850K .......... .......... .......... .......... .......... 34% 13.4M 21s 176900K .......... .......... .......... .......... .......... 34% 15.3M 21s 176950K .......... .......... .......... .......... .......... 34% 11.8M 21s 177000K .......... .......... .......... .......... .......... 34% 19.0M 21s 177050K .......... .......... .......... .......... .......... 34% 16.5M 21s 177100K .......... .......... .......... .......... .......... 34% 15.3M 21s 177150K .......... .......... .......... .......... .......... 34% 14.0M 21s 177200K .......... .......... .......... .......... .......... 34% 14.4M 21s 177250K .......... .......... .......... .......... .......... 34% 17.4M 21s 177300K .......... .......... .......... .......... .......... 34% 15.1M 21s 177350K .......... .......... .......... .......... .......... 34% 13.7M 21s 177400K .......... .......... .......... .......... .......... 34% 21.0M 21s 177450K .......... .......... .......... .......... .......... 34% 43.9M 21s 177500K .......... .......... .......... .......... .......... 34% 24.6M 21s 177550K .......... .......... .......... .......... .......... 34% 20.8M 21s 177600K .......... .......... .......... .......... .......... 34% 17.3M 21s 177650K .......... .......... .......... .......... .......... 34% 17.8M 21s 177700K .......... .......... .......... .......... .......... 34% 18.8M 21s 177750K .......... .......... .......... .......... .......... 34% 18.1M 21s 177800K .......... .......... .......... .......... .......... 34% 16.5M 21s 177850K .......... .......... .......... .......... .......... 34% 12.2M 21s 177900K .......... .......... .......... .......... .......... 34% 12.5M 21s 177950K .......... .......... .......... .......... .......... 34% 9.05M 21s 178000K .......... .......... .......... .......... .......... 34% 14.2M 21s 178050K .......... .......... .......... .......... .......... 34% 15.9M 21s 178100K .......... .......... .......... .......... .......... 34% 10.3M 21s 178150K .......... .......... .......... .......... .......... 34% 14.1M 21s 178200K .......... .......... .......... .......... .......... 34% 8.20M 21s 178250K .......... .......... .......... .......... .......... 34% 9.38M 21s 178300K .......... .......... .......... .......... .......... 34% 11.3M 21s 178350K .......... .......... .......... .......... .......... 34% 3.38M 21s 178400K .......... .......... .......... .......... .......... 35% 10.6M 21s 178450K .......... .......... .......... .......... .......... 35% 18.1M 21s 178500K .......... .......... .......... .......... .......... 35% 17.4M 21s 178550K .......... .......... .......... .......... .......... 35% 30.3M 21s 178600K .......... .......... .......... .......... .......... 35% 19.1M 21s 178650K .......... .......... .......... .......... .......... 35% 21.3M 21s 178700K .......... .......... .......... .......... .......... 35% 18.9M 21s 178750K .......... .......... .......... .......... .......... 35% 18.0M 21s 178800K .......... .......... .......... .......... .......... 35% 20.1M 21s 178850K .......... .......... .......... .......... .......... 35% 13.9M 21s 178900K .......... .......... .......... .......... .......... 35% 21.0M 21s 178950K .......... .......... .......... .......... .......... 35% 19.1M 21s 179000K .......... .......... .......... .......... .......... 35% 18.1M 21s 179050K .......... .......... .......... .......... .......... 35% 12.0M 21s 179100K .......... .......... .......... .......... .......... 35% 12.3M 21s 179150K .......... .......... .......... .......... .......... 35% 15.7M 21s 179200K .......... .......... .......... .......... .......... 35% 9.49M 21s 179250K .......... .......... .......... .......... .......... 35% 18.0M 21s 179300K .......... .......... .......... .......... .......... 35% 18.0M 21s 179350K .......... .......... .......... .......... .......... 35% 14.5M 21s 179400K .......... .......... .......... .......... .......... 35% 16.5M 21s 179450K .......... .......... .......... .......... .......... 35% 15.0M 21s 179500K .......... .......... .......... .......... .......... 35% 10.3M 21s 179550K .......... .......... .......... .......... .......... 35% 9.77M 21s 179600K .......... .......... .......... .......... .......... 35% 9.67M 21s 179650K .......... .......... .......... .......... .......... 35% 9.82M 21s 179700K .......... .......... .......... .......... .......... 35% 7.46M 21s 179750K .......... .......... .......... .......... .......... 35% 12.0M 21s 179800K .......... .......... .......... .......... .......... 35% 19.0M 21s 179850K .......... .......... .......... .......... .......... 35% 12.6M 21s 179900K .......... .......... .......... .......... .......... 35% 12.1M 21s 179950K .......... .......... .......... .......... .......... 35% 15.7M 21s 180000K .......... .......... .......... .......... .......... 35% 14.3M 21s 180050K .......... .......... .......... .......... .......... 35% 17.2M 21s 180100K .......... .......... .......... .......... .......... 35% 13.0M 21s 180150K .......... .......... .......... .......... .......... 35% 16.5M 21s 180200K .......... .......... .......... .......... .......... 35% 13.4M 21s 180250K .......... .......... .......... .......... .......... 35% 22.2M 21s 180300K .......... .......... .......... .......... .......... 35% 19.7M 21s 180350K .......... .......... .......... .......... .......... 35% 16.1M 21s 180400K .......... .......... .......... .......... .......... 35% 15.9M 21s 180450K .......... .......... .......... .......... .......... 35% 13.5M 21s 180500K .......... .......... .......... .......... .......... 35% 10.5M 21s 180550K .......... .......... .......... .......... .......... 35% 13.0M 21s 180600K .......... .......... .......... .......... .......... 35% 7.34M 21s 180650K .......... .......... .......... .......... .......... 35% 9.39M 21s 180700K .......... .......... .......... .......... .......... 35% 7.98M 21s 180750K .......... .......... .......... .......... .......... 35% 9.58M 21s 180800K .......... .......... .......... .......... .......... 35% 7.90M 21s 180850K .......... .......... .......... .......... .......... 35% 7.74M 21s 180900K .......... .......... .......... .......... .......... 35% 9.57M 21s 180950K .......... .......... .......... .......... .......... 35% 15.0M 21s 181000K .......... .......... .......... .......... .......... 35% 35.8M 21s 181050K .......... .......... .......... .......... .......... 35% 42.3M 21s 181100K .......... .......... .......... .......... .......... 35% 22.7M 21s 181150K .......... .......... .......... .......... .......... 35% 29.9M 21s 181200K .......... .......... .......... .......... .......... 35% 18.7M 21s 181250K .......... .......... .......... .......... .......... 35% 42.0M 21s 181300K .......... .......... .......... .......... .......... 35% 18.0M 21s 181350K .......... .......... .......... .......... .......... 35% 25.1M 21s 181400K .......... .......... .......... .......... .......... 35% 22.6M 21s 181450K .......... .......... .......... .......... .......... 35% 15.8M 21s 181500K .......... .......... .......... .......... .......... 35% 26.2M 21s 181550K .......... .......... .......... .......... .......... 35% 18.3M 21s 181600K .......... .......... .......... .......... .......... 35% 19.0M 21s 181650K .......... .......... .......... .......... .......... 35% 15.9M 21s 181700K .......... .......... .......... .......... .......... 35% 16.2M 21s 181750K .......... .......... .......... .......... .......... 35% 17.9M 21s 181800K .......... .......... .......... .......... .......... 35% 26.4M 21s 181850K .......... .......... .......... .......... .......... 35% 17.4M 21s 181900K .......... .......... .......... .......... .......... 35% 18.8M 21s 181950K .......... .......... .......... .......... .......... 35% 16.6M 21s 182000K .......... .......... .......... .......... .......... 35% 22.0M 21s 182050K .......... .......... .......... .......... .......... 35% 20.1M 21s 182100K .......... .......... .......... .......... .......... 35% 18.2M 21s 182150K .......... .......... .......... .......... .......... 35% 24.0M 21s 182200K .......... .......... .......... .......... .......... 35% 18.9M 21s 182250K .......... .......... .......... .......... .......... 35% 23.7M 21s 182300K .......... .......... .......... .......... .......... 35% 21.0M 21s 182350K .......... .......... .......... .......... .......... 35% 18.0M 21s 182400K .......... .......... .......... .......... .......... 35% 34.2M 21s 182450K .......... .......... .......... .......... .......... 35% 34.5M 21s 182500K .......... .......... .......... .......... .......... 35% 30.7M 21s 182550K .......... .......... .......... .......... .......... 35% 213M 21s 182600K .......... .......... .......... .......... .......... 35% 27.8M 21s 182650K .......... .......... .......... .......... .......... 35% 143M 21s 182700K .......... .......... .......... .......... .......... 35% 26.4M 21s 182750K .......... .......... .......... .......... .......... 35% 32.3M 21s 182800K .......... .......... .......... .......... .......... 35% 28.3M 21s 182850K .......... .......... .......... .......... .......... 35% 19.7M 21s 182900K .......... .......... .......... .......... .......... 35% 24.5M 21s 182950K .......... .......... .......... .......... .......... 35% 22.2M 21s 183000K .......... .......... .......... .......... .......... 35% 38.3M 21s 183050K .......... .......... .......... .......... .......... 35% 22.7M 21s 183100K .......... .......... .......... .......... .......... 35% 20.1M 21s 183150K .......... .......... .......... .......... .......... 35% 20.1M 21s 183200K .......... .......... .......... .......... .......... 35% 20.0M 21s 183250K .......... .......... .......... .......... .......... 35% 20.7M 21s 183300K .......... .......... .......... .......... .......... 35% 18.2M 21s 183350K .......... .......... .......... .......... .......... 35% 16.4M 21s 183400K .......... .......... .......... .......... .......... 35% 20.9M 21s 183450K .......... .......... .......... .......... .......... 35% 18.3M 21s 183500K .......... .......... .......... .......... .......... 36% 17.6M 21s 183550K .......... .......... .......... .......... .......... 36% 23.9M 21s 183600K .......... .......... .......... .......... .......... 36% 16.3M 21s 183650K .......... .......... .......... .......... .......... 36% 22.1M 21s 183700K .......... .......... .......... .......... .......... 36% 12.8M 21s 183750K .......... .......... .......... .......... .......... 36% 11.6M 21s 183800K .......... .......... .......... .......... .......... 36% 17.2M 21s 183850K .......... .......... .......... .......... .......... 36% 19.8M 21s 183900K .......... .......... .......... .......... .......... 36% 31.2M 21s 183950K .......... .......... .......... .......... .......... 36% 22.1M 21s 184000K .......... .......... .......... .......... .......... 36% 24.4M 21s 184050K .......... .......... .......... .......... .......... 36% 25.0M 21s 184100K .......... .......... .......... .......... .......... 36% 25.6M 21s 184150K .......... .......... .......... .......... .......... 36% 14.5M 21s 184200K .......... .......... .......... .......... .......... 36% 17.2M 21s 184250K .......... .......... .......... .......... .......... 36% 13.4M 21s 184300K .......... .......... .......... .......... .......... 36% 11.6M 21s 184350K .......... .......... .......... .......... .......... 36% 11.4M 21s 184400K .......... .......... .......... .......... .......... 36% 13.7M 21s 184450K .......... .......... .......... .......... .......... 36% 11.8M 21s 184500K .......... .......... .......... .......... .......... 36% 15.3M 21s 184550K .......... .......... .......... .......... .......... 36% 16.6M 21s 184600K .......... .......... .......... .......... .......... 36% 12.0M 21s 184650K .......... .......... .......... .......... .......... 36% 15.2M 21s 184700K .......... .......... .......... .......... .......... 36% 15.8M 21s 184750K .......... .......... .......... .......... .......... 36% 15.4M 21s 184800K .......... .......... .......... .......... .......... 36% 15.3M 21s 184850K .......... .......... .......... .......... .......... 36% 10.9M 21s 184900K .......... .......... .......... .......... .......... 36% 18.9M 21s 184950K .......... .......... .......... .......... .......... 36% 19.6M 21s 185000K .......... .......... .......... .......... .......... 36% 19.4M 21s 185050K .......... .......... .......... .......... .......... 36% 150M 21s 185100K .......... .......... .......... .......... .......... 36% 45.2M 21s 185150K .......... .......... .......... .......... .......... 36% 26.1M 21s 185200K .......... .......... .......... .......... .......... 36% 80.6M 21s 185250K .......... .......... .......... .......... .......... 36% 27.2M 21s 185300K .......... .......... .......... .......... .......... 36% 31.8M 21s 185350K .......... .......... .......... .......... .......... 36% 26.7M 21s 185400K .......... .......... .......... .......... .......... 36% 37.4M 21s 185450K .......... .......... .......... .......... .......... 36% 31.5M 21s 185500K .......... .......... .......... .......... .......... 36% 30.4M 21s 185550K .......... .......... .......... .......... .......... 36% 31.3M 21s 185600K .......... .......... .......... .......... .......... 36% 22.4M 21s 185650K .......... .......... .......... .......... .......... 36% 26.6M 21s 185700K .......... .......... .......... .......... .......... 36% 22.6M 21s 185750K .......... .......... .......... .......... .......... 36% 33.5M 21s 185800K .......... .......... .......... .......... .......... 36% 25.8M 21s 185850K .......... .......... .......... .......... .......... 36% 24.8M 21s 185900K .......... .......... .......... .......... .......... 36% 15.3M 21s 185950K .......... .......... .......... .......... .......... 36% 24.1M 20s 186000K .......... .......... .......... .......... .......... 36% 21.2M 20s 186050K .......... .......... .......... .......... .......... 36% 18.8M 20s 186100K .......... .......... .......... .......... .......... 36% 17.4M 20s 186150K .......... .......... .......... .......... .......... 36% 19.1M 20s 186200K .......... .......... .......... .......... .......... 36% 17.3M 20s 186250K .......... .......... .......... .......... .......... 36% 18.0M 20s 186300K .......... .......... .......... .......... .......... 36% 16.5M 20s 186350K .......... .......... .......... .......... .......... 36% 12.2M 20s 186400K .......... .......... .......... .......... .......... 36% 20.9M 20s 186450K .......... .......... .......... .......... .......... 36% 11.6M 20s 186500K .......... .......... .......... .......... .......... 36% 9.75M 20s 186550K .......... .......... .......... .......... .......... 36% 14.7M 20s 186600K .......... .......... .......... .......... .......... 36% 11.6M 20s 186650K .......... .......... .......... .......... .......... 36% 13.5M 20s 186700K .......... .......... .......... .......... .......... 36% 12.6M 20s 186750K .......... .......... .......... .......... .......... 36% 12.0M 20s 186800K .......... .......... .......... .......... .......... 36% 12.4M 20s 186850K .......... .......... .......... .......... .......... 36% 9.84M 20s 186900K .......... .......... .......... .......... .......... 36% 12.1M 20s 186950K .......... .......... .......... .......... .......... 36% 10.9M 20s 187000K .......... .......... .......... .......... .......... 36% 12.4M 20s 187050K .......... .......... .......... .......... .......... 36% 19.1M 20s 187100K .......... .......... .......... .......... .......... 36% 20.1M 20s 187150K .......... .......... .......... .......... .......... 36% 37.5M 20s 187200K .......... .......... .......... .......... .......... 36% 19.6M 20s 187250K .......... .......... .......... .......... .......... 36% 53.4M 20s 187300K .......... .......... .......... .......... .......... 36% 22.3M 20s 187350K .......... .......... .......... .......... .......... 36% 54.2M 20s 187400K .......... .......... .......... .......... .......... 36% 21.2M 20s 187450K .......... .......... .......... .......... .......... 36% 21.9M 20s 187500K .......... .......... .......... .......... .......... 36% 25.3M 20s 187550K .......... .......... .......... .......... .......... 36% 22.0M 20s 187600K .......... .......... .......... .......... .......... 36% 23.3M 20s 187650K .......... .......... .......... .......... .......... 36% 25.1M 20s 187700K .......... .......... .......... .......... .......... 36% 24.4M 20s 187750K .......... .......... .......... .......... .......... 36% 23.6M 20s 187800K .......... .......... .......... .......... .......... 36% 33.6M 20s 187850K .......... .......... .......... .......... .......... 36% 17.8M 20s 187900K .......... .......... .......... .......... .......... 36% 27.1M 20s 187950K .......... .......... .......... .......... .......... 36% 22.3M 20s 188000K .......... .......... .......... .......... .......... 36% 29.2M 20s 188050K .......... .......... .......... .......... .......... 36% 21.0M 20s 188100K .......... .......... .......... .......... .......... 36% 20.8M 20s 188150K .......... .......... .......... .......... .......... 36% 20.9M 20s 188200K .......... .......... .......... .......... .......... 36% 26.6M 20s 188250K .......... .......... .......... .......... .......... 36% 40.3M 20s 188300K .......... .......... .......... .......... .......... 36% 29.1M 20s 188350K .......... .......... .......... .......... .......... 36% 25.2M 20s 188400K .......... .......... .......... .......... .......... 36% 29.9M 20s 188450K .......... .......... .......... .......... .......... 36% 27.7M 20s 188500K .......... .......... .......... .......... .......... 36% 20.2M 20s 188550K .......... .......... .......... .......... .......... 36% 33.8M 20s 188600K .......... .......... .......... .......... .......... 37% 19.9M 20s 188650K .......... .......... .......... .......... .......... 37% 21.6M 20s 188700K .......... .......... .......... .......... .......... 37% 25.2M 20s 188750K .......... .......... .......... .......... .......... 37% 21.0M 20s 188800K .......... .......... .......... .......... .......... 37% 28.3M 20s 188850K .......... .......... .......... .......... .......... 37% 20.7M 20s 188900K .......... .......... .......... .......... .......... 37% 23.3M 20s 188950K .......... .......... .......... .......... .......... 37% 19.4M 20s 189000K .......... .......... .......... .......... .......... 37% 25.5M 20s 189050K .......... .......... .......... .......... .......... 37% 22.0M 20s 189100K .......... .......... .......... .......... .......... 37% 21.6M 20s 189150K .......... .......... .......... .......... .......... 37% 17.8M 20s 189200K .......... .......... .......... .......... .......... 37% 15.1M 20s 189250K .......... .......... .......... .......... .......... 37% 20.0M 20s 189300K .......... .......... .......... .......... .......... 37% 22.3M 20s 189350K .......... .......... .......... .......... .......... 37% 17.1M 20s 189400K .......... .......... .......... .......... .......... 37% 14.5M 20s 189450K .......... .......... .......... .......... .......... 37% 9.70M 20s 189500K .......... .......... .......... .......... .......... 37% 13.0M 20s 189550K .......... .......... .......... .......... .......... 37% 13.1M 20s 189600K .......... .......... .......... .......... .......... 37% 12.5M 20s 189650K .......... .......... .......... .......... .......... 37% 17.4M 20s 189700K .......... .......... .......... .......... .......... 37% 13.9M 20s 189750K .......... .......... .......... .......... .......... 37% 15.1M 20s 189800K .......... .......... .......... .......... .......... 37% 17.3M 20s 189850K .......... .......... .......... .......... .......... 37% 16.6M 20s 189900K .......... .......... .......... .......... .......... 37% 18.5M 20s 189950K .......... .......... .......... .......... .......... 37% 12.2M 20s 190000K .......... .......... .......... .......... .......... 37% 16.3M 20s 190050K .......... .......... .......... .......... .......... 37% 13.8M 20s 190100K .......... .......... .......... .......... .......... 37% 11.5M 20s 190150K .......... .......... .......... .......... .......... 37% 13.1M 20s 190200K .......... .......... .......... .......... .......... 37% 9.87M 20s 190250K .......... .......... .......... .......... .......... 37% 10.6M 20s 190300K .......... .......... .......... .......... .......... 37% 12.2M 20s 190350K .......... .......... .......... .......... .......... 37% 10.1M 20s 190400K .......... .......... .......... .......... .......... 37% 11.5M 20s 190450K .......... .......... .......... .......... .......... 37% 8.80M 20s 190500K .......... .......... .......... .......... .......... 37% 5.93M 20s 190550K .......... .......... .......... .......... .......... 37% 6.57M 20s 190600K .......... .......... .......... .......... .......... 37% 5.30M 20s 190650K .......... .......... .......... .......... .......... 37% 7.03M 20s 190700K .......... .......... .......... .......... .......... 37% 8.07M 20s 190750K .......... .......... .......... .......... .......... 37% 36.8M 20s 190800K .......... .......... .......... .......... .......... 37% 23.6M 20s 190850K .......... .......... .......... .......... .......... 37% 37.4M 20s 190900K .......... .......... .......... .......... .......... 37% 34.7M 20s 190950K .......... .......... .......... .......... .......... 37% 25.0M 20s 191000K .......... .......... .......... .......... .......... 37% 22.2M 20s 191050K .......... .......... .......... .......... .......... 37% 23.1M 20s 191100K .......... .......... .......... .......... .......... 37% 22.4M 20s 191150K .......... .......... .......... .......... .......... 37% 17.9M 20s 191200K .......... .......... .......... .......... .......... 37% 13.2M 20s 191250K .......... .......... .......... .......... .......... 37% 22.5M 20s 191300K .......... .......... .......... .......... .......... 37% 20.0M 20s 191350K .......... .......... .......... .......... .......... 37% 17.6M 20s 191400K .......... .......... .......... .......... .......... 37% 23.2M 20s 191450K .......... .......... .......... .......... .......... 37% 17.2M 20s 191500K .......... .......... .......... .......... .......... 37% 17.4M 20s 191550K .......... .......... .......... .......... .......... 37% 18.4M 20s 191600K .......... .......... .......... .......... .......... 37% 16.7M 20s 191650K .......... .......... .......... .......... .......... 37% 14.3M 20s 191700K .......... .......... .......... .......... .......... 37% 9.88M 20s 191750K .......... .......... .......... .......... .......... 37% 13.1M 20s 191800K .......... .......... .......... .......... .......... 37% 23.3M 20s 191850K .......... .......... .......... .......... .......... 37% 18.4M 20s 191900K .......... .......... .......... .......... .......... 37% 147M 20s 191950K .......... .......... .......... .......... .......... 37% 20.4M 20s 192000K .......... .......... .......... .......... .......... 37% 44.8M 20s 192050K .......... .......... .......... .......... .......... 37% 13.1M 20s 192100K .......... .......... .......... .......... .......... 37% 27.6M 20s 192150K .......... .......... .......... .......... .......... 37% 20.2M 20s 192200K .......... .......... .......... .......... .......... 37% 12.9M 20s 192250K .......... .......... .......... .......... .......... 37% 11.5M 20s 192300K .......... .......... .......... .......... .......... 37% 12.6M 20s 192350K .......... .......... .......... .......... .......... 37% 14.0M 20s 192400K .......... .......... .......... .......... .......... 37% 15.0M 20s 192450K .......... .......... .......... .......... .......... 37% 14.5M 20s 192500K .......... .......... .......... .......... .......... 37% 17.5M 20s 192550K .......... .......... .......... .......... .......... 37% 17.0M 20s 192600K .......... .......... .......... .......... .......... 37% 15.1M 20s 192650K .......... .......... .......... .......... .......... 37% 13.5M 20s 192700K .......... .......... .......... .......... .......... 37% 11.4M 20s 192750K .......... .......... .......... .......... .......... 37% 14.7M 20s 192800K .......... .......... .......... .......... .......... 37% 18.8M 20s 192850K .......... .......... .......... .......... .......... 37% 13.2M 20s 192900K .......... .......... .......... .......... .......... 37% 19.0M 20s 192950K .......... .......... .......... .......... .......... 37% 15.7M 20s 193000K .......... .......... .......... .......... .......... 37% 8.46M 20s 193050K .......... .......... .......... .......... .......... 37% 16.3M 20s 193100K .......... .......... .......... .......... .......... 37% 15.5M 20s 193150K .......... .......... .......... .......... .......... 37% 15.3M 20s 193200K .......... .......... .......... .......... .......... 37% 6.40M 20s 193250K .......... .......... .......... .......... .......... 37% 15.2M 20s 193300K .......... .......... .......... .......... .......... 37% 14.9M 20s 193350K .......... .......... .......... .......... .......... 37% 10.9M 20s 193400K .......... .......... .......... .......... .......... 37% 17.6M 20s 193450K .......... .......... .......... .......... .......... 37% 13.3M 20s 193500K .......... .......... .......... .......... .......... 37% 15.8M 20s 193550K .......... .......... .......... .......... .......... 37% 16.7M 20s 193600K .......... .......... .......... .......... .......... 37% 11.5M 20s 193650K .......... .......... .......... .......... .......... 37% 12.3M 20s 193700K .......... .......... .......... .......... .......... 38% 10.6M 20s 193750K .......... .......... .......... .......... .......... 38% 13.1M 20s 193800K .......... .......... .......... .......... .......... 38% 15.3M 20s 193850K .......... .......... .......... .......... .......... 38% 14.5M 20s 193900K .......... .......... .......... .......... .......... 38% 13.4M 20s 193950K .......... .......... .......... .......... .......... 38% 9.69M 20s 194000K .......... .......... .......... .......... .......... 38% 12.7M 20s 194050K .......... .......... .......... .......... .......... 38% 11.1M 20s 194100K .......... .......... .......... .......... .......... 38% 9.71M 20s 194150K .......... .......... .......... .......... .......... 38% 12.8M 20s 194200K .......... .......... .......... .......... .......... 38% 10.2M 20s 194250K .......... .......... .......... .......... .......... 38% 11.9M 20s 194300K .......... .......... .......... .......... .......... 38% 20.9M 20s 194350K .......... .......... .......... .......... .......... 38% 19.6M 20s 194400K .......... .......... .......... .......... .......... 38% 19.6M 20s 194450K .......... .......... .......... .......... .......... 38% 16.4M 20s 194500K .......... .......... .......... .......... .......... 38% 21.7M 20s 194550K .......... .......... .......... .......... .......... 38% 15.2M 20s 194600K .......... .......... .......... .......... .......... 38% 11.7M 20s 194650K .......... .......... .......... .......... .......... 38% 13.5M 20s 194700K .......... .......... .......... .......... .......... 38% 12.3M 20s 194750K .......... .......... .......... .......... .......... 38% 14.5M 20s 194800K .......... .......... .......... .......... .......... 38% 12.9M 20s 194850K .......... .......... .......... .......... .......... 38% 10.9M 20s 194900K .......... .......... .......... .......... .......... 38% 12.3M 20s 194950K .......... .......... .......... .......... .......... 38% 8.87M 20s 195000K .......... .......... .......... .......... .......... 38% 11.2M 20s 195050K .......... .......... .......... .......... .......... 38% 18.3M 20s 195100K .......... .......... .......... .......... .......... 38% 23.5M 20s 195150K .......... .......... .......... .......... .......... 38% 19.8M 20s 195200K .......... .......... .......... .......... .......... 38% 42.0M 20s 195250K .......... .......... .......... .......... .......... 38% 22.5M 20s 195300K .......... .......... .......... .......... .......... 38% 16.3M 20s 195350K .......... .......... .......... .......... .......... 38% 18.2M 20s 195400K .......... .......... .......... .......... .......... 38% 16.9M 20s 195450K .......... .......... .......... .......... .......... 38% 13.3M 20s 195500K .......... .......... .......... .......... .......... 38% 16.5M 20s 195550K .......... .......... .......... .......... .......... 38% 12.4M 20s 195600K .......... .......... .......... .......... .......... 38% 12.8M 20s 195650K .......... .......... .......... .......... .......... 38% 16.9M 20s 195700K .......... .......... .......... .......... .......... 38% 11.9M 20s 195750K .......... .......... .......... .......... .......... 38% 15.6M 20s 195800K .......... .......... .......... .......... .......... 38% 13.6M 20s 195850K .......... .......... .......... .......... .......... 38% 12.2M 20s 195900K .......... .......... .......... .......... .......... 38% 17.1M 20s 195950K .......... .......... .......... .......... .......... 38% 12.1M 20s 196000K .......... .......... .......... .......... .......... 38% 14.6M 20s 196050K .......... .......... .......... .......... .......... 38% 15.8M 20s 196100K .......... .......... .......... .......... .......... 38% 22.2M 20s 196150K .......... .......... .......... .......... .......... 38% 24.6M 20s 196200K .......... .......... .......... .......... .......... 38% 61.5M 20s 196250K .......... .......... .......... .......... .......... 38% 40.7M 20s 196300K .......... .......... .......... .......... .......... 38% 57.7M 20s 196350K .......... .......... .......... .......... .......... 38% 26.8M 20s 196400K .......... .......... .......... .......... .......... 38% 31.4M 20s 196450K .......... .......... .......... .......... .......... 38% 23.8M 20s 196500K .......... .......... .......... .......... .......... 38% 33.9M 20s 196550K .......... .......... .......... .......... .......... 38% 34.2M 20s 196600K .......... .......... .......... .......... .......... 38% 21.1M 20s 196650K .......... .......... .......... .......... .......... 38% 19.1M 20s 196700K .......... .......... .......... .......... .......... 38% 12.0M 20s 196750K .......... .......... .......... .......... .......... 38% 14.6M 20s 196800K .......... .......... .......... .......... .......... 38% 11.8M 20s 196850K .......... .......... .......... .......... .......... 38% 10.6M 20s 196900K .......... .......... .......... .......... .......... 38% 16.3M 20s 196950K .......... .......... .......... .......... .......... 38% 10.9M 20s 197000K .......... .......... .......... .......... .......... 38% 11.5M 20s 197050K .......... .......... .......... .......... .......... 38% 14.0M 20s 197100K .......... .......... .......... .......... .......... 38% 13.1M 20s 197150K .......... .......... .......... .......... .......... 38% 13.1M 20s 197200K .......... .......... .......... .......... .......... 38% 11.1M 20s 197250K .......... .......... .......... .......... .......... 38% 12.0M 20s 197300K .......... .......... .......... .......... .......... 38% 11.8M 20s 197350K .......... .......... .......... .......... .......... 38% 9.89M 20s 197400K .......... .......... .......... .......... .......... 38% 11.9M 20s 197450K .......... .......... .......... .......... .......... 38% 9.73M 20s 197500K .......... .......... .......... .......... .......... 38% 12.3M 20s 197550K .......... .......... .......... .......... .......... 38% 11.2M 20s 197600K .......... .......... .......... .......... .......... 38% 13.3M 20s 197650K .......... .......... .......... .......... .......... 38% 21.2M 20s 197700K .......... .......... .......... .......... .......... 38% 186M 20s 197750K .......... .......... .......... .......... .......... 38% 27.3M 20s 197800K .......... .......... .......... .......... .......... 38% 41.5M 20s 197850K .......... .......... .......... .......... .......... 38% 29.1M 20s 197900K .......... .......... .......... .......... .......... 38% 32.3M 20s 197950K .......... .......... .......... .......... .......... 38% 21.9M 20s 198000K .......... .......... .......... .......... .......... 38% 25.4M 20s 198050K .......... .......... .......... .......... .......... 38% 33.3M 20s 198100K .......... .......... .......... .......... .......... 38% 27.2M 20s 198150K .......... .......... .......... .......... .......... 38% 26.6M 20s 198200K .......... .......... .......... .......... .......... 38% 23.6M 20s 198250K .......... .......... .......... .......... .......... 38% 18.4M 20s 198300K .......... .......... .......... .......... .......... 38% 42.4M 20s 198350K .......... .......... .......... .......... .......... 38% 16.5M 20s 198400K .......... .......... .......... .......... .......... 38% 21.9M 20s 198450K .......... .......... .......... .......... .......... 38% 17.9M 20s 198500K .......... .......... .......... .......... .......... 38% 19.2M 20s 198550K .......... .......... .......... .......... .......... 38% 26.9M 20s 198600K .......... .......... .......... .......... .......... 38% 15.4M 20s 198650K .......... .......... .......... .......... .......... 38% 19.0M 20s 198700K .......... .......... .......... .......... .......... 38% 19.5M 20s 198750K .......... .......... .......... .......... .......... 38% 18.0M 20s 198800K .......... .......... .......... .......... .......... 39% 18.3M 20s 198850K .......... .......... .......... .......... .......... 39% 19.8M 20s 198900K .......... .......... .......... .......... .......... 39% 19.5M 20s 198950K .......... .......... .......... .......... .......... 39% 14.9M 20s 199000K .......... .......... .......... .......... .......... 39% 16.4M 20s 199050K .......... .......... .......... .......... .......... 39% 12.9M 20s 199100K .......... .......... .......... .......... .......... 39% 9.08M 20s 199150K .......... .......... .......... .......... .......... 39% 11.3M 20s 199200K .......... .......... .......... .......... .......... 39% 9.16M 20s 199250K .......... .......... .......... .......... .......... 39% 8.51M 20s 199300K .......... .......... .......... .......... .......... 39% 8.34M 20s 199350K .......... .......... .......... .......... .......... 39% 8.28M 20s 199400K .......... .......... .......... .......... .......... 39% 9.86M 20s 199450K .......... .......... .......... .......... .......... 39% 10.2M 20s 199500K .......... .......... .......... .......... .......... 39% 10.4M 20s 199550K .......... .......... .......... .......... .......... 39% 10.8M 20s 199600K .......... .......... .......... .......... .......... 39% 15.1M 20s 199650K .......... .......... .......... .......... .......... 39% 31.7M 20s 199700K .......... .......... .......... .......... .......... 39% 20.3M 20s 199750K .......... .......... .......... .......... .......... 39% 115M 20s 199800K .......... .......... .......... .......... .......... 39% 32.5M 20s 199850K .......... .......... .......... .......... .......... 39% 25.0M 20s 199900K .......... .......... .......... .......... .......... 39% 31.6M 20s 199950K .......... .......... .......... .......... .......... 39% 29.6M 20s 200000K .......... .......... .......... .......... .......... 39% 19.8M 20s 200050K .......... .......... .......... .......... .......... 39% 35.0M 20s 200100K .......... .......... .......... .......... .......... 39% 18.1M 20s 200150K .......... .......... .......... .......... .......... 39% 26.6M 20s 200200K .......... .......... .......... .......... .......... 39% 25.4M 20s 200250K .......... .......... .......... .......... .......... 39% 17.0M 20s 200300K .......... .......... .......... .......... .......... 39% 23.5M 20s 200350K .......... .......... .......... .......... .......... 39% 15.0M 20s 200400K .......... .......... .......... .......... .......... 39% 23.4M 20s 200450K .......... .......... .......... .......... .......... 39% 14.3M 20s 200500K .......... .......... .......... .......... .......... 39% 15.8M 20s 200550K .......... .......... .......... .......... .......... 39% 16.2M 20s 200600K .......... .......... .......... .......... .......... 39% 9.86M 20s 200650K .......... .......... .......... .......... .......... 39% 11.9M 20s 200700K .......... .......... .......... .......... .......... 39% 10.4M 20s 200750K .......... .......... .......... .......... .......... 39% 12.6M 20s 200800K .......... .......... .......... .......... .......... 39% 11.8M 20s 200850K .......... .......... .......... .......... .......... 39% 10.4M 20s 200900K .......... .......... .......... .......... .......... 39% 11.4M 20s 200950K .......... .......... .......... .......... .......... 39% 6.85M 20s 201000K .......... .......... .......... .......... .......... 39% 17.9M 20s 201050K .......... .......... .......... .......... .......... 39% 18.3M 20s 201100K .......... .......... .......... .......... .......... 39% 15.7M 20s 201150K .......... .......... .......... .......... .......... 39% 21.7M 20s 201200K .......... .......... .......... .......... .......... 39% 21.6M 20s 201250K .......... .......... .......... .......... .......... 39% 28.8M 20s 201300K .......... .......... .......... .......... .......... 39% 29.1M 19s 201350K .......... .......... .......... .......... .......... 39% 25.3M 19s 201400K .......... .......... .......... .......... .......... 39% 26.7M 19s 201450K .......... .......... .......... .......... .......... 39% 34.5M 19s 201500K .......... .......... .......... .......... .......... 39% 26.0M 19s 201550K .......... .......... .......... .......... .......... 39% 27.4M 19s 201600K .......... .......... .......... .......... .......... 39% 20.3M 19s 201650K .......... .......... .......... .......... .......... 39% 33.9M 19s 201700K .......... .......... .......... .......... .......... 39% 26.4M 19s 201750K .......... .......... .......... .......... .......... 39% 27.5M 19s 201800K .......... .......... .......... .......... .......... 39% 35.0M 19s 201850K .......... .......... .......... .......... .......... 39% 25.0M 19s 201900K .......... .......... .......... .......... .......... 39% 26.9M 19s 201950K .......... .......... .......... .......... .......... 39% 26.0M 19s 202000K .......... .......... .......... .......... .......... 39% 43.3M 19s 202050K .......... .......... .......... .......... .......... 39% 29.1M 19s 202100K .......... .......... .......... .......... .......... 39% 407M 19s 202150K .......... .......... .......... .......... .......... 39% 31.5M 19s 202200K .......... .......... .......... .......... .......... 39% 51.7M 19s 202250K .......... .......... .......... .......... .......... 39% 57.5M 19s 202300K .......... .......... .......... .......... .......... 39% 41.1M 19s 202350K .......... .......... .......... .......... .......... 39% 24.6M 19s 202400K .......... .......... .......... .......... .......... 39% 55.7M 19s 202450K .......... .......... .......... .......... .......... 39% 23.9M 19s 202500K .......... .......... .......... .......... .......... 39% 23.5M 19s 202550K .......... .......... .......... .......... .......... 39% 37.9M 19s 202600K .......... .......... .......... .......... .......... 39% 23.4M 19s 202650K .......... .......... .......... .......... .......... 39% 19.9M 19s 202700K .......... .......... .......... .......... .......... 39% 17.3M 19s 202750K .......... .......... .......... .......... .......... 39% 24.0M 19s 202800K .......... .......... .......... .......... .......... 39% 21.9M 19s 202850K .......... .......... .......... .......... .......... 39% 18.5M 19s 202900K .......... .......... .......... .......... .......... 39% 21.7M 19s 202950K .......... .......... .......... .......... .......... 39% 18.1M 19s 203000K .......... .......... .......... .......... .......... 39% 25.1M 19s 203050K .......... .......... .......... .......... .......... 39% 19.1M 19s 203100K .......... .......... .......... .......... .......... 39% 14.6M 19s 203150K .......... .......... .......... .......... .......... 39% 24.8M 19s 203200K .......... .......... .......... .......... .......... 39% 21.7M 19s 203250K .......... .......... .......... .......... .......... 39% 24.0M 19s 203300K .......... .......... .......... .......... .......... 39% 41.3M 19s 203350K .......... .......... .......... .......... .......... 39% 38.9M 19s 203400K .......... .......... .......... .......... .......... 39% 119M 19s 203450K .......... .......... .......... .......... .......... 39% 21.7M 19s 203500K .......... .......... .......... .......... .......... 39% 71.1M 19s 203550K .......... .......... .......... .......... .......... 39% 26.0M 19s 203600K .......... .......... .......... .......... .......... 39% 41.9M 19s 203650K .......... .......... .......... .......... .......... 39% 32.1M 19s 203700K .......... .......... .......... .......... .......... 39% 26.4M 19s 203750K .......... .......... .......... .......... .......... 39% 28.1M 19s 203800K .......... .......... .......... .......... .......... 39% 21.1M 19s 203850K .......... .......... .......... .......... .......... 39% 20.6M 19s 203900K .......... .......... .......... .......... .......... 40% 20.3M 19s 203950K .......... .......... .......... .......... .......... 40% 22.6M 19s 204000K .......... .......... .......... .......... .......... 40% 37.6M 19s 204050K .......... .......... .......... .......... .......... 40% 15.5M 19s 204100K .......... .......... .......... .......... .......... 40% 18.1M 19s 204150K .......... .......... .......... .......... .......... 40% 18.1M 19s 204200K .......... .......... .......... .......... .......... 40% 15.8M 19s 204250K .......... .......... .......... .......... .......... 40% 18.9M 19s 204300K .......... .......... .......... .......... .......... 40% 15.3M 19s 204350K .......... .......... .......... .......... .......... 40% 17.3M 19s 204400K .......... .......... .......... .......... .......... 40% 13.0M 19s 204450K .......... .......... .......... .......... .......... 40% 12.4M 19s 204500K .......... .......... .......... .......... .......... 40% 9.50M 19s 204550K .......... .......... .......... .......... .......... 40% 5.81M 19s 204600K .......... .......... .......... .......... .......... 40% 7.78M 19s 204650K .......... .......... .......... .......... .......... 40% 9.08M 19s 204700K .......... .......... .......... .......... .......... 40% 7.88M 19s 204750K .......... .......... .......... .......... .......... 40% 8.72M 19s 204800K .......... .......... .......... .......... .......... 40% 7.31M 19s 204850K .......... .......... .......... .......... .......... 40% 12.7M 19s 204900K .......... .......... .......... .......... .......... 40% 21.1M 19s 204950K .......... .......... .......... .......... .......... 40% 41.8M 19s 205000K .......... .......... .......... .......... .......... 40% 41.3M 19s 205050K .......... .......... .......... .......... .......... 40% 45.2M 19s 205100K .......... .......... .......... .......... .......... 40% 23.9M 19s 205150K .......... .......... .......... .......... .......... 40% 30.5M 19s 205200K .......... .......... .......... .......... .......... 40% 27.9M 19s 205250K .......... .......... .......... .......... .......... 40% 17.6M 19s 205300K .......... .......... .......... .......... .......... 40% 18.2M 19s 205350K .......... .......... .......... .......... .......... 40% 17.2M 19s 205400K .......... .......... .......... .......... .......... 40% 23.3M 19s 205450K .......... .......... .......... .......... .......... 40% 15.2M 19s 205500K .......... .......... .......... .......... .......... 40% 22.4M 19s 205550K .......... .......... .......... .......... .......... 40% 18.1M 19s 205600K .......... .......... .......... .......... .......... 40% 13.9M 19s 205650K .......... .......... .......... .......... .......... 40% 21.6M 19s 205700K .......... .......... .......... .......... .......... 40% 14.2M 19s 205750K .......... .......... .......... .......... .......... 40% 19.6M 19s 205800K .......... .......... .......... .......... .......... 40% 14.8M 19s 205850K .......... .......... .......... .......... .......... 40% 18.5M 19s 205900K .......... .......... .......... .......... .......... 40% 14.3M 19s 205950K .......... .......... .......... .......... .......... 40% 19.8M 19s 206000K .......... .......... .......... .......... .......... 40% 41.8M 19s 206050K .......... .......... .......... .......... .......... 40% 75.6M 19s 206100K .......... .......... .......... .......... .......... 40% 21.5M 19s 206150K .......... .......... .......... .......... .......... 40% 98.6M 19s 206200K .......... .......... .......... .......... .......... 40% 26.5M 19s 206250K .......... .......... .......... .......... .......... 40% 110M 19s 206300K .......... .......... .......... .......... .......... 40% 32.7M 19s 206350K .......... .......... .......... .......... .......... 40% 23.0M 19s 206400K .......... .......... .......... .......... .......... 40% 26.0M 19s 206450K .......... .......... .......... .......... .......... 40% 14.8M 19s 206500K .......... .......... .......... .......... .......... 40% 15.7M 19s 206550K .......... .......... .......... .......... .......... 40% 9.17M 19s 206600K .......... .......... .......... .......... .......... 40% 13.9M 19s 206650K .......... .......... .......... .......... .......... 40% 15.4M 19s 206700K .......... .......... .......... .......... .......... 40% 15.3M 19s 206750K .......... .......... .......... .......... .......... 40% 18.4M 19s 206800K .......... .......... .......... .......... .......... 40% 15.2M 19s 206850K .......... .......... .......... .......... .......... 40% 11.5M 19s 206900K .......... .......... .......... .......... .......... 40% 16.3M 19s 206950K .......... .......... .......... .......... .......... 40% 11.2M 19s 207000K .......... .......... .......... .......... .......... 40% 15.6M 19s 207050K .......... .......... .......... .......... .......... 40% 8.93M 19s 207100K .......... .......... .......... .......... .......... 40% 6.23M 19s 207150K .......... .......... .......... .......... .......... 40% 7.61M 19s 207200K .......... .......... .......... .......... .......... 40% 5.49M 19s 207250K .......... .......... .......... .......... .......... 40% 6.41M 19s 207300K .......... .......... .......... .......... .......... 40% 6.60M 19s 207350K .......... .......... .......... .......... .......... 40% 6.12M 19s 207400K .......... .......... .......... .......... .......... 40% 6.56M 19s 207450K .......... .......... .......... .......... .......... 40% 11.2M 19s 207500K .......... .......... .......... .......... .......... 40% 22.5M 19s 207550K .......... .......... .......... .......... .......... 40% 20.0M 19s 207600K .......... .......... .......... .......... .......... 40% 21.8M 19s 207650K .......... .......... .......... .......... .......... 40% 30.7M 19s 207700K .......... .......... .......... .......... .......... 40% 19.7M 19s 207750K .......... .......... .......... .......... .......... 40% 23.5M 19s 207800K .......... .......... .......... .......... .......... 40% 19.7M 19s 207850K .......... .......... .......... .......... .......... 40% 13.7M 19s 207900K .......... .......... .......... .......... .......... 40% 17.9M 19s 207950K .......... .......... .......... .......... .......... 40% 11.4M 19s 208000K .......... .......... .......... .......... .......... 40% 13.0M 19s 208050K .......... .......... .......... .......... .......... 40% 15.9M 19s 208100K .......... .......... .......... .......... .......... 40% 10.2M 19s 208150K .......... .......... .......... .......... .......... 40% 16.2M 19s 208200K .......... .......... .......... .......... .......... 40% 9.82M 19s 208250K .......... .......... .......... .......... .......... 40% 15.9M 19s 208300K .......... .......... .......... .......... .......... 40% 11.8M 19s 208350K .......... .......... .......... .......... .......... 40% 11.9M 19s 208400K .......... .......... .......... .......... .......... 40% 37.7M 19s 208450K .......... .......... .......... .......... .......... 40% 42.3M 19s 208500K .......... .......... .......... .......... .......... 40% 45.1M 19s 208550K .......... .......... .......... .......... .......... 40% 31.3M 19s 208600K .......... .......... .......... .......... .......... 40% 70.0M 19s 208650K .......... .......... .......... .......... .......... 40% 29.0M 19s 208700K .......... .......... .......... .......... .......... 40% 30.9M 19s 208750K .......... .......... .......... .......... .......... 40% 24.6M 19s 208800K .......... .......... .......... .......... .......... 40% 15.9M 19s 208850K .......... .......... .......... .......... .......... 40% 17.8M 19s 208900K .......... .......... .......... .......... .......... 40% 12.2M 19s 208950K .......... .......... .......... .......... .......... 40% 11.6M 19s 209000K .......... .......... .......... .......... .......... 41% 12.3M 19s 209050K .......... .......... .......... .......... .......... 41% 13.0M 19s 209100K .......... .......... .......... .......... .......... 41% 11.9M 19s 209150K .......... .......... .......... .......... .......... 41% 13.1M 19s 209200K .......... .......... .......... .......... .......... 41% 10.9M 19s 209250K .......... .......... .......... .......... .......... 41% 11.5M 19s 209300K .......... .......... .......... .......... .......... 41% 12.4M 19s 209350K .......... .......... .......... .......... .......... 41% 8.60M 19s 209400K .......... .......... .......... .......... .......... 41% 9.82M 19s 209450K .......... .......... .......... .......... .......... 41% 9.78M 19s 209500K .......... .......... .......... .......... .......... 41% 8.67M 19s 209550K .......... .......... .......... .......... .......... 41% 8.59M 19s 209600K .......... .......... .......... .......... .......... 41% 10.6M 19s 209650K .......... .......... .......... .......... .......... 41% 16.5M 19s 209700K .......... .......... .......... .......... .......... 41% 76.1M 19s 209750K .......... .......... .......... .......... .......... 41% 19.9M 19s 209800K .......... .......... .......... .......... .......... 41% 17.7M 19s 209850K .......... .......... .......... .......... .......... 41% 15.7M 19s 209900K .......... .......... .......... .......... .......... 41% 14.8M 19s 209950K .......... .......... .......... .......... .......... 41% 14.0M 19s 210000K .......... .......... .......... .......... .......... 41% 15.3M 19s 210050K .......... .......... .......... .......... .......... 41% 17.2M 19s 210100K .......... .......... .......... .......... .......... 41% 15.9M 19s 210150K .......... .......... .......... .......... .......... 41% 15.8M 19s 210200K .......... .......... .......... .......... .......... 41% 16.4M 19s 210250K .......... .......... .......... .......... .......... 41% 14.7M 19s 210300K .......... .......... .......... .......... .......... 41% 22.1M 19s 210350K .......... .......... .......... .......... .......... 41% 11.7M 19s 210400K .......... .......... .......... .......... .......... 41% 49.0M 19s 210450K .......... .......... .......... .......... .......... 41% 16.3M 19s 210500K .......... .......... .......... .......... .......... 41% 15.5M 19s 210550K .......... .......... .......... .......... .......... 41% 16.6M 19s 210600K .......... .......... .......... .......... .......... 41% 11.8M 19s 210650K .......... .......... .......... .......... .......... 41% 17.4M 19s 210700K .......... .......... .......... .......... .......... 41% 12.3M 19s 210750K .......... .......... .......... .......... .......... 41% 17.3M 19s 210800K .......... .......... .......... .......... .......... 41% 11.0M 19s 210850K .......... .......... .......... .......... .......... 41% 12.6M 19s 210900K .......... .......... .......... .......... .......... 41% 10.2M 19s 210950K .......... .......... .......... .......... .......... 41% 6.64M 19s 211000K .......... .......... .......... .......... .......... 41% 6.31M 19s 211050K .......... .......... .......... .......... .......... 41% 6.97M 19s 211100K .......... .......... .......... .......... .......... 41% 6.11M 19s 211150K .......... .......... .......... .......... .......... 41% 9.16M 19s 211200K .......... .......... .......... .......... .......... 41% 31.8M 19s 211250K .......... .......... .......... .......... .......... 41% 19.4M 19s 211300K .......... .......... .......... .......... .......... 41% 48.0M 19s 211350K .......... .......... .......... .......... .......... 41% 28.7M 19s 211400K .......... .......... .......... .......... .......... 41% 24.0M 19s 211450K .......... .......... .......... .......... .......... 41% 19.1M 19s 211500K .......... .......... .......... .......... .......... 41% 17.6M 19s 211550K .......... .......... .......... .......... .......... 41% 15.7M 19s 211600K .......... .......... .......... .......... .......... 41% 17.3M 19s 211650K .......... .......... .......... .......... .......... 41% 18.8M 19s 211700K .......... .......... .......... .......... .......... 41% 15.8M 19s 211750K .......... .......... .......... .......... .......... 41% 18.1M 19s 211800K .......... .......... .......... .......... .......... 41% 22.5M 19s 211850K .......... .......... .......... .......... .......... 41% 15.8M 19s 211900K .......... .......... .......... .......... .......... 41% 18.8M 19s 211950K .......... .......... .......... .......... .......... 41% 17.8M 19s 212000K .......... .......... .......... .......... .......... 41% 20.4M 19s 212050K .......... .......... .......... .......... .......... 41% 19.3M 19s 212100K .......... .......... .......... .......... .......... 41% 15.9M 19s 212150K .......... .......... .......... .......... .......... 41% 23.4M 19s 212200K .......... .......... .......... .......... .......... 41% 17.2M 19s 212250K .......... .......... .......... .......... .......... 41% 17.2M 19s 212300K .......... .......... .......... .......... .......... 41% 20.0M 19s 212350K .......... .......... .......... .......... .......... 41% 24.9M 19s 212400K .......... .......... .......... .......... .......... 41% 44.8M 19s 212450K .......... .......... .......... .......... .......... 41% 42.3M 19s 212500K .......... .......... .......... .......... .......... 41% 30.5M 19s 212550K .......... .......... .......... .......... .......... 41% 432M 19s 212600K .......... .......... .......... .......... .......... 41% 29.3M 19s 212650K .......... .......... .......... .......... .......... 41% 90.6M 19s 212700K .......... .......... .......... .......... .......... 41% 37.5M 19s 212750K .......... .......... .......... .......... .......... 41% 30.5M 19s 212800K .......... .......... .......... .......... .......... 41% 31.5M 19s 212850K .......... .......... .......... .......... .......... 41% 24.6M 19s 212900K .......... .......... .......... .......... .......... 41% 25.7M 19s 212950K .......... .......... .......... .......... .......... 41% 18.0M 19s 213000K .......... .......... .......... .......... .......... 41% 23.7M 19s 213050K .......... .......... .......... .......... .......... 41% 25.2M 19s 213100K .......... .......... .......... .......... .......... 41% 18.9M 19s 213150K .......... .......... .......... .......... .......... 41% 25.1M 19s 213200K .......... .......... .......... .......... .......... 41% 13.2M 19s 213250K .......... .......... .......... .......... .......... 41% 15.4M 19s 213300K .......... .......... .......... .......... .......... 41% 23.5M 19s 213350K .......... .......... .......... .......... .......... 41% 12.3M 19s 213400K .......... .......... .......... .......... .......... 41% 18.2M 19s 213450K .......... .......... .......... .......... .......... 41% 13.4M 19s 213500K .......... .......... .......... .......... .......... 41% 14.1M 19s 213550K .......... .......... .......... .......... .......... 41% 15.8M 19s 213600K .......... .......... .......... .......... .......... 41% 10.2M 19s 213650K .......... .......... .......... .......... .......... 41% 16.5M 19s 213700K .......... .......... .......... .......... .......... 41% 14.0M 19s 213750K .......... .......... .......... .......... .......... 41% 8.20M 19s 213800K .......... .......... .......... .......... .......... 41% 8.65M 19s 213850K .......... .......... .......... .......... .......... 41% 7.30M 19s 213900K .......... .......... .......... .......... .......... 41% 9.83M 19s 213950K .......... .......... .......... .......... .......... 41% 6.93M 19s 214000K .......... .......... .......... .......... .......... 41% 13.6M 19s 214050K .......... .......... .......... .......... .......... 41% 12.6M 19s 214100K .......... .......... .......... .......... .......... 42% 9.24M 19s 214150K .......... .......... .......... .......... .......... 42% 13.6M 19s 214200K .......... .......... .......... .......... .......... 42% 14.1M 19s 214250K .......... .......... .......... .......... .......... 42% 11.5M 19s 214300K .......... .......... .......... .......... .......... 42% 10.6M 19s 214350K .......... .......... .......... .......... .......... 42% 6.92M 19s 214400K .......... .......... .......... .......... .......... 42% 8.99M 19s 214450K .......... .......... .......... .......... .......... 42% 8.09M 19s 214500K .......... .......... .......... .......... .......... 42% 17.2M 19s 214550K .......... .......... .......... .......... .......... 42% 10.7M 19s 214600K .......... .......... .......... .......... .......... 42% 213M 19s 214650K .......... .......... .......... .......... .......... 42% 17.0M 19s 214700K .......... .......... .......... .......... .......... 42% 25.2M 19s 214750K .......... .......... .......... .......... .......... 42% 27.1M 19s 214800K .......... .......... .......... .......... .......... 42% 29.2M 19s 214850K .......... .......... .......... .......... .......... 42% 14.5M 19s 214900K .......... .......... .......... .......... .......... 42% 19.9M 19s 214950K .......... .......... .......... .......... .......... 42% 20.8M 19s 215000K .......... .......... .......... .......... .......... 42% 13.3M 19s 215050K .......... .......... .......... .......... .......... 42% 10.5M 19s 215100K .......... .......... .......... .......... .......... 42% 10.0M 19s 215150K .......... .......... .......... .......... .......... 42% 12.5M 19s 215200K .......... .......... .......... .......... .......... 42% 9.73M 19s 215250K .......... .......... .......... .......... .......... 42% 12.0M 19s 215300K .......... .......... .......... .......... .......... 42% 12.0M 19s 215350K .......... .......... .......... .......... .......... 42% 6.94M 19s 215400K .......... .......... .......... .......... .......... 42% 9.55M 19s 215450K .......... .......... .......... .......... .......... 42% 21.2M 19s 215500K .......... .......... .......... .......... .......... 42% 21.0M 19s 215550K .......... .......... .......... .......... .......... 42% 24.8M 19s 215600K .......... .......... .......... .......... .......... 42% 29.3M 19s 215650K .......... .......... .......... .......... .......... 42% 22.8M 19s 215700K .......... .......... .......... .......... .......... 42% 39.3M 19s 215750K .......... .......... .......... .......... .......... 42% 19.0M 19s 215800K .......... .......... .......... .......... .......... 42% 17.7M 19s 215850K .......... .......... .......... .......... .......... 42% 14.5M 19s 215900K .......... .......... .......... .......... .......... 42% 17.3M 19s 215950K .......... .......... .......... .......... .......... 42% 14.7M 19s 216000K .......... .......... .......... .......... .......... 42% 14.0M 19s 216050K .......... .......... .......... .......... .......... 42% 14.6M 19s 216100K .......... .......... .......... .......... .......... 42% 13.5M 19s 216150K .......... .......... .......... .......... .......... 42% 12.6M 19s 216200K .......... .......... .......... .......... .......... 42% 9.54M 19s 216250K .......... .......... .......... .......... .......... 42% 13.2M 19s 216300K .......... .......... .......... .......... .......... 42% 12.6M 19s 216350K .......... .......... .......... .......... .......... 42% 11.4M 19s 216400K .......... .......... .......... .......... .......... 42% 11.1M 19s 216450K .......... .......... .......... .......... .......... 42% 12.1M 19s 216500K .......... .......... .......... .......... .......... 42% 12.8M 19s 216550K .......... .......... .......... .......... .......... 42% 11.8M 19s 216600K .......... .......... .......... .......... .......... 42% 13.9M 19s 216650K .......... .......... .......... .......... .......... 42% 25.4M 18s 216700K .......... .......... .......... .......... .......... 42% 20.9M 18s 216750K .......... .......... .......... .......... .......... 42% 18.8M 18s 216800K .......... .......... .......... .......... .......... 42% 23.8M 18s 216850K .......... .......... .......... .......... .......... 42% 20.8M 18s 216900K .......... .......... .......... .......... .......... 42% 19.3M 18s 216950K .......... .......... .......... .......... .......... 42% 16.4M 18s 217000K .......... .......... .......... .......... .......... 42% 15.9M 18s 217050K .......... .......... .......... .......... .......... 42% 15.8M 18s 217100K .......... .......... .......... .......... .......... 42% 14.4M 18s 217150K .......... .......... .......... .......... .......... 42% 16.5M 18s 217200K .......... .......... .......... .......... .......... 42% 11.4M 18s 217250K .......... .......... .......... .......... .......... 42% 16.4M 18s 217300K .......... .......... .......... .......... .......... 42% 10.6M 18s 217350K .......... .......... .......... .......... .......... 42% 7.13M 18s 217400K .......... .......... .......... .......... .......... 42% 7.17M 18s 217450K .......... .......... .......... .......... .......... 42% 7.19M 18s 217500K .......... .......... .......... .......... .......... 42% 16.7M 18s 217550K .......... .......... .......... .......... .......... 42% 28.5M 18s 217600K .......... .......... .......... .......... .......... 42% 23.9M 18s 217650K .......... .......... .......... .......... .......... 42% 21.4M 18s 217700K .......... .......... .......... .......... .......... 42% 11.7M 18s 217750K .......... .......... .......... .......... .......... 42% 22.5M 18s 217800K .......... .......... .......... .......... .......... 42% 24.6M 18s 217850K .......... .......... .......... .......... .......... 42% 18.6M 18s 217900K .......... .......... .......... .......... .......... 42% 19.9M 18s 217950K .......... .......... .......... .......... .......... 42% 25.2M 18s 218000K .......... .......... .......... .......... .......... 42% 18.1M 18s 218050K .......... .......... .......... .......... .......... 42% 21.2M 18s 218100K .......... .......... .......... .......... .......... 42% 15.2M 18s 218150K .......... .......... .......... .......... .......... 42% 25.1M 18s 218200K .......... .......... .......... .......... .......... 42% 18.1M 18s 218250K .......... .......... .......... .......... .......... 42% 20.9M 18s 218300K .......... .......... .......... .......... .......... 42% 20.8M 18s 218350K .......... .......... .......... .......... .......... 42% 17.6M 18s 218400K .......... .......... .......... .......... .......... 42% 12.6M 18s 218450K .......... .......... .......... .......... .......... 42% 11.8M 18s 218500K .......... .......... .......... .......... .......... 42% 10.6M 18s 218550K .......... .......... .......... .......... .......... 42% 7.34M 18s 218600K .......... .......... .......... .......... .......... 42% 10.7M 18s 218650K .......... .......... .......... .......... .......... 42% 8.92M 18s 218700K .......... .......... .......... .......... .......... 42% 10.3M 18s 218750K .......... .......... .......... .......... .......... 42% 17.9M 18s 218800K .......... .......... .......... .......... .......... 42% 22.4M 18s 218850K .......... .......... .......... .......... .......... 42% 15.0M 18s 218900K .......... .......... .......... .......... .......... 42% 22.6M 18s 218950K .......... .......... .......... .......... .......... 42% 12.5M 18s 219000K .......... .......... .......... .......... .......... 42% 18.9M 18s 219050K .......... .......... .......... .......... .......... 42% 18.1M 18s 219100K .......... .......... .......... .......... .......... 42% 12.3M 18s 219150K .......... .......... .......... .......... .......... 42% 11.4M 18s 219200K .......... .......... .......... .......... .......... 43% 9.98M 18s 219250K .......... .......... .......... .......... .......... 43% 14.0M 18s 219300K .......... .......... .......... .......... .......... 43% 8.23M 18s 219350K .......... .......... .......... .......... .......... 43% 7.82M 18s 219400K .......... .......... .......... .......... .......... 43% 9.69M 18s 219450K .......... .......... .......... .......... .......... 43% 8.89M 18s 219500K .......... .......... .......... .......... .......... 43% 9.93M 18s 219550K .......... .......... .......... .......... .......... 43% 10.9M 18s 219600K .......... .......... .......... .......... .......... 43% 8.44M 18s 219650K .......... .......... .......... .......... .......... 43% 14.3M 18s 219700K .......... .......... .......... .......... .......... 43% 22.7M 18s 219750K .......... .......... .......... .......... .......... 43% 20.1M 18s 219800K .......... .......... .......... .......... .......... 43% 25.4M 18s 219850K .......... .......... .......... .......... .......... 43% 23.7M 18s 219900K .......... .......... .......... .......... .......... 43% 25.3M 18s 219950K .......... .......... .......... .......... .......... 43% 20.7M 18s 220000K .......... .......... .......... .......... .......... 43% 20.4M 18s 220050K .......... .......... .......... .......... .......... 43% 27.2M 18s 220100K .......... .......... .......... .......... .......... 43% 16.3M 18s 220150K .......... .......... .......... .......... .......... 43% 16.9M 18s 220200K .......... .......... .......... .......... .......... 43% 19.0M 18s 220250K .......... .......... .......... .......... .......... 43% 19.0M 18s 220300K .......... .......... .......... .......... .......... 43% 17.8M 18s 220350K .......... .......... .......... .......... .......... 43% 14.1M 18s 220400K .......... .......... .......... .......... .......... 43% 20.8M 18s 220450K .......... .......... .......... .......... .......... 43% 14.6M 18s 220500K .......... .......... .......... .......... .......... 43% 23.4M 18s 220550K .......... .......... .......... .......... .......... 43% 14.9M 18s 220600K .......... .......... .......... .......... .......... 43% 11.0M 18s 220650K .......... .......... .......... .......... .......... 43% 10.8M 18s 220700K .......... .......... .......... .......... .......... 43% 7.44M 18s 220750K .......... .......... .......... .......... .......... 43% 9.97M 18s 220800K .......... .......... .......... .......... .......... 43% 13.0M 18s 220850K .......... .......... .......... .......... .......... 43% 9.31M 18s 220900K .......... .......... .......... .......... .......... 43% 9.49M 18s 220950K .......... .......... .......... .......... .......... 43% 7.64M 18s 221000K .......... .......... .......... .......... .......... 43% 8.58M 18s 221050K .......... .......... .......... .......... .......... 43% 12.1M 18s 221100K .......... .......... .......... .......... .......... 43% 11.0M 18s 221150K .......... .......... .......... .......... .......... 43% 10.2M 18s 221200K .......... .......... .......... .......... .......... 43% 10.1M 18s 221250K .......... .......... .......... .......... .......... 43% 11.6M 18s 221300K .......... .......... .......... .......... .......... 43% 9.66M 18s 221350K .......... .......... .......... .......... .......... 43% 9.22M 18s 221400K .......... .......... .......... .......... .......... 43% 21.7M 18s 221450K .......... .......... .......... .......... .......... 43% 20.1M 18s 221500K .......... .......... .......... .......... .......... 43% 23.3M 18s 221550K .......... .......... .......... .......... .......... 43% 132M 18s 221600K .......... .......... .......... .......... .......... 43% 22.3M 18s 221650K .......... .......... .......... .......... .......... 43% 28.0M 18s 221700K .......... .......... .......... .......... .......... 43% 24.8M 18s 221750K .......... .......... .......... .......... .......... 43% 25.7M 18s 221800K .......... .......... .......... .......... .......... 43% 28.2M 18s 221850K .......... .......... .......... .......... .......... 43% 24.2M 18s 221900K .......... .......... .......... .......... .......... 43% 22.2M 18s 221950K .......... .......... .......... .......... .......... 43% 37.7M 18s 222000K .......... .......... .......... .......... .......... 43% 24.6M 18s 222050K .......... .......... .......... .......... .......... 43% 27.0M 18s 222100K .......... .......... .......... .......... .......... 43% 15.0M 18s 222150K .......... .......... .......... .......... .......... 43% 41.8M 18s 222200K .......... .......... .......... .......... .......... 43% 21.1M 18s 222250K .......... .......... .......... .......... .......... 43% 23.8M 18s 222300K .......... .......... .......... .......... .......... 43% 27.2M 18s 222350K .......... .......... .......... .......... .......... 43% 22.9M 18s 222400K .......... .......... .......... .......... .......... 43% 25.4M 18s 222450K .......... .......... .......... .......... .......... 43% 19.3M 18s 222500K .......... .......... .......... .......... .......... 43% 26.0M 18s 222550K .......... .......... .......... .......... .......... 43% 27.0M 18s 222600K .......... .......... .......... .......... .......... 43% 18.1M 18s 222650K .......... .......... .......... .......... .......... 43% 22.3M 18s 222700K .......... .......... .......... .......... .......... 43% 14.6M 18s 222750K .......... .......... .......... .......... .......... 43% 25.4M 18s 222800K .......... .......... .......... .......... .......... 43% 19.0M 18s 222850K .......... .......... .......... .......... .......... 43% 18.0M 18s 222900K .......... .......... .......... .......... .......... 43% 25.1M 18s 222950K .......... .......... .......... .......... .......... 43% 16.7M 18s 223000K .......... .......... .......... .......... .......... 43% 16.5M 18s 223050K .......... .......... .......... .......... .......... 43% 509M 18s 223100K .......... .......... .......... .......... .......... 43% 11.7M 18s 223150K .......... .......... .......... .......... .......... 43% 165M 18s 223200K .......... .......... .......... .......... .......... 43% 21.6M 18s 223250K .......... .......... .......... .......... .......... 43% 17.1M 18s 223300K .......... .......... .......... .......... .......... 43% 12.7M 18s 223350K .......... .......... .......... .......... .......... 43% 11.9M 18s 223400K .......... .......... .......... .......... .......... 43% 16.5M 18s 223450K .......... .......... .......... .......... .......... 43% 15.7M 18s 223500K .......... .......... .......... .......... .......... 43% 12.3M 18s 223550K .......... .......... .......... .......... .......... 43% 15.6M 18s 223600K .......... .......... .......... .......... .......... 43% 15.1M 18s 223650K .......... .......... .......... .......... .......... 43% 16.5M 18s 223700K .......... .......... .......... .......... .......... 43% 14.7M 18s 223750K .......... .......... .......... .......... .......... 43% 15.1M 18s 223800K .......... .......... .......... .......... .......... 43% 15.5M 18s 223850K .......... .......... .......... .......... .......... 43% 10.7M 18s 223900K .......... .......... .......... .......... .......... 43% 17.1M 18s 223950K .......... .......... .......... .......... .......... 43% 13.2M 18s 224000K .......... .......... .......... .......... .......... 43% 16.4M 18s 224050K .......... .......... .......... .......... .......... 43% 16.6M 18s 224100K .......... .......... .......... .......... .......... 43% 13.1M 18s 224150K .......... .......... .......... .......... .......... 43% 15.7M 18s 224200K .......... .......... .......... .......... .......... 43% 12.4M 18s 224250K .......... .......... .......... .......... .......... 43% 15.9M 18s 224300K .......... .......... .......... .......... .......... 44% 16.0M 18s 224350K .......... .......... .......... .......... .......... 44% 15.9M 18s 224400K .......... .......... .......... .......... .......... 44% 17.4M 18s 224450K .......... .......... .......... .......... .......... 44% 23.7M 18s 224500K .......... .......... .......... .......... .......... 44% 26.3M 18s 224550K .......... .......... .......... .......... .......... 44% 75.4M 18s 224600K .......... .......... .......... .......... .......... 44% 26.9M 18s 224650K .......... .......... .......... .......... .......... 44% 34.7M 18s 224700K .......... .......... .......... .......... .......... 44% 34.6M 18s 224750K .......... .......... .......... .......... .......... 44% 23.5M 18s 224800K .......... .......... .......... .......... .......... 44% 17.1M 18s 224850K .......... .......... .......... .......... .......... 44% 26.7M 18s 224900K .......... .......... .......... .......... .......... 44% 22.2M 18s 224950K .......... .......... .......... .......... .......... 44% 17.4M 18s 225000K .......... .......... .......... .......... .......... 44% 26.9M 18s 225050K .......... .......... .......... .......... .......... 44% 16.7M 18s 225100K .......... .......... .......... .......... .......... 44% 20.6M 18s 225150K .......... .......... .......... .......... .......... 44% 17.8M 18s 225200K .......... .......... .......... .......... .......... 44% 21.7M 18s 225250K .......... .......... .......... .......... .......... 44% 21.2M 18s 225300K .......... .......... .......... .......... .......... 44% 22.0M 18s 225350K .......... .......... .......... .......... .......... 44% 19.7M 18s 225400K .......... .......... .......... .......... .......... 44% 11.1M 18s 225450K .......... .......... .......... .......... .......... 44% 15.8M 18s 225500K .......... .......... .......... .......... .......... 44% 14.7M 18s 225550K .......... .......... .......... .......... .......... 44% 14.2M 18s 225600K .......... .......... .......... .......... .......... 44% 10.9M 18s 225650K .......... .......... .......... .......... .......... 44% 16.5M 18s 225700K .......... .......... .......... .......... .......... 44% 10.9M 18s 225750K .......... .......... .......... .......... .......... 44% 14.4M 18s 225800K .......... .......... .......... .......... .......... 44% 12.0M 18s 225850K .......... .......... .......... .......... .......... 44% 12.2M 18s 225900K .......... .......... .......... .......... .......... 44% 11.9M 18s 225950K .......... .......... .......... .......... .......... 44% 10.2M 18s 226000K .......... .......... .......... .......... .......... 44% 10.3M 18s 226050K .......... .......... .......... .......... .......... 44% 12.6M 18s 226100K .......... .......... .......... .......... .......... 44% 9.72M 18s 226150K .......... .......... .......... .......... .......... 44% 9.11M 18s 226200K .......... .......... .......... .......... .......... 44% 10.2M 18s 226250K .......... .......... .......... .......... .......... 44% 9.66M 18s 226300K .......... .......... .......... .......... .......... 44% 8.86M 18s 226350K .......... .......... .......... .......... .......... 44% 8.63M 18s 226400K .......... .......... .......... .......... .......... 44% 9.80M 18s 226450K .......... .......... .......... .......... .......... 44% 8.22M 18s 226500K .......... .......... .......... .......... .......... 44% 9.27M 18s 226550K .......... .......... .......... .......... .......... 44% 18.2M 18s 226600K .......... .......... .......... .......... .......... 44% 27.5M 18s 226650K .......... .......... .......... .......... .......... 44% 36.1M 18s 226700K .......... .......... .......... .......... .......... 44% 23.3M 18s 226750K .......... .......... .......... .......... .......... 44% 25.0M 18s 226800K .......... .......... .......... .......... .......... 44% 15.7M 18s 226850K .......... .......... .......... .......... .......... 44% 15.8M 18s 226900K .......... .......... .......... .......... .......... 44% 18.2M 18s 226950K .......... .......... .......... .......... .......... 44% 15.8M 18s 227000K .......... .......... .......... .......... .......... 44% 17.2M 18s 227050K .......... .......... .......... .......... .......... 44% 16.5M 18s 227100K .......... .......... .......... .......... .......... 44% 16.1M 18s 227150K .......... .......... .......... .......... .......... 44% 13.1M 18s 227200K .......... .......... .......... .......... .......... 44% 15.7M 18s 227250K .......... .......... .......... .......... .......... 44% 14.2M 18s 227300K .......... .......... .......... .......... .......... 44% 13.3M 18s 227350K .......... .......... .......... .......... .......... 44% 13.2M 18s 227400K .......... .......... .......... .......... .......... 44% 13.6M 18s 227450K .......... .......... .......... .......... .......... 44% 10.3M 18s 227500K .......... .......... .......... .......... .......... 44% 10.8M 18s 227550K .......... .......... .......... .......... .......... 44% 12.5M 18s 227600K .......... .......... .......... .......... .......... 44% 8.67M 18s 227650K .......... .......... .......... .......... .......... 44% 13.8M 18s 227700K .......... .......... .......... .......... .......... 44% 26.2M 18s 227750K .......... .......... .......... .......... .......... 44% 17.1M 18s 227800K .......... .......... .......... .......... .......... 44% 18.9M 18s 227850K .......... .......... .......... .......... .......... 44% 16.9M 18s 227900K .......... .......... .......... .......... .......... 44% 16.7M 18s 227950K .......... .......... .......... .......... .......... 44% 21.2M 18s 228000K .......... .......... .......... .......... .......... 44% 19.2M 18s 228050K .......... .......... .......... .......... .......... 44% 14.1M 18s 228100K .......... .......... .......... .......... .......... 44% 11.3M 18s 228150K .......... .......... .......... .......... .......... 44% 11.2M 18s 228200K .......... .......... .......... .......... .......... 44% 9.36M 18s 228250K .......... .......... .......... .......... .......... 44% 11.5M 18s 228300K .......... .......... .......... .......... .......... 44% 11.3M 18s 228350K .......... .......... .......... .......... .......... 44% 9.96M 18s 228400K .......... .......... .......... .......... .......... 44% 12.0M 18s 228450K .......... .......... .......... .......... .......... 44% 8.31M 18s 228500K .......... .......... .......... .......... .......... 44% 8.55M 18s 228550K .......... .......... .......... .......... .......... 44% 7.96M 18s 228600K .......... .......... .......... .......... .......... 44% 7.00M 18s 228650K .......... .......... .......... .......... .......... 44% 9.11M 18s 228700K .......... .......... .......... .......... .......... 44% 7.45M 18s 228750K .......... .......... .......... .......... .......... 44% 8.11M 18s 228800K .......... .......... .......... .......... .......... 44% 11.9M 18s 228850K .......... .......... .......... .......... .......... 44% 8.32M 18s 228900K .......... .......... .......... .......... .......... 44% 10.7M 18s 228950K .......... .......... .......... .......... .......... 44% 8.75M 18s 229000K .......... .......... .......... .......... .......... 44% 9.85M 18s 229050K .......... .......... .......... .......... .......... 44% 10.9M 18s 229100K .......... .......... .......... .......... .......... 44% 16.6M 18s 229150K .......... .......... .......... .......... .......... 44% 25.4M 18s 229200K .......... .......... .......... .......... .......... 44% 37.6M 18s 229250K .......... .......... .......... .......... .......... 44% 24.6M 18s 229300K .......... .......... .......... .......... .......... 44% 38.6M 18s 229350K .......... .......... .......... .......... .......... 44% 38.7M 18s 229400K .......... .......... .......... .......... .......... 45% 16.2M 18s 229450K .......... .......... .......... .......... .......... 45% 25.6M 18s 229500K .......... .......... .......... .......... .......... 45% 20.9M 18s 229550K .......... .......... .......... .......... .......... 45% 26.9M 18s 229600K .......... .......... .......... .......... .......... 45% 19.5M 18s 229650K .......... .......... .......... .......... .......... 45% 18.8M 18s 229700K .......... .......... .......... .......... .......... 45% 21.9M 18s 229750K .......... .......... .......... .......... .......... 45% 19.9M 18s 229800K .......... .......... .......... .......... .......... 45% 26.9M 18s 229850K .......... .......... .......... .......... .......... 45% 17.4M 18s 229900K .......... .......... .......... .......... .......... 45% 27.0M 18s 229950K .......... .......... .......... .......... .......... 45% 14.6M 18s 230000K .......... .......... .......... .......... .......... 45% 16.7M 18s 230050K .......... .......... .......... .......... .......... 45% 17.2M 18s 230100K .......... .......... .......... .......... .......... 45% 17.7M 18s 230150K .......... .......... .......... .......... .......... 45% 15.5M 18s 230200K .......... .......... .......... .......... .......... 45% 15.8M 18s 230250K .......... .......... .......... .......... .......... 45% 16.7M 18s 230300K .......... .......... .......... .......... .......... 45% 17.3M 18s 230350K .......... .......... .......... .......... .......... 45% 12.5M 18s 230400K .......... .......... .......... .......... .......... 45% 14.6M 18s 230450K .......... .......... .......... .......... .......... 45% 12.3M 18s 230500K .......... .......... .......... .......... .......... 45% 12.7M 18s 230550K .......... .......... .......... .......... .......... 45% 10.3M 18s 230600K .......... .......... .......... .......... .......... 45% 9.48M 18s 230650K .......... .......... .......... .......... .......... 45% 7.81M 18s 230700K .......... .......... .......... .......... .......... 45% 10.3M 18s 230750K .......... .......... .......... .......... .......... 45% 22.2M 18s 230800K .......... .......... .......... .......... .......... 45% 20.0M 18s 230850K .......... .......... .......... .......... .......... 45% 24.0M 18s 230900K .......... .......... .......... .......... .......... 45% 23.5M 18s 230950K .......... .......... .......... .......... .......... 45% 24.4M 18s 231000K .......... .......... .......... .......... .......... 45% 21.2M 18s 231050K .......... .......... .......... .......... .......... 45% 23.7M 18s 231100K .......... .......... .......... .......... .......... 45% 15.9M 18s 231150K .......... .......... .......... .......... .......... 45% 25.0M 18s 231200K .......... .......... .......... .......... .......... 45% 23.1M 18s 231250K .......... .......... .......... .......... .......... 45% 16.8M 18s 231300K .......... .......... .......... .......... .......... 45% 18.7M 18s 231350K .......... .......... .......... .......... .......... 45% 17.9M 18s 231400K .......... .......... .......... .......... .......... 45% 11.9M 18s 231450K .......... .......... .......... .......... .......... 45% 12.6M 18s 231500K .......... .......... .......... .......... .......... 45% 15.3M 18s 231550K .......... .......... .......... .......... .......... 45% 13.6M 18s 231600K .......... .......... .......... .......... .......... 45% 11.0M 18s 231650K .......... .......... .......... .......... .......... 45% 12.3M 18s 231700K .......... .......... .......... .......... .......... 45% 10.5M 18s 231750K .......... .......... .......... .......... .......... 45% 11.2M 18s 231800K .......... .......... .......... .......... .......... 45% 12.0M 18s 231850K .......... .......... .......... .......... .......... 45% 9.33M 18s 231900K .......... .......... .......... .......... .......... 45% 11.9M 18s 231950K .......... .......... .......... .......... .......... 45% 10.1M 18s 232000K .......... .......... .......... .......... .......... 45% 21.2M 18s 232050K .......... .......... .......... .......... .......... 45% 24.3M 18s 232100K .......... .......... .......... .......... .......... 45% 30.9M 18s 232150K .......... .......... .......... .......... .......... 45% 17.1M 18s 232200K .......... .......... .......... .......... .......... 45% 34.5M 18s 232250K .......... .......... .......... .......... .......... 45% 27.7M 18s 232300K .......... .......... .......... .......... .......... 45% 26.2M 18s 232350K .......... .......... .......... .......... .......... 45% 16.6M 18s 232400K .......... .......... .......... .......... .......... 45% 18.2M 18s 232450K .......... .......... .......... .......... .......... 45% 13.5M 18s 232500K .......... .......... .......... .......... .......... 45% 14.1M 18s 232550K .......... .......... .......... .......... .......... 45% 17.4M 18s 232600K .......... .......... .......... .......... .......... 45% 12.7M 18s 232650K .......... .......... .......... .......... .......... 45% 16.0M 18s 232700K .......... .......... .......... .......... .......... 45% 12.7M 18s 232750K .......... .......... .......... .......... .......... 45% 16.4M 18s 232800K .......... .......... .......... .......... .......... 45% 13.0M 18s 232850K .......... .......... .......... .......... .......... 45% 13.2M 18s 232900K .......... .......... .......... .......... .......... 45% 17.3M 18s 232950K .......... .......... .......... .......... .......... 45% 25.2M 18s 233000K .......... .......... .......... .......... .......... 45% 26.3M 18s 233050K .......... .......... .......... .......... .......... 45% 29.6M 18s 233100K .......... .......... .......... .......... .......... 45% 31.5M 18s 233150K .......... .......... .......... .......... .......... 45% 27.0M 17s 233200K .......... .......... .......... .......... .......... 45% 37.9M 17s 233250K .......... .......... .......... .......... .......... 45% 16.5M 17s 233300K .......... .......... .......... .......... .......... 45% 568M 17s 233350K .......... .......... .......... .......... .......... 45% 30.6M 17s 233400K .......... .......... .......... .......... .......... 45% 31.6M 17s 233450K .......... .......... .......... .......... .......... 45% 37.2M 17s 233500K .......... .......... .......... .......... .......... 45% 21.7M 17s 233550K .......... .......... .......... .......... .......... 45% 49.0M 17s 233600K .......... .......... .......... .......... .......... 45% 22.3M 17s 233650K .......... .......... .......... .......... .......... 45% 26.5M 17s 233700K .......... .......... .......... .......... .......... 45% 34.9M 17s 233750K .......... .......... .......... .......... .......... 45% 25.6M 17s 233800K .......... .......... .......... .......... .......... 45% 23.7M 17s 233850K .......... .......... .......... .......... .......... 45% 17.0M 17s 233900K .......... .......... .......... .......... .......... 45% 35.1M 17s 233950K .......... .......... .......... .......... .......... 45% 16.5M 17s 234000K .......... .......... .......... .......... .......... 45% 23.8M 17s 234050K .......... .......... .......... .......... .......... 45% 25.3M 17s 234100K .......... .......... .......... .......... .......... 45% 30.6M 17s 234150K .......... .......... .......... .......... .......... 45% 19.1M 17s 234200K .......... .......... .......... .......... .......... 45% 23.6M 17s 234250K .......... .......... .......... .......... .......... 45% 25.4M 17s 234300K .......... .......... .......... .......... .......... 45% 25.0M 17s 234350K .......... .......... .......... .......... .......... 45% 14.3M 17s 234400K .......... .......... .......... .......... .......... 45% 12.3M 17s 234450K .......... .......... .......... .......... .......... 45% 8.16M 17s 234500K .......... .......... .......... .......... .......... 46% 14.0M 17s 234550K .......... .......... .......... .......... .......... 46% 11.3M 17s 234600K .......... .......... .......... .......... .......... 46% 9.08M 17s 234650K .......... .......... .......... .......... .......... 46% 15.0M 17s 234700K .......... .......... .......... .......... .......... 46% 13.1M 17s 234750K .......... .......... .......... .......... .......... 46% 14.1M 17s 234800K .......... .......... .......... .......... .......... 46% 14.5M 17s 234850K .......... .......... .......... .......... .......... 46% 14.0M 17s 234900K .......... .......... .......... .......... .......... 46% 14.1M 17s 234950K .......... .......... .......... .......... .......... 46% 12.2M 17s 235000K .......... .......... .......... .......... .......... 46% 13.9M 17s 235050K .......... .......... .......... .......... .......... 46% 16.5M 17s 235100K .......... .......... .......... .......... .......... 46% 15.8M 17s 235150K .......... .......... .......... .......... .......... 46% 22.5M 17s 235200K .......... .......... .......... .......... .......... 46% 30.4M 17s 235250K .......... .......... .......... .......... .......... 46% 46.0M 17s 235300K .......... .......... .......... .......... .......... 46% 18.9M 17s 235350K .......... .......... .......... .......... .......... 46% 20.2M 17s 235400K .......... .......... .......... .......... .......... 46% 24.9M 17s 235450K .......... .......... .......... .......... .......... 46% 15.4M 17s 235500K .......... .......... .......... .......... .......... 46% 23.9M 17s 235550K .......... .......... .......... .......... .......... 46% 17.4M 17s 235600K .......... .......... .......... .......... .......... 46% 22.0M 17s 235650K .......... .......... .......... .......... .......... 46% 16.2M 17s 235700K .......... .......... .......... .......... .......... 46% 14.6M 17s 235750K .......... .......... .......... .......... .......... 46% 17.3M 17s 235800K .......... .......... .......... .......... .......... 46% 18.1M 17s 235850K .......... .......... .......... .......... .......... 46% 15.3M 17s 235900K .......... .......... .......... .......... .......... 46% 17.3M 17s 235950K .......... .......... .......... .......... .......... 46% 15.0M 17s 236000K .......... .......... .......... .......... .......... 46% 9.34M 17s 236050K .......... .......... .......... .......... .......... 46% 8.62M 17s 236100K .......... .......... .......... .......... .......... 46% 8.10M 17s 236150K .......... .......... .......... .......... .......... 46% 12.7M 17s 236200K .......... .......... .......... .......... .......... 46% 19.2M 17s 236250K .......... .......... .......... .......... .......... 46% 10.5M 17s 236300K .......... .......... .......... .......... .......... 46% 38.0M 17s 236350K .......... .......... .......... .......... .......... 46% 10.3M 17s 236400K .......... .......... .......... .......... .......... 46% 21.3M 17s 236450K .......... .......... .......... .......... .......... 46% 13.7M 17s 236500K .......... .......... .......... .......... .......... 46% 16.9M 17s 236550K .......... .......... .......... .......... .......... 46% 13.2M 17s 236600K .......... .......... .......... .......... .......... 46% 15.1M 17s 236650K .......... .......... .......... .......... .......... 46% 15.9M 17s 236700K .......... .......... .......... .......... .......... 46% 13.4M 17s 236750K .......... .......... .......... .......... .......... 46% 16.0M 17s 236800K .......... .......... .......... .......... .......... 46% 18.2M 17s 236850K .......... .......... .......... .......... .......... 46% 15.1M 17s 236900K .......... .......... .......... .......... .......... 46% 12.7M 17s 236950K .......... .......... .......... .......... .......... 46% 11.9M 17s 237000K .......... .......... .......... .......... .......... 46% 11.5M 17s 237050K .......... .......... .......... .......... .......... 46% 14.5M 17s 237100K .......... .......... .......... .......... .......... 46% 9.95M 17s 237150K .......... .......... .......... .......... .......... 46% 15.3M 17s 237200K .......... .......... .......... .......... .......... 46% 8.93M 17s 237250K .......... .......... .......... .......... .......... 46% 16.7M 17s 237300K .......... .......... .......... .......... .......... 46% 14.8M 17s 237350K .......... .......... .......... .......... .......... 46% 11.4M 17s 237400K .......... .......... .......... .......... .......... 46% 15.1M 17s 237450K .......... .......... .......... .......... .......... 46% 12.5M 17s 237500K .......... .......... .......... .......... .......... 46% 13.2M 17s 237550K .......... .......... .......... .......... .......... 46% 11.0M 17s 237600K .......... .......... .......... .......... .......... 46% 11.3M 17s 237650K .......... .......... .......... .......... .......... 46% 16.5M 17s 237700K .......... .......... .......... .......... .......... 46% 21.3M 17s 237750K .......... .......... .......... .......... .......... 46% 33.5M 17s 237800K .......... .......... .......... .......... .......... 46% 22.6M 17s 237850K .......... .......... .......... .......... .......... 46% 21.7M 17s 237900K .......... .......... .......... .......... .......... 46% 44.0M 17s 237950K .......... .......... .......... .......... .......... 46% 24.6M 17s 238000K .......... .......... .......... .......... .......... 46% 30.7M 17s 238050K .......... .......... .......... .......... .......... 46% 25.4M 17s 238100K .......... .......... .......... .......... .......... 46% 23.4M 17s 238150K .......... .......... .......... .......... .......... 46% 22.5M 17s 238200K .......... .......... .......... .......... .......... 46% 21.8M 17s 238250K .......... .......... .......... .......... .......... 46% 27.4M 17s 238300K .......... .......... .......... .......... .......... 46% 24.9M 17s 238350K .......... .......... .......... .......... .......... 46% 22.2M 17s 238400K .......... .......... .......... .......... .......... 46% 30.7M 17s 238450K .......... .......... .......... .......... .......... 46% 16.2M 17s 238500K .......... .......... .......... .......... .......... 46% 13.0M 17s 238550K .......... .......... .......... .......... .......... 46% 16.6M 17s 238600K .......... .......... .......... .......... .......... 46% 16.6M 17s 238650K .......... .......... .......... .......... .......... 46% 15.0M 17s 238700K .......... .......... .......... .......... .......... 46% 15.0M 17s 238750K .......... .......... .......... .......... .......... 46% 16.9M 17s 238800K .......... .......... .......... .......... .......... 46% 15.2M 17s 238850K .......... .......... .......... .......... .......... 46% 15.2M 17s 238900K .......... .......... .......... .......... .......... 46% 16.0M 17s 238950K .......... .......... .......... .......... .......... 46% 15.9M 17s 239000K .......... .......... .......... .......... .......... 46% 15.7M 17s 239050K .......... .......... .......... .......... .......... 46% 20.2M 17s 239100K .......... .......... .......... .......... .......... 46% 24.7M 17s 239150K .......... .......... .......... .......... .......... 46% 20.7M 17s 239200K .......... .......... .......... .......... .......... 46% 407M 17s 239250K .......... .......... .......... .......... .......... 46% 25.7M 17s 239300K .......... .......... .......... .......... .......... 46% 24.7M 17s 239350K .......... .......... .......... .......... .......... 46% 20.3M 17s 239400K .......... .......... .......... .......... .......... 46% 20.6M 17s 239450K .......... .......... .......... .......... .......... 46% 17.9M 17s 239500K .......... .......... .......... .......... .......... 46% 21.3M 17s 239550K .......... .......... .......... .......... .......... 46% 23.8M 17s 239600K .......... .......... .......... .......... .......... 47% 19.6M 17s 239650K .......... .......... .......... .......... .......... 47% 23.5M 17s 239700K .......... .......... .......... .......... .......... 47% 17.0M 17s 239750K .......... .......... .......... .......... .......... 47% 23.4M 17s 239800K .......... .......... .......... .......... .......... 47% 23.9M 17s 239850K .......... .......... .......... .......... .......... 47% 20.0M 17s 239900K .......... .......... .......... .......... .......... 47% 15.1M 17s 239950K .......... .......... .......... .......... .......... 47% 24.9M 17s 240000K .......... .......... .......... .......... .......... 47% 20.4M 17s 240050K .......... .......... .......... .......... .......... 47% 22.0M 17s 240100K .......... .......... .......... .......... .......... 47% 11.2M 17s 240150K .......... .......... .......... .......... .......... 47% 26.8M 17s 240200K .......... .......... .......... .......... .......... 47% 14.0M 17s 240250K .......... .......... .......... .......... .......... 47% 16.4M 17s 240300K .......... .......... .......... .......... .......... 47% 17.3M 17s 240350K .......... .......... .......... .......... .......... 47% 12.7M 17s 240400K .......... .......... .......... .......... .......... 47% 12.4M 17s 240450K .......... .......... .......... .......... .......... 47% 12.7M 17s 240500K .......... .......... .......... .......... .......... 47% 12.8M 17s 240550K .......... .......... .......... .......... .......... 47% 11.5M 17s 240600K .......... .......... .......... .......... .......... 47% 13.2M 17s 240650K .......... .......... .......... .......... .......... 47% 13.2M 17s 240700K .......... .......... .......... .......... .......... 47% 11.5M 17s 240750K .......... .......... .......... .......... .......... 47% 13.1M 17s 240800K .......... .......... .......... .......... .......... 47% 12.1M 17s 240850K .......... .......... .......... .......... .......... 47% 18.9M 17s 240900K .......... .......... .......... .......... .......... 47% 23.1M 17s 240950K .......... .......... .......... .......... .......... 47% 23.4M 17s 241000K .......... .......... .......... .......... .......... 47% 35.7M 17s 241050K .......... .......... .......... .......... .......... 47% 21.7M 17s 241100K .......... .......... .......... .......... .......... 47% 13.0M 17s 241150K .......... .......... .......... .......... .......... 47% 15.6M 17s 241200K .......... .......... .......... .......... .......... 47% 12.6M 17s 241250K .......... .......... .......... .......... .......... 47% 15.7M 17s 241300K .......... .......... .......... .......... .......... 47% 15.7M 17s 241350K .......... .......... .......... .......... .......... 47% 12.6M 17s 241400K .......... .......... .......... .......... .......... 47% 14.0M 17s 241450K .......... .......... .......... .......... .......... 47% 10.5M 17s 241500K .......... .......... .......... .......... .......... 47% 18.2M 17s 241550K .......... .......... .......... .......... .......... 47% 17.9M 17s 241600K .......... .......... .......... .......... .......... 47% 25.2M 17s 241650K .......... .......... .......... .......... .......... 47% 38.2M 17s 241700K .......... .......... .......... .......... .......... 47% 41.9M 17s 241750K .......... .......... .......... .......... .......... 47% 26.6M 17s 241800K .......... .......... .......... .......... .......... 47% 103M 17s 241850K .......... .......... .......... .......... .......... 47% 51.4M 17s 241900K .......... .......... .......... .......... .......... 47% 37.7M 17s 241950K .......... .......... .......... .......... .......... 47% 25.1M 17s 242000K .......... .......... .......... .......... .......... 47% 46.6M 17s 242050K .......... .......... .......... .......... .......... 47% 29.8M 17s 242100K .......... .......... .......... .......... .......... 47% 25.3M 17s 242150K .......... .......... .......... .......... .......... 47% 28.9M 17s 242200K .......... .......... .......... .......... .......... 47% 25.3M 17s 242250K .......... .......... .......... .......... .......... 47% 31.7M 17s 242300K .......... .......... .......... .......... .......... 47% 23.3M 17s 242350K .......... .......... .......... .......... .......... 47% 13.3M 17s 242400K .......... .......... .......... .......... .......... 47% 32.5M 17s 242450K .......... .......... .......... .......... .......... 47% 23.3M 17s 242500K .......... .......... .......... .......... .......... 47% 27.0M 17s 242550K .......... .......... .......... .......... .......... 47% 23.6M 17s 242600K .......... .......... .......... .......... .......... 47% 16.7M 17s 242650K .......... .......... .......... .......... .......... 47% 18.9M 17s 242700K .......... .......... .......... .......... .......... 47% 21.4M 17s 242750K .......... .......... .......... .......... .......... 47% 22.1M 17s 242800K .......... .......... .......... .......... .......... 47% 17.8M 17s 242850K .......... .......... .......... .......... .......... 47% 16.4M 17s 242900K .......... .......... .......... .......... .......... 47% 18.1M 17s 242950K .......... .......... .......... .......... .......... 47% 14.6M 17s 243000K .......... .......... .......... .......... .......... 47% 19.0M 17s 243050K .......... .......... .......... .......... .......... 47% 21.2M 17s 243100K .......... .......... .......... .......... .......... 47% 16.5M 17s 243150K .......... .......... .......... .......... .......... 47% 17.8M 17s 243200K .......... .......... .......... .......... .......... 47% 17.3M 17s 243250K .......... .......... .......... .......... .......... 47% 16.9M 17s 243300K .......... .......... .......... .......... .......... 47% 15.8M 17s 243350K .......... .......... .......... .......... .......... 47% 16.0M 17s 243400K .......... .......... .......... .......... .......... 47% 12.7M 17s 243450K .......... .......... .......... .......... .......... 47% 16.7M 17s 243500K .......... .......... .......... .......... .......... 47% 16.3M 17s 243550K .......... .......... .......... .......... .......... 47% 12.7M 17s 243600K .......... .......... .......... .......... .......... 47% 9.21M 17s 243650K .......... .......... .......... .......... .......... 47% 15.8M 17s 243700K .......... .......... .......... .......... .......... 47% 8.44M 17s 243750K .......... .......... .......... .......... .......... 47% 16.6M 17s 243800K .......... .......... .......... .......... .......... 47% 14.5M 17s 243850K .......... .......... .......... .......... .......... 47% 15.8M 17s 243900K .......... .......... .......... .......... .......... 47% 15.7M 17s 243950K .......... .......... .......... .......... .......... 47% 14.0M 17s 244000K .......... .......... .......... .......... .......... 47% 17.1M 17s 244050K .......... .......... .......... .......... .......... 47% 16.6M 17s 244100K .......... .......... .......... .......... .......... 47% 9.19M 17s 244150K .......... .......... .......... .......... .......... 47% 12.3M 17s 244200K .......... .......... .......... .......... .......... 47% 9.24M 17s 244250K .......... .......... .......... .......... .......... 47% 9.95M 17s 244300K .......... .......... .......... .......... .......... 47% 9.27M 17s 244350K .......... .......... .......... .......... .......... 47% 7.93M 17s 244400K .......... .......... .......... .......... .......... 47% 10.3M 17s 244450K .......... .......... .......... .......... .......... 47% 7.50M 17s 244500K .......... .......... .......... .......... .......... 47% 8.81M 17s 244550K .......... .......... .......... .......... .......... 47% 9.57M 17s 244600K .......... .......... .......... .......... .......... 47% 21.1M 17s 244650K .......... .......... .......... .......... .......... 47% 26.7M 17s 244700K .......... .......... .......... .......... .......... 48% 25.8M 17s 244750K .......... .......... .......... .......... .......... 48% 32.9M 17s 244800K .......... .......... .......... .......... .......... 48% 35.5M 17s 244850K .......... .......... .......... .......... .......... 48% 23.5M 17s 244900K .......... .......... .......... .......... .......... 48% 28.7M 17s 244950K .......... .......... .......... .......... .......... 48% 29.2M 17s 245000K .......... .......... .......... .......... .......... 48% 23.7M 17s 245050K .......... .......... .......... .......... .......... 48% 34.0M 17s 245100K .......... .......... .......... .......... .......... 48% 24.8M 17s 245150K .......... .......... .......... .......... .......... 48% 34.1M 17s 245200K .......... .......... .......... .......... .......... 48% 19.7M 17s 245250K .......... .......... .......... .......... .......... 48% 25.9M 17s 245300K .......... .......... .......... .......... .......... 48% 17.4M 17s 245350K .......... .......... .......... .......... .......... 48% 17.3M 17s 245400K .......... .......... .......... .......... .......... 48% 19.0M 17s 245450K .......... .......... .......... .......... .......... 48% 17.2M 17s 245500K .......... .......... .......... .......... .......... 48% 21.0M 17s 245550K .......... .......... .......... .......... .......... 48% 17.3M 17s 245600K .......... .......... .......... .......... .......... 48% 19.9M 17s 245650K .......... .......... .......... .......... .......... 48% 19.8M 17s 245700K .......... .......... .......... .......... .......... 48% 16.3M 17s 245750K .......... .......... .......... .......... .......... 48% 20.7M 17s 245800K .......... .......... .......... .......... .......... 48% 12.3M 17s 245850K .......... .......... .......... .......... .......... 48% 11.9M 17s 245900K .......... .......... .......... .......... .......... 48% 19.1M 17s 245950K .......... .......... .......... .......... .......... 48% 11.4M 17s 246000K .......... .......... .......... .......... .......... 48% 61.3M 17s 246050K .......... .......... .......... .......... .......... 48% 31.3M 17s 246100K .......... .......... .......... .......... .......... 48% 22.8M 17s 246150K .......... .......... .......... .......... .......... 48% 25.8M 17s 246200K .......... .......... .......... .......... .......... 48% 19.9M 17s 246250K .......... .......... .......... .......... .......... 48% 23.0M 17s 246300K .......... .......... .......... .......... .......... 48% 38.2M 17s 246350K .......... .......... .......... .......... .......... 48% 17.3M 17s 246400K .......... .......... .......... .......... .......... 48% 31.2M 17s 246450K .......... .......... .......... .......... .......... 48% 17.0M 17s 246500K .......... .......... .......... .......... .......... 48% 19.4M 17s 246550K .......... .......... .......... .......... .......... 48% 18.1M 17s 246600K .......... .......... .......... .......... .......... 48% 20.6M 17s 246650K .......... .......... .......... .......... .......... 48% 20.9M 17s 246700K .......... .......... .......... .......... .......... 48% 17.4M 17s 246750K .......... .......... .......... .......... .......... 48% 25.4M 17s 246800K .......... .......... .......... .......... .......... 48% 22.2M 17s 246850K .......... .......... .......... .......... .......... 48% 12.1M 17s 246900K .......... .......... .......... .......... .......... 48% 16.0M 17s 246950K .......... .......... .......... .......... .......... 48% 15.8M 17s 247000K .......... .......... .......... .......... .......... 48% 23.3M 17s 247050K .......... .......... .......... .......... .......... 48% 14.4M 17s 247100K .......... .......... .......... .......... .......... 48% 10.5M 17s 247150K .......... .......... .......... .......... .......... 48% 25.6M 17s 247200K .......... .......... .......... .......... .......... 48% 14.1M 17s 247250K .......... .......... .......... .......... .......... 48% 15.9M 17s 247300K .......... .......... .......... .......... .......... 48% 14.0M 17s 247350K .......... .......... .......... .......... .......... 48% 11.8M 17s 247400K .......... .......... .......... .......... .......... 48% 22.8M 17s 247450K .......... .......... .......... .......... .......... 48% 12.8M 16s 247500K .......... .......... .......... .......... .......... 48% 19.7M 16s 247550K .......... .......... .......... .......... .......... 48% 17.4M 16s 247600K .......... .......... .......... .......... .......... 48% 13.6M 16s 247650K .......... .......... .......... .......... .......... 48% 21.0M 16s 247700K .......... .......... .......... .......... .......... 48% 13.1M 16s 247750K .......... .......... .......... .......... .......... 48% 16.8M 16s 247800K .......... .......... .......... .......... .......... 48% 16.7M 16s 247850K .......... .......... .......... .......... .......... 48% 15.1M 16s 247900K .......... .......... .......... .......... .......... 48% 17.9M 16s 247950K .......... .......... .......... .......... .......... 48% 14.1M 16s 248000K .......... .......... .......... .......... .......... 48% 15.7M 16s 248050K .......... .......... .......... .......... .......... 48% 17.1M 16s 248100K .......... .......... .......... .......... .......... 48% 14.5M 16s 248150K .......... .......... .......... .......... .......... 48% 17.8M 16s 248200K .......... .......... .......... .......... .......... 48% 12.7M 16s 248250K .......... .......... .......... .......... .......... 48% 18.0M 16s 248300K .......... .......... .......... .......... .......... 48% 14.1M 16s 248350K .......... .......... .......... .......... .......... 48% 15.1M 16s 248400K .......... .......... .......... .......... .......... 48% 27.5M 16s 248450K .......... .......... .......... .......... .......... 48% 22.9M 16s 248500K .......... .......... .......... .......... .......... 48% 45.1M 16s 248550K .......... .......... .......... .......... .......... 48% 41.1M 16s 248600K .......... .......... .......... .......... .......... 48% 18.1M 16s 248650K .......... .......... .......... .......... .......... 48% 48.7M 16s 248700K .......... .......... .......... .......... .......... 48% 27.4M 16s 248750K .......... .......... .......... .......... .......... 48% 29.1M 16s 248800K .......... .......... .......... .......... .......... 48% 25.4M 16s 248850K .......... .......... .......... .......... .......... 48% 23.4M 16s 248900K .......... .......... .......... .......... .......... 48% 25.4M 16s 248950K .......... .......... .......... .......... .......... 48% 17.4M 16s 249000K .......... .......... .......... .......... .......... 48% 25.3M 16s 249050K .......... .......... .......... .......... .......... 48% 22.9M 16s 249100K .......... .......... .......... .......... .......... 48% 21.3M 16s 249150K .......... .......... .......... .......... .......... 48% 25.1M 16s 249200K .......... .......... .......... .......... .......... 48% 17.3M 16s 249250K .......... .......... .......... .......... .......... 48% 26.8M 16s 249300K .......... .......... .......... .......... .......... 48% 17.2M 16s 249350K .......... .......... .......... .......... .......... 48% 15.5M 16s 249400K .......... .......... .......... .......... .......... 48% 14.9M 16s 249450K .......... .......... .......... .......... .......... 48% 13.1M 16s 249500K .......... .......... .......... .......... .......... 48% 9.50M 16s 249550K .......... .......... .......... .......... .......... 48% 13.6M 16s 249600K .......... .......... .......... .......... .......... 48% 11.5M 16s 249650K .......... .......... .......... .......... .......... 48% 13.6M 16s 249700K .......... .......... .......... .......... .......... 48% 11.5M 16s 249750K .......... .......... .......... .......... .......... 48% 15.7M 16s 249800K .......... .......... .......... .......... .......... 49% 12.5M 16s 249850K .......... .......... .......... .......... .......... 49% 12.0M 16s 249900K .......... .......... .......... .......... .......... 49% 15.8M 16s 249950K .......... .......... .......... .......... .......... 49% 14.1M 16s 250000K .......... .......... .......... .......... .......... 49% 18.4M 16s 250050K .......... .......... .......... .......... .......... 49% 179M 16s 250100K .......... .......... .......... .......... .......... 49% 26.9M 16s 250150K .......... .......... .......... .......... .......... 49% 37.0M 16s 250200K .......... .......... .......... .......... .......... 49% 23.8M 16s 250250K .......... .......... .......... .......... .......... 49% 23.6M 16s 250300K .......... .......... .......... .......... .......... 49% 18.2M 16s 250350K .......... .......... .......... .......... .......... 49% 20.8M 16s 250400K .......... .......... .......... .......... .......... 49% 16.5M 16s 250450K .......... .......... .......... .......... .......... 49% 22.2M 16s 250500K .......... .......... .......... .......... .......... 49% 18.8M 16s 250550K .......... .......... .......... .......... .......... 49% 20.2M 16s 250600K .......... .......... .......... .......... .......... 49% 15.3M 16s 250650K .......... .......... .......... .......... .......... 49% 17.7M 16s 250700K .......... .......... .......... .......... .......... 49% 18.0M 16s 250750K .......... .......... .......... .......... .......... 49% 16.5M 16s 250800K .......... .......... .......... .......... .......... 49% 15.4M 16s 250850K .......... .......... .......... .......... .......... 49% 14.0M 16s 250900K .......... .......... .......... .......... .......... 49% 14.6M 16s 250950K .......... .......... .......... .......... .......... 49% 8.48M 16s 251000K .......... .......... .......... .......... .......... 49% 7.01M 16s 251050K .......... .......... .......... .......... .......... 49% 8.65M 16s 251100K .......... .......... .......... .......... .......... 49% 7.81M 16s 251150K .......... .......... .......... .......... .......... 49% 10.0M 16s 251200K .......... .......... .......... .......... .......... 49% 6.63M 16s 251250K .......... .......... .......... .......... .......... 49% 11.3M 16s 251300K .......... .......... .......... .......... .......... 49% 11.4M 16s 251350K .......... .......... .......... .......... .......... 49% 19.3M 16s 251400K .......... .......... .......... .......... .......... 49% 35.3M 16s 251450K .......... .......... .......... .......... .......... 49% 19.5M 16s 251500K .......... .......... .......... .......... .......... 49% 41.8M 16s 251550K .......... .......... .......... .......... .......... 49% 34.6M 16s 251600K .......... .......... .......... .......... .......... 49% 30.1M 16s 251650K .......... .......... .......... .......... .......... 49% 38.5M 16s 251700K .......... .......... .......... .......... .......... 49% 21.5M 16s 251750K .......... .......... .......... .......... .......... 49% 25.5M 16s 251800K .......... .......... .......... .......... .......... 49% 22.8M 16s 251850K .......... .......... .......... .......... .......... 49% 16.2M 16s 251900K .......... .......... .......... .......... .......... 49% 14.3M 16s 251950K .......... .......... .......... .......... .......... 49% 14.4M 16s 252000K .......... .......... .......... .......... .......... 49% 14.6M 16s 252050K .......... .......... .......... .......... .......... 49% 18.2M 16s 252100K .......... .......... .......... .......... .......... 49% 14.2M 16s 252150K .......... .......... .......... .......... .......... 49% 15.2M 16s 252200K .......... .......... .......... .......... .......... 49% 17.1M 16s 252250K .......... .......... .......... .......... .......... 49% 15.7M 16s 252300K .......... .......... .......... .......... .......... 49% 12.4M 16s 252350K .......... .......... .......... .......... .......... 49% 11.1M 16s 252400K .......... .......... .......... .......... .......... 49% 14.1M 16s 252450K .......... .......... .......... .......... .......... 49% 13.1M 16s 252500K .......... .......... .......... .......... .......... 49% 16.2M 16s 252550K .......... .......... .......... .......... .......... 49% 15.4M 16s 252600K .......... .......... .......... .......... .......... 49% 12.4M 16s 252650K .......... .......... .......... .......... .......... 49% 14.6M 16s 252700K .......... .......... .......... .......... .......... 49% 14.6M 16s 252750K .......... .......... .......... .......... .......... 49% 13.6M 16s 252800K .......... .......... .......... .......... .......... 49% 14.0M 16s 252850K .......... .......... .......... .......... .......... 49% 11.3M 16s 252900K .......... .......... .......... .......... .......... 49% 16.6M 16s 252950K .......... .......... .......... .......... .......... 49% 11.9M 16s 253000K .......... .......... .......... .......... .......... 49% 13.2M 16s 253050K .......... .......... .......... .......... .......... 49% 21.0M 16s 253100K .......... .......... .......... .......... .......... 49% 22.3M 16s 253150K .......... .......... .......... .......... .......... 49% 37.0M 16s 253200K .......... .......... .......... .......... .......... 49% 22.6M 16s 253250K .......... .......... .......... .......... .......... 49% 603M 16s 253300K .......... .......... .......... .......... .......... 49% 28.7M 16s 253350K .......... .......... .......... .......... .......... 49% 26.1M 16s 253400K .......... .......... .......... .......... .......... 49% 22.7M 16s 253450K .......... .......... .......... .......... .......... 49% 15.7M 16s 253500K .......... .......... .......... .......... .......... 49% 11.5M 16s 253550K .......... .......... .......... .......... .......... 49% 16.4M 16s 253600K .......... .......... .......... .......... .......... 49% 10.9M 16s 253650K .......... .......... .......... .......... .......... 49% 13.3M 16s 253700K .......... .......... .......... .......... .......... 49% 17.9M 16s 253750K .......... .......... .......... .......... .......... 49% 11.9M 16s 253800K .......... .......... .......... .......... .......... 49% 14.2M 16s 253850K .......... .......... .......... .......... .......... 49% 9.08M 16s 253900K .......... .......... .......... .......... .......... 49% 11.3M 16s 253950K .......... .......... .......... .......... .......... 49% 8.74M 16s 254000K .......... .......... .......... .......... .......... 49% 10.1M 16s 254050K .......... .......... .......... .......... .......... 49% 7.36M 16s 254100K .......... .......... .......... .......... .......... 49% 7.07M 16s 254150K .......... .......... .......... .......... .......... 49% 8.68M 16s 254200K .......... .......... .......... .......... .......... 49% 7.18M 16s 254250K .......... .......... .......... .......... .......... 49% 7.33M 16s 254300K .......... .......... .......... .......... .......... 49% 8.68M 16s 254350K .......... .......... .......... .......... .......... 49% 10.2M 16s 254400K .......... .......... .......... .......... .......... 49% 31.0M 16s 254450K .......... .......... .......... .......... .......... 49% 14.6M 16s 254500K .......... .......... .......... .......... .......... 49% 12.1M 16s 254550K .......... .......... .......... .......... .......... 49% 9.68M 16s 254600K .......... .......... .......... .......... .......... 49% 8.08M 16s 254650K .......... .......... .......... .......... .......... 49% 9.02M 16s 254700K .......... .......... .......... .......... .......... 49% 9.51M 16s 254750K .......... .......... .......... .......... .......... 49% 13.1M 16s 254800K .......... .......... .......... .......... .......... 49% 9.06M 16s 254850K .......... .......... .......... .......... .......... 50% 12.4M 16s 254900K .......... .......... .......... .......... .......... 50% 15.9M 16s 254950K .......... .......... .......... .......... .......... 50% 13.5M 16s 255000K .......... .......... .......... .......... .......... 50% 16.4M 16s 255050K .......... .......... .......... .......... .......... 50% 17.3M 16s 255100K .......... .......... .......... .......... .......... 50% 14.5M 16s 255150K .......... .......... .......... .......... .......... 50% 21.7M 16s 255200K .......... .......... .......... .......... .......... 50% 16.5M 16s 255250K .......... .......... .......... .......... .......... 50% 19.6M 16s 255300K .......... .......... .......... .......... .......... 50% 16.4M 16s 255350K .......... .......... .......... .......... .......... 50% 16.5M 16s 255400K .......... .......... .......... .......... .......... 50% 19.0M 16s 255450K .......... .......... .......... .......... .......... 50% 26.3M 16s 255500K .......... .......... .......... .......... .......... 50% 46.1M 16s 255550K .......... .......... .......... .......... .......... 50% 46.4M 16s 255600K .......... .......... .......... .......... .......... 50% 73.6M 16s 255650K .......... .......... .......... .......... .......... 50% 26.9M 16s 255700K .......... .......... .......... .......... .......... 50% 112M 16s 255750K .......... .......... .......... .......... .......... 50% 115M 16s 255800K .......... .......... .......... .......... .......... 50% 30.2M 16s 255850K .......... .......... .......... .......... .......... 50% 25.5M 16s 255900K .......... .......... .......... .......... .......... 50% 129M 16s 255950K .......... .......... .......... .......... .......... 50% 16.6M 16s 256000K .......... .......... .......... .......... .......... 50% 21.0M 16s 256050K .......... .......... .......... .......... .......... 50% 22.7M 16s 256100K .......... .......... .......... .......... .......... 50% 14.6M 16s 256150K .......... .......... .......... .......... .......... 50% 17.3M 16s 256200K .......... .......... .......... .......... .......... 50% 15.1M 16s 256250K .......... .......... .......... .......... .......... 50% 17.4M 16s 256300K .......... .......... .......... .......... .......... 50% 20.7M 16s 256350K .......... .......... .......... .......... .......... 50% 15.1M 16s 256400K .......... .......... .......... .......... .......... 50% 19.7M 16s 256450K .......... .......... .......... .......... .......... 50% 14.6M 16s 256500K .......... .......... .......... .......... .......... 50% 20.0M 16s 256550K .......... .......... .......... .......... .......... 50% 19.1M 16s 256600K .......... .......... .......... .......... .......... 50% 16.3M 16s 256650K .......... .......... .......... .......... .......... 50% 15.0M 16s 256700K .......... .......... .......... .......... .......... 50% 15.1M 16s 256750K .......... .......... .......... .......... .......... 50% 31.0M 16s 256800K .......... .......... .......... .......... .......... 50% 26.7M 16s 256850K .......... .......... .......... .......... .......... 50% 69.5M 16s 256900K .......... .......... .......... .......... .......... 50% 26.3M 16s 256950K .......... .......... .......... .......... .......... 50% 22.7M 16s 257000K .......... .......... .......... .......... .......... 50% 41.8M 16s 257050K .......... .......... .......... .......... .......... 50% 18.4M 16s 257100K .......... .......... .......... .......... .......... 50% 26.8M 16s 257150K .......... .......... .......... .......... .......... 50% 25.1M 16s 257200K .......... .......... .......... .......... .......... 50% 14.0M 16s 257250K .......... .......... .......... .......... .......... 50% 25.0M 16s 257300K .......... .......... .......... .......... .......... 50% 23.3M 16s 257350K .......... .......... .......... .......... .......... 50% 22.6M 16s 257400K .......... .......... .......... .......... .......... 50% 19.1M 16s 257450K .......... .......... .......... .......... .......... 50% 22.8M 16s 257500K .......... .......... .......... .......... .......... 50% 19.4M 16s 257550K .......... .......... .......... .......... .......... 50% 16.4M 16s 257600K .......... .......... .......... .......... .......... 50% 14.2M 16s 257650K .......... .......... .......... .......... .......... 50% 19.8M 16s 257700K .......... .......... .......... .......... .......... 50% 13.6M 16s 257750K .......... .......... .......... .......... .......... 50% 19.1M 16s 257800K .......... .......... .......... .......... .......... 50% 17.3M 16s 257850K .......... .......... .......... .......... .......... 50% 11.8M 16s 257900K .......... .......... .......... .......... .......... 50% 11.9M 16s 257950K .......... .......... .......... .......... .......... 50% 9.68M 16s 258000K .......... .......... .......... .......... .......... 50% 10.4M 16s 258050K .......... .......... .......... .......... .......... 50% 9.98M 16s 258100K .......... .......... .......... .......... .......... 50% 6.87M 16s 258150K .......... .......... .......... .......... .......... 50% 12.7M 16s 258200K .......... .......... .......... .......... .......... 50% 7.93M 16s 258250K .......... .......... .......... .......... .......... 50% 10.3M 16s 258300K .......... .......... .......... .......... .......... 50% 11.9M 16s 258350K .......... .......... .......... .......... .......... 50% 8.69M 16s 258400K .......... .......... .......... .......... .......... 50% 11.2M 16s 258450K .......... .......... .......... .......... .......... 50% 8.09M 16s 258500K .......... .......... .......... .......... .......... 50% 18.0M 16s 258550K .......... .......... .......... .......... .......... 50% 15.0M 16s 258600K .......... .......... .......... .......... .......... 50% 12.8M 16s 258650K .......... .......... .......... .......... .......... 50% 12.0M 16s 258700K .......... .......... .......... .......... .......... 50% 15.3M 16s 258750K .......... .......... .......... .......... .......... 50% 12.1M 16s 258800K .......... .......... .......... .......... .......... 50% 16.6M 16s 258850K .......... .......... .......... .......... .......... 50% 14.9M 16s 258900K .......... .......... .......... .......... .......... 50% 15.9M 16s 258950K .......... .......... .......... .......... .......... 50% 13.5M 16s 259000K .......... .......... .......... .......... .......... 50% 18.4M 16s 259050K .......... .......... .......... .......... .......... 50% 14.2M 16s 259100K .......... .......... .......... .......... .......... 50% 11.5M 16s 259150K .......... .......... .......... .......... .......... 50% 12.2M 16s 259200K .......... .......... .......... .......... .......... 50% 7.40M 16s 259250K .......... .......... .......... .......... .......... 50% 9.37M 16s 259300K .......... .......... .......... .......... .......... 50% 11.9M 16s 259350K .......... .......... .......... .......... .......... 50% 8.30M 16s 259400K .......... .......... .......... .......... .......... 50% 10.1M 16s 259450K .......... .......... .......... .......... .......... 50% 7.63M 16s 259500K .......... .......... .......... .......... .......... 50% 6.71M 16s 259550K .......... .......... .......... .......... .......... 50% 11.1M 16s 259600K .......... .......... .......... .......... .......... 50% 26.6M 16s 259650K .......... .......... .......... .......... .......... 50% 19.3M 16s 259700K .......... .......... .......... .......... .......... 50% 21.9M 16s 259750K .......... .......... .......... .......... .......... 50% 29.2M 16s 259800K .......... .......... .......... .......... .......... 50% 24.9M 16s 259850K .......... .......... .......... .......... .......... 50% 19.5M 16s 259900K .......... .......... .......... .......... .......... 50% 23.3M 16s 259950K .......... .......... .......... .......... .......... 51% 22.5M 16s 260000K .......... .......... .......... .......... .......... 51% 25.6M 16s 260050K .......... .......... .......... .......... .......... 51% 31.0M 16s 260100K .......... .......... .......... .......... .......... 51% 20.0M 16s 260150K .......... .......... .......... .......... .......... 51% 20.3M 16s 260200K .......... .......... .......... .......... .......... 51% 21.2M 16s 260250K .......... .......... .......... .......... .......... 51% 22.3M 16s 260300K .......... .......... .......... .......... .......... 51% 21.1M 16s 260350K .......... .......... .......... .......... .......... 51% 22.3M 16s 260400K .......... .......... .......... .......... .......... 51% 31.4M 16s 260450K .......... .......... .......... .......... .......... 51% 22.5M 16s 260500K .......... .......... .......... .......... .......... 51% 27.2M 16s 260550K .......... .......... .......... .......... .......... 51% 23.4M 16s 260600K .......... .......... .......... .......... .......... 51% 14.2M 16s 260650K .......... .......... .......... .......... .......... 51% 25.3M 16s 260700K .......... .......... .......... .......... .......... 51% 15.8M 16s 260750K .......... .......... .......... .......... .......... 51% 18.3M 16s 260800K .......... .......... .......... .......... .......... 51% 12.8M 16s 260850K .......... .......... .......... .......... .......... 51% 13.2M 16s 260900K .......... .......... .......... .......... .......... 51% 13.6M 16s 260950K .......... .......... .......... .......... .......... 51% 13.1M 16s 261000K .......... .......... .......... .......... .......... 51% 8.31M 16s 261050K .......... .......... .......... .......... .......... 51% 9.79M 16s 261100K .......... .......... .......... .......... .......... 51% 8.10M 16s 261150K .......... .......... .......... .......... .......... 51% 7.50M 16s 261200K .......... .......... .......... .......... .......... 51% 8.46M 16s 261250K .......... .......... .......... .......... .......... 51% 11.5M 16s 261300K .......... .......... .......... .......... .......... 51% 12.1M 16s 261350K .......... .......... .......... .......... .......... 51% 9.34M 16s 261400K .......... .......... .......... .......... .......... 51% 12.2M 16s 261450K .......... .......... .......... .......... .......... 51% 9.73M 16s 261500K .......... .......... .......... .......... .......... 51% 10.0M 16s 261550K .......... .......... .......... .......... .......... 51% 17.2M 16s 261600K .......... .......... .......... .......... .......... 51% 25.8M 16s 261650K .......... .......... .......... .......... .......... 51% 20.8M 16s 261700K .......... .......... .......... .......... .......... 51% 30.8M 16s 261750K .......... .......... .......... .......... .......... 51% 38.1M 16s 261800K .......... .......... .......... .......... .......... 51% 28.2M 16s 261850K .......... .......... .......... .......... .......... 51% 15.9M 16s 261900K .......... .......... .......... .......... .......... 51% 62.8M 16s 261950K .......... .......... .......... .......... .......... 51% 17.7M 16s 262000K .......... .......... .......... .......... .......... 51% 27.4M 16s 262050K .......... .......... .......... .......... .......... 51% 22.2M 16s 262100K .......... .......... .......... .......... .......... 51% 19.6M 16s 262150K .......... .......... .......... .......... .......... 51% 20.6M 16s 262200K .......... .......... .......... .......... .......... 51% 17.7M 16s 262250K .......... .......... .......... .......... .......... 51% 18.3M 16s 262300K .......... .......... .......... .......... .......... 51% 23.2M 16s 262350K .......... .......... .......... .......... .......... 51% 13.7M 16s 262400K .......... .......... .......... .......... .......... 51% 21.0M 16s 262450K .......... .......... .......... .......... .......... 51% 11.0M 16s 262500K .......... .......... .......... .......... .......... 51% 21.3M 16s 262550K .......... .......... .......... .......... .......... 51% 16.2M 16s 262600K .......... .......... .......... .......... .......... 51% 11.5M 16s 262650K .......... .......... .......... .......... .......... 51% 11.4M 16s 262700K .......... .......... .......... .......... .......... 51% 11.6M 16s 262750K .......... .......... .......... .......... .......... 51% 11.0M 16s 262800K .......... .......... .......... .......... .......... 51% 12.7M 16s 262850K .......... .......... .......... .......... .......... 51% 10.6M 16s 262900K .......... .......... .......... .......... .......... 51% 14.1M 16s 262950K .......... .......... .......... .......... .......... 51% 11.3M 16s 263000K .......... .......... .......... .......... .......... 51% 12.2M 16s 263050K .......... .......... .......... .......... .......... 51% 13.0M 16s 263100K .......... .......... .......... .......... .......... 51% 10.9M 16s 263150K .......... .......... .......... .......... .......... 51% 13.1M 16s 263200K .......... .......... .......... .......... .......... 51% 9.10M 16s 263250K .......... .......... .......... .......... .......... 51% 13.1M 16s 263300K .......... .......... .......... .......... .......... 51% 11.4M 16s 263350K .......... .......... .......... .......... .......... 51% 7.59M 16s 263400K .......... .......... .......... .......... .......... 51% 9.37M 16s 263450K .......... .......... .......... .......... .......... 51% 7.56M 16s 263500K .......... .......... .......... .......... .......... 51% 9.51M 16s 263550K .......... .......... .......... .......... .......... 51% 9.25M 16s 263600K .......... .......... .......... .......... .......... 51% 7.95M 16s 263650K .......... .......... .......... .......... .......... 51% 10.4M 16s 263700K .......... .......... .......... .......... .......... 51% 21.1M 16s 263750K .......... .......... .......... .......... .......... 51% 32.1M 16s 263800K .......... .......... .......... .......... .......... 51% 33.2M 16s 263850K .......... .......... .......... .......... .......... 51% 31.5M 15s 263900K .......... .......... .......... .......... .......... 51% 26.0M 15s 263950K .......... .......... .......... .......... .......... 51% 32.9M 15s 264000K .......... .......... .......... .......... .......... 51% 29.0M 15s 264050K .......... .......... .......... .......... .......... 51% 27.1M 15s 264100K .......... .......... .......... .......... .......... 51% 18.3M 15s 264150K .......... .......... .......... .......... .......... 51% 22.4M 15s 264200K .......... .......... .......... .......... .......... 51% 22.3M 15s 264250K .......... .......... .......... .......... .......... 51% 16.5M 15s 264300K .......... .......... .......... .......... .......... 51% 18.3M 15s 264350K .......... .......... .......... .......... .......... 51% 11.9M 15s 264400K .......... .......... .......... .......... .......... 51% 17.1M 15s 264450K .......... .......... .......... .......... .......... 51% 12.7M 15s 264500K .......... .......... .......... .......... .......... 51% 15.9M 15s 264550K .......... .......... .......... .......... .......... 51% 14.0M 15s 264600K .......... .......... .......... .......... .......... 51% 9.58M 15s 264650K .......... .......... .......... .......... .......... 51% 10.6M 15s 264700K .......... .......... .......... .......... .......... 51% 11.5M 15s 264750K .......... .......... .......... .......... .......... 51% 11.1M 15s 264800K .......... .......... .......... .......... .......... 51% 10.5M 15s 264850K .......... .......... .......... .......... .......... 51% 9.98M 15s 264900K .......... .......... .......... .......... .......... 51% 12.8M 15s 264950K .......... .......... .......... .......... .......... 51% 10.3M 15s 265000K .......... .......... .......... .......... .......... 51% 11.6M 15s 265050K .......... .......... .......... .......... .......... 52% 15.2M 15s 265100K .......... .......... .......... .......... .......... 52% 9.79M 15s 265150K .......... .......... .......... .......... .......... 52% 11.6M 15s 265200K .......... .......... .......... .......... .......... 52% 10.6M 15s 265250K .......... .......... .......... .......... .......... 52% 16.7M 15s 265300K .......... .......... .......... .......... .......... 52% 27.2M 15s 265350K .......... .......... .......... .......... .......... 52% 23.7M 15s 265400K .......... .......... .......... .......... .......... 52% 28.9M 15s 265450K .......... .......... .......... .......... .......... 52% 24.0M 15s 265500K .......... .......... .......... .......... .......... 52% 25.2M 15s 265550K .......... .......... .......... .......... .......... 52% 42.1M 15s 265600K .......... .......... .......... .......... .......... 52% 22.0M 15s 265650K .......... .......... .......... .......... .......... 52% 31.1M 15s 265700K .......... .......... .......... .......... .......... 52% 22.3M 15s 265750K .......... .......... .......... .......... .......... 52% 25.2M 15s 265800K .......... .......... .......... .......... .......... 52% 23.2M 15s 265850K .......... .......... .......... .......... .......... 52% 20.9M 15s 265900K .......... .......... .......... .......... .......... 52% 20.0M 15s 265950K .......... .......... .......... .......... .......... 52% 26.7M 15s 266000K .......... .......... .......... .......... .......... 52% 16.9M 15s 266050K .......... .......... .......... .......... .......... 52% 27.4M 15s 266100K .......... .......... .......... .......... .......... 52% 19.0M 15s 266150K .......... .......... .......... .......... .......... 52% 24.7M 15s 266200K .......... .......... .......... .......... .......... 52% 13.6M 15s 266250K .......... .......... .......... .......... .......... 52% 15.7M 15s 266300K .......... .......... .......... .......... .......... 52% 12.4M 15s 266350K .......... .......... .......... .......... .......... 52% 9.13M 15s 266400K .......... .......... .......... .......... .......... 52% 12.8M 15s 266450K .......... .......... .......... .......... .......... 52% 12.4M 15s 266500K .......... .......... .......... .......... .......... 52% 9.52M 15s 266550K .......... .......... .......... .......... .......... 52% 10.3M 15s 266600K .......... .......... .......... .......... .......... 52% 8.83M 15s 266650K .......... .......... .......... .......... .......... 52% 13.6M 15s 266700K .......... .......... .......... .......... .......... 52% 11.3M 15s 266750K .......... .......... .......... .......... .......... 52% 15.1M 15s 266800K .......... .......... .......... .......... .......... 52% 12.3M 15s 266850K .......... .......... .......... .......... .......... 52% 13.0M 15s 266900K .......... .......... .......... .......... .......... 52% 12.6M 15s 266950K .......... .......... .......... .......... .......... 52% 12.7M 15s 267000K .......... .......... .......... .......... .......... 52% 10.2M 15s 267050K .......... .......... .......... .......... .......... 52% 10.3M 15s 267100K .......... .......... .......... .......... .......... 52% 9.78M 15s 267150K .......... .......... .......... .......... .......... 52% 8.31M 15s 267200K .......... .......... .......... .......... .......... 52% 7.86M 15s 267250K .......... .......... .......... .......... .......... 52% 11.2M 15s 267300K .......... .......... .......... .......... .......... 52% 10.5M 15s 267350K .......... .......... .......... .......... .......... 52% 8.17M 15s 267400K .......... .......... .......... .......... .......... 52% 10.1M 15s 267450K .......... .......... .......... .......... .......... 52% 8.08M 15s 267500K .......... .......... .......... .......... .......... 52% 19.9M 15s 267550K .......... .......... .......... .......... .......... 52% 29.3M 15s 267600K .......... .......... .......... .......... .......... 52% 33.3M 15s 267650K .......... .......... .......... .......... .......... 52% 27.9M 15s 267700K .......... .......... .......... .......... .......... 52% 25.5M 15s 267750K .......... .......... .......... .......... .......... 52% 16.9M 15s 267800K .......... .......... .......... .......... .......... 52% 11.6M 15s 267850K .......... .......... .......... .......... .......... 52% 9.55M 15s 267900K .......... .......... .......... .......... .......... 52% 14.0M 15s 267950K .......... .......... .......... .......... .......... 52% 8.13M 15s 268000K .......... .......... .......... .......... .......... 52% 15.2M 15s 268050K .......... .......... .......... .......... .......... 52% 13.6M 15s 268100K .......... .......... .......... .......... .......... 52% 13.4M 15s 268150K .......... .......... .......... .......... .......... 52% 14.5M 15s 268200K .......... .......... .......... .......... .......... 52% 10.9M 15s 268250K .......... .......... .......... .......... .......... 52% 12.4M 15s 268300K .......... .......... .......... .......... .......... 52% 16.3M 15s 268350K .......... .......... .......... .......... .......... 52% 11.5M 15s 268400K .......... .......... .......... .......... .......... 52% 13.5M 15s 268450K .......... .......... .......... .......... .......... 52% 15.1M 15s 268500K .......... .......... .......... .......... .......... 52% 37.9M 15s 268550K .......... .......... .......... .......... .......... 52% 72.8M 15s 268600K .......... .......... .......... .......... .......... 52% 14.9M 15s 268650K .......... .......... .......... .......... .......... 52% 58.8M 15s 268700K .......... .......... .......... .......... .......... 52% 29.3M 15s 268750K .......... .......... .......... .......... .......... 52% 31.7M 15s 268800K .......... .......... .......... .......... .......... 52% 18.9M 15s 268850K .......... .......... .......... .......... .......... 52% 34.8M 15s 268900K .......... .......... .......... .......... .......... 52% 42.3M 15s 268950K .......... .......... .......... .......... .......... 52% 23.3M 15s 269000K .......... .......... .......... .......... .......... 52% 29.0M 15s 269050K .......... .......... .......... .......... .......... 52% 23.2M 15s 269100K .......... .......... .......... .......... .......... 52% 23.0M 15s 269150K .......... .......... .......... .......... .......... 52% 25.9M 15s 269200K .......... .......... .......... .......... .......... 52% 19.8M 15s 269250K .......... .......... .......... .......... .......... 52% 20.6M 15s 269300K .......... .......... .......... .......... .......... 52% 14.7M 15s 269350K .......... .......... .......... .......... .......... 52% 11.7M 15s 269400K .......... .......... .......... .......... .......... 52% 17.3M 15s 269450K .......... .......... .......... .......... .......... 52% 15.1M 15s 269500K .......... .......... .......... .......... .......... 52% 10.6M 15s 269550K .......... .......... .......... .......... .......... 52% 14.1M 15s 269600K .......... .......... .......... .......... .......... 52% 9.79M 15s 269650K .......... .......... .......... .......... .......... 52% 9.49M 15s 269700K .......... .......... .......... .......... .......... 52% 13.3M 15s 269750K .......... .......... .......... .......... .......... 52% 11.7M 15s 269800K .......... .......... .......... .......... .......... 52% 12.7M 15s 269850K .......... .......... .......... .......... .......... 52% 10.9M 15s 269900K .......... .......... .......... .......... .......... 52% 15.1M 15s 269950K .......... .......... .......... .......... .......... 52% 10.5M 15s 270000K .......... .......... .......... .......... .......... 52% 14.7M 15s 270050K .......... .......... .......... .......... .......... 52% 12.3M 15s 270100K .......... .......... .......... .......... .......... 52% 10.2M 15s 270150K .......... .......... .......... .......... .......... 53% 24.6M 15s 270200K .......... .......... .......... .......... .......... 53% 30.9M 15s 270250K .......... .......... .......... .......... .......... 53% 19.6M 15s 270300K .......... .......... .......... .......... .......... 53% 37.5M 15s 270350K .......... .......... .......... .......... .......... 53% 54.5M 15s 270400K .......... .......... .......... .......... .......... 53% 22.8M 15s 270450K .......... .......... .......... .......... .......... 53% 15.2M 15s 270500K .......... .......... .......... .......... .......... 53% 17.7M 15s 270550K .......... .......... .......... .......... .......... 53% 24.6M 15s 270600K .......... .......... .......... .......... .......... 53% 16.5M 15s 270650K .......... .......... .......... .......... .......... 53% 15.9M 15s 270700K .......... .......... .......... .......... .......... 53% 15.6M 15s 270750K .......... .......... .......... .......... .......... 53% 23.3M 15s 270800K .......... .......... .......... .......... .......... 53% 17.5M 15s 270850K .......... .......... .......... .......... .......... 53% 16.9M 15s 270900K .......... .......... .......... .......... .......... 53% 25.2M 15s 270950K .......... .......... .......... .......... .......... 53% 13.1M 15s 271000K .......... .......... .......... .......... .......... 53% 18.1M 15s 271050K .......... .......... .......... .......... .......... 53% 18.5M 15s 271100K .......... .......... .......... .......... .......... 53% 14.6M 15s 271150K .......... .......... .......... .......... .......... 53% 9.19M 15s 271200K .......... .......... .......... .......... .......... 53% 8.85M 15s 271250K .......... .......... .......... .......... .......... 53% 15.9M 15s 271300K .......... .......... .......... .......... .......... 53% 15.5M 15s 271350K .......... .......... .......... .......... .......... 53% 11.3M 15s 271400K .......... .......... .......... .......... .......... 53% 15.2M 15s 271450K .......... .......... .......... .......... .......... 53% 13.5M 15s 271500K .......... .......... .......... .......... .......... 53% 13.1M 15s 271550K .......... .......... .......... .......... .......... 53% 18.2M 15s 271600K .......... .......... .......... .......... .......... 53% 14.6M 15s 271650K .......... .......... .......... .......... .......... 53% 18.0M 15s 271700K .......... .......... .......... .......... .......... 53% 21.8M 15s 271750K .......... .......... .......... .......... .......... 53% 23.4M 15s 271800K .......... .......... .......... .......... .......... 53% 241M 15s 271850K .......... .......... .......... .......... .......... 53% 86.4M 15s 271900K .......... .......... .......... .......... .......... 53% 42.1M 15s 271950K .......... .......... .......... .......... .......... 53% 46.5M 15s 272000K .......... .......... .......... .......... .......... 53% 50.7M 15s 272050K .......... .......... .......... .......... .......... 53% 42.1M 15s 272100K .......... .......... .......... .......... .......... 53% 31.7M 15s 272150K .......... .......... .......... .......... .......... 53% 47.5M 15s 272200K .......... .......... .......... .......... .......... 53% 37.3M 15s 272250K .......... .......... .......... .......... .......... 53% 27.2M 15s 272300K .......... .......... .......... .......... .......... 53% 44.1M 15s 272350K .......... .......... .......... .......... .......... 53% 21.0M 15s 272400K .......... .......... .......... .......... .......... 53% 28.8M 15s 272450K .......... .......... .......... .......... .......... 53% 31.7M 15s 272500K .......... .......... .......... .......... .......... 53% 28.4M 15s 272550K .......... .......... .......... .......... .......... 53% 41.8M 15s 272600K .......... .......... .......... .......... .......... 53% 23.7M 15s 272650K .......... .......... .......... .......... .......... 53% 28.3M 15s 272700K .......... .......... .......... .......... .......... 53% 27.1M 15s 272750K .......... .......... .......... .......... .......... 53% 31.3M 15s 272800K .......... .......... .......... .......... .......... 53% 27.0M 15s 272850K .......... .......... .......... .......... .......... 53% 23.8M 15s 272900K .......... .......... .......... .......... .......... 53% 21.9M 15s 272950K .......... .......... .......... .......... .......... 53% 19.8M 15s 273000K .......... .......... .......... .......... .......... 53% 17.9M 15s 273050K .......... .......... .......... .......... .......... 53% 25.7M 15s 273100K .......... .......... .......... .......... .......... 53% 13.5M 15s 273150K .......... .......... .......... .......... .......... 53% 30.5M 15s 273200K .......... .......... .......... .......... .......... 53% 23.3M 15s 273250K .......... .......... .......... .......... .......... 53% 35.6M 15s 273300K .......... .......... .......... .......... .......... 53% 21.4M 15s 273350K .......... .......... .......... .......... .......... 53% 44.6M 15s 273400K .......... .......... .......... .......... .......... 53% 132M 15s 273450K .......... .......... .......... .......... .......... 53% 29.1M 15s 273500K .......... .......... .......... .......... .......... 53% 28.8M 15s 273550K .......... .......... .......... .......... .......... 53% 25.0M 15s 273600K .......... .......... .......... .......... .......... 53% 21.0M 15s 273650K .......... .......... .......... .......... .......... 53% 21.7M 15s 273700K .......... .......... .......... .......... .......... 53% 14.7M 15s 273750K .......... .......... .......... .......... .......... 53% 16.1M 15s 273800K .......... .......... .......... .......... .......... 53% 13.8M 15s 273850K .......... .......... .......... .......... .......... 53% 10.8M 15s 273900K .......... .......... .......... .......... .......... 53% 17.0M 15s 273950K .......... .......... .......... .......... .......... 53% 13.2M 15s 274000K .......... .......... .......... .......... .......... 53% 15.5M 15s 274050K .......... .......... .......... .......... .......... 53% 16.4M 15s 274100K .......... .......... .......... .......... .......... 53% 12.8M 15s 274150K .......... .......... .......... .......... .......... 53% 13.5M 15s 274200K .......... .......... .......... .......... .......... 53% 13.2M 15s 274250K .......... .......... .......... .......... .......... 53% 18.0M 15s 274300K .......... .......... .......... .......... .......... 53% 14.7M 15s 274350K .......... .......... .......... .......... .......... 53% 18.8M 15s 274400K .......... .......... .......... .......... .......... 53% 36.4M 15s 274450K .......... .......... .......... .......... .......... 53% 26.1M 15s 274500K .......... .......... .......... .......... .......... 53% 32.5M 15s 274550K .......... .......... .......... .......... .......... 53% 79.5M 15s 274600K .......... .......... .......... .......... .......... 53% 19.5M 15s 274650K .......... .......... .......... .......... .......... 53% 20.4M 15s 274700K .......... .......... .......... .......... .......... 53% 13.2M 15s 274750K .......... .......... .......... .......... .......... 53% 16.0M 15s 274800K .......... .......... .......... .......... .......... 53% 11.3M 15s 274850K .......... .......... .......... .......... .......... 53% 11.6M 15s 274900K .......... .......... .......... .......... .......... 53% 15.2M 15s 274950K .......... .......... .......... .......... .......... 53% 11.1M 15s 275000K .......... .......... .......... .......... .......... 53% 17.2M 15s 275050K .......... .......... .......... .......... .......... 53% 18.1M 15s 275100K .......... .......... .......... .......... .......... 53% 12.9M 15s 275150K .......... .......... .......... .......... .......... 53% 16.6M 15s 275200K .......... .......... .......... .......... .......... 53% 17.7M 15s 275250K .......... .......... .......... .......... .......... 54% 21.8M 15s 275300K .......... .......... .......... .......... .......... 54% 22.3M 15s 275350K .......... .......... .......... .......... .......... 54% 17.1M 15s 275400K .......... .......... .......... .......... .......... 54% 17.8M 15s 275450K .......... .......... .......... .......... .......... 54% 17.1M 15s 275500K .......... .......... .......... .......... .......... 54% 25.0M 15s 275550K .......... .......... .......... .......... .......... 54% 24.8M 15s 275600K .......... .......... .......... .......... .......... 54% 14.1M 15s 275650K .......... .......... .......... .......... .......... 54% 20.2M 15s 275700K .......... .......... .......... .......... .......... 54% 19.8M 15s 275750K .......... .......... .......... .......... .......... 54% 14.8M 15s 275800K .......... .......... .......... .......... .......... 54% 21.1M 15s 275850K .......... .......... .......... .......... .......... 54% 14.2M 15s 275900K .......... .......... .......... .......... .......... 54% 12.1M 15s 275950K .......... .......... .......... .......... .......... 54% 10.7M 15s 276000K .......... .......... .......... .......... .......... 54% 15.2M 15s 276050K .......... .......... .......... .......... .......... 54% 16.0M 15s 276100K .......... .......... .......... .......... .......... 54% 11.5M 15s 276150K .......... .......... .......... .......... .......... 54% 15.8M 15s 276200K .......... .......... .......... .......... .......... 54% 14.2M 15s 276250K .......... .......... .......... .......... .......... 54% 16.0M 15s 276300K .......... .......... .......... .......... .......... 54% 15.3M 15s 276350K .......... .......... .......... .......... .......... 54% 11.9M 15s 276400K .......... .......... .......... .......... .......... 54% 12.1M 15s 276450K .......... .......... .......... .......... .......... 54% 18.0M 15s 276500K .......... .......... .......... .......... .......... 54% 15.6M 15s 276550K .......... .......... .......... .......... .......... 54% 15.3M 15s 276600K .......... .......... .......... .......... .......... 54% 15.8M 15s 276650K .......... .......... .......... .......... .......... 54% 17.8M 15s 276700K .......... .......... .......... .......... .......... 54% 13.8M 15s 276750K .......... .......... .......... .......... .......... 54% 15.9M 15s 276800K .......... .......... .......... .......... .......... 54% 17.3M 15s 276850K .......... .......... .......... .......... .......... 54% 14.4M 15s 276900K .......... .......... .......... .......... .......... 54% 12.7M 15s 276950K .......... .......... .......... .......... .......... 54% 14.9M 15s 277000K .......... .......... .......... .......... .......... 54% 15.7M 15s 277050K .......... .......... .......... .......... .......... 54% 9.28M 15s 277100K .......... .......... .......... .......... .......... 54% 9.79M 15s 277150K .......... .......... .......... .......... .......... 54% 14.1M 15s 277200K .......... .......... .......... .......... .......... 54% 8.68M 15s 277250K .......... .......... .......... .......... .......... 54% 12.2M 15s 277300K .......... .......... .......... .......... .......... 54% 12.8M 15s 277350K .......... .......... .......... .......... .......... 54% 12.6M 15s 277400K .......... .......... .......... .......... .......... 54% 13.8M 15s 277450K .......... .......... .......... .......... .......... 54% 14.1M 15s 277500K .......... .......... .......... .......... .......... 54% 11.7M 15s 277550K .......... .......... .......... .......... .......... 54% 16.6M 15s 277600K .......... .......... .......... .......... .......... 54% 11.2M 15s 277650K .......... .......... .......... .......... .......... 54% 14.7M 15s 277700K .......... .......... .......... .......... .......... 54% 10.8M 15s 277750K .......... .......... .......... .......... .......... 54% 17.9M 15s 277800K .......... .......... .......... .......... .......... 54% 15.0M 15s 277850K .......... .......... .......... .......... .......... 54% 12.6M 15s 277900K .......... .......... .......... .......... .......... 54% 14.1M 15s 277950K .......... .......... .......... .......... .......... 54% 10.6M 15s 278000K .......... .......... .......... .......... .......... 54% 27.2M 15s 278050K .......... .......... .......... .......... .......... 54% 24.9M 15s 278100K .......... .......... .......... .......... .......... 54% 11.9M 15s 278150K .......... .......... .......... .......... .......... 54% 42.9M 15s 278200K .......... .......... .......... .......... .......... 54% 18.0M 15s 278250K .......... .......... .......... .......... .......... 54% 19.8M 15s 278300K .......... .......... .......... .......... .......... 54% 27.2M 15s 278350K .......... .......... .......... .......... .......... 54% 12.7M 15s 278400K .......... .......... .......... .......... .......... 54% 91.4M 15s 278450K .......... .......... .......... .......... .......... 54% 18.7M 15s 278500K .......... .......... .......... .......... .......... 54% 16.5M 15s 278550K .......... .......... .......... .......... .......... 54% 16.6M 15s 278600K .......... .......... .......... .......... .......... 54% 15.9M 15s 278650K .......... .......... .......... .......... .......... 54% 12.0M 15s 278700K .......... .......... .......... .......... .......... 54% 12.1M 15s 278750K .......... .......... .......... .......... .......... 54% 11.2M 15s 278800K .......... .......... .......... .......... .......... 54% 12.6M 15s 278850K .......... .......... .......... .......... .......... 54% 11.4M 15s 278900K .......... .......... .......... .......... .......... 54% 9.51M 15s 278950K .......... .......... .......... .......... .......... 54% 11.5M 15s 279000K .......... .......... .......... .......... .......... 54% 8.15M 15s 279050K .......... .......... .......... .......... .......... 54% 9.51M 15s 279100K .......... .......... .......... .......... .......... 54% 8.47M 15s 279150K .......... .......... .......... .......... .......... 54% 9.54M 15s 279200K .......... .......... .......... .......... .......... 54% 8.04M 15s 279250K .......... .......... .......... .......... .......... 54% 15.0M 15s 279300K .......... .......... .......... .......... .......... 54% 25.4M 15s 279350K .......... .......... .......... .......... .......... 54% 19.7M 15s 279400K .......... .......... .......... .......... .......... 54% 30.1M 14s 279450K .......... .......... .......... .......... .......... 54% 16.7M 14s 279500K .......... .......... .......... .......... .......... 54% 19.2M 14s 279550K .......... .......... .......... .......... .......... 54% 12.6M 14s 279600K .......... .......... .......... .......... .......... 54% 11.1M 14s 279650K .......... .......... .......... .......... .......... 54% 14.4M 14s 279700K .......... .......... .......... .......... .......... 54% 12.0M 14s 279750K .......... .......... .......... .......... .......... 54% 12.1M 14s 279800K .......... .......... .......... .......... .......... 54% 9.66M 14s 279850K .......... .......... .......... .......... .......... 54% 10.0M 14s 279900K .......... .......... .......... .......... .......... 54% 7.07M 14s 279950K .......... .......... .......... .......... .......... 54% 13.6M 14s 280000K .......... .......... .......... .......... .......... 54% 16.4M 14s 280050K .......... .......... .......... .......... .......... 54% 15.1M 14s 280100K .......... .......... .......... .......... .......... 54% 11.5M 14s 280150K .......... .......... .......... .......... .......... 54% 10.8M 14s 280200K .......... .......... .......... .......... .......... 54% 9.19M 14s 280250K .......... .......... .......... .......... .......... 54% 10.3M 14s 280300K .......... .......... .......... .......... .......... 54% 10.6M 14s 280350K .......... .......... .......... .......... .......... 55% 15.9M 14s 280400K .......... .......... .......... .......... .......... 55% 30.4M 14s 280450K .......... .......... .......... .......... .......... 55% 24.0M 14s 280500K .......... .......... .......... .......... .......... 55% 19.5M 14s 280550K .......... .......... .......... .......... .......... 55% 58.5M 14s 280600K .......... .......... .......... .......... .......... 55% 26.3M 14s 280650K .......... .......... .......... .......... .......... 55% 31.5M 14s 280700K .......... .......... .......... .......... .......... 55% 25.5M 14s 280750K .......... .......... .......... .......... .......... 55% 30.4M 14s 280800K .......... .......... .......... .......... .......... 55% 46.5M 14s 280850K .......... .......... .......... .......... .......... 55% 33.5M 14s 280900K .......... .......... .......... .......... .......... 55% 25.3M 14s 280950K .......... .......... .......... .......... .......... 55% 37.9M 14s 281000K .......... .......... .......... .......... .......... 55% 28.5M 14s 281050K .......... .......... .......... .......... .......... 55% 23.5M 14s 281100K .......... .......... .......... .......... .......... 55% 28.4M 14s 281150K .......... .......... .......... .......... .......... 55% 21.2M 14s 281200K .......... .......... .......... .......... .......... 55% 20.9M 14s 281250K .......... .......... .......... .......... .......... 55% 31.1M 14s 281300K .......... .......... .......... .......... .......... 55% 26.9M 14s 281350K .......... .......... .......... .......... .......... 55% 12.6M 14s 281400K .......... .......... .......... .......... .......... 55% 34.4M 14s 281450K .......... .......... .......... .......... .......... 55% 13.0M 14s 281500K .......... .......... .......... .......... .......... 55% 13.1M 14s 281550K .......... .......... .......... .......... .......... 55% 14.7M 14s 281600K .......... .......... .......... .......... .......... 55% 12.6M 14s 281650K .......... .......... .......... .......... .......... 55% 14.6M 14s 281700K .......... .......... .......... .......... .......... 55% 13.9M 14s 281750K .......... .......... .......... .......... .......... 55% 15.1M 14s 281800K .......... .......... .......... .......... .......... 55% 11.8M 14s 281850K .......... .......... .......... .......... .......... 55% 9.68M 14s 281900K .......... .......... .......... .......... .......... 55% 13.9M 14s 281950K .......... .......... .......... .......... .......... 55% 9.87M 14s 282000K .......... .......... .......... .......... .......... 55% 13.0M 14s 282050K .......... .......... .......... .......... .......... 55% 13.1M 14s 282100K .......... .......... .......... .......... .......... 55% 11.1M 14s 282150K .......... .......... .......... .......... .......... 55% 11.2M 14s 282200K .......... .......... .......... .......... .......... 55% 9.96M 14s 282250K .......... .......... .......... .......... .......... 55% 11.8M 14s 282300K .......... .......... .......... .......... .......... 55% 11.4M 14s 282350K .......... .......... .......... .......... .......... 55% 10.3M 14s 282400K .......... .......... .......... .......... .......... 55% 9.06M 14s 282450K .......... .......... .......... .......... .......... 55% 6.45M 14s 282500K .......... .......... .......... .......... .......... 55% 6.93M 14s 282550K .......... .......... .......... .......... .......... 55% 9.77M 14s 282600K .......... .......... .......... .......... .......... 55% 5.73M 14s 282650K .......... .......... .......... .......... .......... 55% 10.4M 14s 282700K .......... .......... .......... .......... .......... 55% 15.2M 14s 282750K .......... .......... .......... .......... .......... 55% 29.0M 14s 282800K .......... .......... .......... .......... .......... 55% 23.2M 14s 282850K .......... .......... .......... .......... .......... 55% 28.9M 14s 282900K .......... .......... .......... .......... .......... 55% 23.8M 14s 282950K .......... .......... .......... .......... .......... 55% 20.8M 14s 283000K .......... .......... .......... .......... .......... 55% 34.8M 14s 283050K .......... .......... .......... .......... .......... 55% 25.5M 14s 283100K .......... .......... .......... .......... .......... 55% 15.2M 14s 283150K .......... .......... .......... .......... .......... 55% 23.4M 14s 283200K .......... .......... .......... .......... .......... 55% 20.0M 14s 283250K .......... .......... .......... .......... .......... 55% 23.5M 14s 283300K .......... .......... .......... .......... .......... 55% 19.3M 14s 283350K .......... .......... .......... .......... .......... 55% 19.7M 14s 283400K .......... .......... .......... .......... .......... 55% 18.6M 14s 283450K .......... .......... .......... .......... .......... 55% 15.1M 14s 283500K .......... .......... .......... .......... .......... 55% 17.9M 14s 283550K .......... .......... .......... .......... .......... 55% 16.6M 14s 283600K .......... .......... .......... .......... .......... 55% 13.5M 14s 283650K .......... .......... .......... .......... .......... 55% 20.2M 14s 283700K .......... .......... .......... .......... .......... 55% 14.0M 14s 283750K .......... .......... .......... .......... .......... 55% 17.5M 14s 283800K .......... .......... .......... .......... .......... 55% 17.9M 14s 283850K .......... .......... .......... .......... .......... 55% 14.7M 14s 283900K .......... .......... .......... .......... .......... 55% 18.9M 14s 283950K .......... .......... .......... .......... .......... 55% 15.3M 14s 284000K .......... .......... .......... .......... .......... 55% 11.5M 14s 284050K .......... .......... .......... .......... .......... 55% 23.6M 14s 284100K .......... .......... .......... .......... .......... 55% 19.8M 14s 284150K .......... .......... .......... .......... .......... 55% 16.5M 14s 284200K .......... .......... .......... .......... .......... 55% 16.4M 14s 284250K .......... .......... .......... .......... .......... 55% 28.9M 14s 284300K .......... .......... .......... .......... .......... 55% 13.9M 14s 284350K .......... .......... .......... .......... .......... 55% 16.4M 14s 284400K .......... .......... .......... .......... .......... 55% 14.8M 14s 284450K .......... .......... .......... .......... .......... 55% 15.1M 14s 284500K .......... .......... .......... .......... .......... 55% 12.5M 14s 284550K .......... .......... .......... .......... .......... 55% 14.6M 14s 284600K .......... .......... .......... .......... .......... 55% 6.81M 14s 284650K .......... .......... .......... .......... .......... 55% 9.52M 14s 284700K .......... .......... .......... .......... .......... 55% 8.33M 14s 284750K .......... .......... .......... .......... .......... 55% 10.1M 14s 284800K .......... .......... .......... .......... .......... 55% 11.1M 14s 284850K .......... .......... .......... .......... .......... 55% 8.46M 14s 284900K .......... .......... .......... .......... .......... 55% 12.2M 14s 284950K .......... .......... .......... .......... .......... 55% 9.23M 14s 285000K .......... .......... .......... .......... .......... 55% 26.4M 14s 285050K .......... .......... .......... .......... .......... 55% 25.4M 14s 285100K .......... .......... .......... .......... .......... 55% 30.8M 14s 285150K .......... .......... .......... .......... .......... 55% 26.5M 14s 285200K .......... .......... .......... .......... .......... 55% 34.7M 14s 285250K .......... .......... .......... .......... .......... 55% 36.1M 14s 285300K .......... .......... .......... .......... .......... 55% 34.3M 14s 285350K .......... .......... .......... .......... .......... 55% 28.7M 14s 285400K .......... .......... .......... .......... .......... 55% 34.0M 14s 285450K .......... .......... .......... .......... .......... 56% 28.5M 14s 285500K .......... .......... .......... .......... .......... 56% 31.0M 14s 285550K .......... .......... .......... .......... .......... 56% 26.5M 14s 285600K .......... .......... .......... .......... .......... 56% 24.4M 14s 285650K .......... .......... .......... .......... .......... 56% 32.4M 14s 285700K .......... .......... .......... .......... .......... 56% 21.9M 14s 285750K .......... .......... .......... .......... .......... 56% 31.4M 14s 285800K .......... .......... .......... .......... .......... 56% 31.4M 14s 285850K .......... .......... .......... .......... .......... 56% 20.7M 14s 285900K .......... .......... .......... .......... .......... 56% 22.3M 14s 285950K .......... .......... .......... .......... .......... 56% 20.4M 14s 286000K .......... .......... .......... .......... .......... 56% 20.6M 14s 286050K .......... .......... .......... .......... .......... 56% 22.6M 14s 286100K .......... .......... .......... .......... .......... 56% 15.6M 14s 286150K .......... .......... .......... .......... .......... 56% 23.0M 14s 286200K .......... .......... .......... .......... .......... 56% 19.1M 14s 286250K .......... .......... .......... .......... .......... 56% 18.6M 14s 286300K .......... .......... .......... .......... .......... 56% 20.5M 14s 286350K .......... .......... .......... .......... .......... 56% 16.1M 14s 286400K .......... .......... .......... .......... .......... 56% 22.0M 14s 286450K .......... .......... .......... .......... .......... 56% 17.8M 14s 286500K .......... .......... .......... .......... .......... 56% 16.6M 14s 286550K .......... .......... .......... .......... .......... 56% 15.1M 14s 286600K .......... .......... .......... .......... .......... 56% 14.5M 14s 286650K .......... .......... .......... .......... .......... 56% 18.9M 14s 286700K .......... .......... .......... .......... .......... 56% 11.1M 14s 286750K .......... .......... .......... .......... .......... 56% 15.1M 14s 286800K .......... .......... .......... .......... .......... 56% 10.0M 14s 286850K .......... .......... .......... .......... .......... 56% 9.40M 14s 286900K .......... .......... .......... .......... .......... 56% 12.2M 14s 286950K .......... .......... .......... .......... .......... 56% 19.6M 14s 287000K .......... .......... .......... .......... .......... 56% 49.5M 14s 287050K .......... .......... .......... .......... .......... 56% 38.0M 14s 287100K .......... .......... .......... .......... .......... 56% 33.6M 14s 287150K .......... .......... .......... .......... .......... 56% 38.4M 14s 287200K .......... .......... .......... .......... .......... 56% 25.4M 14s 287250K .......... .......... .......... .......... .......... 56% 22.5M 14s 287300K .......... .......... .......... .......... .......... 56% 38.6M 14s 287350K .......... .......... .......... .......... .......... 56% 22.2M 14s 287400K .......... .......... .......... .......... .......... 56% 24.2M 14s 287450K .......... .......... .......... .......... .......... 56% 10.5M 14s 287500K .......... .......... .......... .......... .......... 56% 10.3M 14s 287550K .......... .......... .......... .......... .......... 56% 8.82M 14s 287600K .......... .......... .......... .......... .......... 56% 8.37M 14s 287650K .......... .......... .......... .......... .......... 56% 8.66M 14s 287700K .......... .......... .......... .......... .......... 56% 8.25M 14s 287750K .......... .......... .......... .......... .......... 56% 6.28M 14s 287800K .......... .......... .......... .......... .......... 56% 11.9M 14s 287850K .......... .......... .......... .......... .......... 56% 7.44M 14s 287900K .......... .......... .......... .......... .......... 56% 8.87M 14s 287950K .......... .......... .......... .......... .......... 56% 8.11M 14s 288000K .......... .......... .......... .......... .......... 56% 9.26M 14s 288050K .......... .......... .......... .......... .......... 56% 11.0M 14s 288100K .......... .......... .......... .......... .......... 56% 22.7M 14s 288150K .......... .......... .......... .......... .......... 56% 71.6M 14s 288200K .......... .......... .......... .......... .......... 56% 16.6M 14s 288250K .......... .......... .......... .......... .......... 56% 211M 14s 288300K .......... .......... .......... .......... .......... 56% 21.6M 14s 288350K .......... .......... .......... .......... .......... 56% 27.1M 14s 288400K .......... .......... .......... .......... .......... 56% 37.0M 14s 288450K .......... .......... .......... .......... .......... 56% 23.4M 14s 288500K .......... .......... .......... .......... .......... 56% 23.5M 14s 288550K .......... .......... .......... .......... .......... 56% 24.0M 14s 288600K .......... .......... .......... .......... .......... 56% 17.4M 14s 288650K .......... .......... .......... .......... .......... 56% 17.3M 14s 288700K .......... .......... .......... .......... .......... 56% 16.2M 14s 288750K .......... .......... .......... .......... .......... 56% 19.2M 14s 288800K .......... .......... .......... .......... .......... 56% 15.0M 14s 288850K .......... .......... .......... .......... .......... 56% 14.4M 14s 288900K .......... .......... .......... .......... .......... 56% 14.1M 14s 288950K .......... .......... .......... .......... .......... 56% 10.8M 14s 289000K .......... .......... .......... .......... .......... 56% 11.2M 14s 289050K .......... .......... .......... .......... .......... 56% 12.6M 14s 289100K .......... .......... .......... .......... .......... 56% 11.9M 14s 289150K .......... .......... .......... .......... .......... 56% 11.2M 14s 289200K .......... .......... .......... .......... .......... 56% 12.2M 14s 289250K .......... .......... .......... .......... .......... 56% 10.7M 14s 289300K .......... .......... .......... .......... .......... 56% 11.2M 14s 289350K .......... .......... .......... .......... .......... 56% 11.5M 14s 289400K .......... .......... .......... .......... .......... 56% 13.3M 14s 289450K .......... .......... .......... .......... .......... 56% 16.3M 14s 289500K .......... .......... .......... .......... .......... 56% 31.4M 14s 289550K .......... .......... .......... .......... .......... 56% 24.3M 14s 289600K .......... .......... .......... .......... .......... 56% 151M 14s 289650K .......... .......... .......... .......... .......... 56% 34.4M 14s 289700K .......... .......... .......... .......... .......... 56% 21.8M 14s 289750K .......... .......... .......... .......... .......... 56% 23.5M 14s 289800K .......... .......... .......... .......... .......... 56% 14.5M 14s 289850K .......... .......... .......... .......... .......... 56% 11.7M 14s 289900K .......... .......... .......... .......... .......... 56% 15.4M 14s 289950K .......... .......... .......... .......... .......... 56% 11.5M 14s 290000K .......... .......... .......... .......... .......... 56% 13.0M 14s 290050K .......... .......... .......... .......... .......... 56% 9.99M 14s 290100K .......... .......... .......... .......... .......... 56% 11.8M 14s 290150K .......... .......... .......... .......... .......... 56% 14.0M 14s 290200K .......... .......... .......... .......... .......... 56% 9.87M 14s 290250K .......... .......... .......... .......... .......... 56% 13.7M 14s 290300K .......... .......... .......... .......... .......... 56% 15.0M 14s 290350K .......... .......... .......... .......... .......... 56% 10.7M 14s 290400K .......... .......... .......... .......... .......... 56% 13.4M 14s 290450K .......... .......... .......... .......... .......... 56% 11.2M 14s 290500K .......... .......... .......... .......... .......... 56% 19.9M 14s 290550K .......... .......... .......... .......... .......... 57% 16.2M 14s 290600K .......... .......... .......... .......... .......... 57% 42.0M 14s 290650K .......... .......... .......... .......... .......... 57% 35.1M 14s 290700K .......... .......... .......... .......... .......... 57% 21.9M 14s 290750K .......... .......... .......... .......... .......... 57% 29.0M 14s 290800K .......... .......... .......... .......... .......... 57% 24.4M 14s 290850K .......... .......... .......... .......... .......... 57% 27.0M 14s 290900K .......... .......... .......... .......... .......... 57% 23.8M 14s 290950K .......... .......... .......... .......... .......... 57% 22.9M 14s 291000K .......... .......... .......... .......... .......... 57% 23.8M 14s 291050K .......... .......... .......... .......... .......... 57% 27.1M 14s 291100K .......... .......... .......... .......... .......... 57% 19.8M 14s 291150K .......... .......... .......... .......... .......... 57% 37.4M 14s 291200K .......... .......... .......... .......... .......... 57% 16.5M 14s 291250K .......... .......... .......... .......... .......... 57% 17.2M 14s 291300K .......... .......... .......... .......... .......... 57% 21.0M 14s 291350K .......... .......... .......... .......... .......... 57% 22.7M 14s 291400K .......... .......... .......... .......... .......... 57% 17.0M 14s 291450K .......... .......... .......... .......... .......... 57% 16.7M 14s 291500K .......... .......... .......... .......... .......... 57% 24.0M 14s 291550K .......... .......... .......... .......... .......... 57% 19.2M 14s 291600K .......... .......... .......... .......... .......... 57% 11.4M 14s 291650K .......... .......... .......... .......... .......... 57% 9.28M 14s 291700K .......... .......... .......... .......... .......... 57% 9.27M 14s 291750K .......... .......... .......... .......... .......... 57% 13.8M 14s 291800K .......... .......... .......... .......... .......... 57% 10.8M 14s 291850K .......... .......... .......... .......... .......... 57% 10.4M 14s 291900K .......... .......... .......... .......... .......... 57% 11.9M 14s 291950K .......... .......... .......... .......... .......... 57% 10.5M 14s 292000K .......... .......... .......... .......... .......... 57% 12.2M 14s 292050K .......... .......... .......... .......... .......... 57% 19.2M 14s 292100K .......... .......... .......... .......... .......... 57% 11.8M 14s 292150K .......... .......... .......... .......... .......... 57% 130M 14s 292200K .......... .......... .......... .......... .......... 57% 20.8M 14s 292250K .......... .......... .......... .......... .......... 57% 19.6M 14s 292300K .......... .......... .......... .......... .......... 57% 19.4M 14s 292350K .......... .......... .......... .......... .......... 57% 9.62M 14s 292400K .......... .......... .......... .......... .......... 57% 16.4M 14s 292450K .......... .......... .......... .......... .......... 57% 10.5M 14s 292500K .......... .......... .......... .......... .......... 57% 12.2M 14s 292550K .......... .......... .......... .......... .......... 57% 10.3M 14s 292600K .......... .......... .......... .......... .......... 57% 9.92M 14s 292650K .......... .......... .......... .......... .......... 57% 13.5M 14s 292700K .......... .......... .......... .......... .......... 57% 9.71M 14s 292750K .......... .......... .......... .......... .......... 57% 10.8M 14s 292800K .......... .......... .......... .......... .......... 57% 9.92M 14s 292850K .......... .......... .......... .......... .......... 57% 6.20M 14s 292900K .......... .......... .......... .......... .......... 57% 12.2M 14s 292950K .......... .......... .......... .......... .......... 57% 25.9M 14s 293000K .......... .......... .......... .......... .......... 57% 19.6M 14s 293050K .......... .......... .......... .......... .......... 57% 42.4M 14s 293100K .......... .......... .......... .......... .......... 57% 22.9M 14s 293150K .......... .......... .......... .......... .......... 57% 22.8M 14s 293200K .......... .......... .......... .......... .......... 57% 21.7M 14s 293250K .......... .......... .......... .......... .......... 57% 27.2M 14s 293300K .......... .......... .......... .......... .......... 57% 21.9M 14s 293350K .......... .......... .......... .......... .......... 57% 18.0M 14s 293400K .......... .......... .......... .......... .......... 57% 22.1M 14s 293450K .......... .......... .......... .......... .......... 57% 16.5M 14s 293500K .......... .......... .......... .......... .......... 57% 17.9M 14s 293550K .......... .......... .......... .......... .......... 57% 19.1M 14s 293600K .......... .......... .......... .......... .......... 57% 12.9M 14s 293650K .......... .......... .......... .......... .......... 57% 15.5M 14s 293700K .......... .......... .......... .......... .......... 57% 13.6M 14s 293750K .......... .......... .......... .......... .......... 57% 17.0M 14s 293800K .......... .......... .......... .......... .......... 57% 13.1M 14s 293850K .......... .......... .......... .......... .......... 57% 13.1M 14s 293900K .......... .......... .......... .......... .......... 57% 14.2M 14s 293950K .......... .......... .......... .......... .......... 57% 10.9M 14s 294000K .......... .......... .......... .......... .......... 57% 14.4M 14s 294050K .......... .......... .......... .......... .......... 57% 23.8M 14s 294100K .......... .......... .......... .......... .......... 57% 37.3M 14s 294150K .......... .......... .......... .......... .......... 57% 23.9M 14s 294200K .......... .......... .......... .......... .......... 57% 367M 14s 294250K .......... .......... .......... .......... .......... 57% 44.4M 14s 294300K .......... .......... .......... .......... .......... 57% 40.0M 14s 294350K .......... .......... .......... .......... .......... 57% 43.9M 14s 294400K .......... .......... .......... .......... .......... 57% 52.3M 14s 294450K .......... .......... .......... .......... .......... 57% 31.0M 14s 294500K .......... .......... .......... .......... .......... 57% 45.8M 14s 294550K .......... .......... .......... .......... .......... 57% 38.7M 14s 294600K .......... .......... .......... .......... .......... 57% 41.5M 14s 294650K .......... .......... .......... .......... .......... 57% 45.8M 14s 294700K .......... .......... .......... .......... .......... 57% 36.7M 14s 294750K .......... .......... .......... .......... .......... 57% 29.8M 14s 294800K .......... .......... .......... .......... .......... 57% 37.0M 14s 294850K .......... .......... .......... .......... .......... 57% 35.1M 14s 294900K .......... .......... .......... .......... .......... 57% 37.8M 14s 294950K .......... .......... .......... .......... .......... 57% 23.4M 14s 295000K .......... .......... .......... .......... .......... 57% 47.6M 13s 295050K .......... .......... .......... .......... .......... 57% 41.0M 13s 295100K .......... .......... .......... .......... .......... 57% 27.0M 13s 295150K .......... .......... .......... .......... .......... 57% 34.0M 13s 295200K .......... .......... .......... .......... .......... 57% 21.0M 13s 295250K .......... .......... .......... .......... .......... 57% 34.7M 13s 295300K .......... .......... .......... .......... .......... 57% 16.7M 13s 295350K .......... .......... .......... .......... .......... 57% 21.8M 13s 295400K .......... .......... .......... .......... .......... 57% 28.5M 13s 295450K .......... .......... .......... .......... .......... 57% 16.5M 13s 295500K .......... .......... .......... .......... .......... 57% 16.4M 13s 295550K .......... .......... .......... .......... .......... 57% 22.2M 13s 295600K .......... .......... .......... .......... .......... 57% 8.18M 13s 295650K .......... .......... .......... .......... .......... 58% 11.6M 13s 295700K .......... .......... .......... .......... .......... 58% 9.67M 13s 295750K .......... .......... .......... .......... .......... 58% 10.6M 13s 295800K .......... .......... .......... .......... .......... 58% 10.8M 13s 295850K .......... .......... .......... .......... .......... 58% 9.98M 13s 295900K .......... .......... .......... .......... .......... 58% 13.6M 13s 295950K .......... .......... .......... .......... .......... 58% 10.8M 13s 296000K .......... .......... .......... .......... .......... 58% 13.6M 13s 296050K .......... .......... .......... .......... .......... 58% 13.5M 13s 296100K .......... .......... .......... .......... .......... 58% 11.5M 13s 296150K .......... .......... .......... .......... .......... 58% 10.2M 13s 296200K .......... .......... .......... .......... .......... 58% 11.9M 13s 296250K .......... .......... .......... .......... .......... 58% 26.5M 13s 296300K .......... .......... .......... .......... .......... 58% 19.9M 13s 296350K .......... .......... .......... .......... .......... 58% 24.7M 13s 296400K .......... .......... .......... .......... .......... 58% 19.8M 13s 296450K .......... .......... .......... .......... .......... 58% 11.2M 13s 296500K .......... .......... .......... .......... .......... 58% 15.1M 13s 296550K .......... .......... .......... .......... .......... 58% 16.9M 13s 296600K .......... .......... .......... .......... .......... 58% 13.0M 13s 296650K .......... .......... .......... .......... .......... 58% 17.3M 13s 296700K .......... .......... .......... .......... .......... 58% 16.2M 13s 296750K .......... .......... .......... .......... .......... 58% 18.5M 13s 296800K .......... .......... .......... .......... .......... 58% 14.8M 13s 296850K .......... .......... .......... .......... .......... 58% 13.0M 13s 296900K .......... .......... .......... .......... .......... 58% 16.4M 13s 296950K .......... .......... .......... .......... .......... 58% 14.1M 13s 297000K .......... .......... .......... .......... .......... 58% 25.2M 13s 297050K .......... .......... .......... .......... .......... 58% 31.1M 13s 297100K .......... .......... .......... .......... .......... 58% 42.1M 13s 297150K .......... .......... .......... .......... .......... 58% 26.1M 13s 297200K .......... .......... .......... .......... .......... 58% 277M 13s 297250K .......... .......... .......... .......... .......... 58% 25.7M 13s 297300K .......... .......... .......... .......... .......... 58% 76.9M 13s 297350K .......... .......... .......... .......... .......... 58% 23.4M 13s 297400K .......... .......... .......... .......... .......... 58% 24.9M 13s 297450K .......... .......... .......... .......... .......... 58% 21.9M 13s 297500K .......... .......... .......... .......... .......... 58% 16.5M 13s 297550K .......... .......... .......... .......... .......... 58% 22.6M 13s 297600K .......... .......... .......... .......... .......... 58% 14.9M 13s 297650K .......... .......... .......... .......... .......... 58% 15.3M 13s 297700K .......... .......... .......... .......... .......... 58% 15.6M 13s 297750K .......... .......... .......... .......... .......... 58% 13.6M 13s 297800K .......... .......... .......... .......... .......... 58% 16.9M 13s 297850K .......... .......... .......... .......... .......... 58% 12.3M 13s 297900K .......... .......... .......... .......... .......... 58% 17.5M 13s 297950K .......... .......... .......... .......... .......... 58% 14.3M 13s 298000K .......... .......... .......... .......... .......... 58% 11.9M 13s 298050K .......... .......... .......... .......... .......... 58% 11.8M 13s 298100K .......... .......... .......... .......... .......... 58% 12.0M 13s 298150K .......... .......... .......... .......... .......... 58% 14.7M 13s 298200K .......... .......... .......... .......... .......... 58% 9.25M 13s 298250K .......... .......... .......... .......... .......... 58% 9.98M 13s 298300K .......... .......... .......... .......... .......... 58% 12.0M 13s 298350K .......... .......... .......... .......... .......... 58% 9.94M 13s 298400K .......... .......... .......... .......... .......... 58% 9.45M 13s 298450K .......... .......... .......... .......... .......... 58% 8.99M 13s 298500K .......... .......... .......... .......... .......... 58% 9.27M 13s 298550K .......... .......... .......... .......... .......... 58% 10.8M 13s 298600K .......... .......... .......... .......... .......... 58% 7.88M 13s 298650K .......... .......... .......... .......... .......... 58% 10.6M 13s 298700K .......... .......... .......... .......... .......... 58% 8.15M 13s 298750K .......... .......... .......... .......... .......... 58% 9.92M 13s 298800K .......... .......... .......... .......... .......... 58% 8.80M 13s 298850K .......... .......... .......... .......... .......... 58% 17.7M 13s 298900K .......... .......... .......... .......... .......... 58% 12.1M 13s 298950K .......... .......... .......... .......... .......... 58% 99.4M 13s 299000K .......... .......... .......... .......... .......... 58% 21.2M 13s 299050K .......... .......... .......... .......... .......... 58% 16.9M 13s 299100K .......... .......... .......... .......... .......... 58% 34.4M 13s 299150K .......... .......... .......... .......... .......... 58% 18.6M 13s 299200K .......... .......... .......... .......... .......... 58% 15.8M 13s 299250K .......... .......... .......... .......... .......... 58% 19.2M 13s 299300K .......... .......... .......... .......... .......... 58% 20.0M 13s 299350K .......... .......... .......... .......... .......... 58% 13.0M 13s 299400K .......... .......... .......... .......... .......... 58% 14.6M 13s 299450K .......... .......... .......... .......... .......... 58% 14.6M 13s 299500K .......... .......... .......... .......... .......... 58% 13.1M 13s 299550K .......... .......... .......... .......... .......... 58% 11.8M 13s 299600K .......... .......... .......... .......... .......... 58% 13.1M 13s 299650K .......... .......... .......... .......... .......... 58% 10.4M 13s 299700K .......... .......... .......... .......... .......... 58% 10.1M 13s 299750K .......... .......... .......... .......... .......... 58% 8.87M 13s 299800K .......... .......... .......... .......... .......... 58% 7.98M 13s 299850K .......... .......... .......... .......... .......... 58% 7.95M 13s 299900K .......... .......... .......... .......... .......... 58% 8.56M 13s 299950K .......... .......... .......... .......... .......... 58% 7.90M 13s 300000K .......... .......... .......... .......... .......... 58% 8.34M 13s 300050K .......... .......... .......... .......... .......... 58% 9.26M 13s 300100K .......... .......... .......... .......... .......... 58% 14.6M 13s 300150K .......... .......... .......... .......... .......... 58% 197M 13s 300200K .......... .......... .......... .......... .......... 58% 23.5M 13s 300250K .......... .......... .......... .......... .......... 58% 32.4M 13s 300300K .......... .......... .......... .......... .......... 58% 33.7M 13s 300350K .......... .......... .......... .......... .......... 58% 27.0M 13s 300400K .......... .......... .......... .......... .......... 58% 31.5M 13s 300450K .......... .......... .......... .......... .......... 58% 26.3M 13s 300500K .......... .......... .......... .......... .......... 58% 37.8M 13s 300550K .......... .......... .......... .......... .......... 58% 26.7M 13s 300600K .......... .......... .......... .......... .......... 58% 37.0M 13s 300650K .......... .......... .......... .......... .......... 58% 23.7M 13s 300700K .......... .......... .......... .......... .......... 58% 20.8M 13s 300750K .......... .......... .......... .......... .......... 59% 23.8M 13s 300800K .......... .......... .......... .......... .......... 59% 18.1M 13s 300850K .......... .......... .......... .......... .......... 59% 14.6M 13s 300900K .......... .......... .......... .......... .......... 59% 18.8M 13s 300950K .......... .......... .......... .......... .......... 59% 12.3M 13s 301000K .......... .......... .......... .......... .......... 59% 13.6M 13s 301050K .......... .......... .......... .......... .......... 59% 15.0M 13s 301100K .......... .......... .......... .......... .......... 59% 11.5M 13s 301150K .......... .......... .......... .......... .......... 59% 15.8M 13s 301200K .......... .......... .......... .......... .......... 59% 9.56M 13s 301250K .......... .......... .......... .......... .......... 59% 11.5M 13s 301300K .......... .......... .......... .......... .......... 59% 8.46M 13s 301350K .......... .......... .......... .......... .......... 59% 7.78M 13s 301400K .......... .......... .......... .......... .......... 59% 11.8M 13s 301450K .......... .......... .......... .......... .......... 59% 9.28M 13s 301500K .......... .......... .......... .......... .......... 59% 9.56M 13s 301550K .......... .......... .......... .......... .......... 59% 10.9M 13s 301600K .......... .......... .......... .......... .......... 59% 10.1M 13s 301650K .......... .......... .......... .......... .......... 59% 9.84M 13s 301700K .......... .......... .......... .......... .......... 59% 13.9M 13s 301750K .......... .......... .......... .......... .......... 59% 38.3M 13s 301800K .......... .......... .......... .......... .......... 59% 45.9M 13s 301850K .......... .......... .......... .......... .......... 59% 21.9M 13s 301900K .......... .......... .......... .......... .......... 59% 120M 13s 301950K .......... .......... .......... .......... .......... 59% 31.9M 13s 302000K .......... .......... .......... .......... .......... 59% 35.4M 13s 302050K .......... .......... .......... .......... .......... 59% 30.0M 13s 302100K .......... .......... .......... .......... .......... 59% 37.0M 13s 302150K .......... .......... .......... .......... .......... 59% 41.5M 13s 302200K .......... .......... .......... .......... .......... 59% 26.7M 13s 302250K .......... .......... .......... .......... .......... 59% 21.2M 13s 302300K .......... .......... .......... .......... .......... 59% 26.3M 13s 302350K .......... .......... .......... .......... .......... 59% 19.7M 13s 302400K .......... .......... .......... .......... .......... 59% 22.3M 13s 302450K .......... .......... .......... .......... .......... 59% 18.9M 13s 302500K .......... .......... .......... .......... .......... 59% 17.8M 13s 302550K .......... .......... .......... .......... .......... 59% 18.1M 13s 302600K .......... .......... .......... .......... .......... 59% 16.1M 13s 302650K .......... .......... .......... .......... .......... 59% 15.2M 13s 302700K .......... .......... .......... .......... .......... 59% 17.8M 13s 302750K .......... .......... .......... .......... .......... 59% 16.5M 13s 302800K .......... .......... .......... .......... .......... 59% 20.0M 13s 302850K .......... .......... .......... .......... .......... 59% 11.1M 13s 302900K .......... .......... .......... .......... .......... 59% 8.54M 13s 302950K .......... .......... .......... .......... .......... 59% 10.8M 13s 303000K .......... .......... .......... .......... .......... 59% 11.6M 13s 303050K .......... .......... .......... .......... .......... 59% 14.4M 13s 303100K .......... .......... .......... .......... .......... 59% 9.46M 13s 303150K .......... .......... .......... .......... .......... 59% 13.1M 13s 303200K .......... .......... .......... .......... .......... 59% 11.5M 13s 303250K .......... .......... .......... .......... .......... 59% 10.5M 13s 303300K .......... .......... .......... .......... .......... 59% 18.1M 13s 303350K .......... .......... .......... .......... .......... 59% 27.0M 13s 303400K .......... .......... .......... .......... .......... 59% 38.5M 13s 303450K .......... .......... .......... .......... .......... 59% 23.9M 13s 303500K .......... .......... .......... .......... .......... 59% 26.0M 13s 303550K .......... .......... .......... .......... .......... 59% 31.2M 13s 303600K .......... .......... .......... .......... .......... 59% 13.2M 13s 303650K .......... .......... .......... .......... .......... 59% 11.9M 13s 303700K .......... .......... .......... .......... .......... 59% 14.7M 13s 303750K .......... .......... .......... .......... .......... 59% 11.6M 13s 303800K .......... .......... .......... .......... .......... 59% 13.8M 13s 303850K .......... .......... .......... .......... .......... 59% 14.0M 13s 303900K .......... .......... .......... .......... .......... 59% 14.5M 13s 303950K .......... .......... .......... .......... .......... 59% 13.0M 13s 304000K .......... .......... .......... .......... .......... 59% 15.7M 13s 304050K .......... .......... .......... .......... .......... 59% 12.7M 13s 304100K .......... .......... .......... .......... .......... 59% 12.0M 13s 304150K .......... .......... .......... .......... .......... 59% 15.2M 13s 304200K .......... .......... .......... .......... .......... 59% 16.7M 13s 304250K .......... .......... .......... .......... .......... 59% 16.5M 13s 304300K .......... .......... .......... .......... .......... 59% 20.2M 13s 304350K .......... .......... .......... .......... .......... 59% 15.9M 13s 304400K .......... .......... .......... .......... .......... 59% 16.5M 13s 304450K .......... .......... .......... .......... .......... 59% 10.8M 13s 304500K .......... .......... .......... .......... .......... 59% 16.4M 13s 304550K .......... .......... .......... .......... .......... 59% 19.9M 13s 304600K .......... .......... .......... .......... .......... 59% 14.0M 13s 304650K .......... .......... .......... .......... .......... 59% 19.1M 13s 304700K .......... .......... .......... .......... .......... 59% 15.4M 13s 304750K .......... .......... .......... .......... .......... 59% 14.5M 13s 304800K .......... .......... .......... .......... .......... 59% 17.3M 13s 304850K .......... .......... .......... .......... .......... 59% 9.18M 13s 304900K .......... .......... .......... .......... .......... 59% 16.6M 13s 304950K .......... .......... .......... .......... .......... 59% 14.5M 13s 305000K .......... .......... .......... .......... .......... 59% 17.3M 13s 305050K .......... .......... .......... .......... .......... 59% 16.1M 13s 305100K .......... .......... .......... .......... .......... 59% 14.0M 13s 305150K .......... .......... .......... .......... .......... 59% 15.8M 13s 305200K .......... .......... .......... .......... .......... 59% 11.0M 13s 305250K .......... .......... .......... .......... .......... 59% 15.8M 13s 305300K .......... .......... .......... .......... .......... 59% 14.2M 13s 305350K .......... .......... .......... .......... .......... 59% 9.30M 13s 305400K .......... .......... .......... .......... .......... 59% 12.7M 13s 305450K .......... .......... .......... .......... .......... 59% 9.19M 13s 305500K .......... .......... .......... .......... .......... 59% 14.0M 13s 305550K .......... .......... .......... .......... .......... 59% 9.24M 13s 305600K .......... .......... .......... .......... .......... 59% 7.40M 13s 305650K .......... .......... .......... .......... .......... 59% 11.5M 13s 305700K .......... .......... .......... .......... .......... 59% 9.73M 13s 305750K .......... .......... .......... .......... .......... 59% 12.6M 13s 305800K .......... .......... .......... .......... .......... 59% 9.77M 13s 305850K .......... .......... .......... .......... .......... 60% 7.64M 13s 305900K .......... .......... .......... .......... .......... 60% 9.72M 13s 305950K .......... .......... .......... .......... .......... 60% 10.4M 13s 306000K .......... .......... .......... .......... .......... 60% 22.0M 13s 306050K .......... .......... .......... .......... .......... 60% 35.4M 13s 306100K .......... .......... .......... .......... .......... 60% 21.6M 13s 306150K .......... .......... .......... .......... .......... 60% 14.4M 13s 306200K .......... .......... .......... .......... .......... 60% 9.09M 13s 306250K .......... .......... .......... .......... .......... 60% 11.3M 13s 306300K .......... .......... .......... .......... .......... 60% 6.81M 13s 306350K .......... .......... .......... .......... .......... 60% 9.31M 13s 306400K .......... .......... .......... .......... .......... 60% 8.67M 13s 306450K .......... .......... .......... .......... .......... 60% 7.79M 13s 306500K .......... .......... .......... .......... .......... 60% 11.3M 13s 306550K .......... .......... .......... .......... .......... 60% 7.78M 13s 306600K .......... .......... .......... .......... .......... 60% 7.61M 13s 306650K .......... .......... .......... .......... .......... 60% 15.9M 13s 306700K .......... .......... .......... .......... .......... 60% 28.9M 13s 306750K .......... .......... .......... .......... .......... 60% 20.6M 13s 306800K .......... .......... .......... .......... .......... 60% 35.9M 13s 306850K .......... .......... .......... .......... .......... 60% 15.1M 13s 306900K .......... .......... .......... .......... .......... 60% 43.2M 13s 306950K .......... .......... .......... .......... .......... 60% 14.1M 13s 307000K .......... .......... .......... .......... .......... 60% 13.7M 13s 307050K .......... .......... .......... .......... .......... 60% 10.9M 13s 307100K .......... .......... .......... .......... .......... 60% 5.88M 13s 307150K .......... .......... .......... .......... .......... 60% 7.38M 13s 307200K .......... .......... .......... .......... .......... 60% 7.18M 13s 307250K .......... .......... .......... .......... .......... 60% 9.22M 13s 307300K .......... .......... .......... .......... .......... 60% 6.84M 13s 307350K .......... .......... .......... .......... .......... 60% 7.52M 13s 307400K .......... .......... .......... .......... .......... 60% 8.66M 13s 307450K .......... .......... .......... .......... .......... 60% 6.91M 13s 307500K .......... .......... .......... .......... .......... 60% 5.80M 13s 307550K .......... .......... .......... .......... .......... 60% 7.84M 13s 307600K .......... .......... .......... .......... .......... 60% 6.36M 13s 307650K .......... .......... .......... .......... .......... 60% 7.50M 13s 307700K .......... .......... .......... .......... .......... 60% 4.84M 13s 307750K .......... .......... .......... .......... .......... 60% 6.06M 13s 307800K .......... .......... .......... .......... .......... 60% 5.11M 13s 307850K .......... .......... .......... .......... .......... 60% 4.78M 13s 307900K .......... .......... .......... .......... .......... 60% 10.2M 13s 307950K .......... .......... .......... .......... .......... 60% 8.57M 13s 308000K .......... .......... .......... .......... .......... 60% 10.3M 13s 308050K .......... .......... .......... .......... .......... 60% 11.3M 13s 308100K .......... .......... .......... .......... .......... 60% 8.88M 13s 308150K .......... .......... .......... .......... .......... 60% 10.0M 13s 308200K .......... .......... .......... .......... .......... 60% 11.3M 13s 308250K .......... .......... .......... .......... .......... 60% 11.5M 13s 308300K .......... .......... .......... .......... .......... 60% 19.8M 13s 308350K .......... .......... .......... .......... .......... 60% 9.19M 13s 308400K .......... .......... .......... .......... .......... 60% 121M 13s 308450K .......... .......... .......... .......... .......... 60% 13.6M 13s 308500K .......... .......... .......... .......... .......... 60% 23.3M 13s 308550K .......... .......... .......... .......... .......... 60% 25.6M 13s 308600K .......... .......... .......... .......... .......... 60% 14.5M 13s 308650K .......... .......... .......... .......... .......... 60% 38.5M 13s 308700K .......... .......... .......... .......... .......... 60% 14.9M 13s 308750K .......... .......... .......... .......... .......... 60% 15.9M 13s 308800K .......... .......... .......... .......... .......... 60% 16.1M 13s 308850K .......... .......... .......... .......... .......... 60% 12.6M 13s 308900K .......... .......... .......... .......... .......... 60% 18.2M 13s 308950K .......... .......... .......... .......... .......... 60% 16.5M 13s 309000K .......... .......... .......... .......... .......... 60% 17.8M 13s 309050K .......... .......... .......... .......... .......... 60% 16.4M 13s 309100K .......... .......... .......... .......... .......... 60% 13.0M 13s 309150K .......... .......... .......... .......... .......... 60% 17.3M 13s 309200K .......... .......... .......... .......... .......... 60% 13.1M 13s 309250K .......... .......... .......... .......... .......... 60% 18.1M 13s 309300K .......... .......... .......... .......... .......... 60% 15.9M 13s 309350K .......... .......... .......... .......... .......... 60% 11.2M 13s 309400K .......... .......... .......... .......... .......... 60% 24.7M 13s 309450K .......... .......... .......... .......... .......... 60% 31.6M 13s 309500K .......... .......... .......... .......... .......... 60% 27.1M 13s 309550K .......... .......... .......... .......... .......... 60% 35.2M 13s 309600K .......... .......... .......... .......... .......... 60% 20.0M 13s 309650K .......... .......... .......... .......... .......... 60% 34.4M 13s 309700K .......... .......... .......... .......... .......... 60% 28.4M 13s 309750K .......... .......... .......... .......... .......... 60% 30.9M 13s 309800K .......... .......... .......... .......... .......... 60% 19.9M 13s 309850K .......... .......... .......... .......... .......... 60% 34.6M 13s 309900K .......... .......... .......... .......... .......... 60% 22.0M 13s 309950K .......... .......... .......... .......... .......... 60% 19.8M 13s 310000K .......... .......... .......... .......... .......... 60% 19.8M 13s 310050K .......... .......... .......... .......... .......... 60% 22.5M 13s 310100K .......... .......... .......... .......... .......... 60% 21.1M 13s 310150K .......... .......... .......... .......... .......... 60% 17.9M 13s 310200K .......... .......... .......... .......... .......... 60% 21.4M 13s 310250K .......... .......... .......... .......... .......... 60% 19.7M 13s 310300K .......... .......... .......... .......... .......... 60% 14.5M 13s 310350K .......... .......... .......... .......... .......... 60% 13.1M 13s 310400K .......... .......... .......... .......... .......... 60% 15.1M 13s 310450K .......... .......... .......... .......... .......... 60% 9.72M 13s 310500K .......... .......... .......... .......... .......... 60% 6.13M 13s 310550K .......... .......... .......... .......... .......... 60% 5.22M 13s 310600K .......... .......... .......... .......... .......... 60% 4.72M 13s 310650K .......... .......... .......... .......... .......... 60% 4.30M 13s 310700K .......... .......... .......... .......... .......... 60% 6.99M 13s 310750K .......... .......... .......... .......... .......... 60% 9.88M 13s 310800K .......... .......... .......... .......... .......... 60% 21.4M 13s 310850K .......... .......... .......... .......... .......... 60% 9.18M 13s 310900K .......... .......... .......... .......... .......... 60% 21.4M 13s 310950K .......... .......... .......... .......... .......... 61% 12.7M 13s 311000K .......... .......... .......... .......... .......... 61% 10.2M 13s 311050K .......... .......... .......... .......... .......... 61% 14.5M 13s 311100K .......... .......... .......... .......... .......... 61% 10.5M 13s 311150K .......... .......... .......... .......... .......... 61% 14.8M 13s 311200K .......... .......... .......... .......... .......... 61% 12.7M 13s 311250K .......... .......... .......... .......... .......... 61% 10.6M 13s 311300K .......... .......... .......... .......... .......... 61% 15.3M 13s 311350K .......... .......... .......... .......... .......... 61% 10.0M 13s 311400K .......... .......... .......... .......... .......... 61% 11.8M 13s 311450K .......... .......... .......... .......... .......... 61% 11.5M 13s 311500K .......... .......... .......... .......... .......... 61% 10.6M 13s 311550K .......... .......... .......... .......... .......... 61% 11.0M 13s 311600K .......... .......... .......... .......... .......... 61% 10.0M 13s 311650K .......... .......... .......... .......... .......... 61% 11.8M 13s 311700K .......... .......... .......... .......... .......... 61% 8.96M 13s 311750K .......... .......... .......... .......... .......... 61% 6.28M 13s 311800K .......... .......... .......... .......... .......... 61% 22.8M 13s 311850K .......... .......... .......... .......... .......... 61% 13.3M 13s 311900K .......... .......... .......... .......... .......... 61% 19.2M 13s 311950K .......... .......... .......... .......... .......... 61% 26.8M 13s 312000K .......... .......... .......... .......... .......... 61% 14.0M 13s 312050K .......... .......... .......... .......... .......... 61% 29.2M 13s 312100K .......... .......... .......... .......... .......... 61% 18.9M 13s 312150K .......... .......... .......... .......... .......... 61% 16.0M 13s 312200K .......... .......... .......... .......... .......... 61% 17.7M 13s 312250K .......... .......... .......... .......... .......... 61% 20.5M 13s 312300K .......... .......... .......... .......... .......... 61% 22.0M 13s 312350K .......... .......... .......... .......... .......... 61% 16.3M 13s 312400K .......... .......... .......... .......... .......... 61% 21.6M 13s 312450K .......... .......... .......... .......... .......... 61% 12.6M 13s 312500K .......... .......... .......... .......... .......... 61% 17.2M 13s 312550K .......... .......... .......... .......... .......... 61% 24.7M 13s 312600K .......... .......... .......... .......... .......... 61% 12.9M 13s 312650K .......... .......... .......... .......... .......... 61% 21.0M 12s 312700K .......... .......... .......... .......... .......... 61% 12.3M 12s 312750K .......... .......... .......... .......... .......... 61% 25.1M 12s 312800K .......... .......... .......... .......... .......... 61% 16.1M 12s 312850K .......... .......... .......... .......... .......... 61% 10.2M 12s 312900K .......... .......... .......... .......... .......... 61% 11.8M 12s 312950K .......... .......... .......... .......... .......... 61% 18.9M 12s 313000K .......... .......... .......... .......... .......... 61% 11.5M 12s 313050K .......... .......... .......... .......... .......... 61% 537M 12s 313100K .......... .......... .......... .......... .......... 61% 12.9M 12s 313150K .......... .......... .......... .......... .......... 61% 15.3M 12s 313200K .......... .......... .......... .......... .......... 61% 16.3M 12s 313250K .......... .......... .......... .......... .......... 61% 17.4M 12s 313300K .......... .......... .......... .......... .......... 61% 19.1M 12s 313350K .......... .......... .......... .......... .......... 61% 12.5M 12s 313400K .......... .......... .......... .......... .......... 61% 26.1M 12s 313450K .......... .......... .......... .......... .......... 61% 17.9M 12s 313500K .......... .......... .......... .......... .......... 61% 15.1M 12s 313550K .......... .......... .......... .......... .......... 61% 22.5M 12s 313600K .......... .......... .......... .......... .......... 61% 13.0M 12s 313650K .......... .......... .......... .......... .......... 61% 24.0M 12s 313700K .......... .......... .......... .......... .......... 61% 14.5M 12s 313750K .......... .......... .......... .......... .......... 61% 15.3M 12s 313800K .......... .......... .......... .......... .......... 61% 18.4M 12s 313850K .......... .......... .......... .......... .......... 61% 14.4M 12s 313900K .......... .......... .......... .......... .......... 61% 18.0M 12s 313950K .......... .......... .......... .......... .......... 61% 18.2M 12s 314000K .......... .......... .......... .......... .......... 61% 16.6M 12s 314050K .......... .......... .......... .......... .......... 61% 18.0M 12s 314100K .......... .......... .......... .......... .......... 61% 17.4M 12s 314150K .......... .......... .......... .......... .......... 61% 14.0M 12s 314200K .......... .......... .......... .......... .......... 61% 63.7M 12s 314250K .......... .......... .......... .......... .......... 61% 18.1M 12s 314300K .......... .......... .......... .......... .......... 61% 14.5M 12s 314350K .......... .......... .......... .......... .......... 61% 9.12M 12s 314400K .......... .......... .......... .......... .......... 61% 12.6M 12s 314450K .......... .......... .......... .......... .......... 61% 9.54M 12s 314500K .......... .......... .......... .......... .......... 61% 10.8M 12s 314550K .......... .......... .......... .......... .......... 61% 9.55M 12s 314600K .......... .......... .......... .......... .......... 61% 11.5M 12s 314650K .......... .......... .......... .......... .......... 61% 10.6M 12s 314700K .......... .......... .......... .......... .......... 61% 10.3M 12s 314750K .......... .......... .......... .......... .......... 61% 19.7M 12s 314800K .......... .......... .......... .......... .......... 61% 18.8M 12s 314850K .......... .......... .......... .......... .......... 61% 12.9M 12s 314900K .......... .......... .......... .......... .......... 61% 15.0M 12s 314950K .......... .......... .......... .......... .......... 61% 11.0M 12s 315000K .......... .......... .......... .......... .......... 61% 12.9M 12s 315050K .......... .......... .......... .......... .......... 61% 10.9M 12s 315100K .......... .......... .......... .......... .......... 61% 9.28M 12s 315150K .......... .......... .......... .......... .......... 61% 9.05M 12s 315200K .......... .......... .......... .......... .......... 61% 6.92M 12s 315250K .......... .......... .......... .......... .......... 61% 6.67M 12s 315300K .......... .......... .......... .......... .......... 61% 7.88M 12s 315350K .......... .......... .......... .......... .......... 61% 6.90M 12s 315400K .......... .......... .......... .......... .......... 61% 5.44M 12s 315450K .......... .......... .......... .......... .......... 61% 2.63M 12s 315500K .......... .......... .......... .......... .......... 61% 3.08M 12s 315550K .......... .......... .......... .......... .......... 61% 3.38M 12s 315600K .......... .......... .......... .......... .......... 61% 3.44M 12s 315650K .......... .......... .......... .......... .......... 61% 12.5M 12s 315700K .......... .......... .......... .......... .......... 61% 25.6M 12s 315750K .......... .......... .......... .......... .......... 61% 23.7M 12s 315800K .......... .......... .......... .......... .......... 61% 16.6M 12s 315850K .......... .......... .......... .......... .......... 61% 16.4M 12s 315900K .......... .......... .......... .......... .......... 61% 16.3M 12s 315950K .......... .......... .......... .......... .......... 61% 14.9M 12s 316000K .......... .......... .......... .......... .......... 61% 15.2M 12s 316050K .......... .......... .......... .......... .......... 62% 13.6M 12s 316100K .......... .......... .......... .......... .......... 62% 13.4M 12s 316150K .......... .......... .......... .......... .......... 62% 9.15M 12s 316200K .......... .......... .......... .......... .......... 62% 6.73M 12s 316250K .......... .......... .......... .......... .......... 62% 5.05M 12s 316300K .......... .......... .......... .......... .......... 62% 5.95M 12s 316350K .......... .......... .......... .......... .......... 62% 3.79M 12s 316400K .......... .......... .......... .......... .......... 62% 5.11M 12s 316450K .......... .......... .......... .......... .......... 62% 11.6M 12s 316500K .......... .......... .......... .......... .......... 62% 27.2M 12s 316550K .......... .......... .......... .......... .......... 62% 27.0M 12s 316600K .......... .......... .......... .......... .......... 62% 21.7M 12s 316650K .......... .......... .......... .......... .......... 62% 34.4M 12s 316700K .......... .......... .......... .......... .......... 62% 21.7M 12s 316750K .......... .......... .......... .......... .......... 62% 20.7M 12s 316800K .......... .......... .......... .......... .......... 62% 33.1M 12s 316850K .......... .......... .......... .......... .......... 62% 13.8M 12s 316900K .......... .......... .......... .......... .......... 62% 24.0M 12s 316950K .......... .......... .......... .......... .......... 62% 11.9M 12s 317000K .......... .......... .......... .......... .......... 62% 14.1M 12s 317050K .......... .......... .......... .......... .......... 62% 18.2M 12s 317100K .......... .......... .......... .......... .......... 62% 12.7M 12s 317150K .......... .......... .......... .......... .......... 62% 11.9M 12s 317200K .......... .......... .......... .......... .......... 62% 15.6M 12s 317250K .......... .......... .......... .......... .......... 62% 16.4M 12s 317300K .......... .......... .......... .......... .......... 62% 12.3M 12s 317350K .......... .......... .......... .......... .......... 62% 17.2M 12s 317400K .......... .......... .......... .......... .......... 62% 16.4M 12s 317450K .......... .......... .......... .......... .......... 62% 13.6M 12s 317500K .......... .......... .......... .......... .......... 62% 16.2M 12s 317550K .......... .......... .......... .......... .......... 62% 17.9M 12s 317600K .......... .......... .......... .......... .......... 62% 13.5M 12s 317650K .......... .......... .......... .......... .......... 62% 5.78M 12s 317700K .......... .......... .......... .......... .......... 62% 6.24M 12s 317750K .......... .......... .......... .......... .......... 62% 7.86M 12s 317800K .......... .......... .......... .......... .......... 62% 11.1M 12s 317850K .......... .......... .......... .......... .......... 62% 9.31M 12s 317900K .......... .......... .......... .......... .......... 62% 12.4M 12s 317950K .......... .......... .......... .......... .......... 62% 13.2M 12s 318000K .......... .......... .......... .......... .......... 62% 14.1M 12s 318050K .......... .......... .......... .......... .......... 62% 18.1M 12s 318100K .......... .......... .......... .......... .......... 62% 24.9M 12s 318150K .......... .......... .......... .......... .......... 62% 111M 12s 318200K .......... .......... .......... .......... .......... 62% 35.8M 12s 318250K .......... .......... .......... .......... .......... 62% 24.7M 12s 318300K .......... .......... .......... .......... .......... 62% 483M 12s 318350K .......... .......... .......... .......... .......... 62% 47.9M 12s 318400K .......... .......... .......... .......... .......... 62% 38.7M 12s 318450K .......... .......... .......... .......... .......... 62% 46.6M 12s 318500K .......... .......... .......... .......... .......... 62% 37.6M 12s 318550K .......... .......... .......... .......... .......... 62% 42.2M 12s 318600K .......... .......... .......... .......... .......... 62% 31.5M 12s 318650K .......... .......... .......... .......... .......... 62% 36.2M 12s 318700K .......... .......... .......... .......... .......... 62% 34.1M 12s 318750K .......... .......... .......... .......... .......... 62% 37.2M 12s 318800K .......... .......... .......... .......... .......... 62% 41.6M 12s 318850K .......... .......... .......... .......... .......... 62% 25.5M 12s 318900K .......... .......... .......... .......... .......... 62% 51.9M 12s 318950K .......... .......... .......... .......... .......... 62% 27.0M 12s 319000K .......... .......... .......... .......... .......... 62% 43.2M 12s 319050K .......... .......... .......... .......... .......... 62% 27.0M 12s 319100K .......... .......... .......... .......... .......... 62% 46.1M 12s 319150K .......... .......... .......... .......... .......... 62% 37.5M 12s 319200K .......... .......... .......... .......... .......... 62% 37.7M 12s 319250K .......... .......... .......... .......... .......... 62% 28.4M 12s 319300K .......... .......... .......... .......... .......... 62% 37.6M 12s 319350K .......... .......... .......... .......... .......... 62% 31.4M 12s 319400K .......... .......... .......... .......... .......... 62% 42.5M 12s 319450K .......... .......... .......... .......... .......... 62% 16.2M 12s 319500K .......... .......... .......... .......... .......... 62% 43.9M 12s 319550K .......... .......... .......... .......... .......... 62% 21.6M 12s 319600K .......... .......... .......... .......... .......... 62% 25.5M 12s 319650K .......... .......... .......... .......... .......... 62% 27.6M 12s 319700K .......... .......... .......... .......... .......... 62% 18.4M 12s 319750K .......... .......... .......... .......... .......... 62% 26.6M 12s 319800K .......... .......... .......... .......... .......... 62% 60.2M 12s 319850K .......... .......... .......... .......... .......... 62% 30.5M 12s 319900K .......... .......... .......... .......... .......... 62% 57.1M 12s 319950K .......... .......... .......... .......... .......... 62% 31.3M 12s 320000K .......... .......... .......... .......... .......... 62% 50.3M 12s 320050K .......... .......... .......... .......... .......... 62% 49.0M 12s 320100K .......... .......... .......... .......... .......... 62% 18.8M 12s 320150K .......... .......... .......... .......... .......... 62% 391M 12s 320200K .......... .......... .......... .......... .......... 62% 96.1M 12s 320250K .......... .......... .......... .......... .......... 62% 30.1M 12s 320300K .......... .......... .......... .......... .......... 62% 25.6M 12s 320350K .......... .......... .......... .......... .......... 62% 30.5M 12s 320400K .......... .......... .......... .......... .......... 62% 20.6M 12s 320450K .......... .......... .......... .......... .......... 62% 17.2M 12s 320500K .......... .......... .......... .......... .......... 62% 22.1M 12s 320550K .......... .......... .......... .......... .......... 62% 17.4M 12s 320600K .......... .......... .......... .......... .......... 62% 17.8M 12s 320650K .......... .......... .......... .......... .......... 62% 15.2M 12s 320700K .......... .......... .......... .......... .......... 62% 10.3M 12s 320750K .......... .......... .......... .......... .......... 62% 16.3M 12s 320800K .......... .......... .......... .......... .......... 62% 15.2M 12s 320850K .......... .......... .......... .......... .......... 62% 11.8M 12s 320900K .......... .......... .......... .......... .......... 62% 14.0M 12s 320950K .......... .......... .......... .......... .......... 62% 11.5M 12s 321000K .......... .......... .......... .......... .......... 62% 10.3M 12s 321050K .......... .......... .......... .......... .......... 62% 10.9M 12s 321100K .......... .......... .......... .......... .......... 62% 13.9M 12s 321150K .......... .......... .......... .......... .......... 63% 14.1M 12s 321200K .......... .......... .......... .......... .......... 63% 12.5M 12s 321250K .......... .......... .......... .......... .......... 63% 14.4M 12s 321300K .......... .......... .......... .......... .......... 63% 14.3M 12s 321350K .......... .......... .......... .......... .......... 63% 23.5M 12s 321400K .......... .......... .......... .......... .......... 63% 34.3M 12s 321450K .......... .......... .......... .......... .......... 63% 22.0M 12s 321500K .......... .......... .......... .......... .......... 63% 334M 12s 321550K .......... .......... .......... .......... .......... 63% 48.4M 12s 321600K .......... .......... .......... .......... .......... 63% 31.2M 12s 321650K .......... .......... .......... .......... .......... 63% 33.6M 12s 321700K .......... .......... .......... .......... .......... 63% 30.1M 12s 321750K .......... .......... .......... .......... .......... 63% 38.6M 12s 321800K .......... .......... .......... .......... .......... 63% 29.3M 12s 321850K .......... .......... .......... .......... .......... 63% 21.9M 12s 321900K .......... .......... .......... .......... .......... 63% 26.1M 12s 321950K .......... .......... .......... .......... .......... 63% 31.2M 12s 322000K .......... .......... .......... .......... .......... 63% 25.1M 12s 322050K .......... .......... .......... .......... .......... 63% 25.4M 12s 322100K .......... .......... .......... .......... .......... 63% 22.4M 12s 322150K .......... .......... .......... .......... .......... 63% 26.8M 12s 322200K .......... .......... .......... .......... .......... 63% 15.2M 12s 322250K .......... .......... .......... .......... .......... 63% 22.3M 12s 322300K .......... .......... .......... .......... .......... 63% 20.1M 12s 322350K .......... .......... .......... .......... .......... 63% 16.6M 12s 322400K .......... .......... .......... .......... .......... 63% 15.7M 12s 322450K .......... .......... .......... .......... .......... 63% 16.9M 12s 322500K .......... .......... .......... .......... .......... 63% 19.1M 12s 322550K .......... .......... .......... .......... .......... 63% 21.1M 12s 322600K .......... .......... .......... .......... .......... 63% 15.2M 12s 322650K .......... .......... .......... .......... .......... 63% 20.0M 12s 322700K .......... .......... .......... .......... .......... 63% 15.7M 12s 322750K .......... .......... .......... .......... .......... 63% 14.1M 12s 322800K .......... .......... .......... .......... .......... 63% 17.1M 12s 322850K .......... .......... .......... .......... .......... 63% 18.8M 12s 322900K .......... .......... .......... .......... .......... 63% 41.0M 12s 322950K .......... .......... .......... .......... .......... 63% 53.4M 12s 323000K .......... .......... .......... .......... .......... 63% 51.3M 12s 323050K .......... .......... .......... .......... .......... 63% 24.3M 12s 323100K .......... .......... .......... .......... .......... 63% 132M 12s 323150K .......... .......... .......... .......... .......... 63% 36.5M 12s 323200K .......... .......... .......... .......... .......... 63% 21.3M 12s 323250K .......... .......... .......... .......... .......... 63% 17.0M 12s 323300K .......... .......... .......... .......... .......... 63% 15.8M 12s 323350K .......... .......... .......... .......... .......... 63% 10.8M 12s 323400K .......... .......... .......... .......... .......... 63% 14.5M 12s 323450K .......... .......... .......... .......... .......... 63% 12.5M 12s 323500K .......... .......... .......... .......... .......... 63% 15.6M 12s 323550K .......... .......... .......... .......... .......... 63% 15.9M 12s 323600K .......... .......... .......... .......... .......... 63% 12.1M 12s 323650K .......... .......... .......... .......... .......... 63% 15.2M 12s 323700K .......... .......... .......... .......... .......... 63% 11.8M 12s 323750K .......... .......... .......... .......... .......... 63% 8.08M 12s 323800K .......... .......... .......... .......... .......... 63% 8.30M 12s 323850K .......... .......... .......... .......... .......... 63% 6.97M 12s 323900K .......... .......... .......... .......... .......... 63% 10.7M 12s 323950K .......... .......... .......... .......... .......... 63% 7.85M 12s 324000K .......... .......... .......... .......... .......... 63% 12.2M 12s 324050K .......... .......... .......... .......... .......... 63% 13.1M 12s 324100K .......... .......... .......... .......... .......... 63% 20.4M 12s 324150K .......... .......... .......... .......... .......... 63% 22.8M 12s 324200K .......... .......... .......... .......... .......... 63% 132M 12s 324250K .......... .......... .......... .......... .......... 63% 30.8M 12s 324300K .......... .......... .......... .......... .......... 63% 24.6M 12s 324350K .......... .......... .......... .......... .......... 63% 18.5M 12s 324400K .......... .......... .......... .......... .......... 63% 21.4M 12s 324450K .......... .......... .......... .......... .......... 63% 19.1M 12s 324500K .......... .......... .......... .......... .......... 63% 24.3M 12s 324550K .......... .......... .......... .......... .......... 63% 18.1M 12s 324600K .......... .......... .......... .......... .......... 63% 21.9M 12s 324650K .......... .......... .......... .......... .......... 63% 23.5M 12s 324700K .......... .......... .......... .......... .......... 63% 16.1M 12s 324750K .......... .......... .......... .......... .......... 63% 18.2M 12s 324800K .......... .......... .......... .......... .......... 63% 27.1M 12s 324850K .......... .......... .......... .......... .......... 63% 15.9M 12s 324900K .......... .......... .......... .......... .......... 63% 25.2M 12s 324950K .......... .......... .......... .......... .......... 63% 17.4M 12s 325000K .......... .......... .......... .......... .......... 63% 26.3M 12s 325050K .......... .......... .......... .......... .......... 63% 22.3M 12s 325100K .......... .......... .......... .......... .......... 63% 19.7M 12s 325150K .......... .......... .......... .......... .......... 63% 43.0M 12s 325200K .......... .......... .......... .......... .......... 63% 34.3M 12s 325250K .......... .......... .......... .......... .......... 63% 40.7M 12s 325300K .......... .......... .......... .......... .......... 63% 97.5M 12s 325350K .......... .......... .......... .......... .......... 63% 36.8M 12s 325400K .......... .......... .......... .......... .......... 63% 63.9M 12s 325450K .......... .......... .......... .......... .......... 63% 33.0M 12s 325500K .......... .......... .......... .......... .......... 63% 25.6M 12s 325550K .......... .......... .......... .......... .......... 63% 95.6M 12s 325600K .......... .......... .......... .......... .......... 63% 34.8M 12s 325650K .......... .......... .......... .......... .......... 63% 25.5M 12s 325700K .......... .......... .......... .......... .......... 63% 330M 12s 325750K .......... .......... .......... .......... .......... 63% 22.2M 12s 325800K .......... .......... .......... .......... .......... 63% 474M 12s 325850K .......... .......... .......... .......... .......... 63% 41.2M 12s 325900K .......... .......... .......... .......... .......... 63% 53.7M 12s 325950K .......... .......... .......... .......... .......... 63% 36.5M 12s 326000K .......... .......... .......... .......... .......... 63% 53.3M 12s 326050K .......... .......... .......... .......... .......... 63% 40.8M 12s 326100K .......... .......... .......... .......... .......... 63% 38.8M 12s 326150K .......... .......... .......... .......... .......... 63% 45.3M 12s 326200K .......... .......... .......... .......... .......... 63% 25.9M 12s 326250K .......... .......... .......... .......... .......... 64% 44.1M 12s 326300K .......... .......... .......... .......... .......... 64% 42.5M 12s 326350K .......... .......... .......... .......... .......... 64% 31.4M 12s 326400K .......... .......... .......... .......... .......... 64% 33.8M 12s 326450K .......... .......... .......... .......... .......... 64% 25.6M 12s 326500K .......... .......... .......... .......... .......... 64% 41.9M 12s 326550K .......... .......... .......... .......... .......... 64% 34.7M 12s 326600K .......... .......... .......... .......... .......... 64% 31.5M 12s 326650K .......... .......... .......... .......... .......... 64% 42.0M 12s 326700K .......... .......... .......... .......... .......... 64% 29.6M 12s 326750K .......... .......... .......... .......... .......... 64% 42.3M 12s 326800K .......... .......... .......... .......... .......... 64% 26.6M 12s 326850K .......... .......... .......... .......... .......... 64% 41.2M 12s 326900K .......... .......... .......... .......... .......... 64% 39.8M 12s 326950K .......... .......... .......... .......... .......... 64% 23.3M 12s 327000K .......... .......... .......... .......... .......... 64% 37.1M 12s 327050K .......... .......... .......... .......... .......... 64% 30.9M 12s 327100K .......... .......... .......... .......... .......... 64% 33.6M 12s 327150K .......... .......... .......... .......... .......... 64% 29.4M 12s 327200K .......... .......... .......... .......... .......... 64% 34.0M 12s 327250K .......... .......... .......... .......... .......... 64% 29.5M 12s 327300K .......... .......... .......... .......... .......... 64% 47.0M 12s 327350K .......... .......... .......... .......... .......... 64% 25.0M 12s 327400K .......... .......... .......... .......... .......... 64% 42.2M 12s 327450K .......... .......... .......... .......... .......... 64% 48.1M 12s 327500K .......... .......... .......... .......... .......... 64% 63.0M 12s 327550K .......... .......... .......... .......... .......... 64% 51.7M 12s 327600K .......... .......... .......... .......... .......... 64% 54.3M 12s 327650K .......... .......... .......... .......... .......... 64% 23.9M 11s 327700K .......... .......... .......... .......... .......... 64% 289M 11s 327750K .......... .......... .......... .......... .......... 64% 364M 11s 327800K .......... .......... .......... .......... .......... 64% 27.6M 11s 327850K .......... .......... .......... .......... .......... 64% 440M 11s 327900K .......... .......... .......... .......... .......... 64% 27.2M 11s 327950K .......... .......... .......... .......... .......... 64% 122M 11s 328000K .......... .......... .......... .......... .......... 64% 44.3M 11s 328050K .......... .......... .......... .......... .......... 64% 45.9M 11s 328100K .......... .......... .......... .......... .......... 64% 31.1M 11s 328150K .......... .......... .......... .......... .......... 64% 38.8M 11s 328200K .......... .......... .......... .......... .......... 64% 37.2M 11s 328250K .......... .......... .......... .......... .......... 64% 31.3M 11s 328300K .......... .......... .......... .......... .......... 64% 37.5M 11s 328350K .......... .......... .......... .......... .......... 64% 20.7M 11s 328400K .......... .......... .......... .......... .......... 64% 52.8M 11s 328450K .......... .......... .......... .......... .......... 64% 29.8M 11s 328500K .......... .......... .......... .......... .......... 64% 42.4M 11s 328550K .......... .......... .......... .......... .......... 64% 41.7M 11s 328600K .......... .......... .......... .......... .......... 64% 28.0M 11s 328650K .......... .......... .......... .......... .......... 64% 41.4M 11s 328700K .......... .......... .......... .......... .......... 64% 25.3M 11s 328750K .......... .......... .......... .......... .......... 64% 61.2M 11s 328800K .......... .......... .......... .......... .......... 64% 37.4M 11s 328850K .......... .......... .......... .......... .......... 64% 28.9M 11s 328900K .......... .......... .......... .......... .......... 64% 36.6M 11s 328950K .......... .......... .......... .......... .......... 64% 31.5M 11s 329000K .......... .......... .......... .......... .......... 64% 33.9M 11s 329050K .......... .......... .......... .......... .......... 64% 36.8M 11s 329100K .......... .......... .......... .......... .......... 64% 29.3M 11s 329150K .......... .......... .......... .......... .......... 64% 37.5M 11s 329200K .......... .......... .......... .......... .......... 64% 36.5M 11s 329250K .......... .......... .......... .......... .......... 64% 29.3M 11s 329300K .......... .......... .......... .......... .......... 64% 34.3M 11s 329350K .......... .......... .......... .......... .......... 64% 29.3M 11s 329400K .......... .......... .......... .......... .......... 64% 41.0M 11s 329450K .......... .......... .......... .......... .......... 64% 25.7M 11s 329500K .......... .......... .......... .......... .......... 64% 45.7M 11s 329550K .......... .......... .......... .......... .......... 64% 35.0M 11s 329600K .......... .......... .......... .......... .......... 64% 27.4M 11s 329650K .......... .......... .......... .......... .......... 64% 17.6M 11s 329700K .......... .......... .......... .......... .......... 64% 23.9M 11s 329750K .......... .......... .......... .......... .......... 64% 36.8M 11s 329800K .......... .......... .......... .......... .......... 64% 23.8M 11s 329850K .......... .......... .......... .......... .......... 64% 46.4M 11s 329900K .......... .......... .......... .......... .......... 64% 20.0M 11s 329950K .......... .......... .......... .......... .......... 64% 111M 11s 330000K .......... .......... .......... .......... .......... 64% 61.0M 11s 330050K .......... .......... .......... .......... .......... 64% 63.2M 11s 330100K .......... .......... .......... .......... .......... 64% 53.3M 11s 330150K .......... .......... .......... .......... .......... 64% 75.1M 11s 330200K .......... .......... .......... .......... .......... 64% 26.7M 11s 330250K .......... .......... .......... .......... .......... 64% 126M 11s 330300K .......... .......... .......... .......... .......... 64% 41.5M 11s 330350K .......... .......... .......... .......... .......... 64% 24.6M 11s 330400K .......... .......... .......... .......... .......... 64% 42.3M 11s 330450K .......... .......... .......... .......... .......... 64% 23.1M 11s 330500K .......... .......... .......... .......... .......... 64% 38.2M 11s 330550K .......... .......... .......... .......... .......... 64% 23.9M 11s 330600K .......... .......... .......... .......... .......... 64% 74.9M 11s 330650K .......... .......... .......... .......... .......... 64% 25.2M 11s 330700K .......... .......... .......... .......... .......... 64% 22.1M 11s 330750K .......... .......... .......... .......... .......... 64% 19.9M 11s 330800K .......... .......... .......... .......... .......... 64% 38.3M 11s 330850K .......... .......... .......... .......... .......... 64% 23.5M 11s 330900K .......... .......... .......... .......... .......... 64% 28.6M 11s 330950K .......... .......... .......... .......... .......... 64% 25.0M 11s 331000K .......... .......... .......... .......... .......... 64% 34.5M 11s 331050K .......... .......... .......... .......... .......... 64% 31.3M 11s 331100K .......... .......... .......... .......... .......... 64% 28.2M 11s 331150K .......... .......... .......... .......... .......... 64% 38.1M 11s 331200K .......... .......... .......... .......... .......... 64% 25.1M 11s 331250K .......... .......... .......... .......... .......... 64% 47.0M 11s 331300K .......... .......... .......... .......... .......... 64% 31.4M 11s 331350K .......... .......... .......... .......... .......... 65% 22.2M 11s 331400K .......... .......... .......... .......... .......... 65% 46.8M 11s 331450K .......... .......... .......... .......... .......... 65% 28.2M 11s 331500K .......... .......... .......... .......... .......... 65% 37.8M 11s 331550K .......... .......... .......... .......... .......... 65% 27.8M 11s 331600K .......... .......... .......... .......... .......... 65% 31.7M 11s 331650K .......... .......... .......... .......... .......... 65% 35.4M 11s 331700K .......... .......... .......... .......... .......... 65% 47.8M 11s 331750K .......... .......... .......... .......... .......... 65% 52.8M 11s 331800K .......... .......... .......... .......... .......... 65% 19.8M 11s 331850K .......... .......... .......... .......... .......... 65% 109M 11s 331900K .......... .......... .......... .......... .......... 65% 479M 11s 331950K .......... .......... .......... .......... .......... 65% 34.4M 11s 332000K .......... .......... .......... .......... .......... 65% 122M 11s 332050K .......... .......... .......... .......... .......... 65% 56.2M 11s 332100K .......... .......... .......... .......... .......... 65% 131M 11s 332150K .......... .......... .......... .......... .......... 65% 53.0M 11s 332200K .......... .......... .......... .......... .......... 65% 39.8M 11s 332250K .......... .......... .......... .......... .......... 65% 36.7M 11s 332300K .......... .......... .......... .......... .......... 65% 41.1M 11s 332350K .......... .......... .......... .......... .......... 65% 34.3M 11s 332400K .......... .......... .......... .......... .......... 65% 30.5M 11s 332450K .......... .......... .......... .......... .......... 65% 37.8M 11s 332500K .......... .......... .......... .......... .......... 65% 34.7M 11s 332550K .......... .......... .......... .......... .......... 65% 33.5M 11s 332600K .......... .......... .......... .......... .......... 65% 28.4M 11s 332650K .......... .......... .......... .......... .......... 65% 42.7M 11s 332700K .......... .......... .......... .......... .......... 65% 41.5M 11s 332750K .......... .......... .......... .......... .......... 65% 27.0M 11s 332800K .......... .......... .......... .......... .......... 65% 45.5M 11s 332850K .......... .......... .......... .......... .......... 65% 25.6M 11s 332900K .......... .......... .......... .......... .......... 65% 46.3M 11s 332950K .......... .......... .......... .......... .......... 65% 37.4M 11s 333000K .......... .......... .......... .......... .......... 65% 31.9M 11s 333050K .......... .......... .......... .......... .......... 65% 7.15M 11s 333100K .......... .......... .......... .......... .......... 65% 29.2M 11s 333150K .......... .......... .......... .......... .......... 65% 37.6M 11s 333200K .......... .......... .......... .......... .......... 65% 28.9M 11s 333250K .......... .......... .......... .......... .......... 65% 41.8M 11s 333300K .......... .......... .......... .......... .......... 65% 41.5M 11s 333350K .......... .......... .......... .......... .......... 65% 25.4M 11s 333400K .......... .......... .......... .......... .......... 65% 47.0M 11s 333450K .......... .......... .......... .......... .......... 65% 42.5M 11s 333500K .......... .......... .......... .......... .......... 65% 27.2M 11s 333550K .......... .......... .......... .......... .......... 65% 53.3M 11s 333600K .......... .......... .......... .......... .......... 65% 24.9M 11s 333650K .......... .......... .......... .......... .......... 65% 42.2M 11s 333700K .......... .......... .......... .......... .......... 65% 28.5M 11s 333750K .......... .......... .......... .......... .......... 65% 14.1M 11s 333800K .......... .......... .......... .......... .......... 65% 123M 11s 333850K .......... .......... .......... .......... .......... 65% 22.8M 11s 333900K .......... .......... .......... .......... .......... 65% 16.2M 11s 333950K .......... .......... .......... .......... .......... 65% 417M 11s 334000K .......... .......... .......... .......... .......... 65% 37.9M 11s 334050K .......... .......... .......... .......... .......... 65% 33.5M 11s 334100K .......... .......... .......... .......... .......... 65% 23.9M 11s 334150K .......... .......... .......... .......... .......... 65% 44.5M 11s 334200K .......... .......... .......... .......... .......... 65% 28.5M 11s 334250K .......... .......... .......... .......... .......... 65% 37.9M 11s 334300K .......... .......... .......... .......... .......... 65% 27.5M 11s 334350K .......... .......... .......... .......... .......... 65% 28.6M 11s 334400K .......... .......... .......... .......... .......... 65% 38.2M 11s 334450K .......... .......... .......... .......... .......... 65% 29.2M 11s 334500K .......... .......... .......... .......... .......... 65% 38.3M 11s 334550K .......... .......... .......... .......... .......... 65% 27.2M 11s 334600K .......... .......... .......... .......... .......... 65% 37.1M 11s 334650K .......... .......... .......... .......... .......... 65% 27.2M 11s 334700K .......... .......... .......... .......... .......... 65% 32.0M 11s 334750K .......... .......... .......... .......... .......... 65% 31.5M 11s 334800K .......... .......... .......... .......... .......... 65% 25.1M 11s 334850K .......... .......... .......... .......... .......... 65% 22.4M 11s 334900K .......... .......... .......... .......... .......... 65% 21.1M 11s 334950K .......... .......... .......... .......... .......... 65% 26.1M 11s 335000K .......... .......... .......... .......... .......... 65% 22.5M 11s 335050K .......... .......... .......... .......... .......... 65% 31.9M 11s 335100K .......... .......... .......... .......... .......... 65% 26.7M 11s 335150K .......... .......... .......... .......... .......... 65% 22.5M 11s 335200K .......... .......... .......... .......... .......... 65% 9.04M 11s 335250K .......... .......... .......... .......... .......... 65% 27.2M 11s 335300K .......... .......... .......... .......... .......... 65% 15.7M 11s 335350K .......... .......... .......... .......... .......... 65% 15.1M 11s 335400K .......... .......... .......... .......... .......... 65% 14.4M 11s 335450K .......... .......... .......... .......... .......... 65% 13.5M 11s 335500K .......... .......... .......... .......... .......... 65% 41.9M 11s 335550K .......... .......... .......... .......... .......... 65% 20.6M 11s 335600K .......... .......... .......... .......... .......... 65% 25.9M 11s 335650K .......... .......... .......... .......... .......... 65% 425M 11s 335700K .......... .......... .......... .......... .......... 65% 26.3M 11s 335750K .......... .......... .......... .......... .......... 65% 33.5M 11s 335800K .......... .......... .......... .......... .......... 65% 43.6M 11s 335850K .......... .......... .......... .......... .......... 65% 24.9M 11s 335900K .......... .......... .......... .......... .......... 65% 22.0M 11s 335950K .......... .......... .......... .......... .......... 65% 20.0M 11s 336000K .......... .......... .......... .......... .......... 65% 20.9M 11s 336050K .......... .......... .......... .......... .......... 65% 38.2M 11s 336100K .......... .......... .......... .......... .......... 65% 24.7M 11s 336150K .......... .......... .......... .......... .......... 65% 20.0M 11s 336200K .......... .......... .......... .......... .......... 65% 21.9M 11s 336250K .......... .......... .......... .......... .......... 65% 24.1M 11s 336300K .......... .......... .......... .......... .......... 65% 25.8M 11s 336350K .......... .......... .......... .......... .......... 65% 23.5M 11s 336400K .......... .......... .......... .......... .......... 65% 37.6M 11s 336450K .......... .......... .......... .......... .......... 66% 25.0M 11s 336500K .......... .......... .......... .......... .......... 66% 26.8M 11s 336550K .......... .......... .......... .......... .......... 66% 26.7M 11s 336600K .......... .......... .......... .......... .......... 66% 22.3M 11s 336650K .......... .......... .......... .......... .......... 66% 33.9M 11s 336700K .......... .......... .......... .......... .......... 66% 42.4M 11s 336750K .......... .......... .......... .......... .......... 66% 46.4M 11s 336800K .......... .......... .......... .......... .......... 66% 55.1M 11s 336850K .......... .......... .......... .......... .......... 66% 60.1M 11s 336900K .......... .......... .......... .......... .......... 66% 93.7M 11s 336950K .......... .......... .......... .......... .......... 66% 19.3M 11s 337000K .......... .......... .......... .......... .......... 66% 34.9M 11s 337050K .......... .......... .......... .......... .......... 66% 257M 11s 337100K .......... .......... .......... .......... .......... 66% 66.2M 11s 337150K .......... .......... .......... .......... .......... 66% 52.4M 11s 337200K .......... .......... .......... .......... .......... 66% 41.5M 11s 337250K .......... .......... .......... .......... .......... 66% 44.9M 11s 337300K .......... .......... .......... .......... .......... 66% 31.5M 11s 337350K .......... .......... .......... .......... .......... 66% 25.1M 11s 337400K .......... .......... .......... .......... .......... 66% 31.1M 11s 337450K .......... .......... .......... .......... .......... 66% 40.4M 11s 337500K .......... .......... .......... .......... .......... 66% 26.9M 11s 337550K .......... .......... .......... .......... .......... 66% 12.0M 11s 337600K .......... .......... .......... .......... .......... 66% 241M 11s 337650K .......... .......... .......... .......... .......... 66% 63.5M 11s 337700K .......... .......... .......... .......... .......... 66% 22.2M 11s 337750K .......... .......... .......... .......... .......... 66% 32.0M 11s 337800K .......... .......... .......... .......... .......... 66% 22.8M 11s 337850K .......... .......... .......... .......... .......... 66% 22.6M 11s 337900K .......... .......... .......... .......... .......... 66% 31.8M 11s 337950K .......... .......... .......... .......... .......... 66% 24.2M 11s 338000K .......... .......... .......... .......... .......... 66% 34.7M 11s 338050K .......... .......... .......... .......... .......... 66% 27.4M 11s 338100K .......... .......... .......... .......... .......... 66% 26.8M 11s 338150K .......... .......... .......... .......... .......... 66% 24.9M 11s 338200K .......... .......... .......... .......... .......... 66% 29.0M 11s 338250K .......... .......... .......... .......... .......... 66% 31.2M 11s 338300K .......... .......... .......... .......... .......... 66% 32.3M 11s 338350K .......... .......... .......... .......... .......... 66% 25.0M 11s 338400K .......... .......... .......... .......... .......... 66% 27.2M 11s 338450K .......... .......... .......... .......... .......... 66% 25.3M 11s 338500K .......... .......... .......... .......... .......... 66% 37.0M 11s 338550K .......... .......... .......... .......... .......... 66% 36.5M 11s 338600K .......... .......... .......... .......... .......... 66% 27.1M 11s 338650K .......... .......... .......... .......... .......... 66% 13.6M 11s 338700K .......... .......... .......... .......... .......... 66% 391M 11s 338750K .......... .......... .......... .......... .......... 66% 45.5M 11s 338800K .......... .......... .......... .......... .......... 66% 25.2M 11s 338850K .......... .......... .......... .......... .......... 66% 26.3M 11s 338900K .......... .......... .......... .......... .......... 66% 18.9M 11s 338950K .......... .......... .......... .......... .......... 66% 76.2M 11s 339000K .......... .......... .......... .......... .......... 66% 71.0M 11s 339050K .......... .......... .......... .......... .......... 66% 32.2M 11s 339100K .......... .......... .......... .......... .......... 66% 34.2M 11s 339150K .......... .......... .......... .......... .......... 66% 38.2M 11s 339200K .......... .......... .......... .......... .......... 66% 29.3M 11s 339250K .......... .......... .......... .......... .......... 66% 41.0M 11s 339300K .......... .......... .......... .......... .......... 66% 30.1M 11s 339350K .......... .......... .......... .......... .......... 66% 29.0M 11s 339400K .......... .......... .......... .......... .......... 66% 34.1M 11s 339450K .......... .......... .......... .......... .......... 66% 31.5M 11s 339500K .......... .......... .......... .......... .......... 66% 36.5M 11s 339550K .......... .......... .......... .......... .......... 66% 36.8M 11s 339600K .......... .......... .......... .......... .......... 66% 27.0M 11s 339650K .......... .......... .......... .......... .......... 66% 29.2M 11s 339700K .......... .......... .......... .......... .......... 66% 34.8M 11s 339750K .......... .......... .......... .......... .......... 66% 29.3M 11s 339800K .......... .......... .......... .......... .......... 66% 31.9M 11s 339850K .......... .......... .......... .......... .......... 66% 29.3M 11s 339900K .......... .......... .......... .......... .......... 66% 46.2M 11s 339950K .......... .......... .......... .......... .......... 66% 29.0M 11s 340000K .......... .......... .......... .......... .......... 66% 30.6M 11s 340050K .......... .......... .......... .......... .......... 66% 22.3M 11s 340100K .......... .......... .......... .......... .......... 66% 18.2M 11s 340150K .......... .......... .......... .......... .......... 66% 25.1M 11s 340200K .......... .......... .......... .......... .......... 66% 22.7M 11s 340250K .......... .......... .......... .......... .......... 66% 25.4M 11s 340300K .......... .......... .......... .......... .......... 66% 87.7M 10s 340350K .......... .......... .......... .......... .......... 66% 20.4M 10s 340400K .......... .......... .......... .......... .......... 66% 452M 10s 340450K .......... .......... .......... .......... .......... 66% 25.8M 10s 340500K .......... .......... .......... .......... .......... 66% 20.3M 10s 340550K .......... .......... .......... .......... .......... 66% 47.6M 10s 340600K .......... .......... .......... .......... .......... 66% 28.6M 10s 340650K .......... .......... .......... .......... .......... 66% 25.3M 10s 340700K .......... .......... .......... .......... .......... 66% 18.9M 10s 340750K .......... .......... .......... .......... .......... 66% 20.8M 10s 340800K .......... .......... .......... .......... .......... 66% 21.3M 10s 340850K .......... .......... .......... .......... .......... 66% 19.0M 10s 340900K .......... .......... .......... .......... .......... 66% 20.1M 10s 340950K .......... .......... .......... .......... .......... 66% 18.0M 10s 341000K .......... .......... .......... .......... .......... 66% 23.2M 10s 341050K .......... .......... .......... .......... .......... 66% 25.3M 10s 341100K .......... .......... .......... .......... .......... 66% 24.7M 10s 341150K .......... .......... .......... .......... .......... 66% 22.1M 10s 341200K .......... .......... .......... .......... .......... 66% 16.6M 10s 341250K .......... .......... .......... .......... .......... 66% 22.1M 10s 341300K .......... .......... .......... .......... .......... 66% 23.5M 10s 341350K .......... .......... .......... .......... .......... 66% 23.3M 10s 341400K .......... .......... .......... .......... .......... 66% 18.1M 10s 341450K .......... .......... .......... .......... .......... 66% 31.7M 10s 341500K .......... .......... .......... .......... .......... 66% 38.3M 10s 341550K .......... .......... .......... .......... .......... 67% 93.4M 10s 341600K .......... .......... .......... .......... .......... 67% 20.6M 10s 341650K .......... .......... .......... .......... .......... 67% 339M 10s 341700K .......... .......... .......... .......... .......... 67% 44.3M 10s 341750K .......... .......... .......... .......... .......... 67% 70.8M 10s 341800K .......... .......... .......... .......... .......... 67% 45.8M 10s 341850K .......... .......... .......... .......... .......... 67% 41.8M 10s 341900K .......... .......... .......... .......... .......... 67% 37.8M 10s 341950K .......... .......... .......... .......... .......... 67% 30.6M 10s 342000K .......... .......... .......... .......... .......... 67% 40.6M 10s 342050K .......... .......... .......... .......... .......... 67% 22.5M 10s 342100K .......... .......... .......... .......... .......... 67% 38.6M 10s 342150K .......... .......... .......... .......... .......... 67% 51.5M 10s 342200K .......... .......... .......... .......... .......... 67% 23.7M 10s 342250K .......... .......... .......... .......... .......... 67% 53.8M 10s 342300K .......... .......... .......... .......... .......... 67% 42.2M 10s 342350K .......... .......... .......... .......... .......... 67% 42.1M 10s 342400K .......... .......... .......... .......... .......... 67% 46.1M 10s 342450K .......... .......... .......... .......... .......... 67% 35.5M 10s 342500K .......... .......... .......... .......... .......... 67% 42.9M 10s 342550K .......... .......... .......... .......... .......... 67% 46.7M 10s 342600K .......... .......... .......... .......... .......... 67% 29.3M 10s 342650K .......... .......... .......... .......... .......... 67% 46.2M 10s 342700K .......... .......... .......... .......... .......... 67% 47.8M 10s 342750K .......... .......... .......... .......... .......... 67% 46.8M 10s 342800K .......... .......... .......... .......... .......... 67% 41.1M 10s 342850K .......... .......... .......... .......... .......... 67% 31.8M 10s 342900K .......... .......... .......... .......... .......... 67% 47.0M 10s 342950K .......... .......... .......... .......... .......... 67% 41.3M 10s 343000K .......... .......... .......... .......... .......... 67% 48.2M 10s 343050K .......... .......... .......... .......... .......... 67% 32.4M 10s 343100K .......... .......... .......... .......... .......... 67% 45.9M 10s 343150K .......... .......... .......... .......... .......... 67% 45.5M 10s 343200K .......... .......... .......... .......... .......... 67% 43.0M 10s 343250K .......... .......... .......... .......... .......... 67% 34.6M 10s 343300K .......... .......... .......... .......... .......... 67% 31.8M 10s 343350K .......... .......... .......... .......... .......... 67% 35.1M 10s 343400K .......... .......... .......... .......... .......... 67% 93.9M 10s 343450K .......... .......... .......... .......... .......... 67% 106M 10s 343500K .......... .......... .......... .......... .......... 67% 29.4M 10s 343550K .......... .......... .......... .......... .......... 67% 53.8M 10s 343600K .......... .......... .......... .......... .......... 67% 24.6M 10s 343650K .......... .......... .......... .......... .......... 67% 31.3M 10s 343700K .......... .......... .......... .......... .......... 67% 28.4M 10s 343750K .......... .......... .......... .......... .......... 67% 28.7M 10s 343800K .......... .......... .......... .......... .......... 67% 33.4M 10s 343850K .......... .......... .......... .......... .......... 67% 27.9M 10s 343900K .......... .......... .......... .......... .......... 67% 23.2M 10s 343950K .......... .......... .......... .......... .......... 67% 19.3M 10s 344000K .......... .......... .......... .......... .......... 67% 53.4M 10s 344050K .......... .......... .......... .......... .......... 67% 23.9M 10s 344100K .......... .......... .......... .......... .......... 67% 24.9M 10s 344150K .......... .......... .......... .......... .......... 67% 28.4M 10s 344200K .......... .......... .......... .......... .......... 67% 23.4M 10s 344250K .......... .......... .......... .......... .......... 67% 26.7M 10s 344300K .......... .......... .......... .......... .......... 67% 30.7M 10s 344350K .......... .......... .......... .......... .......... 67% 24.0M 10s 344400K .......... .......... .......... .......... .......... 67% 28.3M 10s 344450K .......... .......... .......... .......... .......... 67% 23.7M 10s 344500K .......... .......... .......... .......... .......... 67% 31.8M 10s 344550K .......... .......... .......... .......... .......... 67% 34.3M 10s 344600K .......... .......... .......... .......... .......... 67% 20.7M 10s 344650K .......... .......... .......... .......... .......... 67% 41.1M 10s 344700K .......... .......... .......... .......... .......... 67% 22.0M 10s 344750K .......... .......... .......... .......... .......... 67% 23.3M 10s 344800K .......... .......... .......... .......... .......... 67% 25.5M 10s 344850K .......... .......... .......... .......... .......... 67% 29.8M 10s 344900K .......... .......... .......... .......... .......... 67% 34.6M 10s 344950K .......... .......... .......... .......... .......... 67% 17.7M 10s 345000K .......... .......... .......... .......... .......... 67% 31.0M 10s 345050K .......... .......... .......... .......... .......... 67% 63.3M 10s 345100K .......... .......... .......... .......... .......... 67% 30.3M 10s 345150K .......... .......... .......... .......... .......... 67% 24.7M 10s 345200K .......... .......... .......... .......... .......... 67% 23.5M 10s 345250K .......... .......... .......... .......... .......... 67% 23.5M 10s 345300K .......... .......... .......... .......... .......... 67% 24.0M 10s 345350K .......... .......... .......... .......... .......... 67% 22.5M 10s 345400K .......... .......... .......... .......... .......... 67% 26.5M 10s 345450K .......... .......... .......... .......... .......... 67% 23.4M 10s 345500K .......... .......... .......... .......... .......... 67% 23.7M 10s 345550K .......... .......... .......... .......... .......... 67% 24.0M 10s 345600K .......... .......... .......... .......... .......... 67% 22.0M 10s 345650K .......... .......... .......... .......... .......... 67% 27.2M 10s 345700K .......... .......... .......... .......... .......... 67% 23.1M 10s 345750K .......... .......... .......... .......... .......... 67% 26.9M 10s 345800K .......... .......... .......... .......... .......... 67% 23.5M 10s 345850K .......... .......... .......... .......... .......... 67% 28.8M 10s 345900K .......... .......... .......... .......... .......... 67% 22.4M 10s 345950K .......... .......... .......... .......... .......... 67% 34.6M 10s 346000K .......... .......... .......... .......... .......... 67% 14.7M 10s 346050K .......... .......... .......... .......... .......... 67% 65.7M 10s 346100K .......... .......... .......... .......... .......... 67% 32.5M 10s 346150K .......... .......... .......... .......... .......... 67% 23.7M 10s 346200K .......... .......... .......... .......... .......... 67% 465M 10s 346250K .......... .......... .......... .......... .......... 67% 31.6M 10s 346300K .......... .......... .......... .......... .......... 67% 25.6M 10s 346350K .......... .......... .......... .......... .......... 67% 22.4M 10s 346400K .......... .......... .......... .......... .......... 67% 31.5M 10s 346450K .......... .......... .......... .......... .......... 67% 23.4M 10s 346500K .......... .......... .......... .......... .......... 67% 31.2M 10s 346550K .......... .......... .......... .......... .......... 67% 25.1M 10s 346600K .......... .......... .......... .......... .......... 67% 30.0M 10s 346650K .......... .......... .......... .......... .......... 68% 19.4M 10s 346700K .......... .......... .......... .......... .......... 68% 19.7M 10s 346750K .......... .......... .......... .......... .......... 68% 15.2M 10s 346800K .......... .......... .......... .......... .......... 68% 22.6M 10s 346850K .......... .......... .......... .......... .......... 68% 22.1M 10s 346900K .......... .......... .......... .......... .......... 68% 23.2M 10s 346950K .......... .......... .......... .......... .......... 68% 20.7M 10s 347000K .......... .......... .......... .......... .......... 68% 21.2M 10s 347050K .......... .......... .......... .......... .......... 68% 27.4M 10s 347100K .......... .......... .......... .......... .......... 68% 21.5M 10s 347150K .......... .......... .......... .......... .......... 68% 19.7M 10s 347200K .......... .......... .......... .......... .......... 68% 22.1M 10s 347250K .......... .......... .......... .......... .......... 68% 16.4M 10s 347300K .......... .......... .......... .......... .......... 68% 18.7M 10s 347350K .......... .......... .......... .......... .......... 68% 9.07M 10s 347400K .......... .......... .......... .......... .......... 68% 4.53M 10s 347450K .......... .......... .......... .......... .......... 68% 11.6M 10s 347500K .......... .......... .......... .......... .......... 68% 16.3M 10s 347550K .......... .......... .......... .......... .......... 68% 17.1M 10s 347600K .......... .......... .......... .......... .......... 68% 14.6M 10s 347650K .......... .......... .......... .......... .......... 68% 12.3M 10s 347700K .......... .......... .......... .......... .......... 68% 15.8M 10s 347750K .......... .......... .......... .......... .......... 68% 15.1M 10s 347800K .......... .......... .......... .......... .......... 68% 11.8M 10s 347850K .......... .......... .......... .......... .......... 68% 11.5M 10s 347900K .......... .......... .......... .......... .......... 68% 16.1M 10s 347950K .......... .......... .......... .......... .......... 68% 14.7M 10s 348000K .......... .......... .......... .......... .......... 68% 12.2M 10s 348050K .......... .......... .......... .......... .......... 68% 9.79M 10s 348100K .......... .......... .......... .......... .......... 68% 5.64M 10s 348150K .......... .......... .......... .......... .......... 68% 176M 10s 348200K .......... .......... .......... .......... .......... 68% 14.6M 10s 348250K .......... .......... .......... .......... .......... 68% 15.2M 10s 348300K .......... .......... .......... .......... .......... 68% 14.7M 10s 348350K .......... .......... .......... .......... .......... 68% 16.4M 10s 348400K .......... .......... .......... .......... .......... 68% 16.5M 10s 348450K .......... .......... .......... .......... .......... 68% 20.8M 10s 348500K .......... .......... .......... .......... .......... 68% 14.1M 10s 348550K .......... .......... .......... .......... .......... 68% 14.0M 10s 348600K .......... .......... .......... .......... .......... 68% 15.8M 10s 348650K .......... .......... .......... .......... .......... 68% 18.1M 10s 348700K .......... .......... .......... .......... .......... 68% 15.2M 10s 348750K .......... .......... .......... .......... .......... 68% 17.2M 10s 348800K .......... .......... .......... .......... .......... 68% 18.0M 10s 348850K .......... .......... .......... .......... .......... 68% 15.8M 10s 348900K .......... .......... .......... .......... .......... 68% 24.1M 10s 348950K .......... .......... .......... .......... .......... 68% 23.0M 10s 349000K .......... .......... .......... .......... .......... 68% 28.8M 10s 349050K .......... .......... .......... .......... .......... 68% 47.8M 10s 349100K .......... .......... .......... .......... .......... 68% 47.3M 10s 349150K .......... .......... .......... .......... .......... 68% 46.5M 10s 349200K .......... .......... .......... .......... .......... 68% 25.4M 10s 349250K .......... .......... .......... .......... .......... 68% 27.1M 10s 349300K .......... .......... .......... .......... .......... 68% 34.0M 10s 349350K .......... .......... .......... .......... .......... 68% 23.1M 10s 349400K .......... .......... .......... .......... .......... 68% 37.1M 10s 349450K .......... .......... .......... .......... .......... 68% 27.3M 10s 349500K .......... .......... .......... .......... .......... 68% 31.1M 10s 349550K .......... .......... .......... .......... .......... 68% 35.1M 10s 349600K .......... .......... .......... .......... .......... 68% 33.4M 10s 349650K .......... .......... .......... .......... .......... 68% 23.3M 10s 349700K .......... .......... .......... .......... .......... 68% 37.6M 10s 349750K .......... .......... .......... .......... .......... 68% 25.5M 10s 349800K .......... .......... .......... .......... .......... 68% 37.4M 10s 349850K .......... .......... .......... .......... .......... 68% 21.2M 10s 349900K .......... .......... .......... .......... .......... 68% 45.9M 10s 349950K .......... .......... .......... .......... .......... 68% 27.0M 10s 350000K .......... .......... .......... .......... .......... 68% 33.9M 10s 350050K .......... .......... .......... .......... .......... 68% 25.3M 10s 350100K .......... .......... .......... .......... .......... 68% 38.8M 10s 350150K .......... .......... .......... .......... .......... 68% 28.6M 10s 350200K .......... .......... .......... .......... .......... 68% 43.8M 10s 350250K .......... .......... .......... .......... .......... 68% 27.2M 10s 350300K .......... .......... .......... .......... .......... 68% 124M 10s 350350K .......... .......... .......... .......... .......... 68% 41.8M 10s 350400K .......... .......... .......... .......... .......... 68% 17.9M 10s 350450K .......... .......... .......... .......... .......... 68% 210M 10s 350500K .......... .......... .......... .......... .......... 68% 25.1M 10s 350550K .......... .......... .......... .......... .......... 68% 407M 10s 350600K .......... .......... .......... .......... .......... 68% 16.6M 10s 350650K .......... .......... .......... .......... .......... 68% 514M 10s 350700K .......... .......... .......... .......... .......... 68% 27.5M 10s 350750K .......... .......... .......... .......... .......... 68% 28.5M 10s 350800K .......... .......... .......... .......... .......... 68% 38.5M 10s 350850K .......... .......... .......... .......... .......... 68% 24.6M 10s 350900K .......... .......... .......... .......... .......... 68% 23.1M 10s 350950K .......... .......... .......... .......... .......... 68% 23.9M 10s 351000K .......... .......... .......... .......... .......... 68% 38.3M 10s 351050K .......... .......... .......... .......... .......... 68% 27.0M 10s 351100K .......... .......... .......... .......... .......... 68% 23.2M 10s 351150K .......... .......... .......... .......... .......... 68% 31.1M 10s 351200K .......... .......... .......... .......... .......... 68% 29.4M 10s 351250K .......... .......... .......... .......... .......... 68% 29.0M 10s 351300K .......... .......... .......... .......... .......... 68% 25.2M 10s 351350K .......... .......... .......... .......... .......... 68% 30.9M 10s 351400K .......... .......... .......... .......... .......... 68% 41.8M 10s 351450K .......... .......... .......... .......... .......... 68% 27.5M 10s 351500K .......... .......... .......... .......... .......... 68% 27.3M 10s 351550K .......... .......... .......... .......... .......... 68% 19.6M 10s 351600K .......... .......... .......... .......... .......... 68% 26.2M 10s 351650K .......... .......... .......... .......... .......... 68% 22.6M 10s 351700K .......... .......... .......... .......... .......... 68% 18.4M 10s 351750K .......... .......... .......... .......... .......... 69% 26.7M 10s 351800K .......... .......... .......... .......... .......... 69% 25.4M 10s 351850K .......... .......... .......... .......... .......... 69% 18.3M 10s 351900K .......... .......... .......... .......... .......... 69% 75.5M 10s 351950K .......... .......... .......... .......... .......... 69% 18.2M 10s 352000K .......... .......... .......... .......... .......... 69% 30.9M 10s 352050K .......... .......... .......... .......... .......... 69% 34.3M 10s 352100K .......... .......... .......... .......... .......... 69% 18.4M 10s 352150K .......... .......... .......... .......... .......... 69% 32.3M 10s 352200K .......... .......... .......... .......... .......... 69% 21.1M 10s 352250K .......... .......... .......... .......... .......... 69% 19.1M 10s 352300K .......... .......... .......... .......... .......... 69% 47.6M 10s 352350K .......... .......... .......... .......... .......... 69% 29.2M 10s 352400K .......... .......... .......... .......... .......... 69% 26.4M 10s 352450K .......... .......... .......... .......... .......... 69% 26.6M 10s 352500K .......... .......... .......... .......... .......... 69% 22.2M 10s 352550K .......... .......... .......... .......... .......... 69% 31.7M 10s 352600K .......... .......... .......... .......... .......... 69% 20.3M 10s 352650K .......... .......... .......... .......... .......... 69% 26.9M 10s 352700K .......... .......... .......... .......... .......... 69% 26.8M 10s 352750K .......... .......... .......... .......... .......... 69% 21.2M 10s 352800K .......... .......... .......... .......... .......... 69% 41.2M 10s 352850K .......... .......... .......... .......... .......... 69% 25.5M 10s 352900K .......... .......... .......... .......... .......... 69% 28.5M 10s 352950K .......... .......... .......... .......... .......... 69% 28.8M 10s 353000K .......... .......... .......... .......... .......... 69% 28.9M 10s 353050K .......... .......... .......... .......... .......... 69% 33.4M 10s 353100K .......... .......... .......... .......... .......... 69% 23.9M 10s 353150K .......... .......... .......... .......... .......... 69% 40.8M 10s 353200K .......... .......... .......... .......... .......... 69% 27.4M 10s 353250K .......... .......... .......... .......... .......... 69% 38.2M 10s 353300K .......... .......... .......... .......... .......... 69% 60.5M 10s 353350K .......... .......... .......... .......... .......... 69% 53.4M 10s 353400K .......... .......... .......... .......... .......... 69% 74.8M 10s 353450K .......... .......... .......... .......... .......... 69% 53.5M 10s 353500K .......... .......... .......... .......... .......... 69% 22.3M 10s 353550K .......... .......... .......... .......... .......... 69% 379M 10s 353600K .......... .......... .......... .......... .......... 69% 72.7M 10s 353650K .......... .......... .......... .......... .......... 69% 391M 10s 353700K .......... .......... .......... .......... .......... 69% 34.3M 10s 353750K .......... .......... .......... .......... .......... 69% 168M 10s 353800K .......... .......... .......... .......... .......... 69% 42.3M 10s 353850K .......... .......... .......... .......... .......... 69% 57.7M 10s 353900K .......... .......... .......... .......... .......... 69% 47.2M 10s 353950K .......... .......... .......... .......... .......... 69% 46.1M 10s 354000K .......... .......... .......... .......... .......... 69% 37.5M 10s 354050K .......... .......... .......... .......... .......... 69% 52.0M 10s 354100K .......... .......... .......... .......... .......... 69% 40.8M 9s 354150K .......... .......... .......... .......... .......... 69% 36.8M 9s 354200K .......... .......... .......... .......... .......... 69% 38.4M 9s 354250K .......... .......... .......... .......... .......... 69% 46.9M 9s 354300K .......... .......... .......... .......... .......... 69% 47.5M 9s 354350K .......... .......... .......... .......... .......... 69% 38.0M 9s 354400K .......... .......... .......... .......... .......... 69% 46.5M 9s 354450K .......... .......... .......... .......... .......... 69% 28.4M 9s 354500K .......... .......... .......... .......... .......... 69% 55.8M 9s 354550K .......... .......... .......... .......... .......... 69% 37.9M 9s 354600K .......... .......... .......... .......... .......... 69% 37.5M 9s 354650K .......... .......... .......... .......... .......... 69% 53.8M 9s 354700K .......... .......... .......... .......... .......... 69% 34.1M 9s 354750K .......... .......... .......... .......... .......... 69% 38.6M 9s 354800K .......... .......... .......... .......... .......... 69% 42.6M 9s 354850K .......... .......... .......... .......... .......... 69% 27.3M 9s 354900K .......... .......... .......... .......... .......... 69% 62.0M 9s 354950K .......... .......... .......... .......... .......... 69% 42.2M 9s 355000K .......... .......... .......... .......... .......... 69% 53.3M 9s 355050K .......... .......... .......... .......... .......... 69% 42.7M 9s 355100K .......... .......... .......... .......... .......... 69% 34.6M 9s 355150K .......... .......... .......... .......... .......... 69% 34.3M 9s 355200K .......... .......... .......... .......... .......... 69% 38.8M 9s 355250K .......... .......... .......... .......... .......... 69% 41.1M 9s 355300K .......... .......... .......... .......... .......... 69% 37.0M 9s 355350K .......... .......... .......... .......... .......... 69% 94.6M 9s 355400K .......... .......... .......... .......... .......... 69% 29.1M 9s 355450K .......... .......... .......... .......... .......... 69% 53.8M 9s 355500K .......... .......... .......... .......... .......... 69% 34.1M 9s 355550K .......... .......... .......... .......... .......... 69% 21.8M 9s 355600K .......... .......... .......... .......... .......... 69% 346M 9s 355650K .......... .......... .......... .......... .......... 69% 21.6M 9s 355700K .......... .......... .......... .......... .......... 69% 317M 9s 355750K .......... .......... .......... .......... .......... 69% 18.3M 9s 355800K .......... .......... .......... .......... .......... 69% 349M 9s 355850K .......... .......... .......... .......... .......... 69% 28.8M 9s 355900K .......... .......... .......... .......... .......... 69% 32.9M 9s 355950K .......... .......... .......... .......... .......... 69% 31.2M 9s 356000K .......... .......... .......... .......... .......... 69% 52.9M 9s 356050K .......... .......... .......... .......... .......... 69% 27.7M 9s 356100K .......... .......... .......... .......... .......... 69% 29.6M 9s 356150K .......... .......... .......... .......... .......... 69% 29.3M 9s 356200K .......... .......... .......... .......... .......... 69% 38.2M 9s 356250K .......... .......... .......... .......... .......... 69% 37.3M 9s 356300K .......... .......... .......... .......... .......... 69% 31.4M 9s 356350K .......... .......... .......... .......... .......... 69% 27.1M 9s 356400K .......... .......... .......... .......... .......... 69% 41.7M 9s 356450K .......... .......... .......... .......... .......... 69% 24.8M 9s 356500K .......... .......... .......... .......... .......... 69% 37.2M 9s 356550K .......... .......... .......... .......... .......... 69% 23.7M 9s 356600K .......... .......... .......... .......... .......... 69% 27.0M 9s 356650K .......... .......... .......... .......... .......... 69% 37.6M 9s 356700K .......... .......... .......... .......... .......... 69% 24.8M 9s 356750K .......... .......... .......... .......... .......... 69% 38.7M 9s 356800K .......... .......... .......... .......... .......... 69% 28.9M 9s 356850K .......... .......... .......... .......... .......... 70% 19.3M 9s 356900K .......... .......... .......... .......... .......... 70% 17.4M 9s 356950K .......... .......... .......... .......... .......... 70% 23.7M 9s 357000K .......... .......... .......... .......... .......... 70% 18.7M 9s 357050K .......... .......... .......... .......... .......... 70% 19.8M 9s 357100K .......... .......... .......... .......... .......... 70% 11.7M 9s 357150K .......... .......... .......... .......... .......... 70% 21.2M 9s 357200K .......... .......... .......... .......... .......... 70% 17.2M 9s 357250K .......... .......... .......... .......... .......... 70% 19.6M 9s 357300K .......... .......... .......... .......... .......... 70% 19.0M 9s 357350K .......... .......... .......... .......... .......... 70% 12.4M 9s 357400K .......... .......... .......... .......... .......... 70% 20.8M 9s 357450K .......... .......... .......... .......... .......... 70% 12.0M 9s 357500K .......... .......... .......... .......... .......... 70% 23.7M 9s 357550K .......... .......... .......... .......... .......... 70% 15.9M 9s 357600K .......... .......... .......... .......... .......... 70% 15.2M 9s 357650K .......... .......... .......... .......... .......... 70% 15.7M 9s 357700K .......... .......... .......... .......... .......... 70% 14.3M 9s 357750K .......... .......... .......... .......... .......... 70% 10.4M 9s 357800K .......... .......... .......... .......... .......... 70% 20.0M 9s 357850K .......... .......... .......... .......... .......... 70% 16.6M 9s 357900K .......... .......... .......... .......... .......... 70% 14.7M 9s 357950K .......... .......... .......... .......... .......... 70% 22.0M 9s 358000K .......... .......... .......... .......... .......... 70% 22.0M 9s 358050K .......... .......... .......... .......... .......... 70% 23.7M 9s 358100K .......... .......... .......... .......... .......... 70% 16.8M 9s 358150K .......... .......... .......... .......... .......... 70% 24.0M 9s 358200K .......... .......... .......... .......... .......... 70% 22.9M 9s 358250K .......... .......... .......... .......... .......... 70% 20.9M 9s 358300K .......... .......... .......... .......... .......... 70% 24.9M 9s 358350K .......... .......... .......... .......... .......... 70% 16.0M 9s 358400K .......... .......... .......... .......... .......... 70% 23.1M 9s 358450K .......... .......... .......... .......... .......... 70% 18.1M 9s 358500K .......... .......... .......... .......... .......... 70% 26.9M 9s 358550K .......... .......... .......... .......... .......... 70% 26.3M 9s 358600K .......... .......... .......... .......... .......... 70% 31.7M 9s 358650K .......... .......... .......... .......... .......... 70% 47.0M 9s 358700K .......... .......... .......... .......... .......... 70% 62.0M 9s 358750K .......... .......... .......... .......... .......... 70% 21.6M 9s 358800K .......... .......... .......... .......... .......... 70% 193M 9s 358850K .......... .......... .......... .......... .......... 70% 192M 9s 358900K .......... .......... .......... .......... .......... 70% 25.2M 9s 358950K .......... .......... .......... .......... .......... 70% 376M 9s 359000K .......... .......... .......... .......... .......... 70% 47.8M 9s 359050K .......... .......... .......... .......... .......... 70% 48.1M 9s 359100K .......... .......... .......... .......... .......... 70% 41.5M 9s 359150K .......... .......... .......... .......... .......... 70% 45.8M 9s 359200K .......... .......... .......... .......... .......... 70% 34.5M 9s 359250K .......... .......... .......... .......... .......... 70% 54.3M 9s 359300K .......... .......... .......... .......... .......... 70% 46.6M 9s 359350K .......... .......... .......... .......... .......... 70% 41.1M 9s 359400K .......... .......... .......... .......... .......... 70% 54.1M 9s 359450K .......... .......... .......... .......... .......... 70% 40.8M 9s 359500K .......... .......... .......... .......... .......... 70% 37.5M 9s 359550K .......... .......... .......... .......... .......... 70% 53.4M 9s 359600K .......... .......... .......... .......... .......... 70% 54.3M 9s 359650K .......... .......... .......... .......... .......... 70% 44.3M 9s 359700K .......... .......... .......... .......... .......... 70% 45.9M 9s 359750K .......... .......... .......... .......... .......... 70% 42.2M 9s 359800K .......... .......... .......... .......... .......... 70% 41.5M 9s 359850K .......... .......... .......... .......... .......... 70% 52.4M 9s 359900K .......... .......... .......... .......... .......... 70% 34.5M 9s 359950K .......... .......... .......... .......... .......... 70% 52.3M 9s 360000K .......... .......... .......... .......... .......... 70% 42.6M 9s 360050K .......... .......... .......... .......... .......... 70% 34.2M 9s 360100K .......... .......... .......... .......... .......... 70% 45.2M 9s 360150K .......... .......... .......... .......... .......... 70% 34.4M 9s 360200K .......... .......... .......... .......... .......... 70% 44.0M 9s 360250K .......... .......... .......... .......... .......... 70% 54.6M 9s 360300K .......... .......... .......... .......... .......... 70% 37.3M 9s 360350K .......... .......... .......... .......... .......... 70% 37.1M 9s 360400K .......... .......... .......... .......... .......... 70% 34.0M 9s 360450K .......... .......... .......... .......... .......... 70% 31.0M 9s 360500K .......... .......... .......... .......... .......... 70% 20.3M 9s 360550K .......... .......... .......... .......... .......... 70% 15.0M 9s 360600K .......... .......... .......... .......... .......... 70% 503M 9s 360650K .......... .......... .......... .......... .......... 70% 15.6M 9s 360700K .......... .......... .......... .......... .......... 70% 84.6M 9s 360750K .......... .......... .......... .......... .......... 70% 20.2M 9s 360800K .......... .......... .......... .......... .......... 70% 15.9M 9s 360850K .......... .......... .......... .......... .......... 70% 16.6M 9s 360900K .......... .......... .......... .......... .......... 70% 41.3M 9s 360950K .......... .......... .......... .......... .......... 70% 20.5M 9s 361000K .......... .......... .......... .......... .......... 70% 23.7M 9s 361050K .......... .......... .......... .......... .......... 70% 23.2M 9s 361100K .......... .......... .......... .......... .......... 70% 21.3M 9s 361150K .......... .......... .......... .......... .......... 70% 31.0M 9s 361200K .......... .......... .......... .......... .......... 70% 22.1M 9s 361250K .......... .......... .......... .......... .......... 70% 26.4M 9s 361300K .......... .......... .......... .......... .......... 70% 27.1M 9s 361350K .......... .......... .......... .......... .......... 70% 22.1M 9s 361400K .......... .......... .......... .......... .......... 70% 21.2M 9s 361450K .......... .......... .......... .......... .......... 70% 27.4M 9s 361500K .......... .......... .......... .......... .......... 70% 24.6M 9s 361550K .......... .......... .......... .......... .......... 70% 25.2M 9s 361600K .......... .......... .......... .......... .......... 70% 25.4M 9s 361650K .......... .......... .......... .......... .......... 70% 21.2M 9s 361700K .......... .......... .......... .......... .......... 70% 23.1M 9s 361750K .......... .......... .......... .......... .......... 70% 27.4M 9s 361800K .......... .......... .......... .......... .......... 70% 28.6M 9s 361850K .......... .......... .......... .......... .......... 70% 28.8M 9s 361900K .......... .......... .......... .......... .......... 70% 42.4M 9s 361950K .......... .......... .......... .......... .......... 71% 52.8M 9s 362000K .......... .......... .......... .......... .......... 71% 43.2M 9s 362050K .......... .......... .......... .......... .......... 71% 121M 9s 362100K .......... .......... .......... .......... .......... 71% 24.9M 9s 362150K .......... .......... .......... .......... .......... 71% 75.6M 9s 362200K .......... .......... .......... .......... .......... 71% 39.2M 9s 362250K .......... .......... .......... .......... .......... 71% 588M 9s 362300K .......... .......... .......... .......... .......... 71% 36.8M 9s 362350K .......... .......... .......... .......... .......... 71% 52.3M 9s 362400K .......... .......... .......... .......... .......... 71% 99.6M 9s 362450K .......... .......... .......... .......... .......... 71% 31.7M 9s 362500K .......... .......... .......... .......... .......... 71% 36.9M 9s 362550K .......... .......... .......... .......... .......... 71% 46.8M 9s 362600K .......... .......... .......... .......... .......... 71% 25.6M 9s 362650K .......... .......... .......... .......... .......... 71% 53.2M 9s 362700K .......... .......... .......... .......... .......... 71% 40.3M 9s 362750K .......... .......... .......... .......... .......... 71% 47.4M 9s 362800K .......... .......... .......... .......... .......... 71% 25.7M 9s 362850K .......... .......... .......... .......... .......... 71% 46.5M 9s 362900K .......... .......... .......... .......... .......... 71% 42.1M 9s 362950K .......... .......... .......... .......... .......... 71% 31.5M 9s 363000K .......... .......... .......... .......... .......... 71% 60.6M 9s 363050K .......... .......... .......... .......... .......... 71% 37.5M 9s 363100K .......... .......... .......... .......... .......... 71% 34.5M 9s 363150K .......... .......... .......... .......... .......... 71% 45.4M 9s 363200K .......... .......... .......... .......... .......... 71% 34.4M 9s 363250K .......... .......... .......... .......... .......... 71% 39.2M 9s 363300K .......... .......... .......... .......... .......... 71% 42.4M 9s 363350K .......... .......... .......... .......... .......... 71% 31.3M 9s 363400K .......... .......... .......... .......... .......... 71% 41.7M 9s 363450K .......... .......... .......... .......... .......... 71% 31.5M 9s 363500K .......... .......... .......... .......... .......... 71% 42.3M 9s 363550K .......... .......... .......... .......... .......... 71% 42.3M 9s 363600K .......... .......... .......... .......... .......... 71% 31.5M 9s 363650K .......... .......... .......... .......... .......... 71% 45.6M 9s 363700K .......... .......... .......... .......... .......... 71% 35.1M 9s 363750K .......... .......... .......... .......... .......... 71% 47.5M 9s 363800K .......... .......... .......... .......... .......... 71% 62.6M 9s 363850K .......... .......... .......... .......... .......... 71% 22.1M 9s 363900K .......... .......... .......... .......... .......... 71% 543M 9s 363950K .......... .......... .......... .......... .......... 71% 65.4M 9s 364000K .......... .......... .......... .......... .......... 71% 503M 9s 364050K .......... .......... .......... .......... .......... 71% 40.3M 9s 364100K .......... .......... .......... .......... .......... 71% 48.2M 9s 364150K .......... .......... .......... .......... .......... 71% 54.4M 9s 364200K .......... .......... .......... .......... .......... 71% 93.7M 9s 364250K .......... .......... .......... .......... .......... 71% 98.6M 9s 364300K .......... .......... .......... .......... .......... 71% 37.2M 9s 364350K .......... .......... .......... .......... .......... 71% 47.6M 9s 364400K .......... .......... .......... .......... .......... 71% 36.2M 9s 364450K .......... .......... .......... .......... .......... 71% 21.6M 9s 364500K .......... .......... .......... .......... .......... 71% 509M 9s 364550K .......... .......... .......... .......... .......... 71% 30.1M 9s 364600K .......... .......... .......... .......... .......... 71% 31.0M 9s 364650K .......... .......... .......... .......... .......... 71% 37.8M 9s 364700K .......... .......... .......... .......... .......... 71% 30.9M 9s 364750K .......... .......... .......... .......... .......... 71% 45.1M 9s 364800K .......... .......... .......... .......... .......... 71% 26.8M 9s 364850K .......... .......... .......... .......... .......... 71% 41.0M 9s 364900K .......... .......... .......... .......... .......... 71% 42.3M 9s 364950K .......... .......... .......... .......... .......... 71% 30.4M 9s 365000K .......... .......... .......... .......... .......... 71% 38.3M 9s 365050K .......... .......... .......... .......... .......... 71% 48.3M 9s 365100K .......... .......... .......... .......... .......... 71% 31.3M 9s 365150K .......... .......... .......... .......... .......... 71% 46.1M 9s 365200K .......... .......... .......... .......... .......... 71% 38.4M 9s 365250K .......... .......... .......... .......... .......... 71% 31.4M 9s 365300K .......... .......... .......... .......... .......... 71% 34.3M 9s 365350K .......... .......... .......... .......... .......... 71% 28.7M 9s 365400K .......... .......... .......... .......... .......... 71% 42.2M 9s 365450K .......... .......... .......... .......... .......... 71% 19.8M 9s 365500K .......... .......... .......... .......... .......... 71% 17.8M 9s 365550K .......... .......... .......... .......... .......... 71% 15.0M 9s 365600K .......... .......... .......... .......... .......... 71% 14.6M 9s 365650K .......... .......... .......... .......... .......... 71% 15.8M 9s 365700K .......... .......... .......... .......... .......... 71% 84.3M 9s 365750K .......... .......... .......... .......... .......... 71% 20.2M 9s 365800K .......... .......... .......... .......... .......... 71% 19.7M 9s 365850K .......... .......... .......... .......... .......... 71% 23.1M 9s 365900K .......... .......... .......... .......... .......... 71% 54.1M 9s 365950K .......... .......... .......... .......... .......... 71% 17.8M 9s 366000K .......... .......... .......... .......... .......... 71% 25.1M 9s 366050K .......... .......... .......... .......... .......... 71% 25.5M 9s 366100K .......... .......... .......... .......... .......... 71% 16.8M 9s 366150K .......... .......... .......... .......... .......... 71% 22.5M 9s 366200K .......... .......... .......... .......... .......... 71% 17.6M 9s 366250K .......... .......... .......... .......... .......... 71% 16.6M 9s 366300K .......... .......... .......... .......... .......... 71% 22.6M 9s 366350K .......... .......... .......... .......... .......... 71% 17.4M 9s 366400K .......... .......... .......... .......... .......... 71% 15.5M 9s 366450K .......... .......... .......... .......... .......... 71% 15.0M 9s 366500K .......... .......... .......... .......... .......... 71% 19.1M 9s 366550K .......... .......... .......... .......... .......... 71% 15.8M 9s 366600K .......... .......... .......... .......... .......... 71% 12.7M 9s 366650K .......... .......... .......... .......... .......... 71% 17.9M 9s 366700K .......... .......... .......... .......... .......... 71% 14.1M 9s 366750K .......... .......... .......... .......... .......... 71% 17.3M 9s 366800K .......... .......... .......... .......... .......... 71% 16.4M 9s 366850K .......... .......... .......... .......... .......... 71% 16.0M 9s 366900K .......... .......... .......... .......... .......... 71% 15.8M 9s 366950K .......... .......... .......... .......... .......... 71% 13.0M 9s 367000K .......... .......... .......... .......... .......... 71% 24.6M 9s 367050K .......... .......... .......... .......... .......... 72% 36.0M 9s 367100K .......... .......... .......... .......... .......... 72% 42.8M 9s 367150K .......... .......... .......... .......... .......... 72% 75.5M 9s 367200K .......... .......... .......... .......... .......... 72% 46.7M 9s 367250K .......... .......... .......... .......... .......... 72% 37.8M 9s 367300K .......... .......... .......... .......... .......... 72% 24.5M 9s 367350K .......... .......... .......... .......... .......... 72% 328M 9s 367400K .......... .......... .......... .......... .......... 72% 26.4M 9s 367450K .......... .......... .......... .......... .......... 72% 16.5M 9s 367500K .......... .......... .......... .......... .......... 72% 53.5M 9s 367550K .......... .......... .......... .......... .......... 72% 20.7M 9s 367600K .......... .......... .......... .......... .......... 72% 23.8M 9s 367650K .......... .......... .......... .......... .......... 72% 20.7M 9s 367700K .......... .......... .......... .......... .......... 72% 19.1M 9s 367750K .......... .......... .......... .......... .......... 72% 21.6M 9s 367800K .......... .......... .......... .......... .......... 72% 19.0M 9s 367850K .......... .......... .......... .......... .......... 72% 23.5M 9s 367900K .......... .......... .......... .......... .......... 72% 24.9M 9s 367950K .......... .......... .......... .......... .......... 72% 12.7M 9s 368000K .......... .......... .......... .......... .......... 72% 23.6M 9s 368050K .......... .......... .......... .......... .......... 72% 29.2M 9s 368100K .......... .......... .......... .......... .......... 72% 20.1M 8s 368150K .......... .......... .......... .......... .......... 72% 26.5M 8s 368200K .......... .......... .......... .......... .......... 72% 17.5M 8s 368250K .......... .......... .......... .......... .......... 72% 26.4M 8s 368300K .......... .......... .......... .......... .......... 72% 51.8M 8s 368350K .......... .......... .......... .......... .......... 72% 47.7M 8s 368400K .......... .......... .......... .......... .......... 72% 31.3M 8s 368450K .......... .......... .......... .......... .......... 72% 44.2M 8s 368500K .......... .......... .......... .......... .......... 72% 18.6M 8s 368550K .......... .......... .......... .......... .......... 72% 379M 8s 368600K .......... .......... .......... .......... .......... 72% 229M 8s 368650K .......... .......... .......... .......... .......... 72% 22.3M 8s 368700K .......... .......... .......... .......... .......... 72% 106M 8s 368750K .......... .......... .......... .......... .......... 72% 25.9M 8s 368800K .......... .......... .......... .......... .......... 72% 71.1M 8s 368850K .......... .......... .......... .......... .......... 72% 25.4M 8s 368900K .......... .......... .......... .......... .......... 72% 34.4M 8s 368950K .......... .......... .......... .......... .......... 72% 33.7M 8s 369000K .......... .......... .......... .......... .......... 72% 29.3M 8s 369050K .......... .......... .......... .......... .......... 72% 33.5M 8s 369100K .......... .......... .......... .......... .......... 72% 24.2M 8s 369150K .......... .......... .......... .......... .......... 72% 41.8M 8s 369200K .......... .......... .......... .......... .......... 72% 27.0M 8s 369250K .......... .......... .......... .......... .......... 72% 34.3M 8s 369300K .......... .......... .......... .......... .......... 72% 36.5M 8s 369350K .......... .......... .......... .......... .......... 72% 25.7M 8s 369400K .......... .......... .......... .......... .......... 72% 42.7M 8s 369450K .......... .......... .......... .......... .......... 72% 26.6M 8s 369500K .......... .......... .......... .......... .......... 72% 34.0M 8s 369550K .......... .......... .......... .......... .......... 72% 33.8M 8s 369600K .......... .......... .......... .......... .......... 72% 28.8M 8s 369650K .......... .......... .......... .......... .......... 72% 37.5M 8s 369700K .......... .......... .......... .......... .......... 72% 31.3M 8s 369750K .......... .......... .......... .......... .......... 72% 39.3M 8s 369800K .......... .......... .......... .......... .......... 72% 30.6M 8s 369850K .......... .......... .......... .......... .......... 72% 29.0M 8s 369900K .......... .......... .......... .......... .......... 72% 47.7M 8s 369950K .......... .......... .......... .......... .......... 72% 42.3M 8s 370000K .......... .......... .......... .......... .......... 72% 85.8M 8s 370050K .......... .......... .......... .......... .......... 72% 73.6M 8s 370100K .......... .......... .......... .......... .......... 72% 65.3M 8s 370150K .......... .......... .......... .......... .......... 72% 126M 8s 370200K .......... .......... .......... .......... .......... 72% 65.3M 8s 370250K .......... .......... .......... .......... .......... 72% 89.1M 8s 370300K .......... .......... .......... .......... .......... 72% 34.9M 8s 370350K .......... .......... .......... .......... .......... 72% 65.6M 8s 370400K .......... .......... .......... .......... .......... 72% 543M 8s 370450K .......... .......... .......... .......... .......... 72% 311M 8s 370500K .......... .......... .......... .......... .......... 72% 98.0M 8s 370550K .......... .......... .......... .......... .......... 72% 39.9M 8s 370600K .......... .......... .......... .......... .......... 72% 154M 8s 370650K .......... .......... .......... .......... .......... 72% 298M 8s 370700K .......... .......... .......... .......... .......... 72% 68.2M 8s 370750K .......... .......... .......... .......... .......... 72% 63.6M 8s 370800K .......... .......... .......... .......... .......... 72% 94.4M 8s 370850K .......... .......... .......... .......... .......... 72% 19.6M 8s 370900K .......... .......... .......... .......... .......... 72% 61.3M 8s 370950K .......... .......... .......... .......... .......... 72% 64.0M 8s 371000K .......... .......... .......... .......... .......... 72% 75.1M 8s 371050K .......... .......... .......... .......... .......... 72% 74.7M 8s 371100K .......... .......... .......... .......... .......... 72% 72.4M 8s 371150K .......... .......... .......... .......... .......... 72% 75.0M 8s 371200K .......... .......... .......... .......... .......... 72% 60.7M 8s 371250K .......... .......... .......... .......... .......... 72% 95.4M 8s 371300K .......... .......... .......... .......... .......... 72% 71.6M 8s 371350K .......... .......... .......... .......... .......... 72% 61.8M 8s 371400K .......... .......... .......... .......... .......... 72% 61.0M 8s 371450K .......... .......... .......... .......... .......... 72% 72.9M 8s 371500K .......... .......... .......... .......... .......... 72% 74.2M 8s 371550K .......... .......... .......... .......... .......... 72% 76.1M 8s 371600K .......... .......... .......... .......... .......... 72% 67.2M 8s 371650K .......... .......... .......... .......... .......... 72% 79.9M 8s 371700K .......... .......... .......... .......... .......... 72% 63.8M 8s 371750K .......... .......... .......... .......... .......... 72% 61.1M 8s 371800K .......... .......... .......... .......... .......... 72% 78.1M 8s 371850K .......... .......... .......... .......... .......... 72% 97.1M 8s 371900K .......... .......... .......... .......... .......... 72% 74.5M 8s 371950K .......... .......... .......... .......... .......... 72% 52.7M 8s 372000K .......... .......... .......... .......... .......... 72% 74.4M 8s 372050K .......... .......... .......... .......... .......... 72% 109M 8s 372100K .......... .......... .......... .......... .......... 72% 54.9M 8s 372150K .......... .......... .......... .......... .......... 73% 95.2M 8s 372200K .......... .......... .......... .......... .......... 73% 62.3M 8s 372250K .......... .......... .......... .......... .......... 73% 95.7M 8s 372300K .......... .......... .......... .......... .......... 73% 72.1M 8s 372350K .......... .......... .......... .......... .......... 73% 64.6M 8s 372400K .......... .......... .......... .......... .......... 73% 74.7M 8s 372450K .......... .......... .......... .......... .......... 73% 74.1M 8s 372500K .......... .......... .......... .......... .......... 73% 63.2M 8s 372550K .......... .......... .......... .......... .......... 73% 92.1M 8s 372600K .......... .......... .......... .......... .......... 73% 54.0M 8s 372650K .......... .......... .......... .......... .......... 73% 63.9M 8s 372700K .......... .......... .......... .......... .......... 73% 86.4M 8s 372750K .......... .......... .......... .......... .......... 73% 60.0M 8s 372800K .......... .......... .......... .......... .......... 73% 75.4M 8s 372850K .......... .......... .......... .......... .......... 73% 73.3M 8s 372900K .......... .......... .......... .......... .......... 73% 74.1M 8s 372950K .......... .......... .......... .......... .......... 73% 73.9M 8s 373000K .......... .......... .......... .......... .......... 73% 72.6M 8s 373050K .......... .......... .......... .......... .......... 73% 75.4M 8s 373100K .......... .......... .......... .......... .......... 73% 41.5M 8s 373150K .......... .......... .......... .......... .......... 73% 200M 8s 373200K .......... .......... .......... .......... .......... 73% 19.8M 8s 373250K .......... .......... .......... .......... .......... 73% 474M 8s 373300K .......... .......... .......... .......... .......... 73% 474M 8s 373350K .......... .......... .......... .......... .......... 73% 432M 8s 373400K .......... .......... .......... .......... .......... 73% 102M 8s 373450K .......... .......... .......... .......... .......... 73% 38.2M 8s 373500K .......... .......... .......... .......... .......... 73% 177M 8s 373550K .......... .......... .......... .......... .......... 73% 73.4M 8s 373600K .......... .......... .......... .......... .......... 73% 48.5M 8s 373650K .......... .......... .......... .......... .......... 73% 90.6M 8s 373700K .......... .......... .......... .......... .......... 73% 61.0M 8s 373750K .......... .......... .......... .......... .......... 73% 21.2M 8s 373800K .......... .......... .......... .......... .......... 73% 174M 8s 373850K .......... .......... .......... .......... .......... 73% 62.5M 8s 373900K .......... .......... .......... .......... .......... 73% 148M 8s 373950K .......... .......... .......... .......... .......... 73% 45.8M 8s 374000K .......... .......... .......... .......... .......... 73% 224M 8s 374050K .......... .......... .......... .......... .......... 73% 72.9M 8s 374100K .......... .......... .......... .......... .......... 73% 139M 8s 374150K .......... .......... .......... .......... .......... 73% 132M 8s 374200K .......... .......... .......... .......... .......... 73% 41.8M 8s 374250K .......... .......... .......... .......... .......... 73% 73.8M 8s 374300K .......... .......... .......... .......... .......... 73% 26.2M 8s 374350K .......... .......... .......... .......... .......... 73% 26.8M 8s 374400K .......... .......... .......... .......... .......... 73% 61.9M 8s 374450K .......... .......... .......... .......... .......... 73% 54.9M 8s 374500K .......... .......... .......... .......... .......... 73% 48.5M 8s 374550K .......... .......... .......... .......... .......... 73% 46.4M 8s 374600K .......... .......... .......... .......... .......... 73% 45.1M 8s 374650K .......... .......... .......... .......... .......... 73% 63.7M 8s 374700K .......... .......... .......... .......... .......... 73% 42.5M 8s 374750K .......... .......... .......... .......... .......... 73% 92.7M 8s 374800K .......... .......... .......... .......... .......... 73% 56.1M 8s 374850K .......... .......... .......... .......... .......... 73% 35.1M 8s 374900K .......... .......... .......... .......... .......... 73% 120M 8s 374950K .......... .......... .......... .......... .......... 73% 39.8M 8s 375000K .......... .......... .......... .......... .......... 73% 48.5M 8s 375050K .......... .......... .......... .......... .......... 73% 62.7M 8s 375100K .......... .......... .......... .......... .......... 73% 47.5M 8s 375150K .......... .......... .......... .......... .......... 73% 54.4M 8s 375200K .......... .......... .......... .......... .......... 73% 35.3M 8s 375250K .......... .......... .......... .......... .......... 73% 54.8M 8s 375300K .......... .......... .......... .......... .......... 73% 62.4M 8s 375350K .......... .......... .......... .......... .......... 73% 54.4M 8s 375400K .......... .......... .......... .......... .......... 73% 54.9M 8s 375450K .......... .......... .......... .......... .......... 73% 54.0M 8s 375500K .......... .......... .......... .......... .......... 73% 59.8M 8s 375550K .......... .......... .......... .......... .......... 73% 52.1M 8s 375600K .......... .......... .......... .......... .......... 73% 42.3M 8s 375650K .......... .......... .......... .......... .......... 73% 46.6M 8s 375700K .......... .......... .......... .......... .......... 73% 48.5M 8s 375750K .......... .......... .......... .......... .......... 73% 54.1M 8s 375800K .......... .......... .......... .......... .......... 73% 50.4M 8s 375850K .......... .......... .......... .......... .......... 73% 31.6M 8s 375900K .......... .......... .......... .......... .......... 73% 45.6M 8s 375950K .......... .......... .......... .......... .......... 73% 36.9M 8s 376000K .......... .......... .......... .......... .......... 73% 26.3M 8s 376050K .......... .......... .......... .......... .......... 73% 264M 8s 376100K .......... .......... .......... .......... .......... 73% 24.5M 8s 376150K .......... .......... .......... .......... .......... 73% 157M 8s 376200K .......... .......... .......... .......... .......... 73% 41.2M 8s 376250K .......... .......... .......... .......... .......... 73% 58.7M 8s 376300K .......... .......... .......... .......... .......... 73% 42.1M 8s 376350K .......... .......... .......... .......... .......... 73% 47.1M 8s 376400K .......... .......... .......... .......... .......... 73% 45.4M 8s 376450K .......... .......... .......... .......... .......... 73% 40.5M 8s 376500K .......... .......... .......... .......... .......... 73% 48.1M 8s 376550K .......... .......... .......... .......... .......... 73% 44.9M 8s 376600K .......... .......... .......... .......... .......... 73% 47.5M 8s 376650K .......... .......... .......... .......... .......... 73% 46.7M 8s 376700K .......... .......... .......... .......... .......... 73% 53.1M 8s 376750K .......... .......... .......... .......... .......... 73% 60.9M 8s 376800K .......... .......... .......... .......... .......... 73% 46.9M 8s 376850K .......... .......... .......... .......... .......... 73% 48.2M 8s 376900K .......... .......... .......... .......... .......... 73% 55.7M 8s 376950K .......... .......... .......... .......... .......... 73% 38.9M 8s 377000K .......... .......... .......... .......... .......... 73% 53.8M 8s 377050K .......... .......... .......... .......... .......... 73% 63.1M 8s 377100K .......... .......... .......... .......... .......... 73% 33.7M 8s 377150K .......... .......... .......... .......... .......... 73% 52.3M 8s 377200K .......... .......... .......... .......... .......... 74% 45.7M 8s 377250K .......... .......... .......... .......... .......... 74% 60.1M 8s 377300K .......... .......... .......... .......... .......... 74% 51.6M 8s 377350K .......... .......... .......... .......... .......... 74% 48.0M 8s 377400K .......... .......... .......... .......... .......... 74% 53.5M 8s 377450K .......... .......... .......... .......... .......... 74% 46.1M 8s 377500K .......... .......... .......... .......... .......... 74% 46.2M 8s 377550K .......... .......... .......... .......... .......... 74% 53.8M 8s 377600K .......... .......... .......... .......... .......... 74% 46.2M 8s 377650K .......... .......... .......... .......... .......... 74% 60.7M 8s 377700K .......... .......... .......... .......... .......... 74% 45.4M 8s 377750K .......... .......... .......... .......... .......... 74% 62.3M 8s 377800K .......... .......... .......... .......... .......... 74% 35.2M 8s 377850K .......... .......... .......... .......... .......... 74% 61.0M 8s 377900K .......... .......... .......... .......... .......... 74% 52.6M 8s 377950K .......... .......... .......... .......... .......... 74% 75.4M 8s 378000K .......... .......... .......... .......... .......... 74% 57.4M 8s 378050K .......... .......... .......... .......... .......... 74% 62.0M 8s 378100K .......... .......... .......... .......... .......... 74% 60.9M 8s 378150K .......... .......... .......... .......... .......... 74% 121M 8s 378200K .......... .......... .......... .......... .......... 74% 17.8M 8s 378250K .......... .......... .......... .......... .......... 74% 483M 8s 378300K .......... .......... .......... .......... .......... 74% 503M 8s 378350K .......... .......... .......... .......... .......... 74% 498M 8s 378400K .......... .......... .......... .......... .......... 74% 581M 8s 378450K .......... .......... .......... .......... .......... 74% 30.9M 8s 378500K .......... .......... .......... .......... .......... 74% 100M 8s 378550K .......... .......... .......... .......... .......... 74% 498M 8s 378600K .......... .......... .......... .......... .......... 74% 25.3M 8s 378650K .......... .......... .......... .......... .......... 74% 407M 8s 378700K .......... .......... .......... .......... .......... 74% 131M 8s 378750K .......... .......... .......... .......... .......... 74% 60.7M 8s 378800K .......... .......... .......... .......... .......... 74% 50.9M 8s 378850K .......... .......... .......... .......... .......... 74% 51.2M 8s 378900K .......... .......... .......... .......... .......... 74% 60.4M 8s 378950K .......... .......... .......... .......... .......... 74% 45.3M 8s 379000K .......... .......... .......... .......... .......... 74% 64.2M 8s 379050K .......... .......... .......... .......... .......... 74% 46.9M 8s 379100K .......... .......... .......... .......... .......... 74% 52.6M 8s 379150K .......... .......... .......... .......... .......... 74% 73.9M 8s 379200K .......... .......... .......... .......... .......... 74% 42.1M 8s 379250K .......... .......... .......... .......... .......... 74% 60.1M 8s 379300K .......... .......... .......... .......... .......... 74% 86.7M 8s 379350K .......... .......... .......... .......... .......... 74% 51.3M 8s 379400K .......... .......... .......... .......... .......... 74% 60.5M 8s 379450K .......... .......... .......... .......... .......... 74% 47.3M 8s 379500K .......... .......... .......... .......... .......... 74% 47.5M 8s 379550K .......... .......... .......... .......... .......... 74% 60.8M 8s 379600K .......... .......... .......... .......... .......... 74% 53.5M 8s 379650K .......... .......... .......... .......... .......... 74% 61.0M 8s 379700K .......... .......... .......... .......... .......... 74% 46.7M 8s 379750K .......... .......... .......... .......... .......... 74% 63.0M 8s 379800K .......... .......... .......... .......... .......... 74% 60.4M 8s 379850K .......... .......... .......... .......... .......... 74% 45.5M 8s 379900K .......... .......... .......... .......... .......... 74% 73.1M 8s 379950K .......... .......... .......... .......... .......... 74% 44.2M 8s 380000K .......... .......... .......... .......... .......... 74% 61.1M 8s 380050K .......... .......... .......... .......... .......... 74% 62.7M 8s 380100K .......... .......... .......... .......... .......... 74% 41.1M 8s 380150K .......... .......... .......... .......... .......... 74% 53.2M 8s 380200K .......... .......... .......... .......... .......... 74% 63.1M 8s 380250K .......... .......... .......... .......... .......... 74% 48.1M 8s 380300K .......... .......... .......... .......... .......... 74% 55.4M 8s 380350K .......... .......... .......... .......... .......... 74% 46.6M 8s 380400K .......... .......... .......... .......... .......... 74% 62.2M 8s 380450K .......... .......... .......... .......... .......... 74% 48.1M 8s 380500K .......... .......... .......... .......... .......... 74% 49.5M 8s 380550K .......... .......... .......... .......... .......... 74% 120M 8s 380600K .......... .......... .......... .......... .......... 74% 37.4M 8s 380650K .......... .......... .......... .......... .......... 74% 63.0M 8s 380700K .......... .......... .......... .......... .......... 74% 61.8M 8s 380750K .......... .......... .......... .......... .......... 74% 97.7M 8s 380800K .......... .......... .......... .......... .......... 74% 15.6M 8s 380850K .......... .......... .......... .......... .......... 74% 270M 8s 380900K .......... .......... .......... .......... .......... 74% 57.8M 8s 380950K .......... .......... .......... .......... .......... 74% 367M 8s 381000K .......... .......... .......... .......... .......... 74% 36.2M 8s 381050K .......... .......... .......... .......... .......... 74% 59.3M 8s 381100K .......... .......... .......... .......... .......... 74% 146M 8s 381150K .......... .......... .......... .......... .......... 74% 109M 8s 381200K .......... .......... .......... .......... .......... 74% 39.3M 8s 381250K .......... .......... .......... .......... .......... 74% 549M 8s 381300K .......... .......... .......... .......... .......... 74% 53.1M 8s 381350K .......... .......... .......... .......... .......... 74% 50.0M 8s 381400K .......... .......... .......... .......... .......... 74% 104M 8s 381450K .......... .......... .......... .......... .......... 74% 30.3M 8s 381500K .......... .......... .......... .......... .......... 74% 46.3M 8s 381550K .......... .......... .......... .......... .......... 74% 45.7M 8s 381600K .......... .......... .......... .......... .......... 74% 31.0M 8s 381650K .......... .......... .......... .......... .......... 74% 57.2M 7s 381700K .......... .......... .......... .......... .......... 74% 29.5M 7s 381750K .......... .......... .......... .......... .......... 74% 40.4M 7s 381800K .......... .......... .......... .......... .......... 74% 46.1M 7s 381850K .......... .......... .......... .......... .......... 74% 31.8M 7s 381900K .......... .......... .......... .......... .......... 74% 52.1M 7s 381950K .......... .......... .......... .......... .......... 74% 53.4M 7s 382000K .......... .......... .......... .......... .......... 74% 30.9M 7s 382050K .......... .......... .......... .......... .......... 74% 61.1M 7s 382100K .......... .......... .......... .......... .......... 74% 33.9M 7s 382150K .......... .......... .......... .......... .......... 74% 42.3M 7s 382200K .......... .......... .......... .......... .......... 74% 41.2M 7s 382250K .......... .......... .......... .......... .......... 74% 45.4M 7s 382300K .......... .......... .......... .......... .......... 75% 38.3M 7s 382350K .......... .......... .......... .......... .......... 75% 36.1M 7s 382400K .......... .......... .......... .......... .......... 75% 41.6M 7s 382450K .......... .......... .......... .......... .......... 75% 34.5M 7s 382500K .......... .......... .......... .......... .......... 75% 53.2M 7s 382550K .......... .......... .......... .......... .......... 75% 50.8M 7s 382600K .......... .......... .......... .......... .......... 75% 41.0M 7s 382650K .......... .......... .......... .......... .......... 75% 46.8M 7s 382700K .......... .......... .......... .......... .......... 75% 33.5M 7s 382750K .......... .......... .......... .......... .......... 75% 41.0M 7s 382800K .......... .......... .......... .......... .......... 75% 46.3M 7s 382850K .......... .......... .......... .......... .......... 75% 42.6M 7s 382900K .......... .......... .......... .......... .......... 75% 128M 7s 382950K .......... .......... .......... .......... .......... 75% 30.7M 7s 383000K .......... .......... .......... .......... .......... 75% 78.4M 7s 383050K .......... .......... .......... .......... .......... 75% 47.3M 7s 383100K .......... .......... .......... .......... .......... 75% 40.9M 7s 383150K .......... .......... .......... .......... .......... 75% 116M 7s 383200K .......... .......... .......... .......... .......... 75% 16.2M 7s 383250K .......... .......... .......... .......... .......... 75% 509M 7s 383300K .......... .......... .......... .......... .......... 75% 19.2M 7s 383350K .......... .......... .......... .......... .......... 75% 294M 7s 383400K .......... .......... .......... .......... .......... 75% 27.6M 7s 383450K .......... .......... .......... .......... .......... 75% 107M 7s 383500K .......... .......... .......... .......... .......... 75% 22.2M 7s 383550K .......... .......... .......... .......... .......... 75% 194M 7s 383600K .......... .......... .......... .......... .......... 75% 37.5M 7s 383650K .......... .......... .......... .......... .......... 75% 24.0M 7s 383700K .......... .......... .......... .......... .......... 75% 31.7M 7s 383750K .......... .......... .......... .......... .......... 75% 25.3M 7s 383800K .......... .......... .......... .......... .......... 75% 40.1M 7s 383850K .......... .......... .......... .......... .......... 75% 33.5M 7s 383900K .......... .......... .......... .......... .......... 75% 24.0M 7s 383950K .......... .......... .......... .......... .......... 75% 23.7M 7s 384000K .......... .......... .......... .......... .......... 75% 41.0M 7s 384050K .......... .......... .......... .......... .......... 75% 37.4M 7s 384100K .......... .......... .......... .......... .......... 75% 20.6M 7s 384150K .......... .......... .......... .......... .......... 75% 48.3M 7s 384200K .......... .......... .......... .......... .......... 75% 22.4M 7s 384250K .......... .......... .......... .......... .......... 75% 59.3M 7s 384300K .......... .......... .......... .......... .......... 75% 33.7M 7s 384350K .......... .......... .......... .......... .......... 75% 16.5M 7s 384400K .......... .......... .......... .......... .......... 75% 43.4M 7s 384450K .......... .......... .......... .......... .......... 75% 21.0M 7s 384500K .......... .......... .......... .......... .......... 75% 32.0M 7s 384550K .......... .......... .......... .......... .......... 75% 44.9M 7s 384600K .......... .......... .......... .......... .......... 75% 30.3M 7s 384650K .......... .......... .......... .......... .......... 75% 40.7M 7s 384700K .......... .......... .......... .......... .......... 75% 34.8M 7s 384750K .......... .......... .......... .......... .......... 75% 45.0M 7s 384800K .......... .......... .......... .......... .......... 75% 25.1M 7s 384850K .......... .......... .......... .......... .......... 75% 26.7M 7s 384900K .......... .......... .......... .......... .......... 75% 404M 7s 384950K .......... .......... .......... .......... .......... 75% 19.8M 7s 385000K .......... .......... .......... .......... .......... 75% 22.1M 7s 385050K .......... .......... .......... .......... .......... 75% 47.7M 7s 385100K .......... .......... .......... .......... .......... 75% 26.7M 7s 385150K .......... .......... .......... .......... .......... 75% 23.2M 7s 385200K .......... .......... .......... .......... .......... 75% 25.1M 7s 385250K .......... .......... .......... .......... .......... 75% 29.2M 7s 385300K .......... .......... .......... .......... .......... 75% 26.5M 7s 385350K .......... .......... .......... .......... .......... 75% 18.8M 7s 385400K .......... .......... .......... .......... .......... 75% 23.9M 7s 385450K .......... .......... .......... .......... .......... 75% 18.2M 7s 385500K .......... .......... .......... .......... .......... 75% 19.9M 7s 385550K .......... .......... .......... .......... .......... 75% 28.8M 7s 385600K .......... .......... .......... .......... .......... 75% 16.9M 7s 385650K .......... .......... .......... .......... .......... 75% 22.7M 7s 385700K .......... .......... .......... .......... .......... 75% 16.4M 7s 385750K .......... .......... .......... .......... .......... 75% 28.1M 7s 385800K .......... .......... .......... .......... .......... 75% 22.4M 7s 385850K .......... .......... .......... .......... .......... 75% 14.6M 7s 385900K .......... .......... .......... .......... .......... 75% 15.1M 7s 385950K .......... .......... .......... .......... .......... 75% 10.3M 7s 386000K .......... .......... .......... .......... .......... 75% 21.9M 7s 386050K .......... .......... .......... .......... .......... 75% 42.8M 7s 386100K .......... .......... .......... .......... .......... 75% 22.4M 7s 386150K .......... .......... .......... .......... .......... 75% 20.5M 7s 386200K .......... .......... .......... .......... .......... 75% 37.3M 7s 386250K .......... .......... .......... .......... .......... 75% 22.2M 7s 386300K .......... .......... .......... .......... .......... 75% 37.9M 7s 386350K .......... .......... .......... .......... .......... 75% 19.9M 7s 386400K .......... .......... .......... .......... .......... 75% 37.2M 7s 386450K .......... .......... .......... .......... .......... 75% 20.4M 7s 386500K .......... .......... .......... .......... .......... 75% 22.9M 7s 386550K .......... .......... .......... .......... .......... 75% 32.4M 7s 386600K .......... .......... .......... .......... .......... 75% 25.8M 7s 386650K .......... .......... .......... .......... .......... 75% 22.5M 7s 386700K .......... .......... .......... .......... .......... 75% 29.8M 7s 386750K .......... .......... .......... .......... .......... 75% 23.9M 7s 386800K .......... .......... .......... .......... .......... 75% 37.5M 7s 386850K .......... .......... .......... .......... .......... 75% 22.4M 7s 386900K .......... .......... .......... .......... .......... 75% 23.9M 7s 386950K .......... .......... .......... .......... .......... 75% 23.5M 7s 387000K .......... .......... .......... .......... .......... 75% 29.8M 7s 387050K .......... .......... .......... .......... .......... 75% 27.4M 7s 387100K .......... .......... .......... .......... .......... 75% 25.0M 7s 387150K .......... .......... .......... .......... .......... 75% 38.9M 7s 387200K .......... .......... .......... .......... .......... 75% 23.3M 7s 387250K .......... .......... .......... .......... .......... 75% 29.7M 7s 387300K .......... .......... .......... .......... .......... 75% 25.2M 7s 387350K .......... .......... .......... .......... .......... 75% 26.4M 7s 387400K .......... .......... .......... .......... .......... 76% 23.5M 7s 387450K .......... .......... .......... .......... .......... 76% 25.0M 7s 387500K .......... .......... .......... .......... .......... 76% 29.7M 7s 387550K .......... .......... .......... .......... .......... 76% 30.0M 7s 387600K .......... .......... .......... .......... .......... 76% 22.5M 7s 387650K .......... .......... .......... .......... .......... 76% 18.9M 7s 387700K .......... .......... .......... .......... .......... 76% 25.5M 7s 387750K .......... .......... .......... .......... .......... 76% 41.5M 7s 387800K .......... .......... .......... .......... .......... 76% 23.2M 7s 387850K .......... .......... .......... .......... .......... 76% 23.9M 7s 387900K .......... .......... .......... .......... .......... 76% 23.3M 7s 387950K .......... .......... .......... .......... .......... 76% 26.4M 7s 388000K .......... .......... .......... .......... .......... 76% 22.5M 7s 388050K .......... .......... .......... .......... .......... 76% 30.7M 7s 388100K .......... .......... .......... .......... .......... 76% 26.3M 7s 388150K .......... .......... .......... .......... .......... 76% 31.1M 7s 388200K .......... .......... .......... .......... .......... 76% 14.2M 7s 388250K .......... .......... .......... .......... .......... 76% 391M 7s 388300K .......... .......... .......... .......... .......... 76% 64.2M 7s 388350K .......... .......... .......... .......... .......... 76% 28.2M 7s 388400K .......... .......... .......... .......... .......... 76% 26.5M 7s 388450K .......... .......... .......... .......... .......... 76% 24.4M 7s 388500K .......... .......... .......... .......... .......... 76% 29.2M 7s 388550K .......... .......... .......... .......... .......... 76% 31.1M 7s 388600K .......... .......... .......... .......... .......... 76% 25.4M 7s 388650K .......... .......... .......... .......... .......... 76% 31.2M 7s 388700K .......... .......... .......... .......... .......... 76% 27.0M 7s 388750K .......... .......... .......... .......... .......... 76% 20.1M 7s 388800K .......... .......... .......... .......... .......... 76% 45.0M 7s 388850K .......... .......... .......... .......... .......... 76% 16.2M 7s 388900K .......... .......... .......... .......... .......... 76% 26.5M 7s 388950K .......... .......... .......... .......... .......... 76% 22.9M 7s 389000K .......... .......... .......... .......... .......... 76% 23.5M 7s 389050K .......... .......... .......... .......... .......... 76% 20.5M 7s 389100K .......... .......... .......... .......... .......... 76% 22.2M 7s 389150K .......... .......... .......... .......... .......... 76% 22.5M 7s 389200K .......... .......... .......... .......... .......... 76% 18.8M 7s 389250K .......... .......... .......... .......... .......... 76% 27.9M 7s 389300K .......... .......... .......... .......... .......... 76% 22.4M 7s 389350K .......... .......... .......... .......... .......... 76% 20.1M 7s 389400K .......... .......... .......... .......... .......... 76% 19.8M 7s 389450K .......... .......... .......... .......... .......... 76% 18.0M 7s 389500K .......... .......... .......... .......... .......... 76% 14.0M 7s 389550K .......... .......... .......... .......... .......... 76% 30.7M 7s 389600K .......... .......... .......... .......... .......... 76% 22.3M 7s 389650K .......... .......... .......... .......... .......... 76% 127M 7s 389700K .......... .......... .......... .......... .......... 76% 35.1M 7s 389750K .......... .......... .......... .......... .......... 76% 24.2M 7s 389800K .......... .......... .......... .......... .......... 76% 57.1M 7s 389850K .......... .......... .......... .......... .......... 76% 28.8M 7s 389900K .......... .......... .......... .......... .......... 76% 42.2M 7s 389950K .......... .......... .......... .......... .......... 76% 36.2M 7s 390000K .......... .......... .......... .......... .......... 76% 31.7M 7s 390050K .......... .......... .......... .......... .......... 76% 42.4M 7s 390100K .......... .......... .......... .......... .......... 76% 28.7M 7s 390150K .......... .......... .......... .......... .......... 76% 46.7M 7s 390200K .......... .......... .......... .......... .......... 76% 31.9M 7s 390250K .......... .......... .......... .......... .......... 76% 31.4M 7s 390300K .......... .......... .......... .......... .......... 76% 47.0M 7s 390350K .......... .......... .......... .......... .......... 76% 29.3M 7s 390400K .......... .......... .......... .......... .......... 76% 34.3M 7s 390450K .......... .......... .......... .......... .......... 76% 37.5M 7s 390500K .......... .......... .......... .......... .......... 76% 41.6M 7s 390550K .......... .......... .......... .......... .......... 76% 34.6M 7s 390600K .......... .......... .......... .......... .......... 76% 42.8M 7s 390650K .......... .......... .......... .......... .......... 76% 44.3M 7s 390700K .......... .......... .......... .......... .......... 76% 26.4M 7s 390750K .......... .......... .......... .......... .......... 76% 54.7M 7s 390800K .......... .......... .......... .......... .......... 76% 39.1M 7s 390850K .......... .......... .......... .......... .......... 76% 33.3M 7s 390900K .......... .......... .......... .......... .......... 76% 41.9M 7s 390950K .......... .......... .......... .......... .......... 76% 28.9M 7s 391000K .......... .......... .......... .......... .......... 76% 46.5M 7s 391050K .......... .......... .......... .......... .......... 76% 34.0M 7s 391100K .......... .......... .......... .......... .......... 76% 35.8M 7s 391150K .......... .......... .......... .......... .......... 76% 45.8M 7s 391200K .......... .......... .......... .......... .......... 76% 37.3M 7s 391250K .......... .......... .......... .......... .......... 76% 64.4M 7s 391300K .......... .......... .......... .......... .......... 76% 93.7M 7s 391350K .......... .......... .......... .......... .......... 76% 49.9M 7s 391400K .......... .......... .......... .......... .......... 76% 114M 7s 391450K .......... .......... .......... .......... .......... 76% 19.5M 7s 391500K .......... .......... .......... .......... .......... 76% 503M 7s 391550K .......... .......... .......... .......... .......... 76% 410M 7s 391600K .......... .......... .......... .......... .......... 76% 425M 7s 391650K .......... .......... .......... .......... .......... 76% 26.0M 7s 391700K .......... .......... .......... .......... .......... 76% 311M 7s 391750K .......... .......... .......... .......... .......... 76% 87.7M 7s 391800K .......... .......... .......... .......... .......... 76% 39.9M 7s 391850K .......... .......... .......... .......... .......... 76% 115M 7s 391900K .......... .......... .......... .......... .......... 76% 39.9M 7s 391950K .......... .......... .......... .......... .......... 76% 60.4M 7s 392000K .......... .......... .......... .......... .......... 76% 59.4M 7s 392050K .......... .......... .......... .......... .......... 76% 47.9M 7s 392100K .......... .......... .......... .......... .......... 76% 36.2M 7s 392150K .......... .......... .......... .......... .......... 76% 53.0M 7s 392200K .......... .......... .......... .......... .......... 76% 38.0M 7s 392250K .......... .......... .......... .......... .......... 76% 61.4M 7s 392300K .......... .......... .......... .......... .......... 76% 37.7M 7s 392350K .......... .......... .......... .......... .......... 76% 47.4M 7s 392400K .......... .......... .......... .......... .......... 76% 46.6M 7s 392450K .......... .......... .......... .......... .......... 76% 48.1M 7s 392500K .......... .......... .......... .......... .......... 77% 43.2M 7s 392550K .......... .......... .......... .......... .......... 77% 50.7M 7s 392600K .......... .......... .......... .......... .......... 77% 59.5M 7s 392650K .......... .......... .......... .......... .......... 77% 37.0M 7s 392700K .......... .......... .......... .......... .......... 77% 51.7M 7s 392750K .......... .......... .......... .......... .......... 77% 53.4M 7s 392800K .......... .......... .......... .......... .......... 77% 42.6M 7s 392850K .......... .......... .......... .......... .......... 77% 48.0M 7s 392900K .......... .......... .......... .......... .......... 77% 46.7M 7s 392950K .......... .......... .......... .......... .......... 77% 37.2M 7s 393000K .......... .......... .......... .......... .......... 77% 48.0M 7s 393050K .......... .......... .......... .......... .......... 77% 70.4M 7s 393100K .......... .......... .......... .......... .......... 77% 31.9M 7s 393150K .......... .......... .......... .......... .......... 77% 51.6M 7s 393200K .......... .......... .......... .......... .......... 77% 46.0M 7s 393250K .......... .......... .......... .......... .......... 77% 34.2M 7s 393300K .......... .......... .......... .......... .......... 77% 92.8M 7s 393350K .......... .......... .......... .......... .......... 77% 41.3M 7s 393400K .......... .......... .......... .......... .......... 77% 62.9M 7s 393450K .......... .......... .......... .......... .......... 77% 62.8M 7s 393500K .......... .......... .......... .......... .......... 77% 40.7M 7s 393550K .......... .......... .......... .......... .......... 77% 170M 7s 393600K .......... .......... .......... .......... .......... 77% 61.2M 7s 393650K .......... .......... .......... .......... .......... 77% 125M 7s 393700K .......... .......... .......... .......... .......... 77% 63.1M 7s 393750K .......... .......... .......... .......... .......... 77% 25.5M 7s 393800K .......... .......... .......... .......... .......... 77% 113M 7s 393850K .......... .......... .......... .......... .......... 77% 479M 7s 393900K .......... .......... .......... .......... .......... 77% 26.8M 7s 393950K .......... .......... .......... .......... .......... 77% 157M 7s 394000K .......... .......... .......... .......... .......... 77% 190M 7s 394050K .......... .......... .......... .......... .......... 77% 574M 7s 394100K .......... .......... .......... .......... .......... 77% 27.8M 7s 394150K .......... .......... .......... .......... .......... 77% 555M 7s 394200K .......... .......... .......... .......... .......... 77% 30.2M 7s 394250K .......... .......... .......... .......... .......... 77% 407M 7s 394300K .......... .......... .......... .......... .......... 77% 46.4M 7s 394350K .......... .......... .......... .......... .......... 77% 32.6M 7s 394400K .......... .......... .......... .......... .......... 77% 59.0M 7s 394450K .......... .......... .......... .......... .......... 77% 33.4M 7s 394500K .......... .......... .......... .......... .......... 77% 46.5M 7s 394550K .......... .......... .......... .......... .......... 77% 47.5M 7s 394600K .......... .......... .......... .......... .......... 77% 46.9M 7s 394650K .......... .......... .......... .......... .......... 77% 40.3M 7s 394700K .......... .......... .......... .......... .......... 77% 33.4M 7s 394750K .......... .......... .......... .......... .......... 77% 55.2M 7s 394800K .......... .......... .......... .......... .......... 77% 60.4M 7s 394850K .......... .......... .......... .......... .......... 77% 45.9M 7s 394900K .......... .......... .......... .......... .......... 77% 54.1M 7s 394950K .......... .......... .......... .......... .......... 77% 47.4M 7s 395000K .......... .......... .......... .......... .......... 77% 36.0M 7s 395050K .......... .......... .......... .......... .......... 77% 46.1M 7s 395100K .......... .......... .......... .......... .......... 77% 39.4M 7s 395150K .......... .......... .......... .......... .......... 77% 68.9M 7s 395200K .......... .......... .......... .......... .......... 77% 37.7M 7s 395250K .......... .......... .......... .......... .......... 77% 34.3M 7s 395300K .......... .......... .......... .......... .......... 77% 53.6M 7s 395350K .......... .......... .......... .......... .......... 77% 34.7M 7s 395400K .......... .......... .......... .......... .......... 77% 82.2M 7s 395450K .......... .......... .......... .......... .......... 77% 27.3M 7s 395500K .......... .......... .......... .......... .......... 77% 53.4M 7s 395550K .......... .......... .......... .......... .......... 77% 47.3M 7s 395600K .......... .......... .......... .......... .......... 77% 45.6M 7s 395650K .......... .......... .......... .......... .......... 77% 38.8M 7s 395700K .......... .......... .......... .......... .......... 77% 45.7M 7s 395750K .......... .......... .......... .......... .......... 77% 46.7M 7s 395800K .......... .......... .......... .......... .......... 77% 44.5M 7s 395850K .......... .......... .......... .......... .......... 77% 42.2M 7s 395900K .......... .......... .......... .......... .......... 77% 90.3M 7s 395950K .......... .......... .......... .......... .......... 77% 31.3M 7s 396000K .......... .......... .......... .......... .......... 77% 61.1M 7s 396050K .......... .......... .......... .......... .......... 77% 46.5M 7s 396100K .......... .......... .......... .......... .......... 77% 61.5M 7s 396150K .......... .......... .......... .......... .......... 77% 22.7M 7s 396200K .......... .......... .......... .......... .......... 77% 509M 7s 396250K .......... .......... .......... .......... .......... 77% 43.7M 7s 396300K .......... .......... .......... .......... .......... 77% 45.6M 7s 396350K .......... .......... .......... .......... .......... 77% 53.2M 7s 396400K .......... .......... .......... .......... .......... 77% 18.2M 7s 396450K .......... .......... .......... .......... .......... 77% 404M 7s 396500K .......... .......... .......... .......... .......... 77% 44.2M 7s 396550K .......... .......... .......... .......... .......... 77% 30.1M 6s 396600K .......... .......... .......... .......... .......... 77% 157M 6s 396650K .......... .......... .......... .......... .......... 77% 58.8M 6s 396700K .......... .......... .......... .......... .......... 77% 31.5M 6s 396750K .......... .......... .......... .......... .......... 77% 33.8M 6s 396800K .......... .......... .......... .......... .......... 77% 22.0M 6s 396850K .......... .......... .......... .......... .......... 77% 376M 6s 396900K .......... .......... .......... .......... .......... 77% 46.5M 6s 396950K .......... .......... .......... .......... .......... 77% 27.0M 6s 397000K .......... .......... .......... .......... .......... 77% 46.2M 6s 397050K .......... .......... .......... .......... .......... 77% 26.7M 6s 397100K .......... .......... .......... .......... .......... 77% 41.3M 6s 397150K .......... .......... .......... .......... .......... 77% 27.6M 6s 397200K .......... .......... .......... .......... .......... 77% 42.1M 6s 397250K .......... .......... .......... .......... .......... 77% 28.7M 6s 397300K .......... .......... .......... .......... .......... 77% 40.8M 6s 397350K .......... .......... .......... .......... .......... 77% 28.7M 6s 397400K .......... .......... .......... .......... .......... 77% 22.1M 6s 397450K .......... .......... .......... .......... .......... 77% 38.6M 6s 397500K .......... .......... .......... .......... .......... 77% 25.1M 6s 397550K .......... .......... .......... .......... .......... 77% 44.8M 6s 397600K .......... .......... .......... .......... .......... 78% 23.5M 6s 397650K .......... .......... .......... .......... .......... 78% 46.1M 6s 397700K .......... .......... .......... .......... .......... 78% 25.6M 6s 397750K .......... .......... .......... .......... .......... 78% 34.1M 6s 397800K .......... .......... .......... .......... .......... 78% 18.1M 6s 397850K .......... .......... .......... .......... .......... 78% 23.8M 6s 397900K .......... .......... .......... .......... .......... 78% 15.7M 6s 397950K .......... .......... .......... .......... .......... 78% 24.9M 6s 398000K .......... .......... .......... .......... .......... 78% 117M 6s 398050K .......... .......... .......... .......... .......... 78% 27.0M 6s 398100K .......... .......... .......... .......... .......... 78% 37.8M 6s 398150K .......... .......... .......... .......... .......... 78% 17.2M 6s 398200K .......... .......... .......... .......... .......... 78% 121M 6s 398250K .......... .......... .......... .......... .......... 78% 35.0M 6s 398300K .......... .......... .......... .......... .......... 78% 51.0M 6s 398350K .......... .......... .......... .......... .......... 78% 32.4M 6s 398400K .......... .......... .......... .......... .......... 78% 48.2M 6s 398450K .......... .......... .......... .......... .......... 78% 28.2M 6s 398500K .......... .......... .......... .......... .......... 78% 34.7M 6s 398550K .......... .......... .......... .......... .......... 78% 29.4M 6s 398600K .......... .......... .......... .......... .......... 78% 38.1M 6s 398650K .......... .......... .......... .......... .......... 78% 38.3M 6s 398700K .......... .......... .......... .......... .......... 78% 41.3M 6s 398750K .......... .......... .......... .......... .......... 78% 41.8M 6s 398800K .......... .......... .......... .......... .......... 78% 27.2M 6s 398850K .......... .......... .......... .......... .......... 78% 36.2M 6s 398900K .......... .......... .......... .......... .......... 78% 45.4M 6s 398950K .......... .......... .......... .......... .......... 78% 31.9M 6s 399000K .......... .......... .......... .......... .......... 78% 29.4M 6s 399050K .......... .......... .......... .......... .......... 78% 34.1M 6s 399100K .......... .......... .......... .......... .......... 78% 41.4M 6s 399150K .......... .......... .......... .......... .......... 78% 35.4M 6s 399200K .......... .......... .......... .......... .......... 78% 28.6M 6s 399250K .......... .......... .......... .......... .......... 78% 42.1M 6s 399300K .......... .......... .......... .......... .......... 78% 34.4M 6s 399350K .......... .......... .......... .......... .......... 78% 29.3M 6s 399400K .......... .......... .......... .......... .......... 78% 45.1M 6s 399450K .......... .......... .......... .......... .......... 78% 32.0M 6s 399500K .......... .......... .......... .......... .......... 78% 25.2M 6s 399550K .......... .......... .......... .......... .......... 78% 52.5M 6s 399600K .......... .......... .......... .......... .......... 78% 38.2M 6s 399650K .......... .......... .......... .......... .......... 78% 29.1M 6s 399700K .......... .......... .......... .......... .......... 78% 63.2M 6s 399750K .......... .......... .......... .......... .......... 78% 38.5M 6s 399800K .......... .......... .......... .......... .......... 78% 90.8M 6s 399850K .......... .......... .......... .......... .......... 78% 16.0M 6s 399900K .......... .......... .......... .......... .......... 78% 428M 6s 399950K .......... .......... .......... .......... .......... 78% 31.9M 6s 400000K .......... .......... .......... .......... .......... 78% 79.1M 6s 400050K .......... .......... .......... .......... .......... 78% 111M 6s 400100K .......... .......... .......... .......... .......... 78% 19.7M 6s 400150K .......... .......... .......... .......... .......... 78% 126M 6s 400200K .......... .......... .......... .......... .......... 78% 41.2M 6s 400250K .......... .......... .......... .......... .......... 78% 54.2M 6s 400300K .......... .......... .......... .......... .......... 78% 40.9M 6s 400350K .......... .......... .......... .......... .......... 78% 28.7M 6s 400400K .......... .......... .......... .......... .......... 78% 46.7M 6s 400450K .......... .......... .......... .......... .......... 78% 42.1M 6s 400500K .......... .......... .......... .......... .......... 78% 38.8M 6s 400550K .......... .......... .......... .......... .......... 78% 41.6M 6s 400600K .......... .......... .......... .......... .......... 78% 37.7M 6s 400650K .......... .......... .......... .......... .......... 78% 42.4M 6s 400700K .......... .......... .......... .......... .......... 78% 21.2M 6s 400750K .......... .......... .......... .......... .......... 78% 43.9M 6s 400800K .......... .......... .......... .......... .......... 78% 47.5M 6s 400850K .......... .......... .......... .......... .......... 78% 29.2M 6s 400900K .......... .......... .......... .......... .......... 78% 63.2M 6s 400950K .......... .......... .......... .......... .......... 78% 41.9M 6s 401000K .......... .......... .......... .......... .......... 78% 53.0M 6s 401050K .......... .......... .......... .......... .......... 78% 37.8M 6s 401100K .......... .......... .......... .......... .......... 78% 43.5M 6s 401150K .......... .......... .......... .......... .......... 78% 43.1M 6s 401200K .......... .......... .......... .......... .......... 78% 30.7M 6s 401250K .......... .......... .......... .......... .......... 78% 47.0M 6s 401300K .......... .......... .......... .......... .......... 78% 42.3M 6s 401350K .......... .......... .......... .......... .......... 78% 36.7M 6s 401400K .......... .......... .......... .......... .......... 78% 46.0M 6s 401450K .......... .......... .......... .......... .......... 78% 48.6M 6s 401500K .......... .......... .......... .......... .......... 78% 26.2M 6s 401550K .......... .......... .......... .......... .......... 78% 55.9M 6s 401600K .......... .......... .......... .......... .......... 78% 90.3M 6s 401650K .......... .......... .......... .......... .......... 78% 46.0M 6s 401700K .......... .......... .......... .......... .......... 78% 48.3M 6s 401750K .......... .......... .......... .......... .......... 78% 35.0M 6s 401800K .......... .......... .......... .......... .......... 78% 17.3M 6s 401850K .......... .......... .......... .......... .......... 78% 111M 6s 401900K .......... .......... .......... .......... .......... 78% 341M 6s 401950K .......... .......... .......... .......... .......... 78% 326M 6s 402000K .......... .......... .......... .......... .......... 78% 52.6M 6s 402050K .......... .......... .......... .......... .......... 78% 23.0M 6s 402100K .......... .......... .......... .......... .......... 78% 388M 6s 402150K .......... .......... .......... .......... .......... 78% 24.9M 6s 402200K .......... .......... .......... .......... .......... 78% 121M 6s 402250K .......... .......... .......... .......... .......... 78% 198M 6s 402300K .......... .......... .......... .......... .......... 78% 32.5M 6s 402350K .......... .......... .......... .......... .......... 78% 42.7M 6s 402400K .......... .......... .......... .......... .......... 78% 41.8M 6s 402450K .......... .......... .......... .......... .......... 78% 25.4M 6s 402500K .......... .......... .......... .......... .......... 78% 40.7M 6s 402550K .......... .......... .......... .......... .......... 78% 27.0M 6s 402600K .......... .......... .......... .......... .......... 78% 41.1M 6s 402650K .......... .......... .......... .......... .......... 78% 51.7M 6s 402700K .......... .......... .......... .......... .......... 79% 25.9M 6s 402750K .......... .......... .......... .......... .......... 79% 34.8M 6s 402800K .......... .......... .......... .......... .......... 79% 34.4M 6s 402850K .......... .......... .......... .......... .......... 79% 34.1M 6s 402900K .......... .......... .......... .......... .......... 79% 34.9M 6s 402950K .......... .......... .......... .......... .......... 79% 29.1M 6s 403000K .......... .......... .......... .......... .......... 79% 45.7M 6s 403050K .......... .......... .......... .......... .......... 79% 41.8M 6s 403100K .......... .......... .......... .......... .......... 79% 26.8M 6s 403150K .......... .......... .......... .......... .......... 79% 55.4M 6s 403200K .......... .......... .......... .......... .......... 79% 31.2M 6s 403250K .......... .......... .......... .......... .......... 79% 40.6M 6s 403300K .......... .......... .......... .......... .......... 79% 27.3M 6s 403350K .......... .......... .......... .......... .......... 79% 46.4M 6s 403400K .......... .......... .......... .......... .......... 79% 42.5M 6s 403450K .......... .......... .......... .......... .......... 79% 30.8M 6s 403500K .......... .......... .......... .......... .......... 79% 42.9M 6s 403550K .......... .......... .......... .......... .......... 79% 44.8M 6s 403600K .......... .......... .......... .......... .......... 79% 41.9M 6s 403650K .......... .......... .......... .......... .......... 79% 93.4M 6s 403700K .......... .......... .......... .......... .......... 79% 46.4M 6s 403750K .......... .......... .......... .......... .......... 79% 126M 6s 403800K .......... .......... .......... .......... .......... 79% 24.2M 6s 403850K .......... .......... .......... .......... .......... 79% 328M 6s 403900K .......... .......... .......... .......... .......... 79% 432M 6s 403950K .......... .......... .......... .......... .......... 79% 41.5M 6s 404000K .......... .......... .......... .......... .......... 79% 23.0M 6s 404050K .......... .......... .......... .......... .......... 79% 531M 6s 404100K .......... .......... .......... .......... .......... 79% 34.6M 6s 404150K .......... .......... .......... .......... .......... 79% 56.6M 6s 404200K .......... .......... .......... .......... .......... 79% 154M 6s 404250K .......... .......... .......... .......... .......... 79% 32.5M 6s 404300K .......... .......... .......... .......... .......... 79% 67.1M 6s 404350K .......... .......... .......... .......... .......... 79% 27.2M 6s 404400K .......... .......... .......... .......... .......... 79% 34.5M 6s 404450K .......... .......... .......... .......... .......... 79% 38.2M 6s 404500K .......... .......... .......... .......... .......... 79% 33.7M 6s 404550K .......... .......... .......... .......... .......... 79% 31.7M 6s 404600K .......... .......... .......... .......... .......... 79% 37.9M 6s 404650K .......... .......... .......... .......... .......... 79% 26.8M 6s 404700K .......... .......... .......... .......... .......... 79% 49.4M 6s 404750K .......... .......... .......... .......... .......... 79% 27.6M 6s 404800K .......... .......... .......... .......... .......... 79% 45.3M 6s 404850K .......... .......... .......... .......... .......... 79% 25.3M 6s 404900K .......... .......... .......... .......... .......... 79% 51.1M 6s 404950K .......... .......... .......... .......... .......... 79% 27.4M 6s 405000K .......... .......... .......... .......... .......... 79% 40.8M 6s 405050K .......... .......... .......... .......... .......... 79% 41.2M 6s 405100K .......... .......... .......... .......... .......... 79% 25.7M 6s 405150K .......... .......... .......... .......... .......... 79% 46.5M 6s 405200K .......... .......... .......... .......... .......... 79% 34.1M 6s 405250K .......... .......... .......... .......... .......... 79% 31.6M 6s 405300K .......... .......... .......... .......... .......... 79% 46.6M 6s 405350K .......... .......... .......... .......... .......... 79% 32.6M 6s 405400K .......... .......... .......... .......... .......... 79% 46.9M 6s 405450K .......... .......... .......... .......... .......... 79% 26.5M 6s 405500K .......... .......... .......... .......... .......... 79% 43.8M 6s 405550K .......... .......... .......... .......... .......... 79% 34.4M 6s 405600K .......... .......... .......... .......... .......... 79% 25.1M 6s 405650K .......... .......... .......... .......... .......... 79% 15.9M 6s 405700K .......... .......... .......... .......... .......... 79% 367M 6s 405750K .......... .......... .......... .......... .......... 79% 537M 6s 405800K .......... .......... .......... .......... .......... 79% 21.3M 6s 405850K .......... .......... .......... .......... .......... 79% 56.5M 6s 405900K .......... .......... .......... .......... .......... 79% 42.4M 6s 405950K .......... .......... .......... .......... .......... 79% 21.7M 6s 406000K .......... .......... .......... .......... .......... 79% 474M 6s 406050K .......... .......... .......... .......... .......... 79% 97.3M 6s 406100K .......... .......... .......... .......... .......... 79% 33.4M 6s 406150K .......... .......... .......... .......... .......... 79% 48.4M 6s 406200K .......... .......... .......... .......... .......... 79% 34.8M 6s 406250K .......... .......... .......... .......... .......... 79% 44.8M 6s 406300K .......... .......... .......... .......... .......... 79% 63.4M 6s 406350K .......... .......... .......... .......... .......... 79% 34.4M 6s 406400K .......... .......... .......... .......... .......... 79% 46.3M 6s 406450K .......... .......... .......... .......... .......... 79% 33.8M 6s 406500K .......... .......... .......... .......... .......... 79% 43.4M 6s 406550K .......... .......... .......... .......... .......... 79% 163M 6s 406600K .......... .......... .......... .......... .......... 79% 34.1M 6s 406650K .......... .......... .......... .......... .......... 79% 42.2M 6s 406700K .......... .......... .......... .......... .......... 79% 52.5M 6s 406750K .......... .......... .......... .......... .......... 79% 46.5M 6s 406800K .......... .......... .......... .......... .......... 79% 22.0M 6s 406850K .......... .......... .......... .......... .......... 79% 77.0M 6s 406900K .......... .......... .......... .......... .......... 79% 54.8M 6s 406950K .......... .......... .......... .......... .......... 79% 47.8M 6s 407000K .......... .......... .......... .......... .......... 79% 58.5M 6s 407050K .......... .......... .......... .......... .......... 79% 29.4M 6s 407100K .......... .......... .......... .......... .......... 79% 52.9M 6s 407150K .......... .......... .......... .......... .......... 79% 48.1M 6s 407200K .......... .......... .......... .......... .......... 79% 41.2M 6s 407250K .......... .......... .......... .......... .......... 79% 33.4M 6s 407300K .......... .......... .......... .......... .......... 79% 53.7M 6s 407350K .......... .......... .......... .......... .......... 79% 28.6M 6s 407400K .......... .......... .......... .......... .......... 79% 52.8M 6s 407450K .......... .......... .......... .......... .......... 79% 34.7M 6s 407500K .......... .......... .......... .......... .......... 79% 54.5M 6s 407550K .......... .......... .......... .......... .......... 79% 33.7M 6s 407600K .......... .......... .......... .......... .......... 79% 40.7M 6s 407650K .......... .......... .......... .......... .......... 79% 38.3M 6s 407700K .......... .......... .......... .......... .......... 79% 45.0M 6s 407750K .......... .......... .......... .......... .......... 79% 39.5M 6s 407800K .......... .......... .......... .......... .......... 80% 37.9M 6s 407850K .......... .......... .......... .......... .......... 80% 44.3M 6s 407900K .......... .......... .......... .......... .......... 80% 43.5M 6s 407950K .......... .......... .......... .......... .......... 80% 33.9M 6s 408000K .......... .......... .......... .......... .......... 80% 53.4M 6s 408050K .......... .......... .......... .......... .......... 80% 53.8M 6s 408100K .......... .......... .......... .......... .......... 80% 30.8M 6s 408150K .......... .......... .......... .......... .......... 80% 53.3M 6s 408200K .......... .......... .......... .......... .......... 80% 36.2M 6s 408250K .......... .......... .......... .......... .......... 80% 36.4M 6s 408300K .......... .......... .......... .......... .......... 80% 53.6M 6s 408350K .......... .......... .......... .......... .......... 80% 34.0M 6s 408400K .......... .......... .......... .......... .......... 80% 119M 6s 408450K .......... .......... .......... .......... .......... 80% 54.3M 6s 408500K .......... .......... .......... .......... .......... 80% 57.8M 6s 408550K .......... .......... .......... .......... .......... 80% 30.1M 6s 408600K .......... .......... .......... .......... .......... 80% 65.5M 6s 408650K .......... .......... .......... .......... .......... 80% 483M 6s 408700K .......... .......... .......... .......... .......... 80% 44.8M 6s 408750K .......... .......... .......... .......... .......... 80% 78.0M 6s 408800K .......... .......... .......... .......... .......... 80% 364M 6s 408850K .......... .......... .......... .......... .......... 80% 28.8M 6s 408900K .......... .......... .......... .......... .......... 80% 158M 6s 408950K .......... .......... .......... .......... .......... 80% 64.8M 6s 409000K .......... .......... .......... .......... .......... 80% 62.8M 6s 409050K .......... .......... .......... .......... .......... 80% 41.6M 6s 409100K .......... .......... .......... .......... .......... 80% 32.9M 6s 409150K .......... .......... .......... .......... .......... 80% 103M 6s 409200K .......... .......... .......... .......... .......... 80% 30.1M 6s 409250K .......... .......... .......... .......... .......... 80% 53.3M 6s 409300K .......... .......... .......... .......... .......... 80% 43.0M 6s 409350K .......... .......... .......... .......... .......... 80% 34.1M 6s 409400K .......... .......... .......... .......... .......... 80% 60.3M 6s 409450K .......... .......... .......... .......... .......... 80% 45.8M 6s 409500K .......... .......... .......... .......... .......... 80% 37.2M 6s 409550K .......... .......... .......... .......... .......... 80% 41.4M 6s 409600K .......... .......... .......... .......... .......... 80% 45.6M 6s 409650K .......... .......... .......... .......... .......... 80% 42.2M 6s 409700K .......... .......... .......... .......... .......... 80% 31.0M 6s 409750K .......... .......... .......... .......... .......... 80% 60.4M 6s 409800K .......... .......... .......... .......... .......... 80% 59.9M 6s 409850K .......... .......... .......... .......... .......... 80% 36.5M 6s 409900K .......... .......... .......... .......... .......... 80% 54.3M 6s 409950K .......... .......... .......... .......... .......... 80% 33.8M 6s 410000K .......... .......... .......... .......... .......... 80% 48.2M 6s 410050K .......... .......... .......... .......... .......... 80% 42.2M 6s 410100K .......... .......... .......... .......... .......... 80% 40.8M 6s 410150K .......... .......... .......... .......... .......... 80% 46.2M 6s 410200K .......... .......... .......... .......... .......... 80% 30.8M 6s 410250K .......... .......... .......... .......... .......... 80% 51.9M 6s 410300K .......... .......... .......... .......... .......... 80% 50.6M 6s 410350K .......... .......... .......... .......... .......... 80% 33.7M 6s 410400K .......... .......... .......... .......... .......... 80% 46.6M 6s 410450K .......... .......... .......... .......... .......... 80% 40.9M 6s 410500K .......... .......... .......... .......... .......... 80% 41.9M 6s 410550K .......... .......... .......... .......... .......... 80% 37.8M 6s 410600K .......... .......... .......... .......... .......... 80% 37.7M 6s 410650K .......... .......... .......... .......... .......... 80% 42.2M 6s 410700K .......... .......... .......... .......... .......... 80% 52.7M 6s 410750K .......... .......... .......... .......... .......... 80% 95.0M 6s 410800K .......... .......... .......... .......... .......... 80% 60.3M 6s 410850K .......... .......... .......... .......... .......... 80% 95.0M 6s 410900K .......... .......... .......... .......... .......... 80% 96.1M 6s 410950K .......... .......... .......... .......... .......... 80% 41.7M 6s 411000K .......... .......... .......... .......... .......... 80% 14.9M 6s 411050K .......... .......... .......... .......... .......... 80% 483M 6s 411100K .......... .......... .......... .......... .......... 80% 474M 6s 411150K .......... .......... .......... .......... .......... 80% 514M 6s 411200K .......... .......... .......... .......... .......... 80% 69.7M 6s 411250K .......... .......... .......... .......... .......... 80% 39.5M 6s 411300K .......... .......... .......... .......... .......... 80% 102M 6s 411350K .......... .......... .......... .......... .......... 80% 376M 6s 411400K .......... .......... .......... .......... .......... 80% 34.2M 6s 411450K .......... .......... .......... .......... .......... 80% 104M 6s 411500K .......... .......... .......... .......... .......... 80% 41.2M 6s 411550K .......... .......... .......... .......... .......... 80% 45.5M 6s 411600K .......... .......... .......... .......... .......... 80% 28.8M 6s 411650K .......... .......... .......... .......... .......... 80% 54.9M 6s 411700K .......... .......... .......... .......... .......... 80% 28.6M 6s 411750K .......... .......... .......... .......... .......... 80% 42.1M 6s 411800K .......... .......... .......... .......... .......... 80% 42.5M 6s 411850K .......... .......... .......... .......... .......... 80% 34.0M 6s 411900K .......... .......... .......... .......... .......... 80% 54.1M 5s 411950K .......... .......... .......... .......... .......... 80% 35.0M 5s 412000K .......... .......... .......... .......... .......... 80% 47.4M 5s 412050K .......... .......... .......... .......... .......... 80% 31.8M 5s 412100K .......... .......... .......... .......... .......... 80% 38.1M 5s 412150K .......... .......... .......... .......... .......... 80% 46.4M 5s 412200K .......... .......... .......... .......... .......... 80% 32.4M 5s 412250K .......... .......... .......... .......... .......... 80% 53.8M 5s 412300K .......... .......... .......... .......... .......... 80% 46.7M 5s 412350K .......... .......... .......... .......... .......... 80% 34.9M 5s 412400K .......... .......... .......... .......... .......... 80% 46.9M 5s 412450K .......... .......... .......... .......... .......... 80% 15.8M 5s 412500K .......... .......... .......... .......... .......... 80% 36.6M 5s 412550K .......... .......... .......... .......... .......... 80% 52.3M 5s 412600K .......... .......... .......... .......... .......... 80% 28.7M 5s 412650K .......... .......... .......... .......... .......... 80% 41.7M 5s 412700K .......... .......... .......... .......... .......... 80% 31.0M 5s 412750K .......... .......... .......... .......... .......... 80% 37.0M 5s 412800K .......... .......... .......... .......... .......... 80% 36.2M 5s 412850K .......... .......... .......... .......... .......... 80% 38.4M 5s 412900K .......... .......... .......... .......... .......... 81% 41.1M 5s 412950K .......... .......... .......... .......... .......... 81% 72.0M 5s 413000K .......... .......... .......... .......... .......... 81% 62.9M 5s 413050K .......... .......... .......... .......... .......... 81% 61.7M 5s 413100K .......... .......... .......... .......... .......... 81% 18.6M 5s 413150K .......... .......... .......... .......... .......... 81% 588M 5s 413200K .......... .......... .......... .......... .......... 81% 40.1M 5s 413250K .......... .......... .......... .......... .......... 81% 549M 5s 413300K .......... .......... .......... .......... .......... 81% 173M 5s 413350K .......... .......... .......... .......... .......... 81% 24.8M 5s 413400K .......... .......... .......... .......... .......... 81% 91.6M 5s 413450K .......... .......... .......... .......... .......... 81% 53.0M 5s 413500K .......... .......... .......... .......... .......... 81% 79.8M 5s 413550K .......... .......... .......... .......... .......... 81% 53.8M 5s 413600K .......... .......... .......... .......... .......... 81% 31.9M 5s 413650K .......... .......... .......... .......... .......... 81% 53.8M 5s 413700K .......... .......... .......... .......... .......... 81% 44.9M 5s 413750K .......... .......... .......... .......... .......... 81% 31.8M 5s 413800K .......... .......... .......... .......... .......... 81% 51.9M 5s 413850K .......... .......... .......... .......... .......... 81% 28.5M 5s 413900K .......... .......... .......... .......... .......... 81% 47.2M 5s 413950K .......... .......... .......... .......... .......... 81% 44.7M 5s 414000K .......... .......... .......... .......... .......... 81% 31.5M 5s 414050K .......... .......... .......... .......... .......... 81% 45.7M 5s 414100K .......... .......... .......... .......... .......... 81% 28.4M 5s 414150K .......... .......... .......... .......... .......... 81% 61.3M 5s 414200K .......... .......... .......... .......... .......... 81% 30.7M 5s 414250K .......... .......... .......... .......... .......... 81% 46.1M 5s 414300K .......... .......... .......... .......... .......... 81% 34.6M 5s 414350K .......... .......... .......... .......... .......... 81% 45.4M 5s 414400K .......... .......... .......... .......... .......... 81% 29.0M 5s 414450K .......... .......... .......... .......... .......... 81% 40.5M 5s 414500K .......... .......... .......... .......... .......... 81% 42.5M 5s 414550K .......... .......... .......... .......... .......... 81% 47.5M 5s 414600K .......... .......... .......... .......... .......... 81% 40.4M 5s 414650K .......... .......... .......... .......... .......... 81% 47.0M 5s 414700K .......... .......... .......... .......... .......... 81% 37.1M 5s 414750K .......... .......... .......... .......... .......... 81% 37.1M 5s 414800K .......... .......... .......... .......... .......... 81% 42.2M 5s 414850K .......... .......... .......... .......... .......... 81% 36.6M 5s 414900K .......... .......... .......... .......... .......... 81% 37.2M 5s 414950K .......... .......... .......... .......... .......... 81% 41.6M 5s 415000K .......... .......... .......... .......... .......... 81% 99.9M 5s 415050K .......... .......... .......... .......... .......... 81% 28.0M 5s 415100K .......... .......... .......... .......... .......... 81% 94.1M 5s 415150K .......... .......... .......... .......... .......... 81% 20.9M 5s 415200K .......... .......... .......... .......... .......... 81% 465M 5s 415250K .......... .......... .......... .......... .......... 81% 574M 5s 415300K .......... .......... .......... .......... .......... 81% 22.2M 5s 415350K .......... .......... .......... .......... .......... 81% 452M 5s 415400K .......... .......... .......... .......... .......... 81% 24.3M 5s 415450K .......... .......... .......... .......... .......... 81% 28.9M 5s 415500K .......... .......... .......... .......... .......... 81% 130M 5s 415550K .......... .......... .......... .......... .......... 81% 34.2M 5s 415600K .......... .......... .......... .......... .......... 81% 28.8M 5s 415650K .......... .......... .......... .......... .......... 81% 33.8M 5s 415700K .......... .......... .......... .......... .......... 81% 18.9M 5s 415750K .......... .......... .......... .......... .......... 81% 41.7M 5s 415800K .......... .......... .......... .......... .......... 81% 31.5M 5s 415850K .......... .......... .......... .......... .......... 81% 30.7M 5s 415900K .......... .......... .......... .......... .......... 81% 38.8M 5s 415950K .......... .......... .......... .......... .......... 81% 24.7M 5s 416000K .......... .......... .......... .......... .......... 81% 46.3M 5s 416050K .......... .......... .......... .......... .......... 81% 29.6M 5s 416100K .......... .......... .......... .......... .......... 81% 41.5M 5s 416150K .......... .......... .......... .......... .......... 81% 34.4M 5s 416200K .......... .......... .......... .......... .......... 81% 25.6M 5s 416250K .......... .......... .......... .......... .......... 81% 41.8M 5s 416300K .......... .......... .......... .......... .......... 81% 28.7M 5s 416350K .......... .......... .......... .......... .......... 81% 31.9M 5s 416400K .......... .......... .......... .......... .......... 81% 52.9M 5s 416450K .......... .......... .......... .......... .......... 81% 28.9M 5s 416500K .......... .......... .......... .......... .......... 81% 62.4M 5s 416550K .......... .......... .......... .......... .......... 81% 34.2M 5s 416600K .......... .......... .......... .......... .......... 81% 31.8M 5s 416650K .......... .......... .......... .......... .......... 81% 34.5M 5s 416700K .......... .......... .......... .......... .......... 81% 53.4M 5s 416750K .......... .......... .......... .......... .......... 81% 51.2M 5s 416800K .......... .......... .......... .......... .......... 81% 55.9M 5s 416850K .......... .......... .......... .......... .......... 81% 94.3M 5s 416900K .......... .......... .......... .......... .......... 81% 111M 5s 416950K .......... .......... .......... .......... .......... 81% 18.4M 5s 417000K .......... .......... .......... .......... .......... 81% 213M 5s 417050K .......... .......... .......... .......... .......... 81% 376M 5s 417100K .......... .......... .......... .......... .......... 81% 27.1M 5s 417150K .......... .......... .......... .......... .......... 81% 414M 5s 417200K .......... .......... .......... .......... .......... 81% 432M 5s 417250K .......... .......... .......... .......... .......... 81% 549M 5s 417300K .......... .......... .......... .......... .......... 81% 250M 5s 417350K .......... .......... .......... .......... .......... 81% 23.9M 5s 417400K .......... .......... .......... .......... .......... 81% 461M 5s 417450K .......... .......... .......... .......... .......... 81% 53.4M 5s 417500K .......... .......... .......... .......... .......... 81% 54.6M 5s 417550K .......... .......... .......... .......... .......... 81% 54.9M 5s 417600K .......... .......... .......... .......... .......... 81% 38.5M 5s 417650K .......... .......... .......... .......... .......... 81% 42.8M 5s 417700K .......... .......... .......... .......... .......... 81% 53.5M 5s 417750K .......... .......... .......... .......... .......... 81% 75.5M 5s 417800K .......... .......... .......... .......... .......... 81% 47.2M 5s 417850K .......... .......... .......... .......... .......... 81% 46.4M 5s 417900K .......... .......... .......... .......... .......... 81% 37.2M 5s 417950K .......... .......... .......... .......... .......... 81% 54.5M 5s 418000K .......... .......... .......... .......... .......... 82% 58.3M 5s 418050K .......... .......... .......... .......... .......... 82% 34.4M 5s 418100K .......... .......... .......... .......... .......... 82% 34.1M 5s 418150K .......... .......... .......... .......... .......... 82% 23.7M 5s 418200K .......... .......... .......... .......... .......... 82% 26.1M 5s 418250K .......... .......... .......... .......... .......... 82% 41.8M 5s 418300K .......... .......... .......... .......... .......... 82% 52.4M 5s 418350K .......... .......... .......... .......... .......... 82% 34.4M 5s 418400K .......... .......... .......... .......... .......... 82% 53.0M 5s 418450K .......... .......... .......... .......... .......... 82% 41.6M 5s 418500K .......... .......... .......... .......... .......... 82% 51.5M 5s 418550K .......... .......... .......... .......... .......... 82% 49.2M 5s 418600K .......... .......... .......... .......... .......... 82% 37.3M 5s 418650K .......... .......... .......... .......... .......... 82% 53.2M 5s 418700K .......... .......... .......... .......... .......... 82% 53.7M 5s 418750K .......... .......... .......... .......... .......... 82% 39.2M 5s 418800K .......... .......... .......... .......... .......... 82% 70.8M 5s 418850K .......... .......... .......... .......... .......... 82% 43.7M 5s 418900K .......... .......... .......... .......... .......... 82% 44.3M 5s 418950K .......... .......... .......... .......... .......... 82% 42.5M 5s 419000K .......... .......... .......... .......... .......... 82% 63.5M 5s 419050K .......... .......... .......... .......... .......... 82% 46.3M 5s 419100K .......... .......... .......... .......... .......... 82% 18.7M 5s 419150K .......... .......... .......... .......... .......... 82% 37.3M 5s 419200K .......... .......... .......... .......... .......... 82% 407M 5s 419250K .......... .......... .......... .......... .......... 82% 115M 5s 419300K .......... .......... .......... .......... .......... 82% 23.5M 5s 419350K .......... .......... .......... .......... .......... 82% 142M 5s 419400K .......... .......... .......... .......... .......... 82% 51.8M 5s 419450K .......... .......... .......... .......... .......... 82% 46.5M 5s 419500K .......... .......... .......... .......... .......... 82% 46.2M 5s 419550K .......... .......... .......... .......... .......... 82% 42.1M 5s 419600K .......... .......... .......... .......... .......... 82% 51.9M 5s 419650K .......... .......... .......... .......... .......... 82% 53.4M 5s 419700K .......... .......... .......... .......... .......... 82% 35.0M 5s 419750K .......... .......... .......... .......... .......... 82% 53.7M 5s 419800K .......... .......... .......... .......... .......... 82% 55.2M 5s 419850K .......... .......... .......... .......... .......... 82% 47.2M 5s 419900K .......... .......... .......... .......... .......... 82% 37.7M 5s 419950K .......... .......... .......... .......... .......... 82% 48.3M 5s 420000K .......... .......... .......... .......... .......... 82% 90.9M 5s 420050K .......... .......... .......... .......... .......... 82% 24.0M 5s 420100K .......... .......... .......... .......... .......... 82% 337M 5s 420150K .......... .......... .......... .......... .......... 82% 35.7M 5s 420200K .......... .......... .......... .......... .......... 82% 50.3M 5s 420250K .......... .......... .......... .......... .......... 82% 41.3M 5s 420300K .......... .......... .......... .......... .......... 82% 39.3M 5s 420350K .......... .......... .......... .......... .......... 82% 24.8M 5s 420400K .......... .......... .......... .......... .......... 82% 53.5M 5s 420450K .......... .......... .......... .......... .......... 82% 40.1M 5s 420500K .......... .......... .......... .......... .......... 82% 42.3M 5s 420550K .......... .......... .......... .......... .......... 82% 46.1M 5s 420600K .......... .......... .......... .......... .......... 82% 46.2M 5s 420650K .......... .......... .......... .......... .......... 82% 31.5M 5s 420700K .......... .......... .......... .......... .......... 82% 45.4M 5s 420750K .......... .......... .......... .......... .......... 82% 37.7M 5s 420800K .......... .......... .......... .......... .......... 82% 53.5M 5s 420850K .......... .......... .......... .......... .......... 82% 38.6M 5s 420900K .......... .......... .......... .......... .......... 82% 37.7M 5s 420950K .......... .......... .......... .......... .......... 82% 34.8M 5s 421000K .......... .......... .......... .......... .......... 82% 40.6M 5s 421050K .......... .......... .......... .......... .......... 82% 33.8M 5s 421100K .......... .......... .......... .......... .......... 82% 29.2M 5s 421150K .......... .......... .......... .......... .......... 82% 22.0M 5s 421200K .......... .......... .......... .......... .......... 82% 10.1M 5s 421250K .......... .......... .......... .......... .......... 82% 135M 5s 421300K .......... .......... .......... .......... .......... 82% 25.5M 5s 421350K .......... .......... .......... .......... .......... 82% 29.2M 5s 421400K .......... .......... .......... .......... .......... 82% 25.5M 5s 421450K .......... .......... .......... .......... .......... 82% 22.3M 5s 421500K .......... .......... .......... .......... .......... 82% 41.0M 5s 421550K .......... .......... .......... .......... .......... 82% 21.1M 5s 421600K .......... .......... .......... .......... .......... 82% 19.8M 5s 421650K .......... .......... .......... .......... .......... 82% 38.1M 5s 421700K .......... .......... .......... .......... .......... 82% 27.0M 5s 421750K .......... .......... .......... .......... .......... 82% 27.2M 5s 421800K .......... .......... .......... .......... .......... 82% 36.6M 5s 421850K .......... .......... .......... .......... .......... 82% 22.5M 5s 421900K .......... .......... .......... .......... .......... 82% 26.9M 5s 421950K .......... .......... .......... .......... .......... 82% 36.5M 5s 422000K .......... .......... .......... .......... .......... 82% 34.0M 5s 422050K .......... .......... .......... .......... .......... 82% 24.0M 5s 422100K .......... .......... .......... .......... .......... 82% 22.2M 5s 422150K .......... .......... .......... .......... .......... 82% 43.5M 5s 422200K .......... .......... .......... .......... .......... 82% 27.0M 5s 422250K .......... .......... .......... .......... .......... 82% 42.9M 5s 422300K .......... .......... .......... .......... .......... 82% 41.5M 5s 422350K .......... .......... .......... .......... .......... 82% 46.6M 5s 422400K .......... .......... .......... .......... .......... 82% 121M 5s 422450K .......... .......... .......... .......... .......... 82% 23.0M 5s 422500K .......... .......... .......... .......... .......... 82% 407M 5s 422550K .......... .......... .......... .......... .......... 82% 31.8M 5s 422600K .......... .......... .......... .......... .......... 82% 157M 5s 422650K .......... .......... .......... .......... .......... 82% 69.5M 5s 422700K .......... .......... .......... .......... .......... 82% 52.7M 5s 422750K .......... .......... .......... .......... .......... 82% 46.8M 5s 422800K .......... .......... .......... .......... .......... 82% 54.3M 5s 422850K .......... .......... .......... .......... .......... 82% 37.9M 5s 422900K .......... .......... .......... .......... .......... 82% 63.2M 5s 422950K .......... .......... .......... .......... .......... 82% 43.4M 5s 423000K .......... .......... .......... .......... .......... 82% 46.9M 5s 423050K .......... .......... .......... .......... .......... 82% 91.1M 5s 423100K .......... .......... .......... .......... .......... 83% 41.3M 5s 423150K .......... .......... .......... .......... .......... 83% 99.4M 5s 423200K .......... .......... .......... .......... .......... 83% 37.6M 5s 423250K .......... .......... .......... .......... .......... 83% 52.9M 5s 423300K .......... .......... .......... .......... .......... 83% 42.3M 5s 423350K .......... .......... .......... .......... .......... 83% 46.6M 5s 423400K .......... .......... .......... .......... .......... 83% 64.8M 5s 423450K .......... .......... .......... .......... .......... 83% 31.0M 5s 423500K .......... .......... .......... .......... .......... 83% 88.3M 5s 423550K .......... .......... .......... .......... .......... 83% 46.8M 5s 423600K .......... .......... .......... .......... .......... 83% 28.9M 5s 423650K .......... .......... .......... .......... .......... 83% 40.0M 5s 423700K .......... .......... .......... .......... .......... 83% 47.5M 5s 423750K .......... .......... .......... .......... .......... 83% 49.0M 5s 423800K .......... .......... .......... .......... .......... 83% 46.4M 5s 423850K .......... .......... .......... .......... .......... 83% 53.5M 5s 423900K .......... .......... .......... .......... .......... 83% 52.5M 5s 423950K .......... .......... .......... .......... .......... 83% 17.8M 5s 424000K .......... .......... .......... .......... .......... 83% 133M 5s 424050K .......... .......... .......... .......... .......... 83% 46.7M 5s 424100K .......... .......... .......... .......... .......... 83% 29.1M 5s 424150K .......... .......... .......... .......... .......... 83% 36.7M 5s 424200K .......... .......... .......... .......... .......... 83% 28.3M 5s 424250K .......... .......... .......... .......... .......... 83% 23.5M 5s 424300K .......... .......... .......... .......... .......... 83% 25.8M 5s 424350K .......... .......... .......... .......... .......... 83% 14.2M 5s 424400K .......... .......... .......... .......... .......... 83% 24.0M 5s 424450K .......... .......... .......... .......... .......... 83% 38.9M 5s 424500K .......... .......... .......... .......... .......... 83% 31.8M 5s 424550K .......... .......... .......... .......... .......... 83% 42.3M 5s 424600K .......... .......... .......... .......... .......... 83% 23.8M 5s 424650K .......... .......... .......... .......... .......... 83% 53.4M 5s 424700K .......... .......... .......... .......... .......... 83% 34.8M 5s 424750K .......... .......... .......... .......... .......... 83% 51.6M 5s 424800K .......... .......... .......... .......... .......... 83% 35.2M 5s 424850K .......... .......... .......... .......... .......... 83% 32.0M 5s 424900K .......... .......... .......... .......... .......... 83% 60.3M 5s 424950K .......... .......... .......... .......... .......... 83% 36.9M 5s 425000K .......... .......... .......... .......... .......... 83% 51.4M 5s 425050K .......... .......... .......... .......... .......... 83% 29.7M 5s 425100K .......... .......... .......... .......... .......... 83% 42.4M 5s 425150K .......... .......... .......... .......... .......... 83% 46.7M 5s 425200K .......... .......... .......... .......... .......... 83% 41.6M 5s 425250K .......... .......... .......... .......... .......... 83% 85.8M 5s 425300K .......... .......... .......... .......... .......... 83% 59.5M 5s 425350K .......... .......... .......... .......... .......... 83% 76.3M 5s 425400K .......... .......... .......... .......... .......... 83% 50.9M 5s 425450K .......... .......... .......... .......... .......... 83% 88.6M 5s 425500K .......... .......... .......... .......... .......... 83% 21.7M 5s 425550K .......... .......... .......... .......... .......... 83% 301M 5s 425600K .......... .......... .......... .......... .......... 83% 394M 5s 425650K .......... .......... .......... .......... .......... 83% 421M 5s 425700K .......... .......... .......... .......... .......... 83% 34.4M 5s 425750K .......... .......... .......... .......... .......... 83% 208M 5s 425800K .......... .......... .......... .......... .......... 83% 39.3M 5s 425850K .......... .......... .......... .......... .......... 83% 432M 5s 425900K .......... .......... .......... .......... .......... 83% 87.8M 5s 425950K .......... .......... .......... .......... .......... 83% 40.8M 5s 426000K .......... .......... .......... .......... .......... 83% 52.4M 5s 426050K .......... .......... .......... .......... .......... 83% 70.9M 5s 426100K .......... .......... .......... .......... .......... 83% 53.5M 5s 426150K .......... .......... .......... .......... .......... 83% 34.2M 5s 426200K .......... .......... .......... .......... .......... 83% 71.8M 5s 426250K .......... .......... .......... .......... .......... 83% 53.4M 5s 426300K .......... .......... .......... .......... .......... 83% 42.1M 5s 426350K .......... .......... .......... .......... .......... 83% 47.8M 5s 426400K .......... .......... .......... .......... .......... 83% 74.0M 5s 426450K .......... .......... .......... .......... .......... 83% 42.1M 5s 426500K .......... .......... .......... .......... .......... 83% 61.9M 5s 426550K .......... .......... .......... .......... .......... 83% 42.6M 5s 426600K .......... .......... .......... .......... .......... 83% 45.8M 5s 426650K .......... .......... .......... .......... .......... 83% 53.4M 5s 426700K .......... .......... .......... .......... .......... 83% 53.1M 5s 426750K .......... .......... .......... .......... .......... 83% 53.1M 5s 426800K .......... .......... .......... .......... .......... 83% 52.0M 5s 426850K .......... .......... .......... .......... .......... 83% 38.2M 5s 426900K .......... .......... .......... .......... .......... 83% 53.0M 5s 426950K .......... .......... .......... .......... .......... 83% 47.5M 5s 427000K .......... .......... .......... .......... .......... 83% 62.1M 5s 427050K .......... .......... .......... .......... .......... 83% 72.7M 5s 427100K .......... .......... .......... .......... .......... 83% 37.2M 5s 427150K .......... .......... .......... .......... .......... 83% 62.7M 5s 427200K .......... .......... .......... .......... .......... 83% 37.1M 5s 427250K .......... .......... .......... .......... .......... 83% 61.4M 5s 427300K .......... .......... .......... .......... .......... 83% 45.7M 5s 427350K .......... .......... .......... .......... .......... 83% 46.9M 5s 427400K .......... .......... .......... .......... .......... 83% 62.2M 5s 427450K .......... .......... .......... .......... .......... 83% 45.7M 5s 427500K .......... .......... .......... .......... .......... 83% 61.6M 5s 427550K .......... .......... .......... .......... .......... 83% 46.2M 5s 427600K .......... .......... .......... .......... .......... 83% 41.5M 5s 427650K .......... .......... .......... .......... .......... 83% 55.5M 5s 427700K .......... .......... .......... .......... .......... 83% 61.5M 5s 427750K .......... .......... .......... .......... .......... 83% 61.4M 5s 427800K .......... .......... .......... .......... .......... 83% 54.2M 5s 427850K .......... .......... .......... .......... .......... 83% 23.9M 5s 427900K .......... .......... .......... .......... .......... 83% 537M 4s 427950K .......... .......... .......... .......... .......... 83% 379M 4s 428000K .......... .......... .......... .......... .......... 83% 19.2M 4s 428050K .......... .......... .......... .......... .......... 83% 300M 4s 428100K .......... .......... .......... .......... .......... 83% 421M 4s 428150K .......... .......... .......... .......... .......... 83% 60.6M 4s 428200K .......... .......... .......... .......... .......... 84% 26.6M 4s 428250K .......... .......... .......... .......... .......... 84% 428M 4s 428300K .......... .......... .......... .......... .......... 84% 64.8M 4s 428350K .......... .......... .......... .......... .......... 84% 41.1M 4s 428400K .......... .......... .......... .......... .......... 84% 54.4M 4s 428450K .......... .......... .......... .......... .......... 84% 42.4M 4s 428500K .......... .......... .......... .......... .......... 84% 72.1M 4s 428550K .......... .......... .......... .......... .......... 84% 54.0M 4s 428600K .......... .......... .......... .......... .......... 84% 43.0M 4s 428650K .......... .......... .......... .......... .......... 84% 41.6M 4s 428700K .......... .......... .......... .......... .......... 84% 40.9M 4s 428750K .......... .......... .......... .......... .......... 84% 46.6M 4s 428800K .......... .......... .......... .......... .......... 84% 62.4M 4s 428850K .......... .......... .......... .......... .......... 84% 46.0M 4s 428900K .......... .......... .......... .......... .......... 84% 47.2M 4s 428950K .......... .......... .......... .......... .......... 84% 61.5M 4s 429000K .......... .......... .......... .......... .......... 84% 91.8M 4s 429050K .......... .......... .......... .......... .......... 84% 54.7M 4s 429100K .......... .......... .......... .......... .......... 84% 37.1M 4s 429150K .......... .......... .......... .......... .......... 84% 53.2M 4s 429200K .......... .......... .......... .......... .......... 84% 41.6M 4s 429250K .......... .......... .......... .......... .......... 84% 48.8M 4s 429300K .......... .......... .......... .......... .......... 84% 88.0M 4s 429350K .......... .......... .......... .......... .......... 84% 46.1M 4s 429400K .......... .......... .......... .......... .......... 84% 54.7M 4s 429450K .......... .......... .......... .......... .......... 84% 54.1M 4s 429500K .......... .......... .......... .......... .......... 84% 54.3M 4s 429550K .......... .......... .......... .......... .......... 84% 52.9M 4s 429600K .......... .......... .......... .......... .......... 84% 37.0M 4s 429650K .......... .......... .......... .......... .......... 84% 76.3M 4s 429700K .......... .......... .......... .......... .......... 84% 42.5M 4s 429750K .......... .......... .......... .......... .......... 84% 60.8M 4s 429800K .......... .......... .......... .......... .......... 84% 53.5M 4s 429850K .......... .......... .......... .......... .......... 84% 40.9M 4s 429900K .......... .......... .......... .......... .......... 84% 62.0M 4s 429950K .......... .......... .......... .......... .......... 84% 46.7M 4s 430000K .......... .......... .......... .......... .......... 84% 63.2M 4s 430050K .......... .......... .......... .......... .......... 84% 61.3M 4s 430100K .......... .......... .......... .......... .......... 84% 92.5M 4s 430150K .......... .......... .......... .......... .......... 84% 58.5M 4s 430200K .......... .......... .......... .......... .......... 84% 18.9M 4s 430250K .......... .......... .......... .......... .......... 84% 111M 4s 430300K .......... .......... .......... .......... .......... 84% 326M 4s 430350K .......... .......... .......... .......... .......... 84% 279M 4s 430400K .......... .......... .......... .......... .......... 84% 36.8M 4s 430450K .......... .......... .......... .......... .......... 84% 95.2M 4s 430500K .......... .......... .......... .......... .......... 84% 226M 4s 430550K .......... .......... .......... .......... .......... 84% 470M 4s 430600K .......... .......... .......... .......... .......... 84% 36.0M 4s 430650K .......... .......... .......... .......... .......... 84% 94.8M 4s 430700K .......... .......... .......... .......... .......... 84% 432M 4s 430750K .......... .......... .......... .......... .......... 84% 27.2M 4s 430800K .......... .......... .......... .......... .......... 84% 425M 4s 430850K .......... .......... .......... .......... .......... 84% 74.0M 4s 430900K .......... .......... .......... .......... .......... 84% 47.3M 4s 430950K .......... .......... .......... .......... .......... 84% 47.0M 4s 431000K .......... .......... .......... .......... .......... 84% 47.0M 4s 431050K .......... .......... .......... .......... .......... 84% 51.6M 4s 431100K .......... .......... .......... .......... .......... 84% 48.2M 4s 431150K .......... .......... .......... .......... .......... 84% 53.5M 4s 431200K .......... .......... .......... .......... .......... 84% 47.1M 4s 431250K .......... .......... .......... .......... .......... 84% 73.9M 4s 431300K .......... .......... .......... .......... .......... 84% 46.4M 4s 431350K .......... .......... .......... .......... .......... 84% 43.1M 4s 431400K .......... .......... .......... .......... .......... 84% 51.8M 4s 431450K .......... .......... .......... .......... .......... 84% 45.7M 4s 431500K .......... .......... .......... .......... .......... 84% 37.6M 4s 431550K .......... .......... .......... .......... .......... 84% 53.5M 4s 431600K .......... .......... .......... .......... .......... 84% 47.1M 4s 431650K .......... .......... .......... .......... .......... 84% 53.7M 4s 431700K .......... .......... .......... .......... .......... 84% 41.8M 4s 431750K .......... .......... .......... .......... .......... 84% 59.3M 4s 431800K .......... .......... .......... .......... .......... 84% 32.4M 4s 431850K .......... .......... .......... .......... .......... 84% 42.0M 4s 431900K .......... .......... .......... .......... .......... 84% 53.9M 4s 431950K .......... .......... .......... .......... .......... 84% 42.4M 4s 432000K .......... .......... .......... .......... .......... 84% 46.1M 4s 432050K .......... .......... .......... .......... .......... 84% 33.7M 4s 432100K .......... .......... .......... .......... .......... 84% 42.3M 4s 432150K .......... .......... .......... .......... .......... 84% 47.5M 4s 432200K .......... .......... .......... .......... .......... 84% 63.6M 4s 432250K .......... .......... .......... .......... .......... 84% 53.2M 4s 432300K .......... .......... .......... .......... .......... 84% 62.4M 4s 432350K .......... .......... .......... .......... .......... 84% 37.5M 4s 432400K .......... .......... .......... .......... .......... 84% 51.5M 4s 432450K .......... .......... .......... .......... .......... 84% 60.1M 4s 432500K .......... .......... .......... .......... .......... 84% 52.6M 4s 432550K .......... .......... .......... .......... .......... 84% 51.8M 4s 432600K .......... .......... .......... .......... .......... 84% 46.8M 4s 432650K .......... .......... .......... .......... .......... 84% 46.5M 4s 432700K .......... .......... .......... .......... .......... 84% 90.1M 4s 432750K .......... .......... .......... .......... .......... 84% 34.8M 4s 432800K .......... .......... .......... .......... .......... 84% 119M 4s 432850K .......... .......... .......... .......... .......... 84% 62.5M 4s 432900K .......... .......... .......... .......... .......... 84% 47.0M 4s 432950K .......... .......... .......... .......... .......... 84% 53.1M 4s 433000K .......... .......... .......... .......... .......... 84% 24.3M 4s 433050K .......... .......... .......... .......... .......... 84% 493M 4s 433100K .......... .......... .......... .......... .......... 84% 31.4M 4s 433150K .......... .......... .......... .......... .......... 84% 54.6M 4s 433200K .......... .......... .......... .......... .......... 84% 48.3M 4s 433250K .......... .......... .......... .......... .......... 84% 488M 4s 433300K .......... .......... .......... .......... .......... 85% 31.8M 4s 433350K .......... .......... .......... .......... .......... 85% 71.6M 4s 433400K .......... .......... .......... .......... .......... 85% 64.5M 4s 433450K .......... .......... .......... .......... .......... 85% 27.3M 4s 433500K .......... .......... .......... .......... .......... 85% 40.0M 4s 433550K .......... .......... .......... .......... .......... 85% 36.9M 4s 433600K .......... .......... .......... .......... .......... 85% 34.8M 4s 433650K .......... .......... .......... .......... .......... 85% 39.3M 4s 433700K .......... .......... .......... .......... .......... 85% 32.1M 4s 433750K .......... .......... .......... .......... .......... 85% 32.0M 4s 433800K .......... .......... .......... .......... .......... 85% 42.2M 4s 433850K .......... .......... .......... .......... .......... 85% 38.3M 4s 433900K .......... .......... .......... .......... .......... 85% 22.0M 4s 433950K .......... .......... .......... .......... .......... 85% 33.5M 4s 434000K .......... .......... .......... .......... .......... 85% 53.1M 4s 434050K .......... .......... .......... .......... .......... 85% 34.5M 4s 434100K .......... .......... .......... .......... .......... 85% 31.5M 4s 434150K .......... .......... .......... .......... .......... 85% 34.2M 4s 434200K .......... .......... .......... .......... .......... 85% 26.4M 4s 434250K .......... .......... .......... .......... .......... 85% 47.3M 4s 434300K .......... .......... .......... .......... .......... 85% 31.1M 4s 434350K .......... .......... .......... .......... .......... 85% 40.9M 4s 434400K .......... .......... .......... .......... .......... 85% 34.2M 4s 434450K .......... .......... .......... .......... .......... 85% 37.0M 4s 434500K .......... .......... .......... .......... .......... 85% 42.0M 4s 434550K .......... .......... .......... .......... .......... 85% 27.2M 4s 434600K .......... .......... .......... .......... .......... 85% 54.7M 4s 434650K .......... .......... .......... .......... .......... 85% 54.7M 4s 434700K .......... .......... .......... .......... .......... 85% 73.3M 4s 434750K .......... .......... .......... .......... .......... 85% 73.4M 4s 434800K .......... .......... .......... .......... .......... 85% 49.8M 4s 434850K .......... .......... .......... .......... .......... 85% 66.0M 4s 434900K .......... .......... .......... .......... .......... 85% 112M 4s 434950K .......... .......... .......... .......... .......... 85% 21.5M 4s 435000K .......... .......... .......... .......... .......... 85% 94.8M 4s 435050K .......... .......... .......... .......... .......... 85% 41.8M 4s 435100K .......... .......... .......... .......... .......... 85% 42.5M 4s 435150K .......... .......... .......... .......... .......... 85% 381M 4s 435200K .......... .......... .......... .......... .......... 85% 27.2M 4s 435250K .......... .......... .......... .......... .......... 85% 96.7M 4s 435300K .......... .......... .......... .......... .......... 85% 323M 4s 435350K .......... .......... .......... .......... .......... 85% 35.2M 4s 435400K .......... .......... .......... .......... .......... 85% 135M 4s 435450K .......... .......... .......... .......... .......... 85% 33.7M 4s 435500K .......... .......... .......... .......... .......... 85% 38.1M 4s 435550K .......... .......... .......... .......... .......... 85% 40.6M 4s 435600K .......... .......... .......... .......... .......... 85% 42.5M 4s 435650K .......... .......... .......... .......... .......... 85% 41.5M 4s 435700K .......... .......... .......... .......... .......... 85% 31.1M 4s 435750K .......... .......... .......... .......... .......... 85% 43.6M 4s 435800K .......... .......... .......... .......... .......... 85% 45.4M 4s 435850K .......... .......... .......... .......... .......... 85% 33.7M 4s 435900K .......... .......... .......... .......... .......... 85% 37.4M 4s 435950K .......... .......... .......... .......... .......... 85% 40.9M 4s 436000K .......... .......... .......... .......... .......... 85% 26.9M 4s 436050K .......... .......... .......... .......... .......... 85% 46.6M 4s 436100K .......... .......... .......... .......... .......... 85% 42.6M 4s 436150K .......... .......... .......... .......... .......... 85% 33.6M 4s 436200K .......... .......... .......... .......... .......... 85% 33.1M 4s 436250K .......... .......... .......... .......... .......... 85% 59.4M 4s 436300K .......... .......... .......... .......... .......... 85% 41.7M 4s 436350K .......... .......... .......... .......... .......... 85% 30.7M 4s 436400K .......... .......... .......... .......... .......... 85% 33.8M 4s 436450K .......... .......... .......... .......... .......... 85% 29.8M 4s 436500K .......... .......... .......... .......... .......... 85% 29.6M 4s 436550K .......... .......... .......... .......... .......... 85% 61.6M 4s 436600K .......... .......... .......... .......... .......... 85% 31.4M 4s 436650K .......... .......... .......... .......... .......... 85% 43.8M 4s 436700K .......... .......... .......... .......... .......... 85% 29.3M 4s 436750K .......... .......... .......... .......... .......... 85% 52.6M 4s 436800K .......... .......... .......... .......... .......... 85% 36.9M 4s 436850K .......... .......... .......... .......... .......... 85% 18.1M 4s 436900K .......... .......... .......... .......... .......... 85% 127M 4s 436950K .......... .......... .......... .......... .......... 85% 165M 4s 437000K .......... .......... .......... .......... .......... 85% 27.2M 4s 437050K .......... .......... .......... .......... .......... 85% 82.5M 4s 437100K .......... .......... .......... .......... .......... 85% 25.2M 4s 437150K .......... .......... .......... .......... .......... 85% 30.5M 4s 437200K .......... .......... .......... .......... .......... 85% 46.8M 4s 437250K .......... .......... .......... .......... .......... 85% 117M 4s 437300K .......... .......... .......... .......... .......... 85% 37.8M 4s 437350K .......... .......... .......... .......... .......... 85% 31.9M 4s 437400K .......... .......... .......... .......... .......... 85% 41.7M 4s 437450K .......... .......... .......... .......... .......... 85% 30.7M 4s 437500K .......... .......... .......... .......... .......... 85% 46.0M 4s 437550K .......... .......... .......... .......... .......... 85% 46.7M 4s 437600K .......... .......... .......... .......... .......... 85% 34.9M 4s 437650K .......... .......... .......... .......... .......... 85% 41.6M 4s 437700K .......... .......... .......... .......... .......... 85% 16.3M 4s 437750K .......... .......... .......... .......... .......... 85% 48.6M 4s 437800K .......... .......... .......... .......... .......... 85% 104M 4s 437850K .......... .......... .......... .......... .......... 85% 42.7M 4s 437900K .......... .......... .......... .......... .......... 85% 46.5M 4s 437950K .......... .......... .......... .......... .......... 85% 35.7M 4s 438000K .......... .......... .......... .......... .......... 85% 51.5M 4s 438050K .......... .......... .......... .......... .......... 85% 50.1M 4s 438100K .......... .......... .......... .......... .......... 85% 36.0M 4s 438150K .......... .......... .......... .......... .......... 85% 38.8M 4s 438200K .......... .......... .......... .......... .......... 85% 34.6M 4s 438250K .......... .......... .......... .......... .......... 85% 77.9M 4s 438300K .......... .......... .......... .......... .......... 85% 24.5M 4s 438350K .......... .......... .......... .......... .......... 85% 45.5M 4s 438400K .......... .......... .......... .......... .......... 86% 34.5M 4s 438450K .......... .......... .......... .......... .......... 86% 46.1M 4s 438500K .......... .......... .......... .......... .......... 86% 80.4M 4s 438550K .......... .......... .......... .......... .......... 86% 55.6M 4s 438600K .......... .......... .......... .......... .......... 86% 74.9M 4s 438650K .......... .......... .......... .......... .......... 86% 68.4M 4s 438700K .......... .......... .......... .......... .......... 86% 103M 4s 438750K .......... .......... .......... .......... .......... 86% 98.4M 4s 438800K .......... .......... .......... .......... .......... 86% 54.6M 4s 438850K .......... .......... .......... .......... .......... 86% 123M 4s 438900K .......... .......... .......... .......... .......... 86% 75.9M 4s 438950K .......... .......... .......... .......... .......... 86% 48.9M 4s 439000K .......... .......... .......... .......... .......... 86% 95.0M 4s 439050K .......... .......... .......... .......... .......... 86% 63.8M 4s 439100K .......... .......... .......... .......... .......... 86% 74.7M 4s 439150K .......... .......... .......... .......... .......... 86% 99.0M 4s 439200K .......... .......... .......... .......... .......... 86% 20.8M 4s 439250K .......... .......... .......... .......... .......... 86% 531M 4s 439300K .......... .......... .......... .......... .......... 86% 62.7M 4s 439350K .......... .......... .......... .......... .......... 86% 303M 4s 439400K .......... .......... .......... .......... .......... 86% 244M 4s 439450K .......... .......... .......... .......... .......... 86% 40.0M 4s 439500K .......... .......... .......... .......... .......... 86% 104M 4s 439550K .......... .......... .......... .......... .......... 86% 87.0M 4s 439600K .......... .......... .......... .......... .......... 86% 394M 4s 439650K .......... .......... .......... .......... .......... 86% 78.9M 4s 439700K .......... .......... .......... .......... .......... 86% 76.8M 4s 439750K .......... .......... .......... .......... .......... 86% 77.5M 4s 439800K .......... .......... .......... .......... .......... 86% 72.4M 4s 439850K .......... .......... .......... .......... .......... 86% 64.1M 4s 439900K .......... .......... .......... .......... .......... 86% 63.9M 4s 439950K .......... .......... .......... .......... .......... 86% 76.4M 4s 440000K .......... .......... .......... .......... .......... 86% 64.1M 4s 440050K .......... .......... .......... .......... .......... 86% 75.5M 4s 440100K .......... .......... .......... .......... .......... 86% 72.1M 4s 440150K .......... .......... .......... .......... .......... 86% 65.3M 4s 440200K .......... .......... .......... .......... .......... 86% 76.4M 4s 440250K .......... .......... .......... .......... .......... 86% 64.8M 4s 440300K .......... .......... .......... .......... .......... 86% 64.6M 4s 440350K .......... .......... .......... .......... .......... 86% 74.8M 4s 440400K .......... .......... .......... .......... .......... 86% 64.8M 4s 440450K .......... .......... .......... .......... .......... 86% 63.7M 4s 440500K .......... .......... .......... .......... .......... 86% 74.2M 4s 440550K .......... .......... .......... .......... .......... 86% 77.4M 4s 440600K .......... .......... .......... .......... .......... 86% 62.9M 4s 440650K .......... .......... .......... .......... .......... 86% 79.0M 4s 440700K .......... .......... .......... .......... .......... 86% 54.7M 4s 440750K .......... .......... .......... .......... .......... 86% 28.9M 4s 440800K .......... .......... .......... .......... .......... 86% 470M 4s 440850K .......... .......... .......... .......... .......... 86% 326M 4s 440900K .......... .......... .......... .......... .......... 86% 53.8M 4s 440950K .......... .......... .......... .......... .......... 86% 61.5M 4s 441000K .......... .......... .......... .......... .......... 86% 63.6M 4s 441050K .......... .......... .......... .......... .......... 86% 75.5M 4s 441100K .......... .......... .......... .......... .......... 86% 59.3M 4s 441150K .......... .......... .......... .......... .......... 86% 48.2M 4s 441200K .......... .......... .......... .......... .......... 86% 74.3M 4s 441250K .......... .......... .......... .......... .......... 86% 62.5M 4s 441300K .......... .......... .......... .......... .......... 86% 94.6M 4s 441350K .......... .......... .......... .......... .......... 86% 54.5M 4s 441400K .......... .......... .......... .......... .......... 86% 55.6M 4s 441450K .......... .......... .......... .......... .......... 86% 54.6M 4s 441500K .......... .......... .......... .......... .......... 86% 95.6M 4s 441550K .......... .......... .......... .......... .......... 86% 74.2M 4s 441600K .......... .......... .......... .......... .......... 86% 55.9M 4s 441650K .......... .......... .......... .......... .......... 86% 62.4M 4s 441700K .......... .......... .......... .......... .......... 86% 43.0M 4s 441750K .......... .......... .......... .......... .......... 86% 55.0M 4s 441800K .......... .......... .......... .......... .......... 86% 93.4M 4s 441850K .......... .......... .......... .......... .......... 86% 54.0M 4s 441900K .......... .......... .......... .......... .......... 86% 75.8M 4s 441950K .......... .......... .......... .......... .......... 86% 52.1M 4s 442000K .......... .......... .......... .......... .......... 86% 72.4M 4s 442050K .......... .......... .......... .......... .......... 86% 75.4M 4s 442100K .......... .......... .......... .......... .......... 86% 53.2M 4s 442150K .......... .......... .......... .......... .......... 86% 43.0M 4s 442200K .......... .......... .......... .......... .......... 86% 34.1M 4s 442250K .......... .......... .......... .......... .......... 86% 124M 4s 442300K .......... .......... .......... .......... .......... 86% 13.3M 4s 442350K .......... .......... .......... .......... .......... 86% 404M 4s 442400K .......... .......... .......... .......... .......... 86% 40.2M 4s 442450K .......... .......... .......... .......... .......... 86% 41.4M 4s 442500K .......... .......... .......... .......... .......... 86% 41.8M 4s 442550K .......... .......... .......... .......... .......... 86% 43.1M 4s 442600K .......... .......... .......... .......... .......... 86% 42.1M 4s 442650K .......... .......... .......... .......... .......... 86% 42.2M 4s 442700K .......... .......... .......... .......... .......... 86% 45.3M 4s 442750K .......... .......... .......... .......... .......... 86% 40.8M 4s 442800K .......... .......... .......... .......... .......... 86% 29.4M 4s 442850K .......... .......... .......... .......... .......... 86% 37.2M 4s 442900K .......... .......... .......... .......... .......... 86% 37.7M 4s 442950K .......... .......... .......... .......... .......... 86% 46.2M 4s 443000K .......... .......... .......... .......... .......... 86% 28.7M 4s 443050K .......... .......... .......... .......... .......... 86% 54.3M 4s 443100K .......... .......... .......... .......... .......... 86% 47.0M 4s 443150K .......... .......... .......... .......... .......... 86% 28.7M 4s 443200K .......... .......... .......... .......... .......... 86% 38.5M 4s 443250K .......... .......... .......... .......... .......... 86% 34.2M 4s 443300K .......... .......... .......... .......... .......... 86% 42.6M 4s 443350K .......... .......... .......... .......... .......... 86% 38.0M 4s 443400K .......... .......... .......... .......... .......... 86% 42.6M 4s 443450K .......... .......... .......... .......... .......... 86% 47.5M 4s 443500K .......... .......... .......... .......... .......... 87% 31.9M 4s 443550K .......... .......... .......... .......... .......... 87% 42.4M 4s 443600K .......... .......... .......... .......... .......... 87% 33.3M 4s 443650K .......... .......... .......... .......... .......... 87% 45.4M 4s 443700K .......... .......... .......... .......... .......... 87% 29.3M 4s 443750K .......... .......... .......... .......... .......... 87% 46.6M 4s 443800K .......... .......... .......... .......... .......... 87% 33.5M 4s 443850K .......... .......... .......... .......... .......... 87% 38.1M 4s 443900K .......... .......... .......... .......... .......... 87% 33.9M 4s 443950K .......... .......... .......... .......... .......... 87% 42.3M 4s 444000K .......... .......... .......... .......... .......... 87% 47.3M 4s 444050K .......... .......... .......... .......... .......... 87% 33.5M 4s 444100K .......... .......... .......... .......... .......... 87% 39.4M 4s 444150K .......... .......... .......... .......... .......... 87% 54.6M 4s 444200K .......... .......... .......... .......... .......... 87% 37.4M 4s 444250K .......... .......... .......... .......... .......... 87% 37.8M 4s 444300K .......... .......... .......... .......... .......... 87% 46.7M 4s 444350K .......... .......... .......... .......... .......... 87% 48.0M 4s 444400K .......... .......... .......... .......... .......... 87% 42.1M 4s 444450K .......... .......... .......... .......... .......... 87% 114M 4s 444500K .......... .......... .......... .......... .......... 87% 17.0M 4s 444550K .......... .......... .......... .......... .......... 87% 483M 3s 444600K .......... .......... .......... .......... .......... 87% 71.9M 3s 444650K .......... .......... .......... .......... .......... 87% 35.4M 3s 444700K .......... .......... .......... .......... .......... 87% 63.3M 3s 444750K .......... .......... .......... .......... .......... 87% 46.6M 3s 444800K .......... .......... .......... .......... .......... 87% 63.7M 3s 444850K .......... .......... .......... .......... .......... 87% 55.4M 3s 444900K .......... .......... .......... .......... .......... 87% 28.6M 3s 444950K .......... .......... .......... .......... .......... 87% 39.5M 3s 445000K .......... .......... .......... .......... .......... 87% 33.6M 3s 445050K .......... .......... .......... .......... .......... 87% 38.6M 3s 445100K .......... .......... .......... .......... .......... 87% 25.3M 3s 445150K .......... .......... .......... .......... .......... 87% 37.8M 3s 445200K .......... .......... .......... .......... .......... 87% 30.3M 3s 445250K .......... .......... .......... .......... .......... 87% 28.8M 3s 445300K .......... .......... .......... .......... .......... 87% 45.6M 3s 445350K .......... .......... .......... .......... .......... 87% 28.7M 3s 445400K .......... .......... .......... .......... .......... 87% 52.5M 3s 445450K .......... .......... .......... .......... .......... 87% 27.3M 3s 445500K .......... .......... .......... .......... .......... 87% 31.2M 3s 445550K .......... .......... .......... .......... .......... 87% 53.2M 3s 445600K .......... .......... .......... .......... .......... 87% 26.5M 3s 445650K .......... .......... .......... .......... .......... 87% 52.0M 3s 445700K .......... .......... .......... .......... .......... 87% 26.8M 3s 445750K .......... .......... .......... .......... .......... 87% 47.8M 3s 445800K .......... .......... .......... .......... .......... 87% 29.3M 3s 445850K .......... .......... .......... .......... .......... 87% 25.5M 3s 445900K .......... .......... .......... .......... .......... 87% 50.9M 3s 445950K .......... .......... .......... .......... .......... 87% 29.1M 3s 446000K .......... .......... .......... .......... .......... 87% 47.1M 3s 446050K .......... .......... .......... .......... .......... 87% 33.1M 3s 446100K .......... .......... .......... .......... .......... 87% 28.7M 3s 446150K .......... .......... .......... .......... .......... 87% 38.6M 3s 446200K .......... .......... .......... .......... .......... 87% 31.8M 3s 446250K .......... .......... .......... .......... .......... 87% 24.2M 3s 446300K .......... .......... .......... .......... .......... 87% 92.5M 3s 446350K .......... .......... .......... .......... .......... 87% 96.3M 3s 446400K .......... .......... .......... .......... .......... 87% 31.2M 3s 446450K .......... .......... .......... .......... .......... 87% 16.3M 3s 446500K .......... .......... .......... .......... .......... 87% 230M 3s 446550K .......... .......... .......... .......... .......... 87% 410M 3s 446600K .......... .......... .......... .......... .......... 87% 29.9M 3s 446650K .......... .......... .......... .......... .......... 87% 156M 3s 446700K .......... .......... .......... .......... .......... 87% 27.5M 3s 446750K .......... .......... .......... .......... .......... 87% 61.5M 3s 446800K .......... .......... .......... .......... .......... 87% 41.1M 3s 446850K .......... .......... .......... .......... .......... 87% 31.1M 3s 446900K .......... .......... .......... .......... .......... 87% 46.1M 3s 446950K .......... .......... .......... .......... .......... 87% 41.1M 3s 447000K .......... .......... .......... .......... .......... 87% 31.4M 3s 447050K .......... .......... .......... .......... .......... 87% 47.0M 3s 447100K .......... .......... .......... .......... .......... 87% 28.3M 3s 447150K .......... .......... .......... .......... .......... 87% 42.6M 3s 447200K .......... .......... .......... .......... .......... 87% 34.4M 3s 447250K .......... .......... .......... .......... .......... 87% 40.4M 3s 447300K .......... .......... .......... .......... .......... 87% 48.2M 3s 447350K .......... .......... .......... .......... .......... 87% 38.0M 3s 447400K .......... .......... .......... .......... .......... 87% 31.3M 3s 447450K .......... .......... .......... .......... .......... 87% 44.4M 3s 447500K .......... .......... .......... .......... .......... 87% 25.7M 3s 447550K .......... .......... .......... .......... .......... 87% 53.2M 3s 447600K .......... .......... .......... .......... .......... 87% 41.9M 3s 447650K .......... .......... .......... .......... .......... 87% 46.2M 3s 447700K .......... .......... .......... .......... .......... 87% 27.6M 3s 447750K .......... .......... .......... .......... .......... 87% 44.7M 3s 447800K .......... .......... .......... .......... .......... 87% 48.8M 3s 447850K .......... .......... .......... .......... .......... 87% 25.4M 3s 447900K .......... .......... .......... .......... .......... 87% 47.6M 3s 447950K .......... .......... .......... .......... .......... 87% 41.8M 3s 448000K .......... .......... .......... .......... .......... 87% 28.9M 3s 448050K .......... .......... .......... .......... .......... 87% 47.5M 3s 448100K .......... .......... .......... .......... .......... 87% 42.2M 3s 448150K .......... .......... .......... .......... .......... 87% 124M 3s 448200K .......... .......... .......... .......... .......... 87% 41.2M 3s 448250K .......... .......... .......... .......... .......... 87% 121M 3s 448300K .......... .......... .......... .......... .......... 87% 41.3M 3s 448350K .......... .......... .......... .......... .......... 87% 113M 3s 448400K .......... .......... .......... .......... .......... 87% 23.3M 3s 448450K .......... .......... .......... .......... .......... 87% 47.3M 3s 448500K .......... .......... .......... .......... .......... 87% 432M 3s 448550K .......... .......... .......... .......... .......... 87% 36.5M 3s 448600K .......... .......... .......... .......... .......... 88% 82.3M 3s 448650K .......... .......... .......... .......... .......... 88% 498M 3s 448700K .......... .......... .......... .......... .......... 88% 24.7M 3s 448750K .......... .......... .......... .......... .......... 88% 168M 3s 448800K .......... .......... .......... .......... .......... 88% 61.0M 3s 448850K .......... .......... .......... .......... .......... 88% 34.9M 3s 448900K .......... .......... .......... .......... .......... 88% 42.5M 3s 448950K .......... .......... .......... .......... .......... 88% 31.2M 3s 449000K .......... .......... .......... .......... .......... 88% 45.9M 3s 449050K .......... .......... .......... .......... .......... 88% 27.3M 3s 449100K .......... .......... .......... .......... .......... 88% 46.1M 3s 449150K .......... .......... .......... .......... .......... 88% 29.2M 3s 449200K .......... .......... .......... .......... .......... 88% 29.7M 3s 449250K .......... .......... .......... .......... .......... 88% 32.0M 3s 449300K .......... .......... .......... .......... .......... 88% 46.2M 3s 449350K .......... .......... .......... .......... .......... 88% 28.8M 3s 449400K .......... .......... .......... .......... .......... 88% 41.5M 3s 449450K .......... .......... .......... .......... .......... 88% 24.9M 3s 449500K .......... .......... .......... .......... .......... 88% 49.4M 3s 449550K .......... .......... .......... .......... .......... 88% 29.0M 3s 449600K .......... .......... .......... .......... .......... 88% 29.2M 3s 449650K .......... .......... .......... .......... .......... 88% 46.4M 3s 449700K .......... .......... .......... .......... .......... 88% 30.6M 3s 449750K .......... .......... .......... .......... .......... 88% 41.7M 3s 449800K .......... .......... .......... .......... .......... 88% 31.4M 3s 449850K .......... .......... .......... .......... .......... 88% 22.6M 3s 449900K .......... .......... .......... .......... .......... 88% 24.5M 3s 449950K .......... .......... .......... .......... .......... 88% 48.0M 3s 450000K .......... .......... .......... .......... .......... 88% 51.6M 3s 450050K .......... .......... .......... .......... .......... 88% 47.0M 3s 450100K .......... .......... .......... .......... .......... 88% 47.3M 3s 450150K .......... .......... .......... .......... .......... 88% 115M 3s 450200K .......... .......... .......... .......... .......... 88% 18.4M 3s 450250K .......... .......... .......... .......... .......... 88% 509M 3s 450300K .......... .......... .......... .......... .......... 88% 87.7M 3s 450350K .......... .......... .......... .......... .......... 88% 425M 3s 450400K .......... .......... .......... .......... .......... 88% 474M 3s 450450K .......... .......... .......... .......... .......... 88% 25.4M 3s 450500K .......... .......... .......... .......... .......... 88% 432M 3s 450550K .......... .......... .......... .......... .......... 88% 52.8M 3s 450600K .......... .......... .......... .......... .......... 88% 388M 3s 450650K .......... .......... .......... .......... .......... 88% 48.4M 3s 450700K .......... .......... .......... .......... .......... 88% 41.6M 3s 450750K .......... .......... .......... .......... .......... 88% 63.6M 3s 450800K .......... .......... .......... .......... .......... 88% 69.7M 3s 450850K .......... .......... .......... .......... .......... 88% 53.0M 3s 450900K .......... .......... .......... .......... .......... 88% 45.0M 3s 450950K .......... .......... .......... .......... .......... 88% 52.4M 3s 451000K .......... .......... .......... .......... .......... 88% 54.3M 3s 451050K .......... .......... .......... .......... .......... 88% 52.8M 3s 451100K .......... .......... .......... .......... .......... 88% 53.6M 3s 451150K .......... .......... .......... .......... .......... 88% 41.5M 3s 451200K .......... .......... .......... .......... .......... 88% 54.4M 3s 451250K .......... .......... .......... .......... .......... 88% 54.0M 3s 451300K .......... .......... .......... .......... .......... 88% 53.3M 3s 451350K .......... .......... .......... .......... .......... 88% 59.1M 3s 451400K .......... .......... .......... .......... .......... 88% 54.1M 3s 451450K .......... .......... .......... .......... .......... 88% 41.2M 3s 451500K .......... .......... .......... .......... .......... 88% 40.4M 3s 451550K .......... .......... .......... .......... .......... 88% 60.5M 3s 451600K .......... .......... .......... .......... .......... 88% 54.8M 3s 451650K .......... .......... .......... .......... .......... 88% 54.2M 3s 451700K .......... .......... .......... .......... .......... 88% 46.7M 3s 451750K .......... .......... .......... .......... .......... 88% 55.4M 3s 451800K .......... .......... .......... .......... .......... 88% 53.1M 3s 451850K .......... .......... .......... .......... .......... 88% 52.8M 3s 451900K .......... .......... .......... .......... .......... 88% 54.7M 3s 451950K .......... .......... .......... .......... .......... 88% 40.9M 3s 452000K .......... .......... .......... .......... .......... 88% 46.2M 3s 452050K .......... .......... .......... .......... .......... 88% 95.2M 3s 452100K .......... .......... .......... .......... .......... 88% 36.4M 3s 452150K .......... .......... .......... .......... .......... 88% 92.7M 3s 452200K .......... .......... .......... .......... .......... 88% 52.4M 3s 452250K .......... .......... .......... .......... .......... 88% 48.9M 3s 452300K .......... .......... .......... .......... .......... 88% 61.0M 3s 452350K .......... .......... .......... .......... .......... 88% 47.4M 3s 452400K .......... .......... .......... .......... .......... 88% 54.0M 3s 452450K .......... .......... .......... .......... .......... 88% 52.1M 3s 452500K .......... .......... .......... .......... .......... 88% 47.6M 3s 452550K .......... .......... .......... .......... .......... 88% 47.5M 3s 452600K .......... .......... .......... .......... .......... 88% 61.9M 3s 452650K .......... .......... .......... .......... .......... 88% 19.2M 3s 452700K .......... .......... .......... .......... .......... 88% 305M 3s 452750K .......... .......... .......... .......... .......... 88% 400M 3s 452800K .......... .......... .......... .......... .......... 88% 21.9M 3s 452850K .......... .......... .......... .......... .......... 88% 321M 3s 452900K .......... .......... .......... .......... .......... 88% 404M 3s 452950K .......... .......... .......... .......... .......... 88% 23.4M 3s 453000K .......... .......... .......... .......... .......... 88% 397M 3s 453050K .......... .......... .......... .......... .......... 88% 52.5M 3s 453100K .......... .......... .......... .......... .......... 88% 67.7M 3s 453150K .......... .......... .......... .......... .......... 88% 37.2M 3s 453200K .......... .......... .......... .......... .......... 88% 46.5M 3s 453250K .......... .......... .......... .......... .......... 88% 46.9M 3s 453300K .......... .......... .......... .......... .......... 88% 44.9M 3s 453350K .......... .......... .......... .......... .......... 88% 33.6M 3s 453400K .......... .......... .......... .......... .......... 88% 48.7M 3s 453450K .......... .......... .......... .......... .......... 88% 37.9M 3s 453500K .......... .......... .......... .......... .......... 88% 42.1M 3s 453550K .......... .......... .......... .......... .......... 88% 51.6M 3s 453600K .......... .......... .......... .......... .......... 88% 48.0M 3s 453650K .......... .......... .......... .......... .......... 88% 47.8M 3s 453700K .......... .......... .......... .......... .......... 89% 31.9M 3s 453750K .......... .......... .......... .......... .......... 89% 34.0M 3s 453800K .......... .......... .......... .......... .......... 89% 52.8M 3s 453850K .......... .......... .......... .......... .......... 89% 48.3M 3s 453900K .......... .......... .......... .......... .......... 89% 34.7M 3s 453950K .......... .......... .......... .......... .......... 89% 46.3M 3s 454000K .......... .......... .......... .......... .......... 89% 41.2M 3s 454050K .......... .......... .......... .......... .......... 89% 29.5M 3s 454100K .......... .......... .......... .......... .......... 89% 52.3M 3s 454150K .......... .......... .......... .......... .......... 89% 41.2M 3s 454200K .......... .......... .......... .......... .......... 89% 40.4M 3s 454250K .......... .......... .......... .......... .......... 89% 38.6M 3s 454300K .......... .......... .......... .......... .......... 89% 46.2M 3s 454350K .......... .......... .......... .......... .......... 89% 40.8M 3s 454400K .......... .......... .......... .......... .......... 89% 41.3M 3s 454450K .......... .......... .......... .......... .......... 89% 38.1M 3s 454500K .......... .......... .......... .......... .......... 89% 25.0M 3s 454550K .......... .......... .......... .......... .......... 89% 26.9M 3s 454600K .......... .......... .......... .......... .......... 89% 17.4M 3s 454650K .......... .......... .......... .......... .......... 89% 46.4M 3s 454700K .......... .......... .......... .......... .......... 89% 14.9M 3s 454750K .......... .......... .......... .......... .......... 89% 440M 3s 454800K .......... .......... .......... .......... .......... 89% 11.7M 3s 454850K .......... .......... .......... .......... .......... 89% 432M 3s 454900K .......... .......... .......... .......... .......... 89% 29.6M 3s 454950K .......... .......... .......... .......... .......... 89% 25.3M 3s 455000K .......... .......... .......... .......... .......... 89% 25.5M 3s 455050K .......... .......... .......... .......... .......... 89% 37.2M 3s 455100K .......... .......... .......... .......... .......... 89% 26.7M 3s 455150K .......... .......... .......... .......... .......... 89% 27.5M 3s 455200K .......... .......... .......... .......... .......... 89% 27.0M 3s 455250K .......... .......... .......... .......... .......... 89% 34.0M 3s 455300K .......... .......... .......... .......... .......... 89% 25.1M 3s 455350K .......... .......... .......... .......... .......... 89% 26.0M 3s 455400K .......... .......... .......... .......... .......... 89% 40.5M 3s 455450K .......... .......... .......... .......... .......... 89% 25.6M 3s 455500K .......... .......... .......... .......... .......... 89% 47.5M 3s 455550K .......... .......... .......... .......... .......... 89% 27.2M 3s 455600K .......... .......... .......... .......... .......... 89% 25.8M 3s 455650K .......... .......... .......... .......... .......... 89% 36.5M 3s 455700K .......... .......... .......... .......... .......... 89% 23.6M 3s 455750K .......... .......... .......... .......... .......... 89% 29.0M 3s 455800K .......... .......... .......... .......... .......... 89% 40.4M 3s 455850K .......... .......... .......... .......... .......... 89% 23.6M 3s 455900K .......... .......... .......... .......... .......... 89% 32.6M 3s 455950K .......... .......... .......... .......... .......... 89% 32.4M 3s 456000K .......... .......... .......... .......... .......... 89% 38.3M 3s 456050K .......... .......... .......... .......... .......... 89% 68.9M 3s 456100K .......... .......... .......... .......... .......... 89% 34.6M 3s 456150K .......... .......... .......... .......... .......... 89% 66.2M 3s 456200K .......... .......... .......... .......... .......... 89% 47.8M 3s 456250K .......... .......... .......... .......... .......... 89% 62.2M 3s 456300K .......... .......... .......... .......... .......... 89% 37.9M 3s 456350K .......... .......... .......... .......... .......... 89% 19.9M 3s 456400K .......... .......... .......... .......... .......... 89% 537M 3s 456450K .......... .......... .......... .......... .......... 89% 39.9M 3s 456500K .......... .......... .......... .......... .......... 89% 24.5M 3s 456550K .......... .......... .......... .......... .......... 89% 40.1M 3s 456600K .......... .......... .......... .......... .......... 89% 92.5M 3s 456650K .......... .......... .......... .......... .......... 89% 45.4M 3s 456700K .......... .......... .......... .......... .......... 89% 34.1M 3s 456750K .......... .......... .......... .......... .......... 89% 34.1M 3s 456800K .......... .......... .......... .......... .......... 89% 40.0M 3s 456850K .......... .......... .......... .......... .......... 89% 29.0M 3s 456900K .......... .......... .......... .......... .......... 89% 38.2M 3s 456950K .......... .......... .......... .......... .......... 89% 41.7M 3s 457000K .......... .......... .......... .......... .......... 89% 26.8M 3s 457050K .......... .......... .......... .......... .......... 89% 45.0M 3s 457100K .......... .......... .......... .......... .......... 89% 43.2M 3s 457150K .......... .......... .......... .......... .......... 89% 51.4M 3s 457200K .......... .......... .......... .......... .......... 89% 31.3M 3s 457250K .......... .......... .......... .......... .......... 89% 46.0M 3s 457300K .......... .......... .......... .......... .......... 89% 41.9M 3s 457350K .......... .......... .......... .......... .......... 89% 34.2M 3s 457400K .......... .......... .......... .......... .......... 89% 41.3M 3s 457450K .......... .......... .......... .......... .......... 89% 46.0M 3s 457500K .......... .......... .......... .......... .......... 89% 40.4M 3s 457550K .......... .......... .......... .......... .......... 89% 40.6M 3s 457600K .......... .......... .......... .......... .......... 89% 38.6M 3s 457650K .......... .......... .......... .......... .......... 89% 41.0M 3s 457700K .......... .......... .......... .......... .......... 89% 28.5M 3s 457750K .......... .......... .......... .......... .......... 89% 46.2M 3s 457800K .......... .......... .......... .......... .......... 89% 45.4M 3s 457850K .......... .......... .......... .......... .......... 89% 41.3M 3s 457900K .......... .......... .......... .......... .......... 89% 46.8M 3s 457950K .......... .......... .......... .......... .......... 89% 31.3M 3s 458000K .......... .......... .......... .......... .......... 89% 50.2M 3s 458050K .......... .......... .......... .......... .......... 89% 34.3M 3s 458100K .......... .......... .......... .......... .......... 89% 48.6M 3s 458150K .......... .......... .......... .......... .......... 89% 54.0M 3s 458200K .......... .......... .......... .......... .......... 89% 45.5M 3s 458250K .......... .......... .......... .......... .......... 89% 93.7M 3s 458300K .......... .......... .......... .......... .......... 89% 88.1M 3s 458350K .......... .......... .......... .......... .......... 89% 22.5M 3s 458400K .......... .......... .......... .......... .......... 89% 179M 3s 458450K .......... .......... .......... .......... .......... 89% 407M 3s 458500K .......... .......... .......... .......... .......... 89% 222M 3s 458550K .......... .......... .......... .......... .......... 89% 26.1M 3s 458600K .......... .......... .......... .......... .......... 89% 114M 3s 458650K .......... .......... .......... .......... .......... 89% 470M 3s 458700K .......... .......... .......... .......... .......... 89% 109M 3s 458750K .......... .......... .......... .......... .......... 89% 77.1M 3s 458800K .......... .......... .......... .......... .......... 90% 74.0M 3s 458850K .......... .......... .......... .......... .......... 90% 70.4M 3s 458900K .......... .......... .......... .......... .......... 90% 47.9M 3s 458950K .......... .......... .......... .......... .......... 90% 61.7M 3s 459000K .......... .......... .......... .......... .......... 90% 124M 3s 459050K .......... .......... .......... .......... .......... 90% 64.1M 3s 459100K .......... .......... .......... .......... .......... 90% 61.0M 3s 459150K .......... .......... .......... .......... .......... 90% 92.1M 3s 459200K .......... .......... .......... .......... .......... 90% 73.9M 3s 459250K .......... .......... .......... .......... .......... 90% 74.8M 3s 459300K .......... .......... .......... .......... .......... 90% 76.1M 3s 459350K .......... .......... .......... .......... .......... 90% 62.0M 3s 459400K .......... .......... .......... .......... .......... 90% 74.4M 3s 459450K .......... .......... .......... .......... .......... 90% 76.8M 3s 459500K .......... .......... .......... .......... .......... 90% 61.7M 3s 459550K .......... .......... .......... .......... .......... 90% 89.9M 3s 459600K .......... .......... .......... .......... .......... 90% 53.4M 3s 459650K .......... .......... .......... .......... .......... 90% 89.4M 3s 459700K .......... .......... .......... .......... .......... 90% 61.6M 3s 459750K .......... .......... .......... .......... .......... 90% 73.0M 3s 459800K .......... .......... .......... .......... .......... 90% 94.4M 3s 459850K .......... .......... .......... .......... .......... 90% 54.9M 3s 459900K .......... .......... .......... .......... .......... 90% 75.1M 3s 459950K .......... .......... .......... .......... .......... 90% 63.5M 3s 460000K .......... .......... .......... .......... .......... 90% 61.0M 3s 460050K .......... .......... .......... .......... .......... 90% 125M 3s 460100K .......... .......... .......... .......... .......... 90% 67.3M 3s 460150K .......... .......... .......... .......... .......... 90% 75.9M 3s 460200K .......... .......... .......... .......... .......... 90% 63.0M 3s 460250K .......... .......... .......... .......... .......... 90% 91.4M 3s 460300K .......... .......... .......... .......... .......... 90% 72.1M 3s 460350K .......... .......... .......... .......... .......... 90% 61.0M 3s 460400K .......... .......... .......... .......... .......... 90% 75.4M 3s 460450K .......... .......... .......... .......... .......... 90% 63.2M 3s 460500K .......... .......... .......... .......... .......... 90% 124M 3s 460550K .......... .......... .......... .......... .......... 90% 71.4M 3s 460600K .......... .......... .......... .......... .......... 90% 61.3M 3s 460650K .......... .......... .......... .......... .......... 90% 64.8M 3s 460700K .......... .......... .......... .......... .......... 90% 76.8M 3s 460750K .......... .......... .......... .......... .......... 90% 75.4M 3s 460800K .......... .......... .......... .......... .......... 90% 76.9M 3s 460850K .......... .......... .......... .......... .......... 90% 62.4M 3s 460900K .......... .......... .......... .......... .......... 90% 76.3M 3s 460950K .......... .......... .......... .......... .......... 90% 90.6M 3s 461000K .......... .......... .......... .......... .......... 90% 65.0M 3s 461050K .......... .......... .......... .......... .......... 90% 61.9M 3s 461100K .......... .......... .......... .......... .......... 90% 93.2M 3s 461150K .......... .......... .......... .......... .......... 90% 76.2M 3s 461200K .......... .......... .......... .......... .......... 90% 54.4M 3s 461250K .......... .......... .......... .......... .......... 90% 91.3M 3s 461300K .......... .......... .......... .......... .......... 90% 77.4M 3s 461350K .......... .......... .......... .......... .......... 90% 71.6M 3s 461400K .......... .......... .......... .......... .......... 90% 19.6M 3s 461450K .......... .......... .......... .......... .......... 90% 182M 3s 461500K .......... .......... .......... .......... .......... 90% 588M 3s 461550K .......... .......... .......... .......... .......... 90% 432M 3s 461600K .......... .......... .......... .......... .......... 90% 38.4M 3s 461650K .......... .......... .......... .......... .......... 90% 65.7M 3s 461700K .......... .......... .......... .......... .......... 90% 127M 3s 461750K .......... .......... .......... .......... .......... 90% 57.7M 3s 461800K .......... .......... .......... .......... .......... 90% 99.9M 3s 461850K .......... .......... .......... .......... .......... 90% 76.9M 3s 461900K .......... .......... .......... .......... .......... 90% 61.8M 3s 461950K .......... .......... .......... .......... .......... 90% 55.1M 3s 462000K .......... .......... .......... .......... .......... 90% 47.4M 3s 462050K .......... .......... .......... .......... .......... 90% 62.8M 3s 462100K .......... .......... .......... .......... .......... 90% 42.1M 3s 462150K .......... .......... .......... .......... .......... 90% 54.1M 2s 462200K .......... .......... .......... .......... .......... 90% 38.0M 2s 462250K .......... .......... .......... .......... .......... 90% 64.9M 2s 462300K .......... .......... .......... .......... .......... 90% 90.9M 2s 462350K .......... .......... .......... .......... .......... 90% 47.0M 2s 462400K .......... .......... .......... .......... .......... 90% 63.3M 2s 462450K .......... .......... .......... .......... .......... 90% 52.3M 2s 462500K .......... .......... .......... .......... .......... 90% 52.8M 2s 462550K .......... .......... .......... .......... .......... 90% 54.0M 2s 462600K .......... .......... .......... .......... .......... 90% 41.0M 2s 462650K .......... .......... .......... .......... .......... 90% 63.7M 2s 462700K .......... .......... .......... .......... .......... 90% 48.5M 2s 462750K .......... .......... .......... .......... .......... 90% 47.5M 2s 462800K .......... .......... .......... .......... .......... 90% 71.3M 2s 462850K .......... .......... .......... .......... .......... 90% 41.9M 2s 462900K .......... .......... .......... .......... .......... 90% 56.1M 2s 462950K .......... .......... .......... .......... .......... 90% 42.2M 2s 463000K .......... .......... .......... .......... .......... 90% 58.6M 2s 463050K .......... .......... .......... .......... .......... 90% 54.6M 2s 463100K .......... .......... .......... .......... .......... 90% 36.7M 2s 463150K .......... .......... .......... .......... .......... 90% 95.9M 2s 463200K .......... .......... .......... .......... .......... 90% 45.3M 2s 463250K .......... .......... .......... .......... .......... 90% 47.4M 2s 463300K .......... .......... .......... .......... .......... 90% 60.5M 2s 463350K .......... .......... .......... .......... .......... 90% 47.0M 2s 463400K .......... .......... .......... .......... .......... 90% 58.0M 2s 463450K .......... .......... .......... .......... .......... 90% 52.4M 2s 463500K .......... .......... .......... .......... .......... 90% 53.0M 2s 463550K .......... .......... .......... .......... .......... 90% 46.8M 2s 463600K .......... .......... .......... .......... .......... 90% 59.1M 2s 463650K .......... .......... .......... .......... .......... 90% 51.5M 2s 463700K .......... .......... .......... .......... .......... 90% 34.9M 2s 463750K .......... .......... .......... .......... .......... 90% 54.5M 2s 463800K .......... .......... .......... .......... .......... 90% 48.2M 2s 463850K .......... .......... .......... .......... .......... 90% 71.9M 2s 463900K .......... .......... .......... .......... .......... 91% 33.1M 2s 463950K .......... .......... .......... .......... .......... 91% 94.1M 2s 464000K .......... .......... .......... .......... .......... 91% 69.9M 2s 464050K .......... .......... .......... .......... .......... 91% 33.9M 2s 464100K .......... .......... .......... .......... .......... 91% 16.4M 2s 464150K .......... .......... .......... .......... .......... 91% 313M 2s 464200K .......... .......... .......... .......... .......... 91% 43.9M 2s 464250K .......... .......... .......... .......... .......... 91% 493M 2s 464300K .......... .......... .......... .......... .......... 91% 206M 2s 464350K .......... .......... .......... .......... .......... 91% 10.4M 2s 464400K .......... .......... .......... .......... .......... 91% 294M 2s 464450K .......... .......... .......... .......... .......... 91% 470M 2s 464500K .......... .......... .......... .......... .......... 91% 42.3M 2s 464550K .......... .......... .......... .......... .......... 91% 41.2M 2s 464600K .......... .......... .......... .......... .......... 91% 45.3M 2s 464650K .......... .......... .......... .......... .......... 91% 50.7M 2s 464700K .......... .......... .......... .......... .......... 91% 35.0M 2s 464750K .......... .......... .......... .......... .......... 91% 63.6M 2s 464800K .......... .......... .......... .......... .......... 91% 73.9M 2s 464850K .......... .......... .......... .......... .......... 91% 23.0M 2s 464900K .......... .......... .......... .......... .......... 91% 531M 2s 464950K .......... .......... .......... .......... .......... 91% 41.0M 2s 465000K .......... .......... .......... .......... .......... 91% 46.7M 2s 465050K .......... .......... .......... .......... .......... 91% 30.4M 2s 465100K .......... .......... .......... .......... .......... 91% 103M 2s 465150K .......... .......... .......... .......... .......... 91% 46.2M 2s 465200K .......... .......... .......... .......... .......... 91% 33.0M 2s 465250K .......... .......... .......... .......... .......... 91% 41.8M 2s 465300K .......... .......... .......... .......... .......... 91% 63.3M 2s 465350K .......... .......... .......... .......... .......... 91% 35.8M 2s 465400K .......... .......... .......... .......... .......... 91% 37.1M 2s 465450K .......... .......... .......... .......... .......... 91% 40.3M 2s 465500K .......... .......... .......... .......... .......... 91% 48.3M 2s 465550K .......... .......... .......... .......... .......... 91% 47.0M 2s 465600K .......... .......... .......... .......... .......... 91% 33.6M 2s 465650K .......... .......... .......... .......... .......... 91% 42.0M 2s 465700K .......... .......... .......... .......... .......... 91% 28.4M 2s 465750K .......... .......... .......... .......... .......... 91% 47.9M 2s 465800K .......... .......... .......... .......... .......... 91% 44.8M 2s 465850K .......... .......... .......... .......... .......... 91% 54.7M 2s 465900K .......... .......... .......... .......... .......... 91% 31.9M 2s 465950K .......... .......... .......... .......... .......... 91% 41.1M 2s 466000K .......... .......... .......... .......... .......... 91% 51.7M 2s 466050K .......... .......... .......... .......... .......... 91% 47.0M 2s 466100K .......... .......... .......... .......... .......... 91% 38.1M 2s 466150K .......... .......... .......... .......... .......... 91% 37.7M 2s 466200K .......... .......... .......... .......... .......... 91% 47.4M 2s 466250K .......... .......... .......... .......... .......... 91% 38.6M 2s 466300K .......... .......... .......... .......... .......... 91% 25.1M 2s 466350K .......... .......... .......... .......... .......... 91% 58.8M 2s 466400K .......... .......... .......... .......... .......... 91% 43.0M 2s 466450K .......... .......... .......... .......... .......... 91% 31.7M 2s 466500K .......... .......... .......... .......... .......... 91% 48.6M 2s 466550K .......... .......... .......... .......... .......... 91% 41.6M 2s 466600K .......... .......... .......... .......... .......... 91% 51.8M 2s 466650K .......... .......... .......... .......... .......... 91% 45.4M 2s 466700K .......... .......... .......... .......... .......... 91% 41.5M 2s 466750K .......... .......... .......... .......... .......... 91% 119M 2s 466800K .......... .......... .......... .......... .......... 91% 15.5M 2s 466850K .......... .......... .......... .......... .......... 91% 231M 2s 466900K .......... .......... .......... .......... .......... 91% 470M 2s 466950K .......... .......... .......... .......... .......... 91% 356M 2s 467000K .......... .......... .......... .......... .......... 91% 24.5M 2s 467050K .......... .......... .......... .......... .......... 91% 543M 2s 467100K .......... .......... .......... .......... .......... 91% 28.8M 2s 467150K .......... .......... .......... .......... .......... 91% 144M 2s 467200K .......... .......... .......... .......... .......... 91% 35.9M 2s 467250K .......... .......... .......... .......... .......... 91% 102M 2s 467300K .......... .......... .......... .......... .......... 91% 31.2M 2s 467350K .......... .......... .......... .......... .......... 91% 41.9M 2s 467400K .......... .......... .......... .......... .......... 91% 27.1M 2s 467450K .......... .......... .......... .......... .......... 91% 45.2M 2s 467500K .......... .......... .......... .......... .......... 91% 43.1M 2s 467550K .......... .......... .......... .......... .......... 91% 25.7M 2s 467600K .......... .......... .......... .......... .......... 91% 47.7M 2s 467650K .......... .......... .......... .......... .......... 91% 45.4M 2s 467700K .......... .......... .......... .......... .......... 91% 26.9M 2s 467750K .......... .......... .......... .......... .......... 91% 40.4M 2s 467800K .......... .......... .......... .......... .......... 91% 29.0M 2s 467850K .......... .......... .......... .......... .......... 91% 41.6M 2s 467900K .......... .......... .......... .......... .......... 91% 52.9M 2s 467950K .......... .......... .......... .......... .......... 91% 26.6M 2s 468000K .......... .......... .......... .......... .......... 91% 48.2M 2s 468050K .......... .......... .......... .......... .......... 91% 30.7M 2s 468100K .......... .......... .......... .......... .......... 91% 40.8M 2s 468150K .......... .......... .......... .......... .......... 91% 51.6M 2s 468200K .......... .......... .......... .......... .......... 91% 26.8M 2s 468250K .......... .......... .......... .......... .......... 91% 46.2M 2s 468300K .......... .......... .......... .......... .......... 91% 47.8M 2s 468350K .......... .......... .......... .......... .......... 91% 26.3M 2s 468400K .......... .......... .......... .......... .......... 91% 39.0M 2s 468450K .......... .......... .......... .......... .......... 91% 31.9M 2s 468500K .......... .......... .......... .......... .......... 91% 51.7M 2s 468550K .......... .......... .......... .......... .......... 91% 45.8M 2s 468600K .......... .......... .......... .......... .......... 91% 35.0M 2s 468650K .......... .......... .......... .......... .......... 91% 61.7M 2s 468700K .......... .......... .......... .......... .......... 91% 41.0M 2s 468750K .......... .......... .......... .......... .......... 91% 79.7M 2s 468800K .......... .......... .......... .......... .......... 91% 26.6M 2s 468850K .......... .......... .......... .......... .......... 91% 94.4M 2s 468900K .......... .......... .......... .......... .......... 91% 20.3M 2s 468950K .......... .......... .......... .......... .......... 91% 379M 2s 469000K .......... .......... .......... .......... .......... 92% 394M 2s 469050K .......... .......... .......... .......... .......... 92% 38.0M 2s 469100K .......... .......... .......... .......... .......... 92% 24.8M 2s 469150K .......... .......... .......... .......... .......... 92% 35.9M 2s 469200K .......... .......... .......... .......... .......... 92% 84.6M 2s 469250K .......... .......... .......... .......... .......... 92% 42.8M 2s 469300K .......... .......... .......... .......... .......... 92% 38.9M 2s 469350K .......... .......... .......... .......... .......... 92% 41.8M 2s 469400K .......... .......... .......... .......... .......... 92% 28.9M 2s 469450K .......... .......... .......... .......... .......... 92% 23.2M 2s 469500K .......... .......... .......... .......... .......... 92% 51.8M 2s 469550K .......... .......... .......... .......... .......... 92% 42.3M 2s 469600K .......... .......... .......... .......... .......... 92% 25.9M 2s 469650K .......... .......... .......... .......... .......... 92% 45.4M 2s 469700K .......... .......... .......... .......... .......... 92% 23.8M 2s 469750K .......... .......... .......... .......... .......... 92% 30.7M 2s 469800K .......... .......... .......... .......... .......... 92% 46.3M 2s 469850K .......... .......... .......... .......... .......... 92% 28.9M 2s 469900K .......... .......... .......... .......... .......... 92% 31.4M 2s 469950K .......... .......... .......... .......... .......... 92% 39.1M 2s 470000K .......... .......... .......... .......... .......... 92% 26.1M 2s 470050K .......... .......... .......... .......... .......... 92% 40.9M 2s 470100K .......... .......... .......... .......... .......... 92% 13.2M 2s 470150K .......... .......... .......... .......... .......... 92% 53.3M 2s 470200K .......... .......... .......... .......... .......... 92% 28.0M 2s 470250K .......... .......... .......... .......... .......... 92% 47.2M 2s 470300K .......... .......... .......... .......... .......... 92% 31.6M 2s 470350K .......... .......... .......... .......... .......... 92% 41.8M 2s 470400K .......... .......... .......... .......... .......... 92% 29.2M 2s 470450K .......... .......... .......... .......... .......... 92% 42.8M 2s 470500K .......... .......... .......... .......... .......... 92% 35.1M 2s 470550K .......... .......... .......... .......... .......... 92% 120M 2s 470600K .......... .......... .......... .......... .......... 92% 27.2M 2s 470650K .......... .......... .......... .......... .......... 92% 98.8M 2s 470700K .......... .......... .......... .......... .......... 92% 22.5M 2s 470750K .......... .......... .......... .......... .......... 92% 94.3M 2s 470800K .......... .......... .......... .......... .......... 92% 27.3M 2s 470850K .......... .......... .......... .......... .......... 92% 19.6M 2s 470900K .......... .......... .......... .......... .......... 92% 410M 2s 470950K .......... .......... .......... .......... .......... 92% 381M 2s 471000K .......... .......... .......... .......... .......... 92% 30.3M 2s 471050K .......... .......... .......... .......... .......... 92% 170M 2s 471100K .......... .......... .......... .......... .......... 92% 33.7M 2s 471150K .......... .......... .......... .......... .......... 92% 26.0M 2s 471200K .......... .......... .......... .......... .......... 92% 193M 2s 471250K .......... .......... .......... .......... .......... 92% 47.1M 2s 471300K .......... .......... .......... .......... .......... 92% 41.0M 2s 471350K .......... .......... .......... .......... .......... 92% 34.5M 2s 471400K .......... .......... .......... .......... .......... 92% 47.7M 2s 471450K .......... .......... .......... .......... .......... 92% 47.0M 2s 471500K .......... .......... .......... .......... .......... 92% 43.6M 2s 471550K .......... .......... .......... .......... .......... 92% 49.8M 2s 471600K .......... .......... .......... .......... .......... 92% 31.4M 2s 471650K .......... .......... .......... .......... .......... 92% 53.0M 2s 471700K .......... .......... .......... .......... .......... 92% 41.8M 2s 471750K .......... .......... .......... .......... .......... 92% 33.6M 2s 471800K .......... .......... .......... .......... .......... 92% 43.4M 2s 471850K .......... .......... .......... .......... .......... 92% 49.7M 2s 471900K .......... .......... .......... .......... .......... 92% 38.8M 2s 471950K .......... .......... .......... .......... .......... 92% 39.9M 2s 472000K .......... .......... .......... .......... .......... 92% 37.6M 2s 472050K .......... .......... .......... .......... .......... 92% 40.0M 2s 472100K .......... .......... .......... .......... .......... 92% 34.3M 2s 472150K .......... .......... .......... .......... .......... 92% 54.8M 2s 472200K .......... .......... .......... .......... .......... 92% 37.9M 2s 472250K .......... .......... .......... .......... .......... 92% 41.8M 2s 472300K .......... .......... .......... .......... .......... 92% 47.3M 2s 472350K .......... .......... .......... .......... .......... 92% 31.6M 2s 472400K .......... .......... .......... .......... .......... 92% 52.0M 2s 472450K .......... .......... .......... .......... .......... 92% 46.2M 2s 472500K .......... .......... .......... .......... .......... 92% 41.6M 2s 472550K .......... .......... .......... .......... .......... 92% 48.9M 2s 472600K .......... .......... .......... .......... .......... 92% 36.1M 2s 472650K .......... .......... .......... .......... .......... 92% 42.1M 2s 472700K .......... .......... .......... .......... .......... 92% 40.4M 2s 472750K .......... .......... .......... .......... .......... 92% 60.3M 2s 472800K .......... .......... .......... .......... .......... 92% 54.5M 2s 472850K .......... .......... .......... .......... .......... 92% 45.5M 2s 472900K .......... .......... .......... .......... .......... 92% 55.2M 2s 472950K .......... .......... .......... .......... .......... 92% 38.5M 2s 473000K .......... .......... .......... .......... .......... 92% 121M 2s 473050K .......... .......... .......... .......... .......... 92% 29.2M 2s 473100K .......... .......... .......... .......... .......... 92% 111M 2s 473150K .......... .......... .......... .......... .......... 92% 22.9M 2s 473200K .......... .......... .......... .......... .......... 92% 364M 2s 473250K .......... .......... .......... .......... .......... 92% 214M 2s 473300K .......... .......... .......... .......... .......... 92% 20.5M 2s 473350K .......... .......... .......... .......... .......... 92% 440M 2s 473400K .......... .......... .......... .......... .......... 92% 191M 2s 473450K .......... .......... .......... .......... .......... 92% 33.4M 2s 473500K .......... .......... .......... .......... .......... 92% 153M 2s 473550K .......... .......... .......... .......... .......... 92% 52.8M 2s 473600K .......... .......... .......... .......... .......... 92% 48.2M 2s 473650K .......... .......... .......... .......... .......... 92% 46.8M 2s 473700K .......... .......... .......... .......... .......... 92% 42.4M 2s 473750K .......... .......... .......... .......... .......... 92% 53.9M 2s 473800K .......... .......... .......... .......... .......... 92% 47.4M 2s 473850K .......... .......... .......... .......... .......... 92% 30.1M 2s 473900K .......... .......... .......... .......... .......... 92% 61.0M 2s 473950K .......... .......... .......... .......... .......... 92% 47.1M 2s 474000K .......... .......... .......... .......... .......... 92% 47.5M 2s 474050K .......... .......... .......... .......... .......... 92% 46.4M 2s 474100K .......... .......... .......... .......... .......... 93% 28.8M 2s 474150K .......... .......... .......... .......... .......... 93% 53.5M 2s 474200K .......... .......... .......... .......... .......... 93% 39.0M 2s 474250K .......... .......... .......... .......... .......... 93% 47.8M 2s 474300K .......... .......... .......... .......... .......... 93% 40.4M 2s 474350K .......... .......... .......... .......... .......... 93% 49.2M 2s 474400K .......... .......... .......... .......... .......... 93% 41.8M 2s 474450K .......... .......... .......... .......... .......... 93% 48.2M 2s 474500K .......... .......... .......... .......... .......... 93% 37.3M 2s 474550K .......... .......... .......... .......... .......... 93% 51.1M 2s 474600K .......... .......... .......... .......... .......... 93% 30.8M 2s 474650K .......... .......... .......... .......... .......... 93% 51.8M 2s 474700K .......... .......... .......... .......... .......... 93% 34.0M 2s 474750K .......... .......... .......... .......... .......... 93% 33.4M 2s 474800K .......... .......... .......... .......... .......... 93% 48.5M 2s 474850K .......... .......... .......... .......... .......... 93% 38.1M 2s 474900K .......... .......... .......... .......... .......... 93% 38.3M 2s 474950K .......... .......... .......... .......... .......... 93% 52.2M 2s 475000K .......... .......... .......... .......... .......... 93% 33.8M 2s 475050K .......... .......... .......... .......... .......... 93% 54.0M 2s 475100K .......... .......... .......... .......... .......... 93% 62.1M 2s 475150K .......... .......... .......... .......... .......... 93% 44.9M 2s 475200K .......... .......... .......... .......... .......... 93% 56.8M 2s 475250K .......... .......... .......... .......... .......... 93% 63.8M 2s 475300K .......... .......... .......... .......... .......... 93% 72.7M 2s 475350K .......... .......... .......... .......... .......... 93% 16.8M 2s 475400K .......... .......... .......... .......... .......... 93% 436M 2s 475450K .......... .......... .......... .......... .......... 93% 444M 2s 475500K .......... .......... .......... .......... .......... 93% 21.2M 2s 475550K .......... .......... .......... .......... .......... 93% 568M 2s 475600K .......... .......... .......... .......... .......... 93% 161M 2s 475650K .......... .......... .......... .......... .......... 93% 22.0M 2s 475700K .......... .......... .......... .......... .......... 93% 46.9M 2s 475750K .......... .......... .......... .......... .......... 93% 41.2M 2s 475800K .......... .......... .......... .......... .......... 93% 63.0M 2s 475850K .......... .......... .......... .......... .......... 93% 47.4M 2s 475900K .......... .......... .......... .......... .......... 93% 113M 2s 475950K .......... .......... .......... .......... .......... 93% 27.2M 2s 476000K .......... .......... .......... .......... .......... 93% 444M 2s 476050K .......... .......... .......... .......... .......... 93% 41.0M 2s 476100K .......... .......... .......... .......... .......... 93% 55.5M 2s 476150K .......... .......... .......... .......... .......... 93% 51.5M 2s 476200K .......... .......... .......... .......... .......... 93% 32.0M 2s 476250K .......... .......... .......... .......... .......... 93% 93.5M 2s 476300K .......... .......... .......... .......... .......... 93% 52.2M 2s 476350K .......... .......... .......... .......... .......... 93% 37.6M 2s 476400K .......... .......... .......... .......... .......... 93% 53.8M 2s 476450K .......... .......... .......... .......... .......... 93% 35.1M 2s 476500K .......... .......... .......... .......... .......... 93% 53.5M 2s 476550K .......... .......... .......... .......... .......... 93% 55.3M 2s 476600K .......... .......... .......... .......... .......... 93% 53.8M 2s 476650K .......... .......... .......... .......... .......... 93% 52.2M 2s 476700K .......... .......... .......... .......... .......... 93% 52.7M 2s 476750K .......... .......... .......... .......... .......... 93% 34.9M 2s 476800K .......... .......... .......... .......... .......... 93% 54.2M 2s 476850K .......... .......... .......... .......... .......... 93% 49.2M 2s 476900K .......... .......... .......... .......... .......... 93% 53.5M 2s 476950K .......... .......... .......... .......... .......... 93% 37.4M 2s 477000K .......... .......... .......... .......... .......... 93% 53.8M 2s 477050K .......... .......... .......... .......... .......... 93% 46.7M 2s 477100K .......... .......... .......... .......... .......... 93% 50.1M 2s 477150K .......... .......... .......... .......... .......... 93% 43.5M 2s 477200K .......... .......... .......... .......... .......... 93% 53.3M 2s 477250K .......... .......... .......... .......... .......... 93% 53.4M 2s 477300K .......... .......... .......... .......... .......... 93% 42.3M 2s 477350K .......... .......... .......... .......... .......... 93% 51.3M 2s 477400K .......... .......... .......... .......... .......... 93% 42.5M 2s 477450K .......... .......... .......... .......... .......... 93% 42.9M 2s 477500K .......... .......... .......... .......... .......... 93% 60.3M 2s 477550K .......... .......... .......... .......... .......... 93% 41.4M 2s 477600K .......... .......... .......... .......... .......... 93% 36.7M 2s 477650K .......... .......... .......... .......... .......... 93% 31.7M 2s 477700K .......... .......... .......... .......... .......... 93% 19.9M 2s 477750K .......... .......... .......... .......... .......... 93% 23.8M 2s 477800K .......... .......... .......... .......... .......... 93% 61.9M 2s 477850K .......... .......... .......... .......... .......... 93% 31.7M 2s 477900K .......... .......... .......... .......... .......... 93% 41.0M 2s 477950K .......... .......... .......... .......... .......... 93% 25.4M 2s 478000K .......... .......... .......... .......... .......... 93% 23.6M 2s 478050K .......... .......... .......... .......... .......... 93% 77.3M 2s 478100K .......... .......... .......... .......... .......... 93% 33.8M 2s 478150K .......... .......... .......... .......... .......... 93% 24.8M 2s 478200K .......... .......... .......... .......... .......... 93% 38.4M 2s 478250K .......... .......... .......... .......... .......... 93% 35.8M 2s 478300K .......... .......... .......... .......... .......... 93% 31.5M 2s 478350K .......... .......... .......... .......... .......... 93% 38.0M 2s 478400K .......... .......... .......... .......... .......... 93% 41.3M 2s 478450K .......... .......... .......... .......... .......... 93% 27.4M 2s 478500K .......... .......... .......... .......... .......... 93% 41.5M 2s 478550K .......... .......... .......... .......... .......... 93% 27.0M 2s 478600K .......... .......... .......... .......... .......... 93% 30.7M 2s 478650K .......... .......... .......... .......... .......... 93% 41.9M 2s 478700K .......... .......... .......... .......... .......... 93% 33.9M 2s 478750K .......... .......... .......... .......... .......... 93% 47.6M 2s 478800K .......... .......... .......... .......... .......... 93% 26.9M 2s 478850K .......... .......... .......... .......... .......... 93% 28.3M 2s 478900K .......... .......... .......... .......... .......... 93% 33.5M 2s 478950K .......... .......... .......... .......... .......... 93% 27.6M 2s 479000K .......... .......... .......... .......... .......... 93% 30.9M 2s 479050K .......... .......... .......... .......... .......... 93% 37.6M 2s 479100K .......... .......... .......... .......... .......... 93% 30.3M 2s 479150K .......... .......... .......... .......... .......... 93% 29.4M 2s 479200K .......... .......... .......... .......... .......... 94% 33.7M 2s 479250K .......... .......... .......... .......... .......... 94% 37.8M 2s 479300K .......... .......... .......... .......... .......... 94% 38.6M 2s 479350K .......... .......... .......... .......... .......... 94% 30.8M 2s 479400K .......... .......... .......... .......... .......... 94% 29.3M 2s 479450K .......... .......... .......... .......... .......... 94% 74.4M 2s 479500K .......... .......... .......... .......... .......... 94% 27.4M 2s 479550K .......... .......... .......... .......... .......... 94% 171M 2s 479600K .......... .......... .......... .......... .......... 94% 18.7M 2s 479650K .......... .......... .......... .......... .......... 94% 77.5M 2s 479700K .......... .......... .......... .......... .......... 94% 20.2M 2s 479750K .......... .......... .......... .......... .......... 94% 37.9M 2s 479800K .......... .......... .......... .......... .......... 94% 128M 2s 479850K .......... .......... .......... .......... .......... 94% 19.9M 2s 479900K .......... .......... .......... .......... .......... 94% 29.0M 2s 479950K .......... .......... .......... .......... .......... 94% 25.1M 2s 480000K .......... .......... .......... .......... .......... 94% 23.4M 2s 480050K .......... .......... .......... .......... .......... 94% 31.4M 2s 480100K .......... .......... .......... .......... .......... 94% 16.7M 2s 480150K .......... .......... .......... .......... .......... 94% 27.1M 2s 480200K .......... .......... .......... .......... .......... 94% 19.1M 2s 480250K .......... .......... .......... .......... .......... 94% 34.7M 2s 480300K .......... .......... .......... .......... .......... 94% 23.7M 2s 480350K .......... .......... .......... .......... .......... 94% 20.1M 2s 480400K .......... .......... .......... .......... .......... 94% 27.1M 2s 480450K .......... .......... .......... .......... .......... 94% 21.9M 2s 480500K .......... .......... .......... .......... .......... 94% 23.9M 2s 480550K .......... .......... .......... .......... .......... 94% 29.6M 2s 480600K .......... .......... .......... .......... .......... 94% 23.9M 1s 480650K .......... .......... .......... .......... .......... 94% 28.5M 1s 480700K .......... .......... .......... .......... .......... 94% 29.8M 1s 480750K .......... .......... .......... .......... .......... 94% 28.9M 1s 480800K .......... .......... .......... .......... .......... 94% 53.7M 1s 480850K .......... .......... .......... .......... .......... 94% 35.6M 1s 480900K .......... .......... .......... .......... .......... 94% 122M 1s 480950K .......... .......... .......... .......... .......... 94% 34.8M 1s 481000K .......... .......... .......... .......... .......... 94% 129M 1s 481050K .......... .......... .......... .......... .......... 94% 22.0M 1s 481100K .......... .......... .......... .......... .......... 94% 313M 1s 481150K .......... .......... .......... .......... .......... 94% 51.7M 1s 481200K .......... .......... .......... .......... .......... 94% 42.6M 1s 481250K .......... .......... .......... .......... .......... 94% 603M 1s 481300K .......... .......... .......... .......... .......... 94% 354M 1s 481350K .......... .......... .......... .......... .......... 94% 52.3M 1s 481400K .......... .......... .......... .......... .......... 94% 46.2M 1s 481450K .......... .......... .......... .......... .......... 94% 64.0M 1s 481500K .......... .......... .......... .......... .......... 94% 40.8M 1s 481550K .......... .......... .......... .......... .......... 94% 48.1M 1s 481600K .......... .......... .......... .......... .......... 94% 42.2M 1s 481650K .......... .......... .......... .......... .......... 94% 38.2M 1s 481700K .......... .......... .......... .......... .......... 94% 47.3M 1s 481750K .......... .......... .......... .......... .......... 94% 48.9M 1s 481800K .......... .......... .......... .......... .......... 94% 55.0M 1s 481850K .......... .......... .......... .......... .......... 94% 34.2M 1s 481900K .......... .......... .......... .......... .......... 94% 41.6M 1s 481950K .......... .......... .......... .......... .......... 94% 47.8M 1s 482000K .......... .......... .......... .......... .......... 94% 47.0M 1s 482050K .......... .......... .......... .......... .......... 94% 59.5M 1s 482100K .......... .......... .......... .......... .......... 94% 37.3M 1s 482150K .......... .......... .......... .......... .......... 94% 47.3M 1s 482200K .......... .......... .......... .......... .......... 94% 42.2M 1s 482250K .......... .......... .......... .......... .......... 94% 47.4M 1s 482300K .......... .......... .......... .......... .......... 94% 62.1M 1s 482350K .......... .......... .......... .......... .......... 94% 35.9M 1s 482400K .......... .......... .......... .......... .......... 94% 52.3M 1s 482450K .......... .......... .......... .......... .......... 94% 47.6M 1s 482500K .......... .......... .......... .......... .......... 94% 46.0M 1s 482550K .......... .......... .......... .......... .......... 94% 52.1M 1s 482600K .......... .......... .......... .......... .......... 94% 51.1M 1s 482650K .......... .......... .......... .......... .......... 94% 22.6M 1s 482700K .......... .......... .......... .......... .......... 94% 53.0M 1s 482750K .......... .......... .......... .......... .......... 94% 49.1M 1s 482800K .......... .......... .......... .......... .......... 94% 62.0M 1s 482850K .......... .......... .......... .......... .......... 94% 43.5M 1s 482900K .......... .......... .......... .......... .......... 94% 46.7M 1s 482950K .......... .......... .......... .......... .......... 94% 38.5M 1s 483000K .......... .......... .......... .......... .......... 94% 43.3M 1s 483050K .......... .......... .......... .......... .......... 94% 28.1M 1s 483100K .......... .......... .......... .......... .......... 94% 27.1M 1s 483150K .......... .......... .......... .......... .......... 94% 36.5M 1s 483200K .......... .......... .......... .......... .......... 94% 42.9M 1s 483250K .......... .......... .......... .......... .......... 94% 17.4M 1s 483300K .......... .......... .......... .......... .......... 94% 452M 1s 483350K .......... .......... .......... .......... .......... 94% 26.9M 1s 483400K .......... .......... .......... .......... .......... 94% 111M 1s 483450K .......... .......... .......... .......... .......... 94% 36.0M 1s 483500K .......... .......... .......... .......... .......... 94% 98.6M 1s 483550K .......... .......... .......... .......... .......... 94% 39.8M 1s 483600K .......... .......... .......... .......... .......... 94% 32.3M 1s 483650K .......... .......... .......... .......... .......... 94% 47.3M 1s 483700K .......... .......... .......... .......... .......... 94% 46.6M 1s 483750K .......... .......... .......... .......... .......... 94% 27.0M 1s 483800K .......... .......... .......... .......... .......... 94% 54.3M 1s 483850K .......... .......... .......... .......... .......... 94% 39.4M 1s 483900K .......... .......... .......... .......... .......... 94% 42.6M 1s 483950K .......... .......... .......... .......... .......... 94% 31.4M 1s 484000K .......... .......... .......... .......... .......... 94% 41.5M 1s 484050K .......... .......... .......... .......... .......... 94% 40.6M 1s 484100K .......... .......... .......... .......... .......... 94% 29.3M 1s 484150K .......... .......... .......... .......... .......... 94% 43.3M 1s 484200K .......... .......... .......... .......... .......... 94% 45.1M 1s 484250K .......... .......... .......... .......... .......... 94% 29.8M 1s 484300K .......... .......... .......... .......... .......... 95% 45.5M 1s 484350K .......... .......... .......... .......... .......... 95% 33.8M 1s 484400K .......... .......... .......... .......... .......... 95% 34.8M 1s 484450K .......... .......... .......... .......... .......... 95% 37.7M 1s 484500K .......... .......... .......... .......... .......... 95% 41.9M 1s 484550K .......... .......... .......... .......... .......... 95% 48.0M 1s 484600K .......... .......... .......... .......... .......... 95% 24.6M 1s 484650K .......... .......... .......... .......... .......... 95% 45.3M 1s 484700K .......... .......... .......... .......... .......... 95% 35.2M 1s 484750K .......... .......... .......... .......... .......... 95% 34.3M 1s 484800K .......... .......... .......... .......... .......... 95% 43.1M 1s 484850K .......... .......... .......... .......... .......... 95% 33.6M 1s 484900K .......... .......... .......... .......... .......... 95% 118M 1s 484950K .......... .......... .......... .......... .......... 95% 21.9M 1s 485000K .......... .......... .......... .......... .......... 95% 177M 1s 485050K .......... .......... .......... .......... .......... 95% 15.0M 1s 485100K .......... .......... .......... .......... .......... 95% 323M 1s 485150K .......... .......... .......... .......... .......... 95% 465M 1s 485200K .......... .......... .......... .......... .......... 95% 48.7M 1s 485250K .......... .......... .......... .......... .......... 95% 26.1M 1s 485300K .......... .......... .......... .......... .......... 95% 75.8M 1s 485350K .......... .......... .......... .......... .......... 95% 33.8M 1s 485400K .......... .......... .......... .......... .......... 95% 73.9M 1s 485450K .......... .......... .......... .......... .......... 95% 44.6M 1s 485500K .......... .......... .......... .......... .......... 95% 50.5M 1s 485550K .......... .......... .......... .......... .......... 95% 29.5M 1s 485600K .......... .......... .......... .......... .......... 95% 38.2M 1s 485650K .......... .......... .......... .......... .......... 95% 39.6M 1s 485700K .......... .......... .......... .......... .......... 95% 33.7M 1s 485750K .......... .......... .......... .......... .......... 95% 29.8M 1s 485800K .......... .......... .......... .......... .......... 95% 40.8M 1s 485850K .......... .......... .......... .......... .......... 95% 27.5M 1s 485900K .......... .......... .......... .......... .......... 95% 40.4M 1s 485950K .......... .......... .......... .......... .......... 95% 39.8M 1s 486000K .......... .......... .......... .......... .......... 95% 31.3M 1s 486050K .......... .......... .......... .......... .......... 95% 34.5M 1s 486100K .......... .......... .......... .......... .......... 95% 40.8M 1s 486150K .......... .......... .......... .......... .......... 95% 26.7M 1s 486200K .......... .......... .......... .......... .......... 95% 48.1M 1s 486250K .......... .......... .......... .......... .......... 95% 37.2M 1s 486300K .......... .......... .......... .......... .......... 95% 42.1M 1s 486350K .......... .......... .......... .......... .......... 95% 33.4M 1s 486400K .......... .......... .......... .......... .......... 95% 45.8M 1s 486450K .......... .......... .......... .......... .......... 95% 26.9M 1s 486500K .......... .......... .......... .......... .......... 95% 34.0M 1s 486550K .......... .......... .......... .......... .......... 95% 41.5M 1s 486600K .......... .......... .......... .......... .......... 95% 31.6M 1s 486650K .......... .......... .......... .......... .......... 95% 44.9M 1s 486700K .......... .......... .......... .......... .......... 95% 25.0M 1s 486750K .......... .......... .......... .......... .......... 95% 27.3M 1s 486800K .......... .......... .......... .......... .......... 95% 53.2M 1s 486850K .......... .......... .......... .......... .......... 95% 34.6M 1s 486900K .......... .......... .......... .......... .......... 95% 118M 1s 486950K .......... .......... .......... .......... .......... 95% 26.7M 1s 487000K .......... .......... .......... .......... .......... 95% 123M 1s 487050K .......... .......... .......... .......... .......... 95% 104M 1s 487100K .......... .......... .......... .......... .......... 95% 16.1M 1s 487150K .......... .......... .......... .......... .......... 95% 56.1M 1s 487200K .......... .......... .......... .......... .......... 95% 414M 1s 487250K .......... .......... .......... .......... .......... 95% 211M 1s 487300K .......... .......... .......... .......... .......... 95% 46.5M 1s 487350K .......... .......... .......... .......... .......... 95% 20.6M 1s 487400K .......... .......... .......... .......... .......... 95% 410M 1s 487450K .......... .......... .......... .......... .......... 95% 93.0M 1s 487500K .......... .......... .......... .......... .......... 95% 35.5M 1s 487550K .......... .......... .......... .......... .......... 95% 69.5M 1s 487600K .......... .......... .......... .......... .......... 95% 33.8M 1s 487650K .......... .......... .......... .......... .......... 95% 54.1M 1s 487700K .......... .......... .......... .......... .......... 95% 33.9M 1s 487750K .......... .......... .......... .......... .......... 95% 54.4M 1s 487800K .......... .......... .......... .......... .......... 95% 46.5M 1s 487850K .......... .......... .......... .......... .......... 95% 47.0M 1s 487900K .......... .......... .......... .......... .......... 95% 40.0M 1s 487950K .......... .......... .......... .......... .......... 95% 45.7M 1s 488000K .......... .......... .......... .......... .......... 95% 42.6M 1s 488050K .......... .......... .......... .......... .......... 95% 52.7M 1s 488100K .......... .......... .......... .......... .......... 95% 33.9M 1s 488150K .......... .......... .......... .......... .......... 95% 47.5M 1s 488200K .......... .......... .......... .......... .......... 95% 54.7M 1s 488250K .......... .......... .......... .......... .......... 95% 34.8M 1s 488300K .......... .......... .......... .......... .......... 95% 45.1M 1s 488350K .......... .......... .......... .......... .......... 95% 53.6M 1s 488400K .......... .......... .......... .......... .......... 95% 45.3M 1s 488450K .......... .......... .......... .......... .......... 95% 41.5M 1s 488500K .......... .......... .......... .......... .......... 95% 42.2M 1s 488550K .......... .......... .......... .......... .......... 95% 41.1M 1s 488600K .......... .......... .......... .......... .......... 95% 61.3M 1s 488650K .......... .......... .......... .......... .......... 95% 46.4M 1s 488700K .......... .......... .......... .......... .......... 95% 45.8M 1s 488750K .......... .......... .......... .......... .......... 95% 52.6M 1s 488800K .......... .......... .......... .......... .......... 95% 52.7M 1s 488850K .......... .......... .......... .......... .......... 95% 34.5M 1s 488900K .......... .......... .......... .......... .......... 95% 42.5M 1s 488950K .......... .......... .......... .......... .......... 95% 45.4M 1s 489000K .......... .......... .......... .......... .......... 95% 36.9M 1s 489050K .......... .......... .......... .......... .......... 95% 50.9M 1s 489100K .......... .......... .......... .......... .......... 95% 28.6M 1s 489150K .......... .......... .......... .......... .......... 95% 31.0M 1s 489200K .......... .......... .......... .......... .......... 95% 27.2M 1s 489250K .......... .......... .......... .......... .......... 95% 11.7M 1s 489300K .......... .......... .......... .......... .......... 95% 349M 1s 489350K .......... .......... .......... .......... .......... 95% 346M 1s 489400K .......... .......... .......... .......... .......... 96% 488M 1s 489450K .......... .......... .......... .......... .......... 96% 33.3M 1s 489500K .......... .......... .......... .......... .......... 96% 103M 1s 489550K .......... .......... .......... .......... .......... 96% 31.6M 1s 489600K .......... .......... .......... .......... .......... 96% 34.6M 1s 489650K .......... .......... .......... .......... .......... 96% 53.2M 1s 489700K .......... .......... .......... .......... .......... 96% 40.9M 1s 489750K .......... .......... .......... .......... .......... 96% 41.9M 1s 489800K .......... .......... .......... .......... .......... 96% 93.7M 1s 489850K .......... .......... .......... .......... .......... 96% 24.6M 1s 489900K .......... .......... .......... .......... .......... 96% 96.3M 1s 489950K .......... .......... .......... .......... .......... 96% 36.4M 1s 490000K .......... .......... .......... .......... .......... 96% 24.8M 1s 490050K .......... .......... .......... .......... .......... 96% 63.5M 1s 490100K .......... .......... .......... .......... .......... 96% 41.0M 1s 490150K .......... .......... .......... .......... .......... 96% 40.7M 1s 490200K .......... .......... .......... .......... .......... 96% 34.5M 1s 490250K .......... .......... .......... .......... .......... 96% 29.1M 1s 490300K .......... .......... .......... .......... .......... 96% 40.3M 1s 490350K .......... .......... .......... .......... .......... 96% 33.8M 1s 490400K .......... .......... .......... .......... .......... 96% 38.0M 1s 490450K .......... .......... .......... .......... .......... 96% 31.5M 1s 490500K .......... .......... .......... .......... .......... 96% 41.2M 1s 490550K .......... .......... .......... .......... .......... 96% 26.9M 1s 490600K .......... .......... .......... .......... .......... 96% 52.6M 1s 490650K .......... .......... .......... .......... .......... 96% 48.1M 1s 490700K .......... .......... .......... .......... .......... 96% 29.2M 1s 490750K .......... .......... .......... .......... .......... 96% 31.4M 1s 490800K .......... .......... .......... .......... .......... 96% 41.0M 1s 490850K .......... .......... .......... .......... .......... 96% 35.3M 1s 490900K .......... .......... .......... .......... .......... 96% 28.7M 1s 490950K .......... .......... .......... .......... .......... 96% 37.2M 1s 491000K .......... .......... .......... .......... .......... 96% 29.0M 1s 491050K .......... .......... .......... .......... .......... 96% 48.6M 1s 491100K .......... .......... .......... .......... .......... 96% 34.0M 1s 491150K .......... .......... .......... .......... .......... 96% 45.9M 1s 491200K .......... .......... .......... .......... .......... 96% 41.2M 1s 491250K .......... .......... .......... .......... .......... 96% 40.5M 1s 491300K .......... .......... .......... .......... .......... 96% 37.9M 1s 491350K .......... .......... .......... .......... .......... 96% 37.8M 1s 491400K .......... .......... .......... .......... .......... 96% 42.5M 1s 491450K .......... .......... .......... .......... .......... 96% 31.5M 1s 491500K .......... .......... .......... .......... .......... 96% 94.8M 1s 491550K .......... .......... .......... .......... .......... 96% 105M 1s 491600K .......... .......... .......... .......... .......... 96% 23.0M 1s 491650K .......... .......... .......... .......... .......... 96% 19.6M 1s 491700K .......... .......... .......... .......... .......... 96% 51.3M 1s 491750K .......... .......... .......... .......... .......... 96% 448M 1s 491800K .......... .......... .......... .......... .......... 96% 198M 1s 491850K .......... .......... .......... .......... .......... 96% 21.1M 1s 491900K .......... .......... .......... .......... .......... 96% 89.3M 1s 491950K .......... .......... .......... .......... .......... 96% 103M 1s 492000K .......... .......... .......... .......... .......... 96% 27.6M 1s 492050K .......... .......... .......... .......... .......... 96% 109M 1s 492100K .......... .......... .......... .......... .......... 96% 29.2M 1s 492150K .......... .......... .......... .......... .......... 96% 37.5M 1s 492200K .......... .......... .......... .......... .......... 96% 40.7M 1s 492250K .......... .......... .......... .......... .......... 96% 42.3M 1s 492300K .......... .......... .......... .......... .......... 96% 38.1M 1s 492350K .......... .......... .......... .......... .......... 96% 37.1M 1s 492400K .......... .......... .......... .......... .......... 96% 37.6M 1s 492450K .......... .......... .......... .......... .......... 96% 46.6M 1s 492500K .......... .......... .......... .......... .......... 96% 35.3M 1s 492550K .......... .......... .......... .......... .......... 96% 37.0M 1s 492600K .......... .......... .......... .......... .......... 96% 34.2M 1s 492650K .......... .......... .......... .......... .......... 96% 54.1M 1s 492700K .......... .......... .......... .......... .......... 96% 41.8M 1s 492750K .......... .......... .......... .......... .......... 96% 47.8M 1s 492800K .......... .......... .......... .......... .......... 96% 46.7M 1s 492850K .......... .......... .......... .......... .......... 96% 29.2M 1s 492900K .......... .......... .......... .......... .......... 96% 54.0M 1s 492950K .......... .......... .......... .......... .......... 96% 46.5M 1s 493000K .......... .......... .......... .......... .......... 96% 46.7M 1s 493050K .......... .......... .......... .......... .......... 96% 52.3M 1s 493100K .......... .......... .......... .......... .......... 96% 46.1M 1s 493150K .......... .......... .......... .......... .......... 96% 41.1M 1s 493200K .......... .......... .......... .......... .......... 96% 45.4M 1s 493250K .......... .......... .......... .......... .......... 96% 50.5M 1s 493300K .......... .......... .......... .......... .......... 96% 39.2M 1s 493350K .......... .......... .......... .......... .......... 96% 30.4M 1s 493400K .......... .......... .......... .......... .......... 96% 59.8M 1s 493450K .......... .......... .......... .......... .......... 96% 31.9M 1s 493500K .......... .......... .......... .......... .......... 96% 41.5M 1s 493550K .......... .......... .......... .......... .......... 96% 36.6M 1s 493600K .......... .......... .......... .......... .......... 96% 28.6M 1s 493650K .......... .......... .......... .......... .......... 96% 42.3M 1s 493700K .......... .......... .......... .......... .......... 96% 41.0M 1s 493750K .......... .......... .......... .......... .......... 96% 38.3M 1s 493800K .......... .......... .......... .......... .......... 96% 42.3M 1s 493850K .......... .......... .......... .......... .......... 96% 34.6M 1s 493900K .......... .......... .......... .......... .......... 96% 29.3M 1s 493950K .......... .......... .......... .......... .......... 96% 33.7M 1s 494000K .......... .......... .......... .......... .......... 96% 41.1M 1s 494050K .......... .......... .......... .......... .......... 96% 31.5M 1s 494100K .......... .......... .......... .......... .......... 96% 36.9M 1s 494150K .......... .......... .......... .......... .......... 96% 45.9M 1s 494200K .......... .......... .......... .......... .......... 96% 27.7M 1s 494250K .......... .......... .......... .......... .......... 96% 45.4M 1s 494300K .......... .......... .......... .......... .......... 96% 46.9M 1s 494350K .......... .......... .......... .......... .......... 96% 28.0M 1s 494400K .......... .......... .......... .......... .......... 96% 53.5M 1s 494450K .......... .......... .......... .......... .......... 96% 33.5M 1s 494500K .......... .......... .......... .......... .......... 97% 42.6M 1s 494550K .......... .......... .......... .......... .......... 97% 30.3M 1s 494600K .......... .......... .......... .......... .......... 97% 41.3M 1s 494650K .......... .......... .......... .......... .......... 97% 61.8M 1s 494700K .......... .......... .......... .......... .......... 97% 26.9M 1s 494750K .......... .......... .......... .......... .......... 97% 59.1M 1s 494800K .......... .......... .......... .......... .......... 97% 41.3M 1s 494850K .......... .......... .......... .......... .......... 97% 38.4M 1s 494900K .......... .......... .......... .......... .......... 97% 31.2M 1s 494950K .......... .......... .......... .......... .......... 97% 91.8M 1s 495000K .......... .......... .......... .......... .......... 97% 22.5M 1s 495050K .......... .......... .......... .......... .......... 97% 161M 1s 495100K .......... .......... .......... .......... .......... 97% 17.0M 1s 495150K .......... .......... .......... .......... .......... 97% 48.9M 1s 495200K .......... .......... .......... .......... .......... 97% 46.8M 1s 495250K .......... .......... .......... .......... .......... 97% 509M 1s 495300K .......... .......... .......... .......... .......... 97% 317M 1s 495350K .......... .......... .......... .......... .......... 97% 20.3M 1s 495400K .......... .......... .......... .......... .......... 97% 479M 1s 495450K .......... .......... .......... .......... .......... 97% 25.4M 1s 495500K .......... .......... .......... .......... .......... 97% 37.5M 1s 495550K .......... .......... .......... .......... .......... 97% 29.5M 1s 495600K .......... .......... .......... .......... .......... 97% 42.1M 1s 495650K .......... .......... .......... .......... .......... 97% 31.5M 1s 495700K .......... .......... .......... .......... .......... 97% 42.2M 1s 495750K .......... .......... .......... .......... .......... 97% 37.2M 1s 495800K .......... .......... .......... .......... .......... 97% 37.0M 1s 495850K .......... .......... .......... .......... .......... 97% 37.9M 1s 495900K .......... .......... .......... .......... .......... 97% 51.9M 1s 495950K .......... .......... .......... .......... .......... 97% 25.4M 1s 496000K .......... .......... .......... .......... .......... 97% 54.8M 1s 496050K .......... .......... .......... .......... .......... 97% 47.0M 1s 496100K .......... .......... .......... .......... .......... 97% 38.0M 1s 496150K .......... .......... .......... .......... .......... 97% 52.8M 1s 496200K .......... .......... .......... .......... .......... 97% 25.5M 1s 496250K .......... .......... .......... .......... .......... 97% 52.8M 1s 496300K .......... .......... .......... .......... .......... 97% 41.7M 1s 496350K .......... .......... .......... .......... .......... 97% 45.5M 1s 496400K .......... .......... .......... .......... .......... 97% 47.1M 1s 496450K .......... .......... .......... .......... .......... 97% 26.6M 1s 496500K .......... .......... .......... .......... .......... 97% 43.3M 1s 496550K .......... .......... .......... .......... .......... 97% 50.8M 1s 496600K .......... .......... .......... .......... .......... 97% 46.3M 1s 496650K .......... .......... .......... .......... .......... 97% 26.3M 1s 496700K .......... .......... .......... .......... .......... 97% 49.2M 1s 496750K .......... .......... .......... .......... .......... 97% 42.2M 1s 496800K .......... .......... .......... .......... .......... 97% 122M 1s 496850K .......... .......... .......... .......... .......... 97% 41.1M 1s 496900K .......... .......... .......... .......... .......... 97% 157M 1s 496950K .......... .......... .......... .......... .......... 97% 94.3M 1s 497000K .......... .......... .......... .......... .......... 97% 43.1M 1s 497050K .......... .......... .......... .......... .......... 97% 118M 1s 497100K .......... .......... .......... .......... .......... 97% 23.6M 1s 497150K .......... .......... .......... .......... .......... 97% 588M 1s 497200K .......... .......... .......... .......... .......... 97% 498M 1s 497250K .......... .......... .......... .......... .......... 97% 35.2M 1s 497300K .......... .......... .......... .......... .......... 97% 120M 1s 497350K .......... .......... .......... .......... .......... 97% 260M 1s 497400K .......... .......... .......... .......... .......... 97% 48.2M 1s 497450K .......... .......... .......... .......... .......... 97% 57.9M 1s 497500K .......... .......... .......... .......... .......... 97% 61.0M 1s 497550K .......... .......... .......... .......... .......... 97% 63.0M 1s 497600K .......... .......... .......... .......... .......... 97% 52.2M 1s 497650K .......... .......... .......... .......... .......... 97% 60.7M 1s 497700K .......... .......... .......... .......... .......... 97% 46.2M 1s 497750K .......... .......... .......... .......... .......... 97% 49.0M 1s 497800K .......... .......... .......... .......... .......... 97% 62.8M 1s 497850K .......... .......... .......... .......... .......... 97% 53.1M 1s 497900K .......... .......... .......... .......... .......... 97% 63.1M 1s 497950K .......... .......... .......... .......... .......... 97% 56.4M 1s 498000K .......... .......... .......... .......... .......... 97% 48.6M 1s 498050K .......... .......... .......... .......... .......... 97% 52.8M 1s 498100K .......... .......... .......... .......... .......... 97% 49.6M 1s 498150K .......... .......... .......... .......... .......... 97% 78.9M 1s 498200K .......... .......... .......... .......... .......... 97% 46.9M 1s 498250K .......... .......... .......... .......... .......... 97% 51.1M 1s 498300K .......... .......... .......... .......... .......... 97% 47.0M 1s 498350K .......... .......... .......... .......... .......... 97% 42.5M 1s 498400K .......... .......... .......... .......... .......... 97% 72.1M 1s 498450K .......... .......... .......... .......... .......... 97% 52.6M 1s 498500K .......... .......... .......... .......... .......... 97% 55.6M 1s 498550K .......... .......... .......... .......... .......... 97% 51.8M 1s 498600K .......... .......... .......... .......... .......... 97% 48.2M 1s 498650K .......... .......... .......... .......... .......... 97% 50.8M 1s 498700K .......... .......... .......... .......... .......... 97% 49.2M 1s 498750K .......... .......... .......... .......... .......... 97% 48.1M 1s 498800K .......... .......... .......... .......... .......... 97% 182M 1s 498850K .......... .......... .......... .......... .......... 97% 51.1M 1s 498900K .......... .......... .......... .......... .......... 97% 52.8M 1s 498950K .......... .......... .......... .......... .......... 97% 50.1M 1s 499000K .......... .......... .......... .......... .......... 97% 19.7M 1s 499050K .......... .......... .......... .......... .......... 97% 48.4M 1s 499100K .......... .......... .......... .......... .......... 97% 51.7M 1s 499150K .......... .......... .......... .......... .......... 97% 55.2M 1s 499200K .......... .......... .......... .......... .......... 97% 76.1M 1s 499250K .......... .......... .......... .......... .......... 97% 38.0M 1s 499300K .......... .......... .......... .......... .......... 97% 61.5M 1s 499350K .......... .......... .......... .......... .......... 97% 38.3M 1s 499400K .......... .......... .......... .......... .......... 97% 29.4M 1s 499450K .......... .......... .......... .......... .......... 97% 24.6M 1s 499500K .......... .......... .......... .......... .......... 97% 414M 1s 499550K .......... .......... .......... .......... .......... 97% 26.5M 1s 499600K .......... .......... .......... .......... .......... 98% 124M 1s 499650K .......... .......... .......... .......... .......... 98% 38.9M 1s 499700K .......... .......... .......... .......... .......... 98% 34.7M 1s 499750K .......... .......... .......... .......... .......... 98% 42.1M 1s 499800K .......... .......... .......... .......... .......... 98% 41.7M 1s 499850K .......... .......... .......... .......... .......... 98% 46.8M 0s 499900K .......... .......... .......... .......... .......... 98% 46.8M 0s 499950K .......... .......... .......... .......... .......... 98% 35.0M 0s 500000K .......... .......... .......... .......... .......... 98% 53.5M 0s 500050K .......... .......... .......... .......... .......... 98% 46.8M 0s 500100K .......... .......... .......... .......... .......... 98% 31.5M 0s 500150K .......... .......... .......... .......... .......... 98% 52.7M 0s 500200K .......... .......... .......... .......... .......... 98% 34.5M 0s 500250K .......... .......... .......... .......... .......... 98% 52.1M 0s 500300K .......... .......... .......... .......... .......... 98% 52.0M 0s 500350K .......... .......... .......... .......... .......... 98% 34.0M 0s 500400K .......... .......... .......... .......... .......... 98% 52.8M 0s 500450K .......... .......... .......... .......... .......... 98% 35.9M 0s 500500K .......... .......... .......... .......... .......... 98% 45.7M 0s 500550K .......... .......... .......... .......... .......... 98% 16.2M 0s 500600K .......... .......... .......... .......... .......... 98% 45.7M 0s 500650K .......... .......... .......... .......... .......... 98% 52.3M 0s 500700K .......... .......... .......... .......... .......... 98% 46.8M 0s 500750K .......... .......... .......... .......... .......... 98% 52.8M 0s 500800K .......... .......... .......... .......... .......... 98% 32.5M 0s 500850K .......... .......... .......... .......... .......... 98% 46.5M 0s 500900K .......... .......... .......... .......... .......... 98% 48.3M 0s 500950K .......... .......... .......... .......... .......... 98% 47.3M 0s 501000K .......... .......... .......... .......... .......... 98% 34.7M 0s 501050K .......... .......... .......... .......... .......... 98% 41.7M 0s 501100K .......... .......... .......... .......... .......... 98% 73.6M 0s 501150K .......... .......... .......... .......... .......... 98% 64.3M 0s 501200K .......... .......... .......... .......... .......... 98% 68.6M 0s 501250K .......... .......... .......... .......... .......... 98% 23.8M 0s 501300K .......... .......... .......... .......... .......... 98% 381M 0s 501350K .......... .......... .......... .......... .......... 98% 397M 0s 501400K .......... .......... .......... .......... .......... 98% 425M 0s 501450K .......... .......... .......... .......... .......... 98% 28.5M 0s 501500K .......... .......... .......... .......... .......... 98% 102M 0s 501550K .......... .......... .......... .......... .......... 98% 493M 0s 501600K .......... .......... .......... .......... .......... 98% 47.8M 0s 501650K .......... .......... .......... .......... .......... 98% 428M 0s 501700K .......... .......... .......... .......... .......... 98% 63.4M 0s 501750K .......... .......... .......... .......... .......... 98% 46.9M 0s 501800K .......... .......... .......... .......... .......... 98% 52.3M 0s 501850K .......... .......... .......... .......... .......... 98% 40.5M 0s 501900K .......... .......... .......... .......... .......... 98% 60.9M 0s 501950K .......... .......... .......... .......... .......... 98% 17.4M 0s 502000K .......... .......... .......... .......... .......... 98% 36.4M 0s 502050K .......... .......... .......... .......... .......... 98% 43.4M 0s 502100K .......... .......... .......... .......... .......... 98% 40.5M 0s 502150K .......... .......... .......... .......... .......... 98% 45.1M 0s 502200K .......... .......... .......... .......... .......... 98% 37.1M 0s 502250K .......... .......... .......... .......... .......... 98% 93.9M 0s 502300K .......... .......... .......... .......... .......... 98% 45.4M 0s 502350K .......... .......... .......... .......... .......... 98% 50.1M 0s 502400K .......... .......... .......... .......... .......... 98% 61.0M 0s 502450K .......... .......... .......... .......... .......... 98% 42.6M 0s 502500K .......... .......... .......... .......... .......... 98% 53.0M 0s 502550K .......... .......... .......... .......... .......... 98% 57.4M 0s 502600K .......... .......... .......... .......... .......... 98% 27.9M 0s 502650K .......... .......... .......... .......... .......... 98% 39.3M 0s 502700K .......... .......... .......... .......... .......... 98% 50.5M 0s 502750K .......... .......... .......... .......... .......... 98% 48.1M 0s 502800K .......... .......... .......... .......... .......... 98% 49.3M 0s 502850K .......... .......... .......... .......... .......... 98% 50.4M 0s 502900K .......... .......... .......... .......... .......... 98% 50.3M 0s 502950K .......... .......... .......... .......... .......... 98% 55.0M 0s 503000K .......... .......... .......... .......... .......... 98% 118M 0s 503050K .......... .......... .......... .......... .......... 98% 57.0M 0s 503100K .......... .......... .......... .......... .......... 98% 53.1M 0s 503150K .......... .......... .......... .......... .......... 98% 66.7M 0s 503200K .......... .......... .......... .......... .......... 98% 54.9M 0s 503250K .......... .......... .......... .......... .......... 98% 54.7M 0s 503300K .......... .......... .......... .......... .......... 98% 48.0M 0s 503350K .......... .......... .......... .......... .......... 98% 54.5M 0s 503400K .......... .......... .......... .......... .......... 98% 127M 0s 503450K .......... .......... .......... .......... .......... 98% 53.7M 0s 503500K .......... .......... .......... .......... .......... 98% 72.9M 0s 503550K .......... .......... .......... .......... .......... 98% 44.7M 0s 503600K .......... .......... .......... .......... .......... 98% 21.1M 0s 503650K .......... .......... .......... .......... .......... 98% 428M 0s 503700K .......... .......... .......... .......... .......... 98% 45.0M 0s 503750K .......... .......... .......... .......... .......... 98% 356M 0s 503800K .......... .......... .......... .......... .......... 98% 29.9M 0s 503850K .......... .......... .......... .......... .......... 98% 42.4M 0s 503900K .......... .......... .......... .......... .......... 98% 163M 0s 503950K .......... .......... .......... .......... .......... 98% 370M 0s 504000K .......... .......... .......... .......... .......... 98% 158M 0s 504050K .......... .......... .......... .......... .......... 98% 25.2M 0s 504100K .......... .......... .......... .......... .......... 98% 49.2M 0s 504150K .......... .......... .......... .......... .......... 98% 71.3M 0s 504200K .......... .......... .......... .......... .......... 98% 50.5M 0s 504250K .......... .......... .......... .......... .......... 98% 44.4M 0s 504300K .......... .......... .......... .......... .......... 98% 44.6M 0s 504350K .......... .......... .......... .......... .......... 98% 46.6M 0s 504400K .......... .......... .......... .......... .......... 98% 53.4M 0s 504450K .......... .......... .......... .......... .......... 98% 41.0M 0s 504500K .......... .......... .......... .......... .......... 98% 54.1M 0s 504550K .......... .......... .......... .......... .......... 98% 38.1M 0s 504600K .......... .......... .......... .......... .......... 98% 48.4M 0s 504650K .......... .......... .......... .......... .......... 99% 29.0M 0s 504700K .......... .......... .......... .......... .......... 99% 51.0M 0s 504750K .......... .......... .......... .......... .......... 99% 47.9M 0s 504800K .......... .......... .......... .......... .......... 99% 46.6M 0s 504850K .......... .......... .......... .......... .......... 99% 36.9M 0s 504900K .......... .......... .......... .......... .......... 99% 26.0M 0s 504950K .......... .......... .......... .......... .......... 99% 60.7M 0s 505000K .......... .......... .......... .......... .......... 99% 52.6M 0s 505050K .......... .......... .......... .......... .......... 99% 44.5M 0s 505100K .......... .......... .......... .......... .......... 99% 46.6M 0s 505150K .......... .......... .......... .......... .......... 99% 45.8M 0s 505200K .......... .......... .......... .......... .......... 99% 31.7M 0s 505250K .......... .......... .......... .......... .......... 99% 47.5M 0s 505300K .......... .......... .......... .......... .......... 99% 46.7M 0s 505350K .......... .......... .......... .......... .......... 99% 33.6M 0s 505400K .......... .......... .......... .......... .......... 99% 46.7M 0s 505450K .......... .......... .......... .......... .......... 99% 45.9M 0s 505500K .......... .......... .......... .......... .......... 99% 37.9M 0s 505550K .......... .......... .......... .......... .......... 99% 47.9M 0s 505600K .......... .......... .......... .......... .......... 99% 47.4M 0s 505650K .......... .......... .......... .......... .......... 99% 47.7M 0s 505700K .......... .......... .......... .......... .......... 99% 40.1M 0s 505750K .......... .......... .......... .......... .......... 99% 39.0M 0s 505800K .......... .......... .......... .......... .......... 99% 45.8M 0s 505850K .......... .......... .......... .......... .......... 99% 61.0M 0s 505900K .......... .......... .......... .......... .......... 99% 116M 0s 505950K .......... .......... .......... .......... .......... 99% 29.0M 0s 506000K .......... .......... .......... .......... .......... 99% 17.9M 0s 506050K .......... .......... .......... .......... .......... 99% 282M 0s 506100K .......... .......... .......... .......... .......... 99% 315M 0s 506150K .......... .......... .......... .......... .......... 99% 18.0M 0s 506200K .......... .......... .......... .......... .......... 99% 470M 0s 506250K .......... .......... .......... .......... .......... 99% 26.6M 0s 506300K .......... .......... .......... .......... .......... 99% 42.3M 0s 506350K .......... .......... .......... .......... .......... 99% 39.7M 0s 506400K .......... .......... .......... .......... .......... 99% 57.0M 0s 506450K .......... .......... .......... .......... .......... 99% 26.3M 0s 506500K .......... .......... .......... .......... .......... 99% 46.4M 0s 506550K .......... .......... .......... .......... .......... 99% 27.9M 0s 506600K .......... .......... .......... .......... .......... 99% 32.2M 0s 506650K .......... .......... .......... .......... .......... 99% 31.6M 0s 506700K .......... .......... .......... .......... .......... 99% 26.3M 0s 506750K .......... .......... .......... .......... .......... 99% 37.2M 0s 506800K .......... .......... .......... .......... .......... 99% 31.7M 0s 506850K .......... .......... .......... .......... .......... 99% 40.8M 0s 506900K .......... .......... .......... .......... .......... 99% 25.6M 0s 506950K .......... .......... .......... .......... .......... 99% 45.2M 0s 507000K .......... .......... .......... .......... .......... 99% 27.0M 0s 507050K .......... .......... .......... .......... .......... 99% 31.8M 0s 507100K .......... .......... .......... .......... .......... 99% 25.4M 0s 507150K .......... .......... .......... .......... .......... 99% 17.8M 0s 507200K .......... .......... .......... .......... .......... 99% 26.3M 0s 507250K .......... .......... .......... .......... .......... 99% 34.0M 0s 507300K .......... .......... .......... .......... .......... 99% 34.1M 0s 507350K .......... .......... .......... .......... .......... 99% 31.6M 0s 507400K .......... .......... .......... .......... .......... 99% 42.0M 0s 507450K .......... .......... .......... .......... .......... 99% 26.9M 0s 507500K .......... .......... .......... .......... .......... 99% 34.1M 0s 507550K .......... .......... .......... .......... .......... 99% 48.7M 0s 507600K .......... .......... .......... .......... .......... 99% 13.7M 0s 507650K .......... .......... .......... .......... .......... 99% 440M 0s 507700K .......... .......... .......... .......... .......... 99% 93.4M 0s 507750K .......... .......... .......... .......... .......... 99% 26.3M 0s 507800K .......... .......... .......... .......... .......... 99% 213M 0s 507850K .......... .......... .......... .......... .......... 99% 27.4M 0s 507900K .......... .......... .......... .......... .......... 99% 45.0M 0s 507950K .......... .......... .......... .......... .......... 99% 26.2M 0s 508000K .......... .......... .......... .......... .......... 99% 41.5M 0s 508050K .......... .......... .......... .......... .......... 99% 42.6M 0s 508100K .......... .......... .......... .......... .......... 99% 28.9M 0s 508150K .......... .......... .......... .......... .......... 99% 39.6M 0s 508200K .......... .......... .......... .......... .......... 99% 27.0M 0s 508250K .......... .......... .......... .......... .......... 99% 41.3M 0s 508300K .......... .......... .......... .......... .......... 99% 41.0M 0s 508350K .......... .......... .......... .......... .......... 99% 26.0M 0s 508400K .......... .......... .......... .......... .......... 99% 34.9M 0s 508450K .......... .......... .......... .......... .......... 99% 26.7M 0s 508500K .......... .......... .......... .......... .......... 99% 34.0M 0s 508550K .......... .......... .......... .......... .......... 99% 37.9M 0s 508600K .......... .......... .......... .......... .......... 99% 26.6M 0s 508650K .......... .......... .......... .......... .......... 99% 46.3M 0s 508700K .......... .......... .......... .......... .......... 99% 31.1M 0s 508750K .......... .......... .......... .......... .......... 99% 41.7M 0s 508800K .......... .......... .......... .......... .......... 99% 53.8M 0s 508850K .......... .......... .......... .......... .......... 99% 28.9M 0s 508900K .......... .......... .......... .......... .......... 99% 37.2M 0s 508950K .......... .......... .......... .......... .......... 99% 26.7M 0s 509000K .......... .......... .......... .......... .......... 99% 51.4M 0s 509050K .......... .......... .......... .......... .......... 99% 42.4M 0s 509100K .......... .......... .......... .......... .......... 99% 43.8M 0s 509150K .......... .......... .......... .......... .......... 99% 37.3M 0s 509200K .......... .......... .......... .......... .......... 99% 25.4M 0s 509250K .......... .......... .......... .......... .......... 99% 176M 0s 509300K .......... .......... .......... .......... .......... 99% 23.9M 0s 509350K .......... .......... .......... .......... .......... 99% 95.6M 0s 509400K .......... .......... .......... .......... .......... 99% 24.2M 0s 509450K .......... .......... .......... .......... .......... 99% 109M 0s 509500K .......... .......... .......... .......... .......... 99% 29.7M 0s 509550K .......... .......... .......... .......... .......... 99% 76.8M 0s 509600K .......... .......... .......... .......... .......... 99% 21.3M 0s 509650K .......... .......... .......... .......... .......... 99% 270M 0s 509700K .......... .......... .......... .......... .......... 99% 21.7M 0s 509750K .......... .......... .......... .......... ...... 100% 473M=25s 2024-07-28 00:00:33 (19.6 MB/s) - ‘ESP126-macos-arm64.tgz’ saved [522032067/522032067] + tar -xf ESP126-macos-arm64.tgz + cd ESP126 + rm -rf /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Slugs ++ uname -a + [[ Darwin VIGGEN.MIT.EDU 23.5.0 Darwin Kernel Version 23.5.0: Wed May 1 20:16:51 PDT 2024; root:xnu-10063.121.3~5/RELEASE_ARM64_T8103 arm64 == *\D\a\r\w\i\n* ]] + ./setup.command Custom icon assigned to '/Users/jenkins/Desktop/ESP126.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/esp_logo.png'. Custom icon assigned to '/Users/jenkins/Desktop/runESP126.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/esp_logo.png'. Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/idle3.11' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pyftsubset' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_op4' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/ttx' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/wingproj' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_op2' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pip3' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_bdf' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/imageio_remove_bin' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/undill' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/bdf' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/run_om_test' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/f90nml' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/webview' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/fonttools' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/openmdao' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pyNastranGUI' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/f2py' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pydoc3.11' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/2to3-3.11' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/imageio_download_bin' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pip3.11' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_pynastrangui' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/numba' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/normalizer' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/virtualenv' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/reset_notebook' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/abaqus_to_nastran' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/get_gprof' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/format_converter' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pyftmerge' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python3.11-config' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/f06' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/get_objgraph' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/config-3.11-darwin/Makefile' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/config-3.11-darwin/python-config.py' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/pkgconfig/python-3.11-embed.pc' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/pkgconfig/python-3.11.pc' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/_sysconfigdata__darwin_darwin.py' Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages/mpi4py/mpi.cfg' Patching 'lib/cmake/libevent/LibeventTargets-shared-release.cmake' Patching 'lib/cmake/libevent/LibeventTargets-shared.cmake' Patching 'lib/pkgconfig/libevent.pc' Patching 'lib/pkgconfig/libevent_core.pc' Patching 'lib/pkgconfig/libevent_extra.pc' Patching 'lib/pkgconfig/libevent_openssl.pc' Patching 'lib/pkgconfig/libevent_pthreads.pc' Patching 'bin/mpirun_esp' Patching 'bin/ompi_info' Patching 'bin/pmix_info' Patching 'bin/prte_info' Patching 'lib/libmpi.40.dylib' Patching 'lib/libopen-pal.80.dylib' Patching 'lib/libpmix.2.dylib' Patching 'lib/libprrte.3.dylib' Patching 'lib/openmpi/mca_io_romio341.so' Patching 'lib/prte/prte_mca_schizo_ompi.so' Patching 'include/pmix/src/include/pmix_config.h' Patching 'lib/pkgconfig/ompi-c.pc' Patching 'lib/pkgconfig/ompi-cxx.pc' Patching 'lib/pkgconfig/ompi-fort.pc' Patching 'lib/pkgconfig/ompi.pc' Patching 'lib/pkgconfig/pmix.pc' Patching 'share/openmpi/mpic++-wrapper-data.txt' Patching 'share/openmpi/mpicc-wrapper-data.txt' Patching 'share/openmpi/mpifort-wrapper-data.txt' Patching 'share/pmix/pmixcc-wrapper-data.txt' + rm -rf /Users/jenkins/Desktop/ESP126.command /Users/jenkins/Desktop/runESP126.command + source /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESPenv.sh ++ export ESP_ARCH=DARWIN_ARM64 ++ ESP_ARCH=DARWIN_ARM64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad ++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad ++ export CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/OpenCASCADE-7.8.1 ++ CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/OpenCASCADE-7.8.1 ++ export CASARCH=. ++ CASARCH=. ++ export CASREV=7.8 ++ CASREV=7.8 ++ '[' -z /Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ']' ++ export PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ export PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/include/python3.11 ++ PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/include/python3.11 ++ export 'PYTHONLIB=-L/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib -lpython3.11' ++ PYTHONLIB='-L/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib -lpython3.11' ++ '[' -z /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ']' ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/udunits/udunits2.xml ++ export CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/pointwise/glyph ++ CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/pointwise/glyph ++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/SLUGS/Slugs.html' ++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/SLUGS/Slugs.html' ++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/ESP-localhost7681.html' ++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/ESP-localhost7681.html' ++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/wvClient/wv.html' ++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/wvClient/wv.html' + which python /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python + python --version Python 3.11.9 + export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data + CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data + cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin ++ uname -a + [[ Darwin VIGGEN.MIT.EDU 23.5.0 Darwin Kernel Version 23.5.0: Wed May 1 20:16:51 PDT 2024; root:xnu-10063.121.3~5/RELEASE_ARM64_T8103 arm64 == *\D\a\r\w\i\n* ]] + sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh + bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh + expectSuccess 01 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/expressions + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/expressions WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/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 0m6.047s user 0m0.104s sys 0m0.017s + set +x ============================================= ESP verification case 01 passed (as expected) ============================================= + expectSuccess 02 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/demo2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/demo2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/demo2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.213s user 0m0.237s sys 0m0.028s + set +x ============================================= ESP verification case 02 passed (as expected) ============================================= + expectSuccess 03 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial1_whole + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial1_whole WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/verify_7.8.1/tutorial1_whole.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m1.365s user 0m2.053s sys 0m0.507s + set +x ============================================= ESP verification case 03 passed (as expected) ============================================= + expectSuccess 04 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/design2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.306s user 0m0.346s sys 0m0.035s + set +x ============================================= ESP verification case 04 passed (as expected) ============================================= + expectSuccess 05 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/design3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.329s user 0m0.451s sys 0m0.030s + set +x ============================================= ESP verification case 05 passed (as expected) ============================================= + expectSuccess 06 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/verify_7.8.1/tutorial2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.346s user 0m0.478s sys 0m0.019s + set +x ============================================= ESP verification case 06 passed (as expected) ============================================= + expectSuccess 07 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/verify_7.8.1/tutorial3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m2.334s user 0m3.588s sys 0m0.366s + set +x ============================================= ESP verification case 07 passed (as expected) ============================================= + expectSuccess 08 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/CAPS/myPlane + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/CAPS/myPlane WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/CAPS/verify_7.8.1/myPlane.vfy", so verification is being skipped ==> serveESP completed successfully with 12 warnings and no verification data real 0m15.772s user 0m28.428s sys 0m1.386s + set +x ============================================= ESP verification case 08 passed (as expected) ============================================= + expectSuccess 09 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/bottle + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/bottle WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/verify_7.8.1/bottle.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.346s user 0m0.412s sys 0m0.015s + set +x ============================================= ESP verification case 09 passed (as expected) ============================================= + expectSuccess 10 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/wingMultiModel + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/wingMultiModel WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/wingMultiModel.vfy", so verification is being skipped ==> serveESP completed successfully with 4 warnings and no verification data real 0m17.906s user 0m50.913s sys 0m27.525s + set +x ============================================= ESP verification case 10 passed (as expected) ============================================= + expectSuccess 11 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/bullet + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/bullet WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/bullet.vfy", so verification is being skipped WARNING:: 8 _hist and/or __trace__ attributes removed WARNING:: 8 _hist and/or __trace__ attributes removed WARNING:: could not find mapping for iedge=10 WARNING:: could not find mapping for iedge=14 WARNING:: could not find mapping for iedge=7 WARNING:: could not find mapping for iedge=11 ==> serveESP completed successfully with 4 warnings and no verification data real 0m0.365s user 0m0.213s sys 0m0.019s + set +x ============================================= ESP verification case 11 passed (as expected) ============================================= + expectSuccess 12 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/connect5 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/connect5 WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/connect5.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.360s user 0m0.556s sys 0m0.009s + set +x ============================================= ESP verification case 12 passed (as expected) ============================================= + expectSuccess 13 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/group2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/group2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/group2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.138s user 0m0.152s sys 0m0.007s + set +x ============================================= ESP verification case 13 passed (as expected) ============================================= + expectSuccess 14 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/csm3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/csm3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/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 0m0.403s user 0m0.313s sys 0m0.011s + set +x ============================================= ESP verification case 14 passed (as expected) ============================================= + cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/testEGADS + make test python --version Python 3.11.9 python -u -m unittest discover ...................................................... PCurve Map: 48 (alloc 48)! Surface Map: 12 (alloc 24)! Curve Map: 28 (alloc 28)! Writing PCurves... Writing Curves... Writing Surfaces... Writing 16 Nodes... Writing 28 Edges... Writing 12 Loops... Writing 12 Faces... Writing 1 Shells... EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close! ................... ---------------------------------------------------------------------- Ran 73 tests in 1.156s OK + cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/testOCSM + source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/test_pyOCSM.sh ++ set -x ++ python -u test_pyOCSM.py -skipHelp real 0m5.000s user 0m5.583s sys 0m0.090s ++ set +x ================================================= test_pyOCSM.py passed (as expected) ================================================= + cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 = 155 Number of elements = 306 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 306 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 298 Combined Number of elements = 588 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 588 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ..Writing D3 Javascript library - d3.v3.min.js ........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .No analysis directory provided - defaulting to altName Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 209 Number of elements = 414 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 414 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 186 Number of elements = 368 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 368 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 395 Combined Number of elements = 782 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 782 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input ..........--> Opening DESPMTR file "unitGeom.param" updating CFGPMTR series [ 1, 1] = 8412.000000 updating CFGPMTR series2 [ 1, 1] = 20.000000 updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000 updating CFGPMTR nrow [ 1, 1] = 3.000000 updating CFGPMTR ncol [ 1, 1] = 2.000000 updating DESPMTR area [ 1, 1] = 40.000000 updating DESPMTR aspect [ 1, 1] = 5.000000 updating DESPMTR taper [ 1, 1] = 0.500000 updating DESPMTR twist [ 1, 1] = 15.000000 updating DESPMTR wing:lesweep [ 1, 1] = 30.000000 updating DESPMTR wing:dihedral [ 1, 1] = 1.000000 updating DESPMTR wing:chord:root [ 1, 1] = 1.560000 updating DESPMTR htail [ 1, 1] = 1.000000 updating DESPMTR htail:chord [ 1, 1] = 2.000000 updating DESPMTR vtail:chord [ 1, 1] = 3.000000 updating DESPMTR vtail [ 1, 1] = 4.000000 updating DESPMTR sphereR [ 1, 1] = 80.000000 updating DESPMTR v@1:d_name [ 1, 1] = 1.000000 updating DESPMTR despMat [ 1, 1] = 11.000000 updating DESPMTR despMat [ 1, 2] = 12.000000 updating DESPMTR despMat [ 2, 1] = 13.000000 updating DESPMTR despMat [ 2, 2] = 14.000000 updating DESPMTR despMat [ 3, 1] = 15.000000 updating DESPMTR despMat [ 3, 2] = 16.000000 updating DESPMTR despCol [ 1, 1] = 11.000000 updating DESPMTR despCol [ 2, 1] = 13.000000 updating DESPMTR despCol [ 3, 1] = 15.000000 updating DESPMTR despRow [ 1, 1] = 11.000000 updating DESPMTR despRow [ 1, 2] = 12.000000 updating DESPMTR despRow [ 1, 3] = 13.000000 ERROR:: DESPMTR file "unitGeom.param" not found CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! ..Linked Parameter Beta to analysis su2 input Beta Linked Parameter Alpha to analysis su2 input Alpha No linkable data found for Altitude No linkable data found for Strings No linkable data found for Strings2 Linked Parameter Beta to analysis su2 input Beta Linked Parameter Alpha to analysis su2 input Alpha ............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . CAPS Info: Hit last success -- going live! ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .--> Opening DESPMTR file "unitGeom.param" updating CFGPMTR series [ 1, 1] = 8412.000000 updating CFGPMTR series2 [ 1, 1] = 20.000000 updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000 updating CFGPMTR nrow [ 1, 1] = 3.000000 updating CFGPMTR ncol [ 1, 1] = 2.000000 updating DESPMTR area [ 1, 1] = 40.000000 updating DESPMTR aspect [ 1, 1] = 5.000000 updating DESPMTR taper [ 1, 1] = 0.500000 updating DESPMTR twist [ 1, 1] = 15.000000 updating DESPMTR wing:lesweep [ 1, 1] = 30.000000 updating DESPMTR wing:dihedral [ 1, 1] = 1.000000 updating DESPMTR wing:chord:root [ 1, 1] = 1.560000 updating DESPMTR htail [ 1, 1] = 1.000000 updating DESPMTR htail:chord [ 1, 1] = 2.000000 updating DESPMTR vtail:chord [ 1, 1] = 3.000000 updating DESPMTR vtail [ 1, 1] = 4.000000 updating DESPMTR sphereR [ 1, 1] = 80.000000 updating DESPMTR v@1:d_name [ 1, 1] = 1.000000 updating DESPMTR despMat [ 1, 1] = 11.000000 updating DESPMTR despMat [ 1, 2] = 12.000000 updating DESPMTR despMat [ 2, 1] = 13.000000 updating DESPMTR despMat [ 2, 2] = 14.000000 updating DESPMTR despMat [ 3, 1] = 15.000000 updating DESPMTR despMat [ 3, 2] = 16.000000 updating DESPMTR despCol [ 1, 1] = 11.000000 updating DESPMTR despCol [ 2, 1] = 13.000000 updating DESPMTR despCol [ 3, 1] = 15.000000 updating DESPMTR despRow [ 1, 1] = 11.000000 updating DESPMTR despRow [ 1, 2] = 12.000000 updating DESPMTR despRow [ 1, 3] = 13.000000 ERROR:: DESPMTR file "unitGeom.param" not found CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ---------------------------------------------------------------------- Ran 100 tests in 10.247s 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 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/ + make test python --version Python 3.11.9 python -u -m unittest discover --verbose test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM 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 = 0.014 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4285 6326 AFLR2 GG : Nodes, Faces = 6135 10026 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9485 16726 AFLR2 GG : Nodes, Faces = 10981 19718 AFLR2 GG : Nodes, Faces = 12372 22500 AFLR2 GG : Nodes, Faces = 13686 25128 AFLR2 GG : Nodes, Faces = 14908 27572 AFLR2 GG : Nodes, Faces = 16063 29882 AFLR2 GG : Nodes, Faces = 17170 32096 AFLR2 GG : Nodes, Faces = 18222 34200 AFLR2 GG : Nodes, Faces = 19208 36172 AFLR2 GG : Nodes, Faces = 20165 38086 AFLR2 GG : Nodes, Faces = 21087 39930 AFLR2 GG : Nodes, Faces = 21975 41706 AFLR2 GG : Nodes, Faces = 22803 43362 AFLR2 GG : Nodes, Faces = 23582 44920 AFLR2 GG : Nodes, Faces = 24330 46416 AFLR2 GG : Nodes, Faces = 25041 47838 AFLR2 GG : Nodes, Faces = 25723 49202 AFLR2 GG : Nodes, Faces = 26365 50486 AFLR2 GG : Nodes, Faces = 26993 51742 AFLR2 GG : Nodes, Faces = 27556 52868 AFLR2 GG : Nodes, Faces = 28054 53864 AFLR2 GG : Nodes, Faces = 28487 54730 AFLR2 GG : Nodes, Faces = 28847 55450 AFLR2 GG : Nodes, Faces = 29118 55992 AFLR2 GG : Nodes, Faces = 29355 56466 AFLR2 GG : Nodes, Faces = 29553 56862 AFLR2 GG : Nodes, Faces = 29735 57226 AFLR2 GG : Nodes, Faces = 29878 57512 AFLR2 GG : Nodes, Faces = 29969 57694 AFLR2 GG : Nodes, Faces = 30009 57774 AFLR2 GG : Nodes, Faces = 30018 57792 AFLR2 GG : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.039 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 30019 Number of elements = 60038 Number of tris = 57794 Number of quad = 0 Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 918 1838 AFLR2 IG : Nodes, Faces = 1033 2068 AFLR2 IG : Nodes, Faces = 1133 2268 AFLR2 IG : Nodes, Faces = 1233 2468 AFLR2 IG : Nodes, Faces = 1333 2668 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1433 2868 AFLR2 IG : Nodes, Faces = 1533 3068 AFLR2 IG : Nodes, Faces = 1633 3268 AFLR2 IG : Nodes, Faces = 1733 3468 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1833 3668 AFLR2 IG : Nodes, Faces = 1858 3718 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.014 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4120 6016 AFLR2 GG : Nodes, Faces = 5820 9416 AFLR2 GG : Nodes, Faces = 7322 12420 AFLR2 GG : Nodes, Faces = 8613 15002 AFLR2 GG : Nodes, Faces = 9793 17362 AFLR2 GG : Nodes, Faces = 10847 19470 AFLR2 GG : Nodes, Faces = 11828 21432 AFLR2 GG : Nodes, Faces = 12749 23274 AFLR2 GG : Nodes, Faces = 13580 24936 AFLR2 GG : Nodes, Faces = 14355 26486 AFLR2 GG : Nodes, Faces = 15088 27952 AFLR2 GG : Nodes, Faces = 15774 29324 AFLR2 GG : Nodes, Faces = 16420 30616 AFLR2 GG : Nodes, Faces = 17013 31802 AFLR2 GG : Nodes, Faces = 17571 32918 AFLR2 GG : Nodes, Faces = 18089 33954 AFLR2 GG : Nodes, Faces = 18573 34922 AFLR2 GG : Nodes, Faces = 19005 35786 AFLR2 GG : Nodes, Faces = 19413 36602 AFLR2 GG : Nodes, Faces = 19779 37334 AFLR2 GG : Nodes, Faces = 20116 38008 AFLR2 GG : Nodes, Faces = 20443 38662 AFLR2 GG : Nodes, Faces = 20756 39288 AFLR2 GG : Nodes, Faces = 21054 39884 AFLR2 GG : Nodes, Faces = 21344 40464 AFLR2 GG : Nodes, Faces = 21621 41018 AFLR2 GG : Nodes, Faces = 21885 41546 AFLR2 GG : Nodes, Faces = 22137 42050 AFLR2 GG : Nodes, Faces = 22387 42550 AFLR2 GG : Nodes, Faces = 22603 42982 AFLR2 GG : Nodes, Faces = 22772 43320 AFLR2 GG : Nodes, Faces = 22912 43600 AFLR2 GG : Nodes, Faces = 23039 43854 AFLR2 GG : Nodes, Faces = 23142 44060 AFLR2 GG : Nodes, Faces = 23205 44186 AFLR2 GG : Nodes, Faces = 23240 44256 AFLR2 GG : Nodes, Faces = 23257 44290 AFLR2 GG : Nodes, Faces = 23269 44314 AFLR2 GG : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.037 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23273 Number of elements = 46546 Number of tris = 44322 Number of quad = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM 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 = 0.014 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4285 6326 AFLR2 GG : Nodes, Faces = 6135 10026 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9485 16726 AFLR2 GG : Nodes, Faces = 10981 19718 AFLR2 GG : Nodes, Faces = 12372 22500 AFLR2 GG : Nodes, Faces = 13686 25128 AFLR2 GG : Nodes, Faces = 14908 27572 AFLR2 GG : Nodes, Faces = 16063 29882 AFLR2 GG : Nodes, Faces = 17170 32096 AFLR2 GG : Nodes, Faces = 18222 34200 AFLR2 GG : Nodes, Faces = 19208 36172 AFLR2 GG : Nodes, Faces = 20165 38086 AFLR2 GG : Nodes, Faces = 21087 39930 AFLR2 GG : Nodes, Faces = 21975 41706 AFLR2 GG : Nodes, Faces = 22803 43362 AFLR2 GG : Nodes, Faces = 23582 44920 AFLR2 GG : Nodes, Faces = 24330 46416 AFLR2 GG : Nodes, Faces = 25041 47838 AFLR2 GG : Nodes, Faces = 25723 49202 AFLR2 GG : Nodes, Faces = 26365 50486 AFLR2 GG : Nodes, Faces = 26993 51742 AFLR2 GG : Nodes, Faces = 27556 52868 AFLR2 GG : Nodes, Faces = 28054 53864 AFLR2 GG : Nodes, Faces = 28487 54730 AFLR2 GG : Nodes, Faces = 28847 55450 AFLR2 GG : Nodes, Faces = 29118 55992 AFLR2 GG : Nodes, Faces = 29355 56466 AFLR2 GG : Nodes, Faces = 29553 56862 AFLR2 GG : Nodes, Faces = 29735 57226 AFLR2 GG : Nodes, Faces = 29878 57512 AFLR2 GG : Nodes, Faces = 29969 57694 AFLR2 GG : Nodes, Faces = 30009 57774 AFLR2 GG : Nodes, Faces = 30018 57792 AFLR2 GG : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.039 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 30019 Number of elements = 60038 Number of tris = 57794 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 918 1838 AFLR2 IG : Nodes, Faces = 1033 2068 AFLR2 IG : Nodes, Faces = 1133 2268 AFLR2 IG : Nodes, Faces = 1233 2468 AFLR2 IG : Nodes, Faces = 1333 2668 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1433 2868 AFLR2 IG : Nodes, Faces = 1533 3068 AFLR2 IG : Nodes, Faces = 1633 3268 AFLR2 IG : Nodes, Faces = 1733 3468 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1833 3668 AFLR2 IG : Nodes, Faces = 1858 3718 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.014 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4120 6016 AFLR2 GG : Nodes, Faces = 5820 9416 AFLR2 GG : Nodes, Faces = 7322 12420 AFLR2 GG : Nodes, Faces = 8613 15002 AFLR2 GG : Nodes, Faces = 9793 17362 AFLR2 GG : Nodes, Faces = 10847 19470 AFLR2 GG : Nodes, Faces = 11828 21432 AFLR2 GG : Nodes, Faces = 12749 23274 AFLR2 GG : Nodes, Faces = 13580 24936 AFLR2 GG : Nodes, Faces = 14355 26486 AFLR2 GG : Nodes, Faces = 15088 27952 AFLR2 GG : Nodes, Faces = 15774 29324 AFLR2 GG : Nodes, Faces = 16420 30616 AFLR2 GG : Nodes, Faces = 17013 31802 AFLR2 GG : Nodes, Faces = 17571 32918 AFLR2 GG : Nodes, Faces = 18089 33954 AFLR2 GG : Nodes, Faces = 18573 34922 AFLR2 GG : Nodes, Faces = 19005 35786 AFLR2 GG : Nodes, Faces = 19413 36602 AFLR2 GG : Nodes, Faces = 19779 37334 AFLR2 GG : Nodes, Faces = 20116 38008 AFLR2 GG : Nodes, Faces = 20443 38662 AFLR2 GG : Nodes, Faces = 20756 39288 AFLR2 GG : Nodes, Faces = 21054 39884 AFLR2 GG : Nodes, Faces = 21344 40464 AFLR2 GG : Nodes, Faces = 21621 41018 AFLR2 GG : Nodes, Faces = 21885 41546 AFLR2 GG : Nodes, Faces = 22137 42050 AFLR2 GG : Nodes, Faces = 22387 42550 AFLR2 GG : Nodes, Faces = 22603 42982 AFLR2 GG : Nodes, Faces = 22772 43320 AFLR2 GG : Nodes, Faces = 22912 43600 AFLR2 GG : Nodes, Faces = 23039 43854 AFLR2 GG : Nodes, Faces = 23142 44060 AFLR2 GG : Nodes, Faces = 23205 44186 AFLR2 GG : Nodes, Faces = 23240 44256 AFLR2 GG : Nodes, Faces = 23257 44290 AFLR2 GG : Nodes, Faces = 23269 44314 AFLR2 GG : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.038 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23273 Number of elements = 46546 Number of tris = 44322 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 ok test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM 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 = 0.015 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4285 6326 AFLR2 GG : Nodes, Faces = 6135 10026 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9485 16726 AFLR2 GG : Nodes, Faces = 10981 19718 AFLR2 GG : Nodes, Faces = 12372 22500 AFLR2 GG : Nodes, Faces = 13686 25128 AFLR2 GG : Nodes, Faces = 14908 27572 AFLR2 GG : Nodes, Faces = 16063 29882 AFLR2 GG : Nodes, Faces = 17170 32096 AFLR2 GG : Nodes, Faces = 18222 34200 AFLR2 GG : Nodes, Faces = 19208 36172 AFLR2 GG : Nodes, Faces = 20165 38086 AFLR2 GG : Nodes, Faces = 21087 39930 AFLR2 GG : Nodes, Faces = 21975 41706 AFLR2 GG : Nodes, Faces = 22803 43362 AFLR2 GG : Nodes, Faces = 23582 44920 AFLR2 GG : Nodes, Faces = 24330 46416 AFLR2 GG : Nodes, Faces = 25041 47838 AFLR2 GG : Nodes, Faces = 25723 49202 AFLR2 GG : Nodes, Faces = 26365 50486 AFLR2 GG : Nodes, Faces = 26993 51742 AFLR2 GG : Nodes, Faces = 27556 52868 AFLR2 GG : Nodes, Faces = 28054 53864 AFLR2 GG : Nodes, Faces = 28487 54730 AFLR2 GG : Nodes, Faces = 28847 55450 AFLR2 GG : Nodes, Faces = 29118 55992 AFLR2 GG : Nodes, Faces = 29355 56466 AFLR2 GG : Nodes, Faces = 29553 56862 AFLR2 GG : Nodes, Faces = 29735 57226 AFLR2 GG : Nodes, Faces = 29878 57512 AFLR2 GG : Nodes, Faces = 29969 57694 AFLR2 GG : Nodes, Faces = 30009 57774 AFLR2 GG : Nodes, Faces = 30018 57792 AFLR2 GG : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.039 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 30019 Number of elements = 60038 Number of tris = 57794 Number of quad = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 48 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 10 22 AFLR2 IG : Nodes, Faces = 20 42 AFLR2 IG : Nodes, Faces = 30 62 AFLR2 IG : Nodes, Faces = 40 82 AFLR2 IG : Nodes, Faces = 45 92 AFLR2 IG : Nodes, Faces = 46 94 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 98 AFLR2 IG : Nodes, Faces = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 48 48 AFLR2 GG : Nodes, Faces = 88 128 AFLR2 GG : Nodes, Faces = 109 170 AFLR2 GG : Nodes, Faces = 124 200 AFLR2 GG : Nodes, Faces = 136 224 AFLR2 GG : Nodes, Faces = 148 248 AFLR2 GG : Nodes, Faces = 160 272 AFLR2 GG : Nodes, Faces = 172 296 AFLR2 GG : Nodes, Faces = 182 316 AFLR2 GG : Nodes, Faces = 188 328 AFLR2 GG : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 190 Number of elements = 380 Number of tris = 332 Number of quad = 0 ok test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 344 344 AFLR2 GG : Nodes, Faces = 679 1014 AFLR2 GG : Nodes, Faces = 1006 1668 AFLR2 GG : Nodes, Faces = 1321 2298 AFLR2 GG : Nodes, Faces = 1604 2864 AFLR2 GG : Nodes, Faces = 1886 3428 AFLR2 GG : Nodes, Faces = 2155 3966 AFLR2 GG : Nodes, Faces = 2409 4474 AFLR2 GG : Nodes, Faces = 2649 4954 AFLR2 GG : Nodes, Faces = 2867 5390 AFLR2 GG : Nodes, Faces = 3063 5782 AFLR2 GG : Nodes, Faces = 3243 6142 AFLR2 GG : Nodes, Faces = 3400 6456 AFLR2 GG : Nodes, Faces = 3540 6736 AFLR2 GG : Nodes, Faces = 3665 6986 AFLR2 GG : Nodes, Faces = 3786 7228 AFLR2 GG : Nodes, Faces = 3900 7456 AFLR2 GG : Nodes, Faces = 4010 7676 AFLR2 GG : Nodes, Faces = 4114 7884 AFLR2 GG : Nodes, Faces = 4209 8074 AFLR2 GG : Nodes, Faces = 4292 8240 AFLR2 GG : Nodes, Faces = 4368 8392 AFLR2 GG : Nodes, Faces = 4439 8534 AFLR2 GG : Nodes, Faces = 4503 8662 AFLR2 GG : Nodes, Faces = 4560 8776 AFLR2 GG : Nodes, Faces = 4611 8878 AFLR2 GG : Nodes, Faces = 4650 8956 AFLR2 GG : Nodes, Faces = 4677 9010 AFLR2 GG : Nodes, Faces = 4695 9046 AFLR2 GG : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.004 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.001 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4705 Number of elements = 9410 Number of tris = 9066 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing FAST file .... Finished writing FAST file Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 682 1020 AFLR2 GGp: Nodes, Faces = 1010 1676 AFLR2 GGp: Nodes, Faces = 1316 2288 AFLR2 GGp: Nodes, Faces = 1592 2840 AFLR2 GGp: Nodes, Faces = 1855 3366 AFLR2 GGp: Nodes, Faces = 2106 3868 AFLR2 GGp: Nodes, Faces = 2341 4338 AFLR2 GGp: Nodes, Faces = 2551 4758 AFLR2 GGp: Nodes, Faces = 2741 5138 AFLR2 GGp: Nodes, Faces = 2917 5490 AFLR2 GGp: Nodes, Faces = 3082 5820 AFLR2 GGp: Nodes, Faces = 3240 6136 AFLR2 GGp: Nodes, Faces = 3379 6414 AFLR2 GGp: Nodes, Faces = 3513 6682 AFLR2 GGp: Nodes, Faces = 3642 6940 AFLR2 GGp: Nodes, Faces = 3748 7152 AFLR2 GGp: Nodes, Faces = 3846 7348 AFLR2 GGp: Nodes, Faces = 3931 7518 AFLR2 GGp: Nodes, Faces = 3999 7654 AFLR2 GGp: Nodes, Faces = 4044 7744 AFLR2 GGp: Nodes, Faces = 4058 7772 AFLR2 : CPU Time = 0.008 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 = 0.004 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 682 1020 AFLR2 GGp: Nodes, Faces = 1010 1676 AFLR2 GGp: Nodes, Faces = 1316 2288 AFLR2 GGp: Nodes, Faces = 1592 2840 AFLR2 GGp: Nodes, Faces = 1855 3366 AFLR2 GGp: Nodes, Faces = 2106 3868 AFLR2 GGp: Nodes, Faces = 2341 4338 AFLR2 GGp: Nodes, Faces = 2551 4758 AFLR2 GGp: Nodes, Faces = 2741 5138 AFLR2 GGp: Nodes, Faces = 2917 5490 AFLR2 GGp: Nodes, Faces = 3082 5820 AFLR2 GGp: Nodes, Faces = 3240 6136 AFLR2 GGp: Nodes, Faces = 3379 6414 AFLR2 GGp: Nodes, Faces = 3513 6682 AFLR2 GGp: Nodes, Faces = 3642 6940 AFLR2 GGp: Nodes, Faces = 3748 7152 AFLR2 GGp: Nodes, Faces = 3846 7348 AFLR2 GGp: Nodes, Faces = 3931 7518 AFLR2 GGp: Nodes, Faces = 3999 7654 AFLR2 GGp: Nodes, Faces = 4044 7744 AFLR2 GGp: Nodes, Faces = 4058 7772 AFLR2 : CPU Time = 0.006 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4058 7772 AFLR2 QI : Nodes, Faces = 4057 364 AFLR2 QI : Nodes, Faces = 4057 3703 AFLR2 QI : Nodes, Faces = 4057 7770 AFLR2 QI : Nodes, Faces = 4056 344 AFLR2 QI : Nodes, Faces = 4056 3712 AFLR2 QI : Nodes, Faces = 4056 7768 AFLR2 QI : Nodes, Faces = 4055 348 AFLR2 QI : Nodes, Faces = 4055 3709 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 392 AFLR2 QI : Nodes, Faces = 4055 3687 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Tecplot file .... Finished writing Tecplot file ok test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 1198 Number of elements = 6307 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4975 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 6226 Number of elements = 34532 Number of triangles = 4438 Number of quadrilatarals = 0 Number of tetrahedrals = 30094 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 13688 Number of elements = 76798 Number of triangles = 8142 Number of quadrilatarals = 0 Number of tetrahedrals = 68656 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 41861 Number of elements = 237846 Number of triangles = 19888 Number of quadrilatarals = 0 Number of tetrahedrals = 217958 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 4339 Number of elements = 24073 Number of triangles = 3010 Number of quadrilatarals = 0 Number of tetrahedrals = 21063 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 11025 Number of elements = 60915 Number of triangles = 8632 Number of quadrilatarals = 0 Number of tetrahedrals = 52283 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 10398 Number of elements = 58234 Number of triangles = 6366 Number of quadrilatarals = 0 Number of tetrahedrals = 51868 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 88735 Number of elements = 498705 Number of triangles = 51808 Number of quadrilatarals = 0 Number of tetrahedrals = 446897 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 17445 Number of elements = 99279 Number of triangles = 8296 Number of quadrilatarals = 0 Number of tetrahedrals = 90983 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2585 Number of elements = 13784 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3615 Number of elements = 19589 Number of triangles = 3392 Number of quadrilatarals = 0 Number of tetrahedrals = 16197 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5438 Number of elements = 30214 Number of triangles = 3654 Number of quadrilatarals = 0 Number of tetrahedrals = 26560 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4697 Number of elements = 26013 Number of triangles = 3324 Number of quadrilatarals = 0 Number of tetrahedrals = 22689 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5467 Number of elements = 30346 Number of triangles = 3754 Number of quadrilatarals = 0 Number of tetrahedrals = 26592 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2273 Number of elements = 12220 Number of triangles = 2222 Number of quadrilatarals = 0 Number of tetrahedrals = 9998 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2405 Number of elements = 12664 Number of triangles = 2666 Number of quadrilatarals = 0 Number of tetrahedrals = 9998 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3357 Number of elements = 18188 Number of triangles = 3110 Number of quadrilatarals = 0 Number of tetrahedrals = 15078 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3622 Number of elements = 19080 Number of triangles = 4002 Number of quadrilatarals = 0 Number of tetrahedrals = 15078 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4425 Number of elements = 24045 Number of triangles = 4000 Number of quadrilatarals = 0 Number of tetrahedrals = 20045 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4822 Number of elements = 25381 Number of triangles = 5336 Number of quadrilatarals = 0 Number of tetrahedrals = 20045 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 4): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 4): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 4): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 4 (of 4): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5483 Number of elements = 29853 Number of triangles = 4890 Number of quadrilatarals = 0 Number of tetrahedrals = 24963 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6012 Number of elements = 31633 Number of triangles = 6670 Number of quadrilatarals = 0 Number of tetrahedrals = 24963 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1190 Number of elements = 6252 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4918 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6555 Number of elements = 35742 Number of triangles = 5780 Number of quadrilatarals = 0 Number of tetrahedrals = 29962 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7216 Number of elements = 37966 Number of triangles = 8004 Number of quadrilatarals = 0 Number of tetrahedrals = 29962 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 6): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 6): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 6): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 4 (of 6): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 5 (of 6): Number of nodes = 1190 Number of elements = 6252 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4918 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 6 (of 6): Number of nodes = 1204 Number of elements = 6333 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4999 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7634 Number of elements = 41677 Number of triangles = 6670 Number of quadrilatarals = 0 Number of tetrahedrals = 35007 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8427 Number of elements = 44345 Number of triangles = 9338 Number of quadrilatarals = 0 Number of tetrahedrals = 35007 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 1190 Number of elements = 6252 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4918 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 1204 Number of elements = 6333 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4999 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 1211 Number of elements = 6379 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5045 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 19879 Number of elements = 110275 Number of triangles = 15558 Number of quadrilatarals = 0 Number of tetrahedrals = 94717 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 8 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 9 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 10 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 11 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 12 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 13 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 14 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 15 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 16 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 17 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 18 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 19 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22822 Number of elements = 120055 Number of triangles = 25338 Number of quadrilatarals = 0 Number of tetrahedrals = 94717 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 19): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 19): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 19): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 4 (of 19): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 5 (of 19): Number of nodes = 1190 Number of elements = 6252 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4918 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 6 (of 19): Number of nodes = 1204 Number of elements = 6333 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4999 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 7 (of 19): Number of nodes = 1211 Number of elements = 6379 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5045 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 8 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 8 (of 19): Number of nodes = 1220 Number of elements = 6413 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5077 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 9 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 9 (of 19): Number of nodes = 1214 Number of elements = 6396 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5060 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 10 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 10 (of 19): Number of nodes = 1192 Number of elements = 6262 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4930 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 11 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 11 (of 19): Number of nodes = 1201 Number of elements = 6326 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4994 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 12 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 12 (of 19): Number of nodes = 1206 Number of elements = 6356 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5022 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 13 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 13 (of 19): Number of nodes = 1187 Number of elements = 6236 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4904 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 14 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 14 (of 19): Number of nodes = 1197 Number of elements = 6293 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4959 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 15 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 15 (of 19): Number of nodes = 1180 Number of elements = 6202 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4870 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 16 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 16 (of 19): Number of nodes = 1197 Number of elements = 6289 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4957 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 17 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 17 (of 19): Number of nodes = 1208 Number of elements = 6351 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 18 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 18 (of 19): Number of nodes = 1193 Number of elements = 6277 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4945 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 19 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 19 (of 19): Number of nodes = 1200 Number of elements = 6309 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4975 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8499 Number of elements = 47040 Number of triangles = 6258 Number of quadrilatarals = 0 Number of tetrahedrals = 40782 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8631 Number of elements = 47484 Number of triangles = 6702 Number of quadrilatarals = 0 Number of tetrahedrals = 40782 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 7444 Number of elements = 41254 Number of triangles = 5370 Number of quadrilatarals = 0 Number of tetrahedrals = 35884 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1187 Number of elements = 6230 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4898 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9625 Number of elements = 53328 Number of triangles = 7146 Number of quadrilatarals = 0 Number of tetrahedrals = 46182 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9899 Number of elements = 54216 Number of triangles = 8034 Number of quadrilatarals = 0 Number of tetrahedrals = 46182 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7485 Number of elements = 41497 Number of triangles = 5370 Number of quadrilatarals = 0 Number of tetrahedrals = 36127 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1212 Number of elements = 6385 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5053 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1202 Number of elements = 6334 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5002 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9302 Number of elements = 51451 Number of triangles = 6968 Number of quadrilatarals = 0 Number of tetrahedrals = 44483 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9522 Number of elements = 52179 Number of triangles = 7696 Number of quadrilatarals = 0 Number of tetrahedrals = 44483 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7466 Number of elements = 41416 Number of triangles = 5368 Number of quadrilatarals = 0 Number of tetrahedrals = 36048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1187 Number of elements = 6230 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4898 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 869 Number of elements = 4533 Number of triangles = 996 Number of quadrilatarals = 0 Number of tetrahedrals = 3537 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8956 Number of elements = 49469 Number of triangles = 6784 Number of quadrilatarals = 0 Number of tetrahedrals = 42685 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9139 Number of elements = 50065 Number of triangles = 7380 Number of quadrilatarals = 0 Number of tetrahedrals = 42685 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7430 Number of elements = 41197 Number of triangles = 5360 Number of quadrilatarals = 0 Number of tetrahedrals = 35837 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1187 Number of elements = 6230 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4898 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 522 Number of elements = 2638 Number of triangles = 688 Number of quadrilatarals = 0 Number of tetrahedrals = 1950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8638 Number of elements = 47663 Number of triangles = 6598 Number of quadrilatarals = 0 Number of tetrahedrals = 41065 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8777 Number of elements = 48099 Number of triangles = 7034 Number of quadrilatarals = 0 Number of tetrahedrals = 41065 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7402 Number of elements = 41032 Number of triangles = 5352 Number of quadrilatarals = 0 Number of tetrahedrals = 35680 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 848 Number of elements = 4402 Number of triangles = 994 Number of quadrilatarals = 0 Number of tetrahedrals = 3408 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 527 Number of elements = 2665 Number of triangles = 688 Number of quadrilatarals = 0 Number of tetrahedrals = 1977 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9771 Number of elements = 54406 Number of triangles = 6748 Number of quadrilatarals = 0 Number of tetrahedrals = 47658 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10261 Number of elements = 56170 Number of triangles = 8512 Number of quadrilatarals = 0 Number of tetrahedrals = 47658 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7355 Number of elements = 40784 Number of triangles = 5334 Number of quadrilatarals = 0 Number of tetrahedrals = 35450 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 2663 Number of elements = 14238 Number of triangles = 2794 Number of quadrilatarals = 0 Number of tetrahedrals = 11444 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 243 Number of elements = 1148 Number of triangles = 384 Number of quadrilatarals = 0 Number of tetrahedrals = 764 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1498 Number of elements = 7735 Number of triangles = 1986 Number of quadrilatarals = 0 Number of tetrahedrals = 5749 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1562 Number of elements = 7859 Number of triangles = 2110 Number of quadrilatarals = 0 Number of tetrahedrals = 5749 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1156 Number of elements = 6055 Number of triangles = 1306 Number of quadrilatarals = 0 Number of tetrahedrals = 4749 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 362 Number of elements = 1644 Number of triangles = 720 Number of quadrilatarals = 0 Number of tetrahedrals = 924 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 44 Number of elements = 160 Number of triangles = 84 Number of quadrilatarals = 0 Number of tetrahedrals = 76 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5096 Number of elements = 27903 Number of triangles = 4076 Number of quadrilatarals = 0 Number of tetrahedrals = 23827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5242 Number of elements = 28455 Number of triangles = 4628 Number of quadrilatarals = 0 Number of tetrahedrals = 23827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 4905 Number of elements = 26939 Number of triangles = 4044 Number of quadrilatarals = 0 Number of tetrahedrals = 22895 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 337 Number of elements = 1516 Number of triangles = 584 Number of quadrilatarals = 0 Number of tetrahedrals = 932 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 33115 Number of elements = 191815 Number of triangles = 8476 Number of quadrilatarals = 0 Number of tetrahedrals = 183339 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 36459 Number of elements = 205159 Number of triangles = 21820 Number of quadrilatarals = 0 Number of tetrahedrals = 183339 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 28820 Number of elements = 163772 Number of triangles = 15148 Number of quadrilatarals = 0 Number of tetrahedrals = 148624 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1416 Number of elements = 7524 Number of triangles = 1456 Number of quadrilatarals = 0 Number of tetrahedrals = 6068 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 4240 Number of elements = 23511 Number of triangles = 2950 Number of quadrilatarals = 0 Number of tetrahedrals = 20561 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 720 Number of elements = 3724 Number of triangles = 842 Number of quadrilatarals = 0 Number of tetrahedrals = 2882 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1263 Number of elements = 6628 Number of triangles = 1424 Number of quadrilatarals = 0 Number of tetrahedrals = 5204 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 16667 Number of elements = 94472 Number of triangles = 8798 Number of quadrilatarals = 0 Number of tetrahedrals = 85674 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 18591 Number of elements = 101848 Number of triangles = 16174 Number of quadrilatarals = 0 Number of tetrahedrals = 85674 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 12023 Number of elements = 67478 Number of triangles = 7138 Number of quadrilatarals = 0 Number of tetrahedrals = 60340 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 6568 Number of elements = 34370 Number of triangles = 9036 Number of quadrilatarals = 0 Number of tetrahedrals = 25334 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 20469 Number of elements = 118417 Number of triangles = 5446 Number of quadrilatarals = 0 Number of tetrahedrals = 112971 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 19887 Number of elements = 115064 Number of triangles = 5256 Number of quadrilatarals = 0 Number of tetrahedrals = 109808 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 20469 Number of elements = 118417 Number of triangles = 5446 Number of quadrilatarals = 0 Number of tetrahedrals = 112971 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 19887 Number of elements = 115064 Number of triangles = 5256 Number of quadrilatarals = 0 Number of tetrahedrals = 109808 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 20469 Number of elements = 118417 Number of triangles = 5446 Number of quadrilatarals = 0 Number of tetrahedrals = 112971 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 19887 Number of elements = 115064 Number of triangles = 5256 Number of quadrilatarals = 0 Number of tetrahedrals = 109808 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_quad (test_aflr3.TestAFLR3.test_quad) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 28277 Number of elements = 127463 Number of triangles = 410 Number of quadrilatarals = 3218 Number of tetrahedrals = 116651 Number of pyramids = 0 Number of prisms = 748 Number of hexahedrals = 6436 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22593 Number of elements = 131265 Number of triangles = 5542 Number of quadrilatarals = 0 Number of tetrahedrals = 125723 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 17015 Number of elements = 97698 Number of triangles = 5384 Number of quadrilatarals = 0 Number of tetrahedrals = 92314 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4972 Number of elements = 27531 Number of triangles = 3460 Number of quadrilatarals = 0 Number of tetrahedrals = 24071 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6395 Number of elements = 35692 Number of triangles = 4048 Number of quadrilatarals = 0 Number of tetrahedrals = 31644 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 43250 Number of elements = 250033 Number of triangles = 11826 Number of quadrilatarals = 0 Number of tetrahedrals = 238207 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 47245 Number of elements = 273764 Number of triangles = 11696 Number of quadrilatarals = 0 Number of tetrahedrals = 262068 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 43250 Number of elements = 249903 Number of triangles = 11696 Number of quadrilatarals = 0 Number of tetrahedrals = 238207 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 test_Edge_scaleFactor (test_aflr4.TestAFLR4.test_Edge_scaleFactor) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - trailingEdge Done getting mesh sizing parameters ok test_Face_scaleFactor (test_aflr4.TestAFLR4.test_Face_scaleFactor) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - leftWing Done getting mesh sizing parameters ok test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_erw (test_aflr4.TestAFLR4.test_erw) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - leftWing Done getting mesh sizing parameters ok test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_ff_cdfr (test_aflr4.TestAFLR4.test_ff_cdfr) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 ok test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 ok test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) ok test_max_min_scale (test_aflr4.TestAFLR4.test_max_min_scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 ok test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_proximity (test_aflr4.TestAFLR4.test_proximity) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wing1 Mesh sizing name - Wing2 Done getting mesh sizing parameters AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wing1 Mesh sizing name - Wing2 Done getting mesh sizing parameters ok test_quad (test_aflr4.TestAFLR4.test_quad) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_regions (test_aflr4.TestAFLR4.test_regions) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = cut, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: box 2: cut Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_aflr4.TestAFLR4.test_setInput) ... ok test_skin (test_aflr4.TestAFLR4.test_skin) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Ribs 2: Skin 3: Spar1 4: Rib_Root 5: Spar2 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Rib_Root, index = 1 Name = Skin, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 46 Number of elements = 44 Number of triangle elements = 0 Number of quadrilateral elements = 44 ---------------------------- Total number of nodes = 47 Total number of elements = 44 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 46 Number of elements = 44 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 44 Combining multiple FEA meshes! Combined Number of nodal coordinates = 47 Combined Number of elements = 45 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 44 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 3 Surface 2: Number of points found for aero-spline = 6 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 8 automatic connections were made for capsConnect Rib_Root (node id 1) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Done running Astros! ok test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG ok test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp ok test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp ok test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. ok test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 ok test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing ok test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. ok test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - VTail1 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - VTail2 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - VTail1 (ID = 0) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - VTail2 (ID = 1) Section 1 of 2 (ID = 0) Section 2 of 2 (ID = 1) Writing surface - Wing (ID = 2) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 ok test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Rudder not found in controls tuple! Only defaults will be used. Warning: Control Rudder not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Control surface 1 of 1 Section 2 of 3 (ID = 1) Control surface 1 of 1 Section 3 of 3 (ID = 0) Control surface 1 of 1 Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 ok test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice control surface data VLM control surface name - Elevator VLM control surface name - LeftAileron VLM control surface name - RightAileron VLM control surface name - Rudder Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Control surface 1 of 1 Section 2 of 3 (ID = 1) Control surface 1 of 1 Section 3 of 3 (ID = 0) Control surface 1 of 1 Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 ok test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 28.284271 -nDiv 9 -maxR 7 -mesh2d > autoInputs.out Executing: ./aero.csh > aero.out ok test_outputs (test_cart3d.TestCart3D.test_outputs) ... ok test_reenter (test_cart3d.TestCart3D.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Getting CFD functional....... Number of design variables - 1 Objective name - Drag Done getting CFD functional Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out Executing: ./aero.csh > aero.out Executing: ./aero.csh > aero.out Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.307131 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out Executing: ./aero.csh > aero.out ok test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - Mach Done getting CFD design variables Getting CFD functional....... Number of design variables - 3 Objective name - C_A Objective name - C_N Objective name - C_Y Done getting CFD functional Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:12) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:13) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:14) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:16) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:04:16) Linearizing cut-cells (00:04:16) ... done o Number of simultaneous xsensit jobs: 1 (00:04:16) Computing gradients (00:04:24) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:25) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:26) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 3 Objective name - C_D Objective name - C_L Objective name - C_S Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:26) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:28) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:28) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:30) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:04:30) Linearizing cut-cells (00:04:30) ... done o Number of simultaneous xsensit jobs: 1 (00:04:30) Computing gradients (00:04:39) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:39) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:40) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_l Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:41) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:42) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:43) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:43) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:04:44) Linearizing cut-cells (00:04:44) ... done o Number of simultaneous xsensit jobs: 1 (00:04:44) Computing gradients (00:04:48) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:48) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:49) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_m Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:50) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:51) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:52) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:53) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:04:53) Linearizing cut-cells (00:04:53) ... done o Number of simultaneous xsensit jobs: 1 (00:04:53) Computing gradients (00:04:57) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:57) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:04:59) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_n Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:04:59) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:00) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:01) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:02) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:05:02) Linearizing cut-cells (00:05:02) ... done o Number of simultaneous xsensit jobs: 1 (00:05:02) Computing gradients (00:05:06) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:06) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:08) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_M_x Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:08) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:09) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:11) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:05:11) Linearizing cut-cells (00:05:11) ... done o Number of simultaneous xsensit jobs: 1 (00:05:11) Computing gradients (00:05:15) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:16) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:17) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_M_y Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:17) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:19) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:19) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:20) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:05:21) Linearizing cut-cells (00:05:21) ... done o Number of simultaneous xsensit jobs: 1 (00:05:21) Computing gradients (00:05:25) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:25) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:27) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_M_z Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:27) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:28) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:29) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:30) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:05:30) Linearizing cut-cells (00:05:30) ... done o Number of simultaneous xsensit jobs: 1 (00:05:30) Computing gradients (00:05:34) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:36) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) ok test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Getting CFD design variables....... Number of design variables - 2 Design Variable name - Mach Design Variable name - area Done getting CFD design variables Getting CFD functional....... Number of design variables - 3 Objective name - C_A Objective name - C_N Objective name - C_Y Done getting CFD functional Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:38) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:39) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:39) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:41) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 2 o Number of simultaneous cutter jobs: 2 (00:05:42) Linearizing cut-cells (00:05:44) ... done o Number of simultaneous xsensit jobs: 2 (00:05:44) Computing gradients Adjusted OMP_NUM_THREADS to 1 for xsensit (00:05:52) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:05:52) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:05:54) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) ok test_Output_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = riteWing, index = 1 Name = leftWing, index = 2 Name = trailingEdge, index = 3 Writing FAST file .... Finished writing FAST file Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 1F924CC00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1F924CC00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1739B7000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1739B7000 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 1739B7000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1739B7000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1F924CC00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1F924CC00 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 1F924CC00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1F924CC00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1739B7000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1739B7000 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 1739B7000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1739B7000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1F924CC00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1F924CC00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 ok test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) ok test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = nodeBody, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ok test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_egadsTess.TestEGADS.test_setInput) ... 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 = 6744 Number of elements = 13484 Number of triangle elements = 13484 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 4919 Number of elements = 9834 Number of triangle elements = 9834 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 193 Number of elements = 382 Number of triangle elements = 382 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 11856 Total number of elements = 23700 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 - 11856, elements - 23700 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.080149 Creating surface mesh ... Surface mesh seconds: 0.009966 Recovering boundaries... Boundary recovery seconds: 0.050642 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.015944 Recovering Delaunayness... Delaunay recovery seconds: 0.035534 Refining mesh... 15804 insertions, added 8282 points, 509703 tetrahedra in queue. 5262 insertions, added 1835 points, 519709 tetrahedra in queue. 7014 insertions, added 1702 points, 478782 tetrahedra in queue. 9350 insertions, added 1438 points, 305677 tetrahedra in queue. 12464 insertions, added 1266 points, 7034 tetrahedra in queue. 16614 insertions, added 1316 points, 8631 tetrahedra in queue. Refinement seconds: 3.89584 Smoothing vertices... Mesh smoothing seconds: 0.883744 Improving mesh... Mesh improvement seconds: 0.022284 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.003849 Total running seconds: 4.99819 Statistics: Input points: 11856 Input facets: 23700 Input segments: 35550 Input holes: 2 Input regions: 0 Mesh points: 28176 Mesh tetrahedra: 136458 Mesh faces: 284766 Mesh faces on exterior boundary: 23700 Mesh faces on input facets: 23700 Mesh edges on input segments: 35550 Steiner points inside domain: 16320 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 = 6744 Number of elements = 13484 Number of triangle elements = 13484 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 4919 Number of elements = 9834 Number of triangle elements = 9834 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 193 Number of elements = 382 Number of triangle elements = 382 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 11856 Total number of elements = 23700 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 - 11856, elements - 23700 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.080074 Creating surface mesh ... Surface mesh seconds: 0.010686 Recovering boundaries... Boundary recovery seconds: 0.05502 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.016588 Recovering Delaunayness... Delaunay recovery seconds: 0.028665 Refining mesh... 15804 insertions, added 8282 points, 509703 tetrahedra in queue. 5262 insertions, added 1835 points, 519709 tetrahedra in queue. 7014 insertions, added 1702 points, 478782 tetrahedra in queue. 9350 insertions, added 1438 points, 305677 tetrahedra in queue. 12464 insertions, added 1266 points, 7034 tetrahedra in queue. 16614 insertions, added 1316 points, 8631 tetrahedra in queue. Refinement seconds: 3.81919 Smoothing vertices... Mesh smoothing seconds: 0.889458 Improving mesh... Mesh improvement seconds: 0.026783 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.005086 Total running seconds: 4.9317 Statistics: Input points: 11856 Input facets: 23700 Input segments: 35550 Input holes: 2 Input regions: 0 Mesh points: 28176 Mesh tetrahedra: 136458 Mesh faces: 284766 Mesh faces on exterior boundary: 23700 Mesh faces on input facets: 23700 Mesh edges on input segments: 35550 Steiner points inside domain: 16320 Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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) /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 - 1205, elements - 2398 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 - 1205, elements - 2398 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 - 11856, elements - 23700 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. ok test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - box2 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ok test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4048 Number of elements = 8092 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8092 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6217 Combined Number of elements = 12425 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12424 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 3908 Number of elements = 7812 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7812 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6077 Combined Number of elements = 12145 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12144 Combined Elemental Quad4 = 0 Updating mesh element types based on properties input EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4048 Number of elements = 8092 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8092 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6217 Combined Number of elements = 12425 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12424 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4048 Number of elements = 8092 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8092 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6217 Combined Number of elements = 12425 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12424 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 3908 Number of elements = 7812 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7812 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6077 Combined Number of elements = 12145 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12144 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 3908 Number of elements = 7812 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7812 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6077 Combined Number of elements = 12145 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12144 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input ok test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ok test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ... Getting CFD design variables....... Number of design variables - 4 Design Variable name - alowervar Design Variable name - auppervar Design Variable name - classvar Design Variable name - ztailvar Done getting CFD design variables CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 ok test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - avar Done getting CFD design variables CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 ok test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables ok test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ... Getting CFD design variables....... Number of design variables - 2 Design Variable name - camber Design Variable name - thick Done getting CFD design variables ok test_journal (test_mses.TestMSES_NACA.test_journal) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables ok test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable' test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable' test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable' test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable' test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable' test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable' test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable' test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable' test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable' test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable' EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 54 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 54 54 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 12 26 AFLR2 IG : Nodes, Faces = 24 50 AFLR2 IG : Nodes, Faces = 36 74 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 106 AFLR2 IG : Nodes, Faces = 53 108 AFLR2 IG : Nodes, Faces = 54 110 AFLR2 IG : Nodes, Faces = 58 110 AFLR2 IG : Nodes, Faces = 54 54 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 54 54 AFLR2 GG : Nodes, Faces = 100 146 AFLR2 GG : Nodes, Faces = 122 190 AFLR2 GG : Nodes, Faces = 138 222 AFLR2 GG : Nodes, Faces = 153 252 AFLR2 GG : Nodes, Faces = 168 282 AFLR2 GG : Nodes, Faces = 180 306 AFLR2 GG : Nodes, Faces = 192 330 AFLR2 GG : Nodes, Faces = 201 348 AFLR2 GG : Nodes, Faces = 210 366 AFLR2 GG : Nodes, Faces = 216 378 AFLR2 GG : Nodes, Faces = 221 388 AFLR2 GG : Nodes, Faces = 224 394 AFLR2 GG : Nodes, Faces = 225 396 AFLR2 : CPU Time = 0.000 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 225 396 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 225 Number of elements = 450 Number of tris = 396 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1612 Number of elements = 8825 Number of triangles = 1216 Number of quadrilatarals = 0 Number of tetrahedrals = 7609 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2600 Number of elements = 13872 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11114 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1039 Number of elements = 5509 Number of triangles = 998 Number of quadrilatarals = 0 Number of tetrahedrals = 4511 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 17015 Number of elements = 97698 Number of triangles = 5384 Number of quadrilatarals = 0 Number of tetrahedrals = 92314 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1612 Number of elements = 8825 Number of triangles = 1216 Number of quadrilatarals = 0 Number of tetrahedrals = 7609 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_inputs (test_refine.TestREFINE.test_inputs) ... ok test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 432 Number of elements = 2132 Number of triangles = 644 Number of quadrilatarals = 0 Number of tetrahedrals = 1488 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 ok test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 935 Number of elements = 5010 Number of triangles = 758 Number of quadrilatarals = 0 Number of tetrahedrals = 4252 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 3 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 8 Faces EGADS : Body 0 has 15 Edges EGADS : Body 0 has 8 Loops EGADS : Body 0 has 9 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 8 Faces EGADS : Body 1 has 15 Edges EGADS : Body 1 has 8 Loops EGADS : Body 1 has 9 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 2 Faces EGADS : Body 2 has 6 Edges EGADS : Body 2 has 2 Loops EGADS : Body 2 has 2 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 4 5 EGADS : 2 Yes 0 0 1 1 1 1 3 4 6 EGADS : 3 Yes 0 0 1 1 1 1 2 4 7 EGADS : 4 Yes 0 0 1 1 1 1 2 3 EGADS : 5 Yes 0 0 1 1 1 1 6 7 8 EGADS : 6 Yes 0 0 1 1 1 2 5 7 8 EGADS : 7 Yes 0 0 1 1 1 3 5 6 8 EGADS : 8 Yes 0 0 1 1 1 5 6 7 EGADS : 9 Yes 1 0 1 0 10 10 11 12 13 EGADS : 10 Yes 1 0 1 0 10 9 11 12 14 EGADS : 11 Yes 1 0 1 0 10 9 10 12 15 EGADS : 12 Yes 1 0 1 0 10 9 10 11 EGADS : 13 Yes 1 0 1 0 10 9 14 15 16 EGADS : 14 Yes 1 0 1 0 10 10 13 15 16 EGADS : 15 Yes 1 0 1 0 10 11 13 14 16 EGADS : 16 Yes 1 0 1 0 10 13 14 15 EGADS : 17 Yes 2 0 1 NA NA 18 EGADS : 18 Yes 2 0 1 NA NA 17 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 4 -3 -2 EGADS : 2 3 7 -6 -5 EGADS : 3 6 9 -1 -8 EGADS : 4 -4 -9 -7 EGADS : 5 -10 2 11 -12 EGADS : 6 -11 5 13 -14 EGADS : 7 -13 8 10 -15 EGADS : 8 12 14 15 EGADS : 9 16 19 -18 -17 EGADS : 10 18 22 -21 -20 EGADS : 11 21 24 -16 -23 EGADS : 12 -19 -24 -22 EGADS : 13 -25 17 26 -27 EGADS : 14 -26 20 28 -29 EGADS : 15 -28 23 25 -30 EGADS : 16 27 29 30 EGADS : 17 -31 -32 33 34 EGADS : 18 -35 -34 36 32 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 4 -3 -2 EGADS : 2 Yes 3 7 -6 -5 EGADS : 3 Yes 6 9 -1 -8 EGADS : 4 Yes -4 -9 -7 EGADS : 5 Yes -10 2 11 -12 EGADS : 6 Yes -11 5 13 -14 EGADS : 7 Yes -13 8 10 -15 EGADS : 8 Yes 12 14 15 EGADS : 9 Yes 16 19 -18 -17 EGADS : 10 Yes 18 22 -21 -20 EGADS : 11 Yes 21 24 -16 -23 EGADS : 12 Yes -19 -24 -22 EGADS : 13 Yes -25 17 26 -27 EGADS : 14 Yes -26 20 28 -29 EGADS : 15 Yes -28 23 25 -30 EGADS : 16 Yes 27 29 30 EGADS : 17 Yes -31 -32 33 34 EGADS : 18 Yes -35 -34 36 32 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 2 1 1 3 EGADS : 2 0 Yes 1 3 1 1 5 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 4 EGADS : 5 0 Yes 3 5 1 2 6 EGADS : 6 0 Yes 5 6 1 2 3 EGADS : 7 0 Yes 4 6 1 2 4 EGADS : 8 0 Yes 5 1 1 3 7 EGADS : 9 0 Yes 6 2 1 3 4 EGADS : 10 0 Yes 1 7 1 5 7 EGADS : 11 0 Yes 3 8 1 5 6 EGADS : 12 0 Yes 7 8 1 5 8 EGADS : 13 0 Yes 5 9 1 6 7 EGADS : 14 0 Yes 8 9 1 6 8 EGADS : 15 0 Yes 9 7 1 7 8 EGADS : 16 1 Yes 10 11 1 9 11 EGADS : 17 1 Yes 10 12 1 9 13 EGADS : 18 1 Yes 12 13 1 9 10 EGADS : 19 1 Yes 11 13 1 9 12 EGADS : 20 1 Yes 12 14 1 10 14 EGADS : 21 1 Yes 14 15 1 10 11 EGADS : 22 1 Yes 13 15 1 10 12 EGADS : 23 1 Yes 14 10 1 11 15 EGADS : 24 1 Yes 15 11 1 11 12 EGADS : 25 1 Yes 10 16 1 13 15 EGADS : 26 1 Yes 12 17 1 13 14 EGADS : 27 1 Yes 16 17 1 13 16 EGADS : 28 1 Yes 14 18 1 14 15 EGADS : 29 1 Yes 17 18 1 14 16 EGADS : 30 1 Yes 18 16 1 15 16 EGADS : 31 2 DEGEN 19 19 - 17 EGADS : 32 2 Yes 20 19 NA 17 18 EGADS : 33 2 DEGEN 20 20 - 17 EGADS : 34 2 Yes 20 19 NA 17 18 EGADS : 35 2 DEGEN 19 19 - 18 EGADS : 36 2 DEGEN 20 20 - 18 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 3.77246052 0 0.00459131419 EGADS : 2 Yes 5.90487498 7.07106781 0 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 4.0824829 7.07106781 0.123425948 EGADS : 5 Yes 3.77001182 0 0 EGADS : 6 Yes 5.90282524 7.07106781 0 EGADS : 7 Yes 5.90487498 0 0 EGADS : 8 Yes 4.0824829 0 0.123425948 EGADS : 9 Yes 5.90282524 0 0 EGADS : 10 Yes 15.2802204 0 0.00183652568 EGADS : 11 Yes 16.1331862 2.82842712 0 EGADS : 12 Yes 13.7712362 0 0 EGADS : 13 Yes 15.4042293 2.82842712 0.0493703791 EGADS : 14 Yes 15.2792409 0 0 EGADS : 15 Yes 16.1323663 2.82842712 0 EGADS : 16 Yes 16.1331862 0 0 EGADS : 17 Yes 15.4042293 0 0.0493703791 EGADS : 18 Yes 16.1323663 0 0 EGADS : 19 Yes 0 0 80 EGADS : 20 Yes 0 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 160 AFLR4 : Min Bounding Box Length = 160 AFLR4 : Max Ref Bounding Box Length = 16.1372 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 0.890888 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 14.7419 AFLR4 : Abs Min Surf Spacing = 0.00222722 AFLR4 : Min Surf Spacing = 0.00445444 AFLR4 : Max Surf Spacing = 0.0890888 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD AFLR4 : 2 CAD geometry 0 STD AFLR4 : 3 CAD geometry 0 STD AFLR4 : 4 CAD geometry 0 STD AFLR4 : 5 CAD geometry 0 STD AFLR4 : 6 CAD geometry 0 STD AFLR4 : 7 CAD geometry 0 STD AFLR4 : 8 CAD geometry 0 STD AFLR4 : 9 CAD geometry 0 STD AFLR4 : 10 CAD geometry 0 STD AFLR4 : 11 CAD geometry 0 STD AFLR4 : 12 CAD geometry 0 STD AFLR4 : 13 CAD geometry 0 STD AFLR4 : 14 CAD geometry 0 STD AFLR4 : 15 CAD geometry 0 STD AFLR4 : 16 CAD geometry 0 STD AFLR4 : 17 CAD geometry 0 FARFIELD AFLR4 : 18 CAD geometry 0 FARFIELD AFLR4 : Case has 2 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR43 : INPUT SURFACE MESH FROM TESS AFLR43 : Quad Surface Faces= 0 AFLR43 : Tria Surface Faces= 11696 AFLR43 : Nodes = 5854 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.50 AFLR3 : Version Date 10/31/23 @ 06:31PM AFLR3 : Compile OS Darwin 23.3.0 arm64 AFLR3 : Compile Date 02/08/24 @ 04:22PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 5854 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid UG3 : 5 Solid UG3 : 6 Solid UG3 : 7 Solid UG3 : 8 Solid UG3 : 9 Solid UG3 : 10 Solid UG3 : 11 Solid UG3 : 12 Solid UG3 : 13 Solid UG3 : 14 Solid UG3 : 15 Solid UG3 : 16 Solid UG3 : 17 FarField UG3 : 18 FarField AFLR3 : CPU Time = 0.007 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 5854 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1172 6979 AFLR3 IG : Nodes, Elements = 2344 15131 AFLR3 IG : Nodes, Elements = 3516 23433 AFLR3 IG : Nodes, Elements = 4688 31720 AFLR3 IG : Nodes, Elements = 5860 39973 AFLR3 IG : Nodes, Elements = 5861 39980 AFLR3 IG : Nodes, Elements = 5861 39927 AFLR3 IG : Nodes, Elements = 5861 39954 AFLR3 IG : Nodes, Elements = 5861 39923 AFLR3 IG : Nodes, Elements = 5854 23727 AFLR3 IG : Nodes, Elements = 5854 23747 AFLR3 IG : Nodes, Elements = 5854 19625 AFLR3 IG : Nodes, Elements = 5854 17542 AFLR3 : CPU Time = 0.078 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 5854 17542 AFLR3 GG : Nodes, Elements = 8536 25786 AFLR3 GG : Nodes, Elements = 8536 37041 AFLR3 GG : Nodes, Elements = 8536 34267 AFLR3 GG : Nodes, Elements = 8536 32820 AFLR3 GG : Nodes, Elements = 10830 40032 AFLR3 GG : Nodes, Elements = 10830 50075 AFLR3 GG : Nodes, Elements = 10830 47051 AFLR3 GG : Nodes, Elements = 10830 46109 AFLR3 GG : Nodes, Elements = 13376 54035 AFLR3 GG : Nodes, Elements = 13376 65160 AFLR3 GG : Nodes, Elements = 13376 61916 AFLR3 GG : Nodes, Elements = 13376 61125 AFLR3 GG : Nodes, Elements = 16078 69394 AFLR3 GG : Nodes, Elements = 16078 81231 AFLR3 GG : Nodes, Elements = 16078 77895 AFLR3 GG : Nodes, Elements = 16078 77138 AFLR3 GG : Nodes, Elements = 18865 85650 AFLR3 GG : Nodes, Elements = 18865 97785 AFLR3 GG : Nodes, Elements = 18865 94474 AFLR3 GG : Nodes, Elements = 18865 93705 AFLR3 GG : Nodes, Elements = 21890 102926 AFLR3 GG : Nodes, Elements = 21890 115968 AFLR3 GG : Nodes, Elements = 21890 112400 AFLR3 GG : Nodes, Elements = 21890 111643 AFLR3 GG : Nodes, Elements = 24980 121053 AFLR3 GG : Nodes, Elements = 24980 134344 AFLR3 GG : Nodes, Elements = 24980 130769 AFLR3 GG : Nodes, Elements = 24980 129945 AFLR3 GG : Nodes, Elements = 28259 139914 AFLR3 GG : Nodes, Elements = 28259 153879 AFLR3 GG : Nodes, Elements = 28259 150133 AFLR3 GG : Nodes, Elements = 28259 149371 AFLR3 GG : Nodes, Elements = 31552 159346 AFLR3 GG : Nodes, Elements = 31552 173336 AFLR3 GG : Nodes, Elements = 31552 169592 AFLR3 GG : Nodes, Elements = 31552 168861 AFLR3 GG : Nodes, Elements = 34922 179042 AFLR3 GG : Nodes, Elements = 34922 193256 AFLR3 GG : Nodes, Elements = 34922 189489 AFLR3 GG : Nodes, Elements = 34922 188777 AFLR3 GG : Nodes, Elements = 38260 198839 AFLR3 GG : Nodes, Elements = 38260 213010 AFLR3 GG : Nodes, Elements = 38260 209379 AFLR3 GG : Nodes, Elements = 38260 208666 AFLR3 GG : Nodes, Elements = 41613 218777 AFLR3 GG : Nodes, Elements = 41613 232830 AFLR3 GG : Nodes, Elements = 41613 229203 AFLR3 GG : Nodes, Elements = 41613 228546 AFLR3 GG : Nodes, Elements = 44853 238311 AFLR3 GG : Nodes, Elements = 44853 251961 AFLR3 GG : Nodes, Elements = 44853 248462 AFLR3 GG : Nodes, Elements = 44853 247841 AFLR3 GG : Nodes, Elements = 47944 257141 AFLR3 GG : Nodes, Elements = 47944 270223 AFLR3 GG : Nodes, Elements = 47944 266837 AFLR3 GG : Nodes, Elements = 47944 266221 AFLR3 GG : Nodes, Elements = 50866 275001 AFLR3 GG : Nodes, Elements = 50866 287403 AFLR3 GG : Nodes, Elements = 50866 284205 AFLR3 GG : Nodes, Elements = 50866 283637 AFLR3 GG : Nodes, Elements = 53688 292120 AFLR3 GG : Nodes, Elements = 53688 303954 AFLR3 GG : Nodes, Elements = 53688 300960 AFLR3 GG : Nodes, Elements = 53688 300453 AFLR3 GG : Nodes, Elements = 56252 308151 AFLR3 GG : Nodes, Elements = 56252 318979 AFLR3 GG : Nodes, Elements = 56252 316224 AFLR3 GG : Nodes, Elements = 56252 315822 AFLR3 GG : Nodes, Elements = 58659 323046 AFLR3 GG : Nodes, Elements = 58659 333156 AFLR3 GG : Nodes, Elements = 58659 330531 AFLR3 GG : Nodes, Elements = 58659 330168 AFLR3 GG : Nodes, Elements = 60799 336591 AFLR3 GG : Nodes, Elements = 60799 345691 AFLR3 GG : Nodes, Elements = 60799 343322 AFLR3 GG : Nodes, Elements = 60799 343001 AFLR3 GG : Nodes, Elements = 62679 348642 AFLR3 GG : Nodes, Elements = 62679 356496 AFLR3 GG : Nodes, Elements = 62679 354509 AFLR3 GG : Nodes, Elements = 62679 354263 AFLR3 GG : Nodes, Elements = 64243 358957 AFLR3 GG : Nodes, Elements = 64243 365517 AFLR3 GG : Nodes, Elements = 64243 363806 AFLR3 GG : Nodes, Elements = 64243 363612 AFLR3 GG : Nodes, Elements = 65573 367606 AFLR3 GG : Nodes, Elements = 65573 373144 AFLR3 GG : Nodes, Elements = 65573 371736 AFLR3 GG : Nodes, Elements = 65573 371580 AFLR3 GG : Nodes, Elements = 66592 374638 AFLR3 GG : Nodes, Elements = 66592 378925 AFLR3 GG : Nodes, Elements = 66592 377763 AFLR3 GG : Nodes, Elements = 66592 377669 AFLR3 GG : Nodes, Elements = 67321 379857 AFLR3 GG : Nodes, Elements = 67321 382993 AFLR3 GG : Nodes, Elements = 67321 382093 AFLR3 GG : Nodes, Elements = 67321 382021 AFLR3 GG : Nodes, Elements = 67827 383540 AFLR3 GG : Nodes, Elements = 67827 385769 AFLR3 GG : Nodes, Elements = 67827 385075 AFLR3 GG : Nodes, Elements = 67827 385031 AFLR3 GG : Nodes, Elements = 68120 385911 AFLR3 GG : Nodes, Elements = 68120 387126 AFLR3 GG : Nodes, Elements = 68120 386804 AFLR3 GG : Nodes, Elements = 68120 386779 AFLR3 GG : Nodes, Elements = 68302 387326 AFLR3 GG : Nodes, Elements = 68302 388056 AFLR3 GG : Nodes, Elements = 68302 387856 AFLR3 GG : Nodes, Elements = 68302 387848 AFLR3 GG : Nodes, Elements = 68376 388070 AFLR3 GG : Nodes, Elements = 68376 388381 AFLR3 GG : Nodes, Elements = 68376 388292 AFLR3 GG : Nodes, Elements = 68376 388290 AFLR3 GG : Nodes, Elements = 68408 388386 AFLR3 GG : Nodes, Elements = 68408 388517 AFLR3 GG : Nodes, Elements = 68408 388474 AFLR3 GG : Nodes, Elements = 68417 388501 AFLR3 GG : Nodes, Elements = 68417 388543 AFLR3 GG : Nodes, Elements = 68417 388528 AFLR3 GG : Nodes, Elements = 68417 388527 AFLR3 GG : Nodes, Elements = 68422 388542 AFLR3 GG : Nodes, Elements = 68422 388567 AFLR3 GG : Nodes, Elements = 68422 388557 AFLR3 GG : Nodes, Elements = 68422 388558 AFLR3 GG : Nodes, Elements = 68424 388564 AFLR3 GG : Nodes, Elements = 68424 388573 AFLR3 GG : Nodes, Elements = 68424 388569 AFLR3 GG : Nodes, Elements = 68441 388620 AFLR3 GG : Nodes, Elements = 68441 388680 AFLR3 GG : Nodes, Elements = 68441 388660 AFLR3 GG : Nodes, Elements = 68441 388661 AFLR3 GG : Nodes, Elements = 68444 388670 AFLR3 GG : Nodes, Elements = 68444 388682 AFLR3 GG : Nodes, Elements = 68444 388678 AFLR3 GG : Nodes, Elements = 68445 388681 AFLR3 GG : Nodes, Elements = 68445 388683 AFLR3 GG : Nodes, Elements = 68445 388682 AFLR3 GG : Nodes, Elements = 68445 388681 AFLR3 : CPU Time = 2.390 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 68445 388681 AFLR3 QI : Nodes, Elements = 67054 380776 AFLR3 QI : Nodes, Elements = 66819 379453 AFLR3 QI : Nodes, Elements = 66795 379315 AFLR3 QI : Nodes, Elements = 66793 379303 AFLR3 QI : Nodes, Elements = 66793 382971 AFLR3 QI : Nodes, Elements = 66793 379109 AFLR3 QI : Nodes, Elements = 66793 378682 AFLR3 QI : Nodes, Elements = 66793 379082 AFLR3 QI : Nodes, Elements = 66793 378439 AFLR3 QI : Nodes, Elements = 66793 378244 AFLR3 QI : Nodes, Elements = 66793 378540 AFLR3 QI : Nodes, Elements = 66793 378214 AFLR3 QI : Nodes, Elements = 66793 378129 AFLR3 QI : Nodes, Elements = 66793 378403 AFLR3 QI : Nodes, Elements = 66793 378131 AFLR3 QI : Nodes, Elements = 66793 378081 AFLR3 QI : Nodes, Elements = 66793 378344 AFLR3 QI : Nodes, Elements = 66793 378087 AFLR3 QI : Nodes, Elements = 66793 378043 AFLR3 QI : Nodes, Elements = 66796 378056 AFLR3 QI : Nodes, Elements = 66796 378318 AFLR3 QI : Nodes, Elements = 66796 378073 AFLR3 QI : Nodes, Elements = 66796 378055 AFLR3 QI : Nodes, Elements = 66796 378331 AFLR3 QI : Nodes, Elements = 66796 378067 AFLR3 QI : Nodes, Elements = 66796 378027 AFLR3 QI : Nodes, Elements = 66796 378055 AFLR3 : CPU Time = 0.798 seconds AFLR3 QRG: QUALITY GRID RE-GENERATION AFLR3 QRG: Nodes, Elements = 66796 378055 AFLR3 QRG: Nodes, Elements = 66802 378089 AFLR3 QRG: Nodes, Elements = 66806 378118 AFLR3 QRG: Nodes, Elements = 66810 378136 AFLR3 QRG: Nodes, Elements = 66813 378151 AFLR3 QRG: Nodes, Elements = 66814 378157 AFLR3 : CPU Time = 0.031 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 378157 UG3 : Min, Max Ang = 0.9306 176.4 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 150 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 378157 UG3 : Min Vol = 6.65e-10 UG3 : Average Vol = 5.61 UG3 : Total-Tet-Vol = 2.12e+06 UG3 : No. Vol160.0 = 150 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 378157 UG3 : Min Vol = 6.65e-10 UG3 : Average Vol = 5.61 UG3 : Total-Tet-Vol = 2.12e+06 UG3 : No. Vol Edge #9 (9) Internally in Loop 4 7, sen = -1! 1F924CC00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1739B7000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1F924CC00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 7 (of 7) Body 1 (of 7) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 2 (of 7) Number of nodes = 298 Number of elements = 592 Number of triangle elements = 592 Number of quadrilateral elements = 0 Body 3 (of 7) Number of nodes = 488 Number of elements = 972 Number of triangle elements = 972 Number of quadrilateral elements = 0 Body 4 (of 7) Number of nodes = 2048 Number of elements = 4096 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 7) Number of nodes = 152 Number of elements = 300 Number of triangle elements = 300 Number of quadrilateral elements = 0 Body 6 (of 7) Number of nodes = 624 Number of elements = 1248 Number of triangle elements = 1248 Number of quadrilateral elements = 0 Body 7 (of 7) Number of nodes = 489 Number of elements = 974 Number of triangle elements = 974 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4197 Total number of elements = 8374 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 298, elements - 592 Body 3 number of surface: nodes - 488, elements - 972 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 489, elements - 974 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 298, elements - 592 Body 3 number of surface: nodes - 488, elements - 972 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 489, elements - 974 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Number of surface: nodes - 4197, elements - 8374 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 374 Number of elements = 744 Number of triangle elements = 744 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 472 Total number of elements = 936 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 374, elements - 744 Body 2 number of surface: nodes - 98, elements - 192 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 374, elements - 744 Body 2 number of surface: nodes - 98, elements - 192 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 386 Number of elements = 768 Number of triangle elements = 768 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 582 Total number of elements = 1152 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 386, elements - 768 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 98, elements - 192 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 386, elements - 768 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 98, elements - 192 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 351 Number of elements = 698 Number of triangle elements = 698 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 491 Total number of elements = 970 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 351, elements - 698 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 351, elements - 698 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 376 Number of elements = 748 Number of triangle elements = 748 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 516 Total number of elements = 1020 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 376, elements - 748 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 376, elements - 748 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 370 Number of elements = 736 Number of triangle elements = 736 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 454 Total number of elements = 896 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 42, elements - 80 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 42, elements - 80 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 370 Number of elements = 736 Number of triangle elements = 736 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 126 Number of elements = 252 Number of triangle elements = 252 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 516 Total number of elements = 1024 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 126, elements - 252 Body 3 number of surface: nodes - 20, elements - 36 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 126, elements - 252 Body 3 number of surface: nodes - 20, elements - 36 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 109 Number of elements = 214 Number of triangle elements = 214 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 48 Number of elements = 96 Number of triangle elements = 96 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 12 Number of elements = 20 Number of triangle elements = 20 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 169 Total number of elements = 330 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 109, elements - 214 Body 2 number of surface: nodes - 48, elements - 96 Body 3 number of surface: nodes - 12, elements - 20 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 109, elements - 214 Body 2 number of surface: nodes - 48, elements - 96 Body 3 number of surface: nodes - 12, elements - 20 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 536 Number of elements = 1072 Number of triangle elements = 1072 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 544 Number of elements = 1084 Number of triangle elements = 1084 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1080 Total number of elements = 2156 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 536, elements - 1072 Body 2 number of surface: nodes - 544, elements - 1084 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 536, elements - 1072 Body 2 number of surface: nodes - 544, elements - 1084 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 5) Getting surface mesh for body 2 (of 5) Getting surface mesh for body 3 (of 5) Getting surface mesh for body 4 (of 5) Getting surface mesh for body 5 (of 5) Body 1 (of 5) Number of nodes = 1351 Number of elements = 2682 Number of triangle elements = 2682 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 288 Number of elements = 572 Number of triangle elements = 572 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 173 Number of elements = 342 Number of triangle elements = 342 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 26 Number of elements = 48 Number of triangle elements = 48 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 482 Number of elements = 960 Number of triangle elements = 960 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2320 Total number of elements = 4604 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 1351, elements - 2682 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 173, elements - 342 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 1351, elements - 2682 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 173, elements - 342 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 443 Number of elements = 882 Number of triangle elements = 882 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 522 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 965 Total number of elements = 1926 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 443, elements - 882 Body 2 number of surface: nodes - 522, elements - 1044 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 443, elements - 882 Body 2 number of surface: nodes - 522, elements - 1044 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7151, elements - 14294 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 - 7151, elements - 14294 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7151, elements - 14294 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7151, elements - 14294 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7151, elements - 14294 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 5882, elements - 11756 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = trailingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 7151 Number of elements = 14294 Number of triangle elements = 14294 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 7151 Total number of elements = 14294 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7151, elements - 14294 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7151, elements - 14294 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_tetgen.TestTETGEN.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok test_Cl (test_xfoil.Testxfoil_Parsec.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_Parsec.test_alpha_custom_increment) ... ok test_Output (test_zaero.TestZAERO.test_Output) ... ok test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1220 Number of elements = 2680 Number of triangle elements = 2680 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1221 Total number of elements = 2680 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1220 Number of elements = 2680 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 2680 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 1221 Combined Number of elements = 2681 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 2680 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 6 Property name - Rib_Root Property name - Rib_Root_Point Property name - Ribs Property name - Skin Property name - Spar1 Property name - Spar2 Done getting FEA properties Updating mesh element types based on properties input 'Smart_Restart' is ON Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting vortex lattice control surface data VLM control surface name - CntrlLE VLM control surface name - CntrlTE Done getting vortex lattice control surface data Getting FEA vortex lattice mesh Getting ZAERO UAIC Configurations....... Number of UAIC Configurations - 2 UAIC Configuration: climb, id = 1 - Mach Number : 0.200000 - Reduced Freq: [0.020000, ... , 0.250000] UAIC Configuration: cruise, id = 2 - Mach Number : 0.700000 - Reduced Freq: [0.040000, ... , 0.350000] Getting ZAERO Analysis Subcases....... Number of Analysis Subcases - 2 Analysis Subcase: FlutterCruise, id = 1 - Discipline : flutter - UAIC : cruise Analysis Subcase: Trim, id = 2 - Discipline : Trim - UAIC : climb Getting ZAERO Trim Variables....... Number of Trim Variables - 2 Trim Variable: ANGLEA - Label : ALPHA - Value : free Trim Variable: URDD3 - Label : NZ - Value : 1.0 Updating StaticAeroelastic subcase: Trim - vectorToCG -> [0.345898, 1.652951, -0.041403] - weight -> 476456.149985 - weightMomentOfInertia -> [304902.643270, 98963.803823, 69822.813293, 6179.981375, 19723.152208, 370546.335525] ok ---------------------------------------------------------------------- Ran 154 tests in 521.325s OK (skipped=10) + cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest + ./execute_CTestRegression.sh No options provided...defaulting to ALL Running.... MINIMAL c-Tests Running.... LINEARAERO c-Tests ================================================= + echo './avlTest test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt ./avlTest test; + ./avlTest 0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt Attention: avlTest is hard coded to look for ../csmData/avlWingTail.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice control surface data VLM control surface name - WingRightLE VLM control surface name - WingRightTE VLM control surface name - Tail Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Writing surface - Vertical_Tail (ID = 1) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Running AVL! Value of Cltot = 0.619913 StripForces Wing = {"Xle":[1.565221892029e+00,1.512117367810e+00,1.409527304938e+00,1.264443046659e+00,1.086751845411e+00,8.885630629098e-01,6.833829371601e-01,4.851941546545e-01,3.075029533974e-01,1.624186951053e-01,5.982863221714e-02,6.724107980270e-03,6.724107971058e-03,5.982863219013e-02,1.624186950623e-01,3.075029533414e-01,4.851941545893e-01,6.833829370902e-01,8.885630628399e-01,1.086751845346e+00,1.264443046603e+00,1.409527304895e+00,1.512117367783e+00,1.565221892020e+00],"Yle":[-3.856416046770e+00,-3.725576361740e+00,-3.472813499993e+00,-3.115352832843e+00,-2.677554714026e+00,-2.189254361841e+00,-1.683728638332e+00,-1.195428286135e+00,-7.576301672945e-01,-4.001695001132e-01,-1.474066383261e-01,-1.656695325269e-02,1.656695322999e-02,1.474066382596e-01,4.001695000074e-01,7.576301671565e-01,1.195428285974e+00,1.683728638159e+00,2.189254361668e+00,2.677554713865e+00,3.115352832706e+00,3.472813499887e+00,3.725576361674e+00,3.856416046747e+00],"Zle":[2.486597711706e-01,2.402232939480e-01,2.239252714835e-01,2.008763870743e-01,1.726473841027e-01,1.411620224705e-01,1.085659775407e-01,7.708061590764e-02,4.885161293456e-02,2.580272852328e-02,9.504706056265e-03,1.068228830823e-03,1.068228829360e-03,9.504706051974e-03,2.580272851645e-02,4.885161292566e-02,7.708061589728e-02,1.085659775295e-01,1.411620224593e-01,1.726473840924e-01,2.008763870654e-01,2.239252714767e-01,2.402232939437e-01,2.486597711692e-01],"Chord":[9.710071581587e-01,9.928137666999e-01,1.034940899447e+00,1.094517661923e+00,1.167483996219e+00,1.248867367237e+00,1.333121632734e+00,1.414505003754e+00,1.487471338054e+00,1.547048100535e+00,1.589175233289e+00,1.610981841837e+00,1.610981841841e+00,1.589175233300e+00,1.547048100553e+00,1.487471338077e+00,1.414505003781e+00,1.333121632763e+00,1.248867367266e+00,1.167483996246e+00,1.094517661946e+00,1.034940899465e+00,9.928137667110e-01,9.710071581625e-01],"Area":[6.420432739224e-02,1.924649501823e-01,3.191588402418e-01,4.398794051499e-01,5.463997379092e-01,6.272332670617e-01,6.695492724342e-01,6.620092145623e-01,5.978048871833e-01,4.770843222898e-01,3.080744268775e-01,1.065203328294e-01,1.065203327570e-01,3.080744268129e-01,4.770843222394e-01,5.978048871514e-01,6.620092145502e-01,6.695492724407e-01,6.272332670835e-01,5.463997379421e-01,4.398794051895e-01,3.191588402846e-01,1.924649502262e-01,6.420432743628e-02],"c_cl":[1.751976980130e-01,4.816388142977e-01,7.134545983421e-01,8.955798774849e-01,1.045275116632e+00,1.165642609065e+00,1.251488483105e+00,1.294909342036e+00,1.290147495293e+00,1.237589733954e+00,1.147354354589e+00,1.069716379937e+00,1.027204841579e+00,9.123069911134e-01,8.271224835183e-01,7.465072383823e-01,6.622506856520e-01,5.718077594714e-01,4.773770050899e-01,3.839108464450e-01,2.965810831876e-01,2.166269422077e-01,1.372747954615e-01,4.847522879848e-02],"ai":[2.423376448059e-01,1.891573605669e-01,1.387726073609e-01,1.136377561110e-01,1.056109957987e-01,1.077519869781e-01,1.163918473303e-01,1.297918603655e-01,1.465983278745e-01,1.624995174599e-01,1.707158095744e-01,1.656351191924e-01,-7.833998870070e-02,-4.190817556553e-02,-1.699095118257e-02,-7.589503463777e-04,7.958849673277e-03,1.019416065188e-02,8.688915578617e-03,6.053380335312e-03,5.120395026966e-03,9.296755297777e-03,2.004804046056e-02,3.330492577563e-02],"cl_norm":[2.044051829731e-01,5.494672225940e-01,7.808579037666e-01,9.268407130704e-01,1.014078158135e+00,1.057019341175e+00,1.062951411331e+00,1.036333388587e+00,9.816462634652e-01,9.051794884118e-01,8.167547094730e-01,7.499676468296e-01,7.211772113978e-01,6.503467495436e-01,6.057660560785e-01,5.686988847404e-01,5.305932247981e-01,4.861412346267e-01,4.332732553833e-01,3.727603475166e-01,3.071901673655e-01,2.373206031154e-01,1.568074209165e-01,5.666485024183e-02],"cl":[1.803741931755e-01,4.848688546456e-01,6.890559834541e-01,8.178762563193e-01,8.948575908400e-01,9.327503738518e-01,9.379850374383e-01,9.144963748396e-01,8.662385668547e-01,7.987616435479e-01,7.207325646086e-01,6.617973538491e-01,6.363916792637e-01,5.738884333901e-01,5.345488897542e-01,5.018395375442e-01,4.682137871228e-01,4.289878157184e-01,3.823352848865e-01,3.289366049978e-01,2.710752133780e-01,2.094198967377e-01,1.383722840114e-01,5.000302093674e-02],"cd":[4.708816796009e-03,1.893013552459e-02,2.388458719214e-02,2.809788812558e-02,3.450496926229e-02,4.310977683932e-02,5.296690620746e-02,6.273588035903e-02,7.092746653689e-02,7.623132904844e-02,7.793919402367e-02,1.330641046360e-01,7.642533954135e-02,1.575280561792e-02,1.020926164298e-02,5.734996040024e-03,2.453990236867e-03,7.034156943368e-05,-1.681061755703e-03,-2.904871637690e-03,-3.696799546923e-03,-4.291551637880e-03,-4.755989795801e-03,-4.178738547363e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-6.175122770628e-02,-1.541367450247e-01,-1.990020049076e-01,-2.179523703797e-01,-2.259241555999e-01,-2.291785023831e-01,-2.301045091167e-01,-2.293937884748e-01,-2.266765134793e-01,-2.205756980543e-01,-2.089282623641e-01,-1.947906406100e-01,-1.847119741766e-01,-1.559354818193e-01,-1.355315131375e-01,-1.232795365876e-01,-1.170486694970e-01,-1.141869860843e-01,-1.128288355903e-01,-1.117855412668e-01,-1.094863434131e-01,-1.016126232938e-01,-7.889656776595e-02,-3.215621313953e-02],"cm_LE":[-9.907391078322e-02,-2.553625521059e-01,-3.443180862959e-01,-3.917771248733e-01,-4.170475207534e-01,-4.288879437377e-01,-4.309998082913e-01,-4.249313258857e-01,-4.112512348867e-01,-3.899661415021e-01,-3.610798550198e-01,-3.345295675167e-01,-3.190696575593e-01,-2.776668920569e-01,-2.496150543392e-01,-2.306580335185e-01,-2.170714278266e-01,-2.053105443163e-01,-1.932221818516e-01,-1.798625218872e-01,-1.643057066256e-01,-1.427050164897e-01,-1.051753523062e-01,-4.137433282272e-02],"C.P.x/c":[5.923506801009e-01,5.678936810396e-01,5.388038268096e-01,5.164857534324e-01,5.024693961503e-01,4.957018606561e-01,4.953178888068e-01,5.008416597224e-01,5.116790825908e-01,5.261470832206e-01,5.398832002652e-01,5.443357803973e-01,5.402488831883e-01,5.217174153488e-01,5.035437183301e-01,4.956552889214e-01,4.999897967898e-01,5.161776906019e-01,5.451044281037e-01,5.898391652627e-01,6.538965497759e-01,7.352099770688e-01,8.201760893059e-01,8.930854083839e-01]} Vertical_Tail = {"Xle":[5.481142821257e+00,5.457739875756e+00,5.413224828118e+00,5.351955121359e+00,5.279928261269e+00,5.204194738752e+00,5.132167878660e+00,5.070898171897e+00,5.026383124254e+00,5.002980178746e+00],"Yle":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"Zle":[1.462285642514e+00,1.415479751513e+00,1.326449656236e+00,1.203910242719e+00,1.059856522538e+00,9.083894775049e-01,7.643357573198e-01,6.417963437947e-01,5.527662485071e-01,5.059603574925e-01],"Chord":[7.291641787429e-01,7.525671242437e-01,7.970821718820e-01,8.583518786405e-01,9.303787387310e-01,1.006112261248e+00,1.078139121340e+00,1.139408828103e+00,1.183923875746e+00,1.207326821254e+00],"Area":[1.727730179136e-02,5.174997687051e-02,8.537019049526e-02,1.158415604078e-01,1.391867381176e-01,1.505166423044e-01,1.455036346588e-01,1.220345306258e-01,8.141205112924e-02,2.860720599220e-02],"c_cl":[4.143502484419e-02,1.146121890397e-01,1.669674480705e-01,2.000258625576e-01,2.165069436650e-01,2.173612378317e-01,2.020982864242e-01,1.687203348327e-01,1.143884794131e-01,4.073751989365e-02],"ai":[2.065296924523e-01,1.849180223915e-01,1.591285664757e-01,1.456224964408e-01,1.435231644007e-01,1.506386553621e-01,1.666466052407e-01,1.914179167695e-01,2.193221173430e-01,2.365321328633e-01],"cl_norm":[6.579957348177e-02,1.763463053601e-01,2.425545992662e-01,2.698370559986e-01,2.694590983040e-01,2.501591871290e-01,2.170544160382e-01,1.714623014106e-01,1.118766125250e-01,3.907064104111e-02],"cl":[5.682537081790e-02,1.522949719002e-01,2.094733190134e-01,2.330348048803e-01,2.327083956801e-01,2.160407403863e-01,1.874510278163e-01,1.480770823179e-01,9.661810337338e-02,3.374191575678e-02],"cd":[4.670566079260e-03,1.374698956983e-02,1.845844898552e-02,2.032218684725e-02,2.072187092673e-02,2.023884851599e-02,1.896705322934e-02,1.657142171121e-02,1.222733795468e-02,5.106244760924e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-3.303465544544e-02,-8.761746958838e-02,-1.194746602282e-01,-1.341488123563e-01,-1.380350789963e-01,-1.339349413680e-01,-1.218867053325e-01,-1.002593790936e-01,-6.716156843032e-02,-2.373448304337e-02],"cm_LE":[-4.232877133357e-02,-1.126299441676e-01,-1.539951982649e-01,-1.724118490116e-01,-1.757829360724e-01,-1.683239687784e-01,-1.510824211718e-01,-1.228726806389e-01,-8.171902803731e-02,-2.878672165377e-02],"C.P.x/c":[8.313363814431e-01,8.253142634661e-01,8.203574125378e-01,8.256599853193e-01,8.431675932569e-01,8.699522420101e-01,9.002322593392e-01,9.270755982234e-01,9.451240614895e-01,9.534124326091e-01]} real 0m0.471s user 0m0.239s sys 0m0.079s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./avlTest passed (as expected) ============================================= ================================================= + echo './msesTest test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt ./msesTest test; + ./msesTest 0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm Value of CL = 0.276892 real 0m1.412s user 0m1.181s sys 0m0.048s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./msesTest passed (as expected) ============================================= ================================================= + echo './frictionTest test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt ./frictionTest test; + ./frictionTest 0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt Attention: frictionTest is hard coded to look for ../csmData/frictionWingTailFuselage.csm To not make system calls to the friction executable the second command line option may be supplied - 0 = no analysis , >0 run analysis (default). 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 Running FRICTION! Value of CDfric = 0.009900 Value of CDfric = 0.009190 real 0m0.648s user 0m0.138s sys 0m0.027s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./frictionTest passed (as expected) ============================================= Running.... MESH c-Tests Running.... CFD c-Tests ================================================= + echo './fun3dAFLR2Test test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt ./fun3dAFLR2Test test; + ./fun3dAFLR2Test 0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt Attention: fun3dAFLR2Test is hard coded to look for ../csmData/cfd2D.csm 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) UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mquad = 1 UG PARAM : mpp = 3 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 841 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 841 841 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 168 338 AFLR2 IG : Nodes, Faces = 336 674 AFLR2 IG : Nodes, Faces = 504 1010 AFLR2 IG : Nodes, Faces = 617 1236 AFLR2 IG : Nodes, Faces = 672 1346 AFLR2 IG : Nodes, Faces = 741 1484 AFLR2 IG : Nodes, Faces = 803 1608 AFLR2 IG : Nodes, Faces = 840 1682 AFLR2 IG : Nodes, Faces = 841 1684 AFLR2 IG : Nodes, Faces = 845 1684 AFLR2 IG : Nodes, Faces = 841 841 AFLR2 : CPU Time = 0.002 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 841 841 AFLR2 GGp: Nodes, Faces = 1648 2455 AFLR2 GGp: Nodes, Faces = 2446 4051 AFLR2 GGp: Nodes, Faces = 3257 5673 AFLR2 GGp: Nodes, Faces = 4054 7267 AFLR2 GGp: Nodes, Faces = 4821 8801 AFLR2 GGp: Nodes, Faces = 5577 10313 AFLR2 GGp: Nodes, Faces = 6325 11809 AFLR2 GGp: Nodes, Faces = 7053 13265 AFLR2 GGp: Nodes, Faces = 7732 14623 AFLR2 GGp: Nodes, Faces = 8394 15947 AFLR2 GGp: Nodes, Faces = 9022 17203 AFLR2 GGp: Nodes, Faces = 9620 18399 AFLR2 GGp: Nodes, Faces = 10176 19511 AFLR2 GGp: Nodes, Faces = 10689 20537 AFLR2 GGp: Nodes, Faces = 11181 21521 AFLR2 GGp: Nodes, Faces = 11646 22451 AFLR2 GGp: Nodes, Faces = 12098 23355 AFLR2 GGp: Nodes, Faces = 12529 24217 AFLR2 GGp: Nodes, Faces = 12943 25045 AFLR2 GGp: Nodes, Faces = 13331 25821 AFLR2 GGp: Nodes, Faces = 13710 26579 AFLR2 GGp: Nodes, Faces = 14061 27281 AFLR2 GGp: Nodes, Faces = 14424 28007 AFLR2 GGp: Nodes, Faces = 14774 28707 AFLR2 GGp: Nodes, Faces = 15107 29373 AFLR2 GGp: Nodes, Faces = 15422 30003 AFLR2 GGp: Nodes, Faces = 15707 30573 AFLR2 GGp: Nodes, Faces = 15982 31123 AFLR2 GGp: Nodes, Faces = 16233 31625 AFLR2 GGp: Nodes, Faces = 16473 32105 AFLR2 GGp: Nodes, Faces = 16685 32529 AFLR2 GGp: Nodes, Faces = 16898 32955 AFLR2 GGp: Nodes, Faces = 17104 33367 AFLR2 GGp: Nodes, Faces = 17291 33741 AFLR2 GGp: Nodes, Faces = 17468 34095 AFLR2 GGp: Nodes, Faces = 17627 34413 AFLR2 GGp: Nodes, Faces = 17781 34721 AFLR2 GGp: Nodes, Faces = 17929 35017 AFLR2 GGp: Nodes, Faces = 18060 35279 AFLR2 GGp: Nodes, Faces = 18186 35531 AFLR2 GGp: Nodes, Faces = 18292 35743 AFLR2 GGp: Nodes, Faces = 18403 35965 AFLR2 GGp: Nodes, Faces = 18499 36157 AFLR2 GGp: Nodes, Faces = 18568 36295 AFLR2 GGp: Nodes, Faces = 18603 36365 AFLR2 GGp: Nodes, Faces = 18615 36389 AFLR2 : CPU Time = 0.038 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 18615 36389 AFLR2 QI : Nodes, Faces = 18608 1893 AFLR2 QI : Nodes, Faces = 18608 17241 AFLR2 QI : Nodes, Faces = 18608 36375 AFLR2 QI : Nodes, Faces = 18606 1789 AFLR2 QI : Nodes, Faces = 18606 17291 AFLR2 QI : Nodes, Faces = 18606 36371 AFLR2 QI : Nodes, Faces = 18604 1971 AFLR2 QI : Nodes, Faces = 18604 17198 AFLR2 QI : Nodes, Faces = 18604 36367 AFLR2 QI : Nodes, Faces = 18604 2161 AFLR2 QI : Nodes, Faces = 18604 17103 AFLR2 QI : Nodes, Faces = 18604 36367 AFLR2 QI : Nodes, Faces = 18604 2149 AFLR2 QI : Nodes, Faces = 18604 17109 AFLR2 QI : Nodes, Faces = 18604 2149 AFLR2 QI : Nodes, Faces = 18604 17109 AFLR2 : CPU Time = 0.015 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 18604 Number of elements = 20099 Number of tris = 2149 Number of quad = 17109 Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file Getting CFD boundary conditions Boundary condition name - Airfoil Boundary condition name - TunnelWall Boundary condition name - InFlow Boundary condition name - OutFlow Done getting CFD boundary conditions Python library was linked, but will not be used! Creating a 3D volume mesh from a 2D surface Number of Nodes = 37208 Number of Prisms = 2149 Number of Hexahedral = 17109 Writing AFLR3 file .... Finished writing AFLR3 file 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. NOT Running fun3d! real 0m0.819s user 0m0.636s sys 0m0.443s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./fun3dAFLR2Test passed (as expected) ============================================= ================================================= + echo './fun3dTetgenTest test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt ./fun3dTetgenTest test; + ./fun3dTetgenTest 0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt Attention: fun3dTetgenTest is hard coded to look for ../csmData/cfdMultiBody.csm 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 = 9573 Number of elements = 19142 Number of triangle elements = 19142 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 6160 Number of elements = 12316 Number of triangle elements = 12316 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 258 Number of elements = 512 Number of triangle elements = 512 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 15991 Total number of elements = 31970 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 - 15991, elements - 31970 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.116084 Creating surface mesh ... Surface mesh seconds: 0.017229 Recovering boundaries... Boundary recovery seconds: 0.098766 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.025039 Recovering Delaunayness... Delaunay recovery seconds: 0.047749 Refining mesh... 21316 insertions, added 16799 points, 789925 tetrahedra in queue. 7098 insertions, added 2909 points, 350791 tetrahedra in queue. Refinement seconds: 0.977631 Smoothing vertices... Mesh smoothing seconds: 1.3135 Improving mesh... Mesh improvement seconds: 0.035755 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.007274 Total running seconds: 2.63922 Statistics: Input points: 15991 Input facets: 31970 Input segments: 47955 Input holes: 2 Input regions: 0 Mesh points: 37026 Mesh tetrahedra: 178572 Mesh faces: 373129 Mesh faces on exterior boundary: 31970 Mesh faces on input facets: 31970 Mesh edges on input segments: 47955 Steiner points inside domain: 21035 Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Wing1 Boundary condition name - Wing2 Boundary condition name - Farfield 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. NOT Running fun3d! real 0m4.584s user 0m4.928s sys 0m0.131s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./fun3dTetgenTest passed (as expected) ============================================= Running.... STRUCTURE c-Tests ================================================= + echo './interferenceTest test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt ./interferenceTest test; + ./interferenceTest + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt Note: interferenceTest uses ../csmData/interference.csm classifyClouds: EG_generalBoolean = -7! classifyClouds: EG_generalBoolean = -7! classifyClouds: EG_generalBoolean = -7! classifyClouds: EG_generalBoolean = -7! 1: 1.000000e+00 Box 2: 5.850521e-01 Sphere 3: 7.191810e-01 Cylinder 4: 4.000000e+01 OuterBox 0.000000e+00 -2.586798e-02 0.000000e+00 0.000000e+00 -2.586798e-02 0.000000e+00 0.000000e+00 -2.804399e-02 0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00 -2.804399e-02 0.000000e+00 1.000000e+00 classifyClouds: EG_generalBoolean = -7! classifyClouds: EG_generalBoolean = -7! 1: 1.000000e+00 Box 2: 5.886885e-01 Sphere 3: 7.235323e-01 Cylinder 0.000000e+00 -2.066118e-02 0.000000e+00 -2.066118e-02 0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00 real 0m2.499s user 0m4.034s sys 0m0.046s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./interferenceTest passed (as expected) ============================================= ================================================= + echo './hsmCantileverPlateTest test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt ./hsmCantileverPlateTest test; + ./hsmCantileverPlateTest 0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt Attention: hsmCantileverPlate is hard coded to look for ../csmData/feaJoinedPlate.csm Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = plate, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - plate Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plateTip, 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 = 40 Number of elements = 51 Elemental Tria3 = 0 Elemental Quad4 = 27 Getting FEA materials....... Number of materials - 1 Material name - Madeupium No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate No "material" specified for Property tuple plate, defaulting to an index of 1 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 - appliedLoad 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 = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 4 ->HSMSOL Matrix Non-zero Entries = 1313 Converging HSM equation system ... iter dr dd dp rlx max 1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00) 1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.07 0.00) 1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.07 0.00) 2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.07 0.00) 3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00) 4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00) 5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.07 0.00) 6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.03 0.00) 7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00) 8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.00 0.00) 9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.10 0.00) 10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) iter dr dd dp rlx max 11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.00 0.00) 11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00) 12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00) 13* 0.335E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00) 15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00) 16 0.573E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00) 17 0.253E-15 0.930E-15 0.713E-15 1.000 ddx @ ( 0.56 0.10 0.00) Converging n vectors ... it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 ) it = 2 dn = 0.583E-15 rlx = 1.000 ( 31 ) Converging e1,e2 vectors ... it = 1 de = 0.285E+01 rlx = 0.351 ( 24 ) it = 2 de = 0.269E+01 rlx = 0.372 ( 14 ) it = 3 de = 0.202E+01 rlx = 0.494 ( 14 ) it = 4 de = 0.122E+01 rlx = 0.820 ( 14 ) it = 5 de = 0.378E+00 rlx = 1.000 ( 14 ) it = 6 de = 0.127E-01 rlx = 1.000 ( 40 ) it = 7 de = 0.524E-06 rlx = 1.000 ( 40 ) it = 8 de = 0.128E-15 rlx = 1.000 ( 22 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - hsm_CAPS.dat real 0m0.583s user 0m0.217s sys 0m0.030s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected) ============================================= ================================================= + echo './hsmSimplePlateTest test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt ./hsmSimplePlateTest test; + ./hsmSimplePlateTest 0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt Attention: hsmTest2 is hard coded to look for ../csmData/feaSimplePlate.csm Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 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 Number of nodal coordinates = 100 Number of elements = 198 Elemental Tria3 = 162 Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - Madeupium No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate No "material" specified for Property tuple plate, defaulting to an index of 1 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 - appliedLoad Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 7 MaxDim = 36, numBCEdge = 0, numBCNode = 36, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 36 ->HSMSOL Matrix Non-zero Entries = 8026 Converging HSM equation system ... iter dr dd dp rlx max 1 0.609E+00 0.519E+01 0.240E+01 0.096 ddy @ ( 0.28 0.25 0.00) 1* 0.571E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00) 1* 0.159E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00) 1* 0.254E-02 0.000E+00 0.000E+00 1.000 drz @ ( 0.11 0.14 0.00) 1* 0.837E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.14 0.00) 2 0.769E-02 0.753E+00 0.105E+01 0.478 dps @ ( 0.00 0.00 0.00) 2* 0.329E-03 0.000E+00 0.000E+00 1.000 drx @ ( 0.06 0.06 0.00) 2* 0.641E-06 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.08 0.00) 3 0.264E-02 0.213E+00 0.280E+00 1.000 dps @ ( 0.50 0.00 0.00) 3* 0.194E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.39 0.11 0.00) 3* 0.741E-06 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.03 0.00) 4 0.119E-03 0.159E-01 0.631E-01 1.000 dps @ ( 0.39 0.14 0.00) 4* 0.306E-05 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.22 0.00) 5 0.133E-05 0.441E-03 0.208E-02 1.000 dps @ ( 0.06 0.06 0.00) 6 0.233E-08 0.153E-06 0.694E-06 1.000 dps @ ( 0.50 0.00 0.00) 7 0.378E-15 0.119E-12 0.317E-12 1.000 dps @ ( 0.50 0.00 0.00) Converging n vectors ... it = 1 dn = 0.117E+01 rlx = 1.000 ( 66 ) it = 2 dn = 0.236E-15 rlx = 1.000 ( 81 ) Converging e1,e2 vectors ... it = 1 de = 0.357E+00 rlx = 1.000 ( 94 ) it = 2 de = 0.167E+00 rlx = 1.000 ( 67 ) it = 3 de = 0.245E-01 rlx = 1.000 ( 76 ) it = 4 de = 0.567E-02 rlx = 1.000 ( 59 ) it = 5 de = 0.192E-02 rlx = 1.000 ( 59 ) it = 6 de = 0.648E-03 rlx = 1.000 ( 59 ) it = 7 de = 0.219E-03 rlx = 1.000 ( 59 ) it = 8 de = 0.740E-04 rlx = 1.000 ( 59 ) it = 9 de = 0.250E-04 rlx = 1.000 ( 59 ) it = 10 de = 0.845E-05 rlx = 1.000 ( 59 ) it = 11 de = 0.286E-05 rlx = 1.000 ( 59 ) it = 12 de = 0.965E-06 rlx = 1.000 ( 59 ) it = 13 de = 0.326E-06 rlx = 1.000 ( 59 ) it = 14 de = 0.110E-06 rlx = 1.000 ( 59 ) it = 15 de = 0.372E-07 rlx = 1.000 ( 59 ) it = 16 de = 0.126E-07 rlx = 1.000 ( 59 ) it = 17 de = 0.425E-08 rlx = 1.000 ( 59 ) it = 18 de = 0.144E-08 rlx = 1.000 ( 59 ) it = 19 de = 0.485E-09 rlx = 1.000 ( 59 ) it = 20 de = 0.164E-09 rlx = 1.000 ( 59 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - hsm_CAPS.dat real 0m0.592s user 0m0.416s sys 0m0.028s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected) ============================================= ================================================= + echo './hsmJoinedPlateTest test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt ./hsmJoinedPlateTest test; + ./hsmJoinedPlateTest 0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt Attention: hsmJoinedPlate is hard coded to look for ../csmData/feaJoinedPlate.csm Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plateTip, 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 = 40 Number of elements = 56 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate No "material" specified for Property tuple plate, defaulting to an index of 1 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 - appliedLoad Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 16 MaxDim = 13, numBCEdge = 2, numBCNode = 4, numJoint = 13 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 4 ->HSMSOL Matrix Non-zero Entries = 1242 Converging HSM equation system ... iter dr dd dp rlx max 1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00) 1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 1* 0.325E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.05 0.00) 1* 0.434E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 2 0.274E+01 0.521E+01 0.118E-07 0.096 ddx @ ( 1.00 0.05 0.00) 2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00) 2* 0.772E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00) 3 0.202E+01 0.439E+01 0.107E-06 0.114 ddz @ ( 1.00 0.05 0.00) 3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00) 3* 0.622E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00) 3* 0.162E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00) 3* 0.163E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4 0.192E+01 0.476E+01 0.147E-07 0.105 ddz @ ( 1.00 0.05 0.00) 4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.448E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 5 0.187E+01 0.395E+01 0.296E-07 0.127 ddz @ ( 1.00 0.05 0.00) 5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 5* 0.636E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 6 0.156E+01 0.301E+01 0.131E-06 0.166 ddx @ ( 1.00 0.05 0.00) 6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.191E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.265E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7 0.103E+01 0.323E+01 0.408E-07 0.155 ddx @ ( 1.00 0.05 0.00) 7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 7* 0.432E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8 0.757E+00 0.260E+01 0.162E-07 0.192 ddx @ ( 1.00 0.05 0.00) 8* 0.296E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8* 0.351E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8* 0.586E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 9 0.680E+00 0.181E+01 0.753E-07 0.276 ddx @ ( 0.88 0.00 0.00) 9* 0.329E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9* 0.452E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 9* 0.159E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 9* 0.238E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 10 0.457E+00 0.172E+01 0.586E-07 0.290 ddz @ ( 1.00 0.10 0.00) 10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 10* 0.392E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) iter dr dd dp rlx max 11 0.258E+00 0.122E+01 0.666E-08 0.411 ddz @ ( 1.00 0.10 0.00) 11* 0.207E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 11* 0.284E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 11* 0.486E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12 0.135E+00 0.660E+00 0.377E-08 0.758 ddz @ ( 0.88 0.00 0.00) 12* 0.242E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12* 0.368E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12* 0.869E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 13 0.430E-01 0.257E+00 0.505E-07 1.000 ddx @ ( 1.00 0.05 0.00) 13* 0.395E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 13* 0.128E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 13* 0.196E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 14 0.656E-03 0.680E-02 0.885E-07 1.000 ddx @ ( 1.00 0.00 0.00) 15 0.156E-05 0.177E-05 0.268E-10 1.000 ddx @ ( 1.00 0.10 0.00) 16 0.273E-09 0.106E-08 0.893E-11 1.000 ddx @ ( 0.50 0.05 0.00) 17 0.138E-15 0.353E-15 0.907E-15 1.000 dps @ ( 0.38 0.10 0.00) Converging n vectors ... it = 1 dn = 0.197E+01 rlx = 1.000 ( 17 ) it = 2 dn = 0.866E-15 rlx = 1.000 ( 18 ) Converging e1,e2 vectors ... it = 1 de = 0.753E+01 rlx = 0.133 ( 1 ) it = 2 de = 0.309E+01 rlx = 0.324 ( 20 ) it = 3 de = 0.324E+01 rlx = 0.309 ( 2 ) it = 4 de = 0.226E+01 rlx = 0.443 ( 2 ) it = 5 de = 0.140E+01 rlx = 0.716 ( 2 ) it = 6 de = 0.660E+00 rlx = 1.000 ( 2 ) it = 7 de = 0.860E-01 rlx = 1.000 ( 2 ) it = 8 de = 0.228E-03 rlx = 1.000 ( 2 ) it = 9 de = 0.428E-11 rlx = 1.000 ( 2 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - hsm_CAPS.dat real 0m0.391s user 0m0.196s sys 0m0.031s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./hsmJoinedPlateTest passed (as expected) ============================================= Running.... AEROELASTIC c-Tests ================================================= Did not run examples for: awave pointwise Mystran ================================================= All tests pass! ================================================= ================================================= + ./execute_PyTestRegression.sh ================================================= Using python : /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python ================================================= No options provided...defaulting to ALL Running.... LINEARAERO PyTests avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/avl ================================================= + echo 'avl_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 0.0006119078685800925 CYtot -6.292592518559147e-15 CZtot -0.3012861394881712 Cltot -4.783069014642483e-14 Cmtot -0.1945055953448147 Cntot -2.338890054396671e-15 Cl'tot -4.786422456048383e-14 Cn'tot -1.50377318550154e-15 CLtot 0.3012509314146395 CDtot 0.00464635348821979 CDvis 0.0 CLff 0.3009503023516151 CYff -7.7198870803959e-15 CDind 0.00464635348821979 CDff 0.004968969500894849 e 0.9669902146155998 StripForces Wing cl = [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407] Wing cd = [-0.004234137763148, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946456, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372442, -0.004494543653152, -0.00423413776453] real 0m0.506s user 0m0.610s sys 0m0.204s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_AutoSpan_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt avl_AutoSpan_PyTest.py test; + python -u avl_AutoSpan_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Loading AIM Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wing3, index = 3 Getting vortex lattice surface data VLM surface name - Wing1 VLM surface name - Wing2 VLM surface name - Wing3 Done getting vortex lattice surface data Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used. Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used. Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used. Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used. Writing surface - Wing1 (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Wing2 (ID = 1) Section 1 of 7 (ID = 0) Section 2 of 7 (ID = 1) Section 3 of 7 (ID = 2) Section 4 of 7 (ID = 3) Section 5 of 7 (ID = 4) Section 6 of 7 (ID = 5) Section 7 of 7 (ID = 6) Writing surface - Wing3 (ID = 2) Section 1 of 7 (ID = 0) Section 2 of 7 (ID = 3) Control surface 1 of 1 Section 3 of 7 (ID = 4) Control surface 1 of 1 Section 4 of 7 (ID = 1) Section 5 of 7 (ID = 5) Control surface 1 of 1 Section 6 of 7 (ID = 6) Control surface 1 of 1 Section 7 of 7 (ID = 2) CXtot -0.04120015660053111 CYtot 2.462543613195682e-10 CZtot -1.125018850856348 Cltot 1.184580814522611e-09 Cmtot -1.954741252395341 Cntot -1.790133030044494e-10 Cl'tot 1.181276184205198e-09 Cn'tot -1.996598242441884e-10 CLtot 1.124128463157939 CDtot 0.06082816785187402 CDvis 0.0 CLff 1.123105484603622 CYff 2.611430934031642e-10 CDind 0.06082816785187402 CDff -0.2032104788139517 e -0.3293015989519321 real 0m6.803s user 0m6.837s sys 0m7.593s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_AutoSpan_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'avl_DesignSweep_PyTest.py test;' avl_DesignSweep_PyTest.py test; + python -u avl_DesignSweep_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002572533601550775 Cl = 0.2009337808873524 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002586364230241802 Cl = 0.2015191856814851 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002609799718816161 Cl = 0.202507529643332 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002643444008424624 Cl = 0.2039185811658769 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002688200920998204 Cl = 0.2057816377790584 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002745342060015943 Cl = 0.2081373840559949 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002816610334298771 Cl = 0.2110406736705562 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002904376657734716 Cl = 0.2145646488015997 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003011879793042747 Cl = 0.2188068842334945 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003143602034586226 Cl = 0.2238987294815726 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003305877285452361 Cl = 0.2300199286487156 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003507917885472537 Cl = 0.2374223860296633 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003763643677259966 Cl = 0.2464707142744908 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004095167898227208 Cl = 0.25771580677477 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004540047408135333 Cl = 0.2720394012163583 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.005168237926851883 Cl = 0.2909701507463254 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.006128930715329168 Cl = 0.317487548593558 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.007818359051271666 Cl = 0.3586078919918751 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.01186220444373961 Cl = 0.4382638635243895 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002572533601550775 Cl = 0.2009337808873524 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002586364230241802 Cl = 0.2015191856814851 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002609799718816161 Cl = 0.202507529643332 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002643444008424624 Cl = 0.2039185811658769 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002688200920998204 Cl = 0.2057816377790584 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002745342060015943 Cl = 0.2081373840559949 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002816610334298771 Cl = 0.2110406736705562 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002904376657734716 Cl = 0.2145646488015997 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003011879793042747 Cl = 0.2188068842334945 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003143602034586226 Cl = 0.2238987294815726 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003305877285452361 Cl = 0.2300199286487156 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003507917885472537 Cl = 0.2374223860296633 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003763643677259966 Cl = 0.2464707142744908 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004095167898227208 Cl = 0.25771580677477 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004540047408135333 Cl = 0.2720394012163583 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.005168237926851883 Cl = 0.2909701507463254 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.006128930715329168 Cl = 0.317487548593558 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.007818359051271666 Cl = 0.3586078919918751 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.01186220444373961 Cl = 0.4382638635243895 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002572533601550775 Cl = 0.2009337808873524 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002586364230241802 Cl = 0.2015191856814851 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002609799718816161 Cl = 0.202507529643332 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002643444008424624 Cl = 0.2039185811658769 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002688200920998204 Cl = 0.2057816377790584 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002745342060015943 Cl = 0.2081373840559949 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002816610334298771 Cl = 0.2110406736705562 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002904376657734716 Cl = 0.2145646488015997 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003011879793042747 Cl = 0.2188068842334945 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003143602034586226 Cl = 0.2238987294815726 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003305877285452361 Cl = 0.2300199286487156 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003507917885472537 Cl = 0.2374223860296633 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003763643677259966 Cl = 0.2464707142744908 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004095167898227208 Cl = 0.25771580677477 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004540047408135333 Cl = 0.2720394012163583 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.005168237926851883 Cl = 0.2909701507463254 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.006128930715329168 Cl = 0.317487548593558 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.007818359051271666 Cl = 0.3586078919918751 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.01186220444373961 Cl = 0.4382638635243895 Cl[0] = 0.2009337808873524 Cd[0] = 0.002572533601550775 real 0m18.435s user 0m9.004s sys 0m9.184s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_ControlSurf_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt avl_ControlSurf_PyTest.py test; + python -u avl_ControlSurf_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Loading AIM Setting design parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice control surface data VLM control surface name - Tail VLM control surface name - WingRightLE VLM control surface name - WingRightTE Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Vertical_Tail 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 WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Alpha 1.0 Beta 0.0 Mach 0.5 pb/2V -0.0 qc/2V 0.0 rb/2V -0.0 p'b/2V -0.0 r'b/2V -0.0 CXtot -0.01911479917641001 CYtot 0.03828770401115553 CZtot -0.6203123021537938 Cltot 0.05803020542928473 Cmtot -0.3649415791575079 Cntot -0.02051317548232544 Cl'tot 0.05766336287208538 Cn'tot -0.02152281795713262 CLtot 0.6198842263414319 CDtot 0.02993783031514586 CDvis 0.0 CLff 0.6192452092592853 CYff 0.03287079625844261 CDind 0.02993783031514586 CDff 0.0286101982265777 e 0.7130586920543264 real 0m0.554s user 0m0.652s sys 0m0.204s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_EigenValue_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt avl_EigenValue_PyTest.py test; + python -u avl_EigenValue_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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) Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO EigenValues {'case 1': [[0.48252996, 1.0092579], [0.48252996, -1.0092579], [-6.42569, 0.0], [-1.2733929, 0.0], [-0.0011487329, 0.0], [-1.2380479, 0.49321593], [-1.2380479, -0.49321593], [0.77888703, 0.0]]} real 0m0.467s user 0m0.578s sys 0m0.186s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_EigenValue_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_OpenMDAO_3_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt avl_OpenMDAO_3_PyTest.py test; + python -u avl_OpenMDAO_3_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt [VIGGEN.MIT.EDU:10775] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/3675717632/sm_segment.VIGGEN.502.db170000.0 could be created. 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) Alpha [2.] Beta [3.] Cmtot2 [0.04166298] Alpha [2.] Beta [3.] Cmtot2 [0.04166298] Cmtot2_Alpha [[0.68007176]] Cmtot2_Beta [[0.0008466]] RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 2 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 4.16630D-02 |proj g|= 6.80072D-01 Alpha [1.31992824] Beta [2.9991534] Cmtot2 [0.03401795] Cmtot2_Alpha [[0.60837327]] Cmtot2_Beta [[0.0015253]] At iterate 1 f= 3.40180D-02 |proj g|= 6.08373D-01 Alpha [-4.45133036] Beta [2.92288326] Cmtot2 [0.00071304] Cmtot2_Alpha [[0.07860089]] Cmtot2_Beta [[0.00107544]] At iterate 2 f= 7.13044D-04 |proj g|= 7.86009D-02 Alpha [-5.30773219] Beta [2.90057802] Cmtot2 [2.43104345e-05] Cmtot2_Alpha [[0.01420175]] Cmtot2_Beta [[0.00021881]] At iterate 3 f= 2.43104D-05 |proj g|= 1.42017D-02 Alpha [-5.49659696] Beta [2.89526135] Cmtot2 [3.72334444e-08] Cmtot2_Alpha [[0.00055304]] Cmtot2_Beta [[8.73257587e-06]] At iterate 4 f= 3.72334D-08 |proj g|= 5.53036D-04 Alpha [-5.50424967] Beta [2.89504288] Cmtot2 [2.19764419e-12] Cmtot2_Alpha [[4.24792989e-06]] Cmtot2_Beta [[6.7141843e-08]] At iterate 5 f= 2.19764D-12 |proj g|= 4.24793D-06 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 2 5 6 5 0 0 4.248D-06 2.198D-12 F = 2.1976441939068914E-012 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-5.50424967] [2.89504288] real 0m29.293s user 0m3.981s sys 0m0.785s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected) ================================================= friction: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/friction ================================================= + echo 'friction_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Loading AIM Setting Mach & Altitude Values Lifting Surface: Body = 1, units m XLE: 1.571946 -3.872983 0.249728 XTE: 2.536563 -3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 2, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.614012 0.000000 0.002015 Chord: 1.614013 Arc: 3.308635 T/C: 0.127839 Type: Wing Lifting Surface: Body = 3, units m XLE: 1.571946 3.872983 0.249728 XTE: 2.536563 3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 4, units m XLE: 5.484123 0.000000 1.468246 XTE: 6.210307 0.000915 1.468246 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: VTail Lifting Surface: Body = 5, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.210307 0.001525 0.500000 Chord: 1.210308 Arc: 2.471195 T/C: 0.120035 Type: VTail Lifting Surface: Body = 6, units m XLE: 5.484123 -0.968246 0.500000 XTE: 6.210307 -0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Lifting Surface: Body = 7, units m XLE: 5.484123 0.968246 0.500000 XTE: 6.210307 0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Body of Revolution: Body = 8, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 9, units m Arc: 3.714180 Diameter: 1.020621 Type: Fuse Body of Revolution: Body = 10, units m Arc: 2.771209 Diameter: 0.645497 Type: Fuse Body of Revolution: Body = 11, units m Arc: 1.013945 Diameter: 0.322749 Type: Fuse Body of Revolution: Body = 12, units m Arc: 0.101394 Diameter: 0.032275 Type: Fuse Number of sections 4, number of revolution sections 1 Number of Mach-Altitude cases = 2 Total drag = [0.0132, 0.01226] Form drag = [0.0033, 0.00307] Friction drag = [0.0099, 0.00919] real 0m0.288s user 0m0.375s sys 0m0.072s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected) ================================================= tsfoil2: /Users/jenkins/util/tsfoil/tsfoil2 ================================================= + echo 'tsfoil_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tsfoil_PyTest.py test; + python -u tsfoil_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results PAUSE Press the ENTER key to exit To resume execution, type go. Other input will terminate the job. Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG Cl = 0.933371 Cd = 0.000284 Cd Wave = 0.0 Cm = -0.203435 Cp _Critcal = -1.303869 real 0m0.440s user 0m0.536s sys 0m0.057s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected) ================================================= mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/mses ================================================= + echo 'mses_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt mses_PyTest.py test; + python -u mses_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Cl = 0.3783791085548177 Cd = 0.007775858417209677 Cm = 0.005262636995835036 real 0m1.990s user 0m2.179s sys 0m0.090s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'mses_OpenMDAO_3_PyTest.py test;' mses_OpenMDAO_3_PyTest.py test; + python -u mses_OpenMDAO_3_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt [VIGGEN.MIT.EDU:11035] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/2039218176/sm_segment.VIGGEN.502.798c0000.0 could be created. Getting CFD design variables....... Number of design variables - 1 Design Variable name - camber Done getting CFD design variables camber [0.1] CD [0.01326534] camber [0.1] CD [0.01326534] CD_camber [[0.1764758]] RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 1 variables are exactly at the bounds At iterate 0 f= 1.32653D-02 |proj g|= 1.76476D-01 camber [-0.0764758] CD [0.01022332] CD_camber [[-0.08759853]] At iterate 1 f= 1.02233D-02 |proj g|= 8.75985D-02 camber [-0.01793539] CD [0.00770373] CD_camber [[-0.01328932]] At iterate 2 f= 7.70373D-03 |proj g|= 1.32893D-02 camber [-0.00746613] CD [0.00760241] CD_camber [[-0.00542337]] At iterate 3 f= 7.60241D-03 |proj g|= 5.42337D-03 camber [-0.00024784] CD [0.00758207] CD_camber [[-0.00011854]] At iterate 4 f= 7.58207D-03 |proj g|= 1.18538D-04 camber [-8.65457493e-05] CD [0.00758207] CD_camber [[-3.94469721e-06]] camber [-0.00019629] CD [0.00758207] CD_camber [[-8.4257979e-05]] At iterate 5 f= 7.58207D-03 |proj g|= 8.42580D-05 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 5 7 5 0 0 8.426D-05 7.582D-03 F = 7.5820667358142552E-003 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-0.00019629] real 0m15.107s user 0m15.397s sys 0m0.384s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected) ================================================= xfoil: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/xfoil ================================================= + echo 'xfoil_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt xfoil_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u xfoil_PyTest.py -outLevel=0 -noPlotData Cl = [1.05475230551148, 1.36488869373725, 1.56607214272246, 2.03059709357768, 1.9727108312095, 1.87307153172323, 1.76050475760053] Cd = [0.0131991208831308, 0.0166540240605859, 0.0200551482562657, 0.0458671341873005, 0.0754256009397268, 0.0994469174479059, 0.127479430989221] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.49604411072842, 0.461377732041756, 0.442376568202227, 0.361251636144409, 0.276104140854608, 0.214381239321802, 0.132988264746433] real 0m2.182s user 0m2.366s sys 0m0.101s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected) ================================================= Running.... MESH PyTests ================================================= + echo 'egadsTess_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt egadsTess_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u egadsTess_PyTest.py -outLevel=0 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 0m4.375s user 0m10.836s sys 0m6.795s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected) ================================================= ================================================= + echo 'egadsTess_Box_Quad_Pytest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt egadsTess_Box_Quad_Pytest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u egadsTess_Box_Quad_Pytest.py -outLevel=0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = box1, index = 1 Name = box2, index = 2 Name = box3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 3 TFI quading disabled with attribute .qParams Face 4 TFI quading disabled with attribute .qParams TFI quading on all faces disabled with .qParams attribute on the body 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 = 602 Number of elements = 600 Number of triangle elements = 0 Number of quadrilateral elements = 600 Body 2 (of 3) Number of nodes = 537 Number of elements = 535 Number of triangle elements = 0 Number of quadrilateral elements = 535 Body 3 (of 3) Number of nodes = 1356 Number of elements = 1354 Number of triangle elements = 0 Number of quadrilateral elements = 1354 ---------------------------- Total number of nodes = 2495 Total number of elements = 2489 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file real 0m2.381s user 0m2.944s sys 0m0.076s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case egadsTess_Box_Quad_Pytest.py passed (as expected) ================================================= ================================================= + echo 'egadsTess_Spheres_Quad_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt egadsTess_Spheres_Quad_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u egadsTess_Spheres_Quad_PyTest.py -outLevel=0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Spheres, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 4 has a degenerate edge - no TFI quading Face 5 has a degenerate edge - no TFI quading Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 5907 Number of elements = 5905 Number of triangle elements = 0 Number of quadrilateral elements = 5905 ---------------------------- Total number of nodes = 5907 Total number of elements = 5905 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file real 0m5.551s user 0m8.897s sys 0m0.132s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case egadsTess_Spheres_Quad_PyTest.py passed (as expected) ================================================= ================================================= + echo 'egadsTess_Nose_Quad_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt egadsTess_Nose_Quad_PyTest.py test; + python -u egadsTess_Nose_Quad_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = nose, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 2 has a degenerate edge - no TFI quading Getting surface mesh for body 1 (of 1) EG_getSidepoint: LineSearch Failed (0.000000 0.973785)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (1.013231 0.966690)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (1.004202 0.966536)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (1.004202 0.966536)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (1.004202 0.966536)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (1.004202 0.966536)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (1.046938 0.962477)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (1.035877 0.957484)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (1.015407 0.966058)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (0.856444 0.971910)! EG_getSidepoint: LineSearch Failed (2.750998 0.986828)! EG_getSidepoint: LineSearch Failed (0.813517 0.972994)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! EG_getSidepoint: LineSearch Failed (0.719835 0.974156)! Body 1 (of 1) Number of nodes = 1498 Number of elements = 1496 Number of triangle elements = 0 Number of quadrilateral elements = 1496 ---------------------------- Total number of nodes = 1498 Total number of elements = 1496 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file real 0m1.937s user 0m2.332s sys 0m0.078s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case egadsTess_Nose_Quad_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr2_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr2_PyTest.py test; + python -u aflr2_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 316 634 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 681 1018 AFLR2 GGp: Nodes, Faces = 1013 1682 AFLR2 GGp: Nodes, Faces = 1339 2334 AFLR2 GGp: Nodes, Faces = 1652 2960 AFLR2 GGp: Nodes, Faces = 1957 3570 AFLR2 GGp: Nodes, Faces = 2252 4160 AFLR2 GGp: Nodes, Faces = 2526 4708 AFLR2 GGp: Nodes, Faces = 2809 5274 AFLR2 GGp: Nodes, Faces = 3083 5822 AFLR2 GGp: Nodes, Faces = 3327 6310 AFLR2 GGp: Nodes, Faces = 3564 6784 AFLR2 GGp: Nodes, Faces = 3788 7232 AFLR2 GGp: Nodes, Faces = 3995 7646 AFLR2 GGp: Nodes, Faces = 4194 8044 AFLR2 GGp: Nodes, Faces = 4394 8444 AFLR2 GGp: Nodes, Faces = 4585 8826 AFLR2 GGp: Nodes, Faces = 4772 9200 AFLR2 GGp: Nodes, Faces = 4943 9542 AFLR2 GGp: Nodes, Faces = 5129 9914 AFLR2 GGp: Nodes, Faces = 5293 10242 AFLR2 GGp: Nodes, Faces = 5447 10550 AFLR2 GGp: Nodes, Faces = 5594 10844 AFLR2 GGp: Nodes, Faces = 5716 11088 AFLR2 GGp: Nodes, Faces = 5830 11316 AFLR2 GGp: Nodes, Faces = 5909 11474 AFLR2 GGp: Nodes, Faces = 5964 11584 AFLR2 GGp: Nodes, Faces = 6006 11668 AFLR2 GGp: Nodes, Faces = 6025 11706 AFLR2 GGp: Nodes, Faces = 6034 11724 AFLR2 : CPU Time = 0.010 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 6034 11724 AFLR2 QI : Nodes, Faces = 6033 454 AFLR2 QI : Nodes, Faces = 6033 5634 AFLR2 QI : Nodes, Faces = 6033 11722 AFLR2 QI : Nodes, Faces = 6032 462 AFLR2 QI : Nodes, Faces = 6032 5629 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 456 AFLR2 QI : Nodes, Faces = 6032 5632 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 474 AFLR2 QI : Nodes, Faces = 6032 5623 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6031 486 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 QI : Nodes, Faces = 6031 488 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 : CPU Time = 0.004 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 0m0.501s user 0m0.723s sys 0m0.414s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr4_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr4_PyTest.py test; + python -u aflr4_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 real 0m1.405s user 0m1.573s sys 0m0.136s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'aflr4_Symmetry_PyTest.py test;' aflr4_Symmetry_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u aflr4_Symmetry_PyTest.py -outLevel=0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Farfield, index = 1 Name = Symmetry, index = 2 Name = Wing1, index = 3 Name = Wing2, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = Symmetry, index = 2 Name = Wing1, index = 3 Name = Wing2, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - Symmetry Done getting mesh sizing parameters AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file real 0m1.471s user 0m1.593s sys 0m0.423s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_Symmetry_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'aflr4_Generic_Missile.py test;' aflr4_Generic_Missile.py test; + python -u aflr4_Generic_Missile.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = MissileOML, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file real 0m4.319s user 0m7.345s sys 0m0.433s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_Generic_Missile.py passed (as expected) ================================================= ================================================= + echo 'aflr4_TipTreat_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr4_TipTreat_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u aflr4_TipTreat_PyTest.py -outLevel=0 -noPlotData Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file real 0m5.298s user 0m5.304s sys 0m0.255s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_TipTreat_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'aflr4_and_aflr3_PyTest.py test;' aflr4_and_aflr3_PyTest.py test; + python -u aflr4_and_aflr3_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wing1 Mesh sizing name - Wing2 Done getting mesh sizing parameters Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 150214 Number of elements = 450024 Number of triangles = 14380 Number of quadrilatarals = 0 Number of tetrahedrals = 214592 Number of pyramids = 425 Number of prisms = 220627 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file real 0m8.162s user 0m8.074s sys 0m0.319s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'aflr4_and_aflr3_Symmetry_PyTest.py test;' aflr4_and_aflr3_Symmetry_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u aflr4_and_aflr3_Symmetry_PyTest.py -outLevel=0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Farfield, index = 1 Name = Symmetry, index = 2 Name = Wing1, index = 3 Name = Wing2, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Farfield, index = 1 Name = Symmetry, index = 2 Name = Wing1, index = 3 Name = Wing2, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - Symmetry Done getting mesh sizing parameters 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 = Farfield, index = 1 Name = Symmetry, index = 2 Name = Wing1, index = 3 Name = Wing2, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Farfield, index = 1 Name = Symmetry, index = 2 Name = Wing1, index = 3 Name = Wing2, index = 4 Getting mesh sizing parameters Mesh sizing name - Wing1 Mesh sizing name - Wing2 Done getting mesh sizing parameters Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 333315 Number of elements = 1070337 Number of triangles = 44382 Number of quadrilatarals = 1613 Number of tetrahedrals = 574947 Number of pyramids = 327 Number of prisms = 449068 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file real 0m18.715s user 0m18.432s sys 0m0.804s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_and_aflr3_Symmetry_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr4_QuadMesh_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr4_QuadMesh_PyTest.py test; + python -u aflr4_QuadMesh_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file real 0m4.956s user 0m11.341s sys 0m6.819s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_QuadMesh_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr4_and_Tetgen_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr4_and_Tetgen_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u aflr4_and_Tetgen_PyTest.py -outLevel=0 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 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 - 30048, elements - 60084 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing Tecplot file .... Finished writing Tecplot file real 0m7.462s user 0m7.394s sys 0m0.307s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_and_Tetgen_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr4_tetgen_Regions_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr4_tetgen_Regions_PyTest.py test; + python -u aflr4_tetgen_Regions_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = cut, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SheetBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 11 Faces EGADS : Body 0 has 20 Edges EGADS : Body 0 has 11 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 6 8 10 11 EGADS : 2 Yes 0 0 1 0 1 1 3 7 9 11 EGADS : 3 Yes 0 0 1 0 1 2 4 6 9 11 EGADS : 4 Yes 0 0 1 0 1 3 5 7 9 11 EGADS : 5 Yes 0 0 1 0 1 4 6 8 10 11 EGADS : 6 Yes 0 0 1 0 1 1 3 5 10 11 EGADS : 7 Yes 0 0 1 0 1 2 4 8 9 11 EGADS : 8 Yes 0 0 1 0 1 1 5 7 10 11 EGADS : 9 Yes 0 0 1 0 1 2 3 4 7 EGADS : 10 Yes 0 0 1 0 1 1 5 6 8 EGADS : 11 Yes 0 0 1 0 1 1 2 3 4 5 6 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 6 7 -2 EGADS : 3 8 5 9 -10 EGADS : 4 10 11 -12 -13 EGADS : 5 14 15 -16 -11 EGADS : 6 1 -17 -14 -9 EGADS : 7 -18 12 -19 -7 EGADS : 8 16 20 -3 19 EGADS : 9 13 18 -6 -8 EGADS : 10 -15 17 4 -20 EGADS : 11 11 -19 -2 9 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 6 7 -2 EGADS : 3 Yes 8 5 9 -10 EGADS : 4 Yes 10 11 -12 -13 EGADS : 5 Yes 14 15 -16 -11 EGADS : 6 Yes 1 -17 -14 -9 EGADS : 7 Yes -18 12 -19 -7 EGADS : 8 Yes 16 20 -3 19 EGADS : 9 Yes 13 18 -6 -8 EGADS : 10 Yes -15 17 4 -20 EGADS : 11 Yes 11 -19 -2 9 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 6 EGADS : 2 0 Yes 1 3 1 1 2 11 EGADS : 3 0 Yes 3 4 1 1 8 EGADS : 4 0 Yes 2 4 1 1 10 EGADS : 5 0 Yes 5 1 1 2 3 EGADS : 6 0 Yes 5 6 1 2 9 EGADS : 7 0 Yes 6 3 1 2 7 EGADS : 8 0 Yes 7 5 1 3 9 EGADS : 9 0 Yes 1 8 1 3 6 11 EGADS : 10 0 Yes 7 8 1 3 4 EGADS : 11 0 Yes 8 9 1 4 5 11 EGADS : 12 0 Yes 10 9 1 4 7 EGADS : 13 0 Yes 7 10 1 4 9 EGADS : 14 0 Yes 8 11 1 5 6 EGADS : 15 0 Yes 11 12 1 5 10 EGADS : 16 0 Yes 9 12 1 5 8 EGADS : 17 0 Yes 11 2 1 6 10 EGADS : 18 0 Yes 10 6 1 7 9 EGADS : 19 0 Yes 3 9 1 7 8 11 EGADS : 20 0 Yes 12 4 1 8 10 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 1 0 0 EGADS : 2 Yes 1 0 2 EGADS : 3 Yes 1 1 1 EGADS : 4 Yes 1 1 2 EGADS : 5 Yes 1 0 0 EGADS : 6 Yes 1 1 0 EGADS : 7 Yes 0 0 0 EGADS : 8 Yes 0 0 0 EGADS : 9 Yes 0 1 1 EGADS : 10 Yes 0 1 0 EGADS : 11 Yes 0 0 2 EGADS : 12 Yes 0 1 2 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 4 AFLR4 : Min Bounding Box Length = 2 AFLR4 : Max Ref Bounding Box Length = 4 AFLR4 : Min Ref Bounding Box Length = 2 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.01 AFLR4 : Max Surf Spacing = 0.2 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 TRANSP 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 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 137 228 0 AFLR4 : Nodes, Trias,Quads= 131 216 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 137 228 0 AFLR4 : Nodes, Trias,Quads= 132 218 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 76 120 0 AFLR4 : Nodes, Trias,Quads= 72 112 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 137 228 0 AFLR4 : Nodes, Trias,Quads= 132 218 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 137 228 0 AFLR4 : Nodes, Trias,Quads= 131 216 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 196 340 0 AFLR4 : Nodes, Trias,Quads= 192 332 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 196 340 0 AFLR4 : Nodes, Trias,Quads= 192 332 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 76 120 0 AFLR4 : Nodes, Trias,Quads= 72 112 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 184 318 0 AFLR4 : Nodes, Trias,Quads= 178 306 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1232 2506 464 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1232 2506 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 140 234 0 AFLR4 : Nodes, Trias,Quads= 134 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 140 234 0 AFLR4 : Nodes, Trias,Quads= 133 220 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 76 120 0 AFLR4 : Nodes, Trias,Quads= 72 112 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 141 236 0 AFLR4 : Nodes, Trias,Quads= 133 220 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 141 236 0 AFLR4 : Nodes, Trias,Quads= 133 220 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 207 362 0 AFLR4 : Nodes, Trias,Quads= 192 332 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 205 358 0 AFLR4 : Nodes, Trias,Quads= 192 332 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 76 120 0 AFLR4 : Nodes, Trias,Quads= 72 112 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 193 336 0 AFLR4 : Nodes, Trias,Quads= 183 316 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1244 2530 464 OVERALL : CPU Time = 0.050 seconds Body 1 (of 1) Number of nodes = 1244 Number of elements = 2530 Number of triangle elements = 2530 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1244 Total number of elements = 2530 Total number of triangle elements = 2530 Total number of quadrilateral elements = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = cut, index = 2 Number of surface: nodes - 1244, elements - 2530 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.020417 Creating surface mesh ... Surface mesh seconds: 0.000774 Recovering boundaries... Boundary recovery seconds: 0.009389 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.000388 Recovering Delaunayness... Delaunay recovery seconds: 0.001008 Refining mesh... Refinement seconds: 0.012853 Smoothing vertices... Mesh smoothing seconds: 0.022027 Improving mesh... Mesh improvement seconds: 0.000782 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001032 Total running seconds: 0.068718 Statistics: Input points: 1244 Input facets: 2530 Input segments: 3771 Input holes: 0 Input regions: 2 Mesh points: 1454 Mesh tetrahedra: 5098 Mesh faces: 11303 Mesh faces on exterior boundary: 2214 Mesh faces on input facets: 2530 Mesh edges on input segments: 3771 Steiner points inside domain: 210 Done meshing using TetGen! Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing Tecplot file .... Finished writing Tecplot file real 0m0.414s user 0m0.606s sys 0m0.094s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_tetgen_Regions_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tetgen_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tetgen_PyTest.py test; + python -u tetgen_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 = 258 Number of elements = 512 Number of triangle elements = 512 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3130 Total number of elements = 6248 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 - 3130, elements - 6248 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.014585 Creating surface mesh ... Surface mesh seconds: 0.002086 Recovering boundaries... Boundary recovery seconds: 0.049679 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.003303 Suppressing Steiner points ... Steiner suppression seconds: 6e-06 Recovering Delaunayness... Delaunay recovery seconds: 0.006515 Refining mesh... 4177 insertions, added 2159 points, 136953 tetrahedra in queue. 1390 insertions, added 372 points, 139199 tetrahedra in queue. 1853 insertions, added 454 points, 136118 tetrahedra in queue. 2470 insertions, added 521 points, 118263 tetrahedra in queue. 3293 insertions, added 464 points, 66933 tetrahedra in queue. 4389 insertions, added 406 points, 1337 tetrahedra in queue. 5851 insertions, added 599 points, 33 tetrahedra in queue. Refinement seconds: 0.441281 Smoothing vertices... Mesh smoothing seconds: 0.22438 Improving mesh... Mesh improvement seconds: 0.006904 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000659 Total running seconds: 0.749556 Statistics: Input points: 3130 Input facets: 6248 Input segments: 9372 Input holes: 2 Input regions: 0 Mesh points: 8156 Mesh tetrahedra: 40155 Mesh faces: 83435 Mesh faces on exterior boundary: 6250 Mesh faces on input facets: 6250 Mesh edges on input segments: 9373 Steiner points on input segments: 1 Steiner points inside domain: 5025 Done meshing using TetGen! Volume mesher did not preserve surface elements - data transfer will NOT be possible. Writing Tecplot file .... Finished writing Tecplot file real 0m1.541s user 0m1.812s sys 0m0.134s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tetgen_Holes_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tetgen_Holes_PyTest.py test; + python -u tetgen_Holes_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = cut, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 8995 Number of elements = 18112 Number of triangle elements = 18112 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 8995 Total number of elements = 18112 Writing Tecplot file .... Finished writing Tecplot file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: box 2: cut Finished writing vtk file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = cut, index = 2 Number of surface: nodes - 8995, elements - 18112 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.168591 Creating surface mesh ... Surface mesh seconds: 0.006764 Recovering boundaries... Boundary recovery seconds: 0.075022 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.006225 Recovering Delaunayness... Delaunay recovery seconds: 0.038559 Refining mesh... Refinement seconds: 0.16553 Smoothing vertices... Mesh smoothing seconds: 0.198694 Improving mesh... Mesh improvement seconds: 0.006157 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001338 Total running seconds: 0.667062 Statistics: Input points: 8995 Input facets: 18112 Input segments: 27104 Input holes: 1 Input regions: 0 Mesh points: 7154 Mesh tetrahedra: 27977 Mesh faces: 60994 Mesh faces on exterior boundary: 10080 Mesh faces on input facets: 10080 Mesh edges on input segments: 15120 Steiner points inside domain: 2112 Done meshing using TetGen! Volume mesher did not preserve surface elements - data transfer will NOT be possible. Writing Tecplot file .... Finished writing Tecplot file Writing vtk file .... Writing vtk general file .... Finished writing vtk file real 0m1.482s user 0m1.664s sys 0m0.128s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tetgen_Holes_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tetgen_Regions_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tetgen_Regions_PyTest.py test; + python -u tetgen_Regions_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = cut, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 8995 Number of elements = 18112 Number of triangle elements = 18112 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 8995 Total number of elements = 18112 Writing Tecplot file .... Finished writing Tecplot file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: box 2: cut Finished writing vtk file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = cut, index = 2 Number of surface: nodes - 8995, elements - 18112 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.178541 Creating surface mesh ... Surface mesh seconds: 0.006544 Recovering boundaries... Boundary recovery seconds: 0.080009 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.004328 Recovering Delaunayness... Delaunay recovery seconds: 0.075006 Refining mesh... Refinement seconds: 0.331747 Smoothing vertices... Mesh smoothing seconds: 0.422037 Improving mesh... Mesh improvement seconds: 0.012228 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.003272 Total running seconds: 1.11392 Statistics: Input points: 8995 Input facets: 18112 Input segments: 27104 Input holes: 0 Input regions: 2 Mesh points: 13174 Mesh tetrahedra: 55665 Mesh faces: 119362 Mesh faces on exterior boundary: 16064 Mesh faces on input facets: 18112 Mesh edges on input segments: 27104 Steiner points inside domain: 4179 Done meshing using TetGen! Writing Tecplot file .... Finished writing Tecplot file Writing vtk file .... Writing vtk general file .... Finished writing vtk file real 0m2.063s user 0m2.191s sys 0m0.158s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tetgen_Regions_PyTest.py passed (as expected) ================================================= delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo ================================================= + echo 'delaundo_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt delaundo_PyTest.py test; + python -u delaundo_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 0m0.729s user 0m0.726s sys 0m0.458s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected) ================================================= Running.... CFD PyTests ================================================= + echo 'su2_and_AFLR2_NodeDist_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt su2_and_AFLR2_NodeDist_PyTest.py test; + python -u su2_and_AFLR2_NodeDist_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 224 224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 46 94 AFLR2 IG : Nodes, Faces = 92 186 AFLR2 IG : Nodes, Faces = 138 278 AFLR2 IG : Nodes, Faces = 184 370 AFLR2 IG : Nodes, Faces = 196 394 AFLR2 IG : Nodes, Faces = 224 450 AFLR2 IG : Nodes, Faces = 228 450 AFLR2 IG : Nodes, Faces = 224 224 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 224 224 AFLR2 GG : Nodes, Faces = 440 656 AFLR2 GG : Nodes, Faces = 649 1074 AFLR2 GG : Nodes, Faces = 853 1482 AFLR2 GG : Nodes, Faces = 1050 1876 AFLR2 GG : Nodes, Faces = 1238 2252 AFLR2 GG : Nodes, Faces = 1421 2618 AFLR2 GG : Nodes, Faces = 1594 2964 AFLR2 GG : Nodes, Faces = 1760 3296 AFLR2 GG : Nodes, Faces = 1915 3606 AFLR2 GG : Nodes, Faces = 2063 3902 AFLR2 GG : Nodes, Faces = 2202 4180 AFLR2 GG : Nodes, Faces = 2314 4404 AFLR2 GG : Nodes, Faces = 2423 4622 AFLR2 GG : Nodes, Faces = 2528 4832 AFLR2 GG : Nodes, Faces = 2634 5044 AFLR2 GG : Nodes, Faces = 2732 5240 AFLR2 GG : Nodes, Faces = 2831 5438 AFLR2 GG : Nodes, Faces = 2927 5630 AFLR2 GG : Nodes, Faces = 3018 5812 AFLR2 GG : Nodes, Faces = 3109 5994 AFLR2 GG : Nodes, Faces = 3202 6180 AFLR2 GG : Nodes, Faces = 3295 6366 AFLR2 GG : Nodes, Faces = 3386 6548 AFLR2 GG : Nodes, Faces = 3464 6704 AFLR2 GG : Nodes, Faces = 3535 6846 AFLR2 GG : Nodes, Faces = 3594 6964 AFLR2 GG : Nodes, Faces = 3639 7054 AFLR2 GG : Nodes, Faces = 3671 7118 AFLR2 GG : Nodes, Faces = 3691 7158 AFLR2 GG : Nodes, Faces = 3705 7186 AFLR2 GG : Nodes, Faces = 3712 7200 AFLR2 GG : Nodes, Faces = 3715 7206 AFLR2 : CPU Time = 0.004 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 3715 7206 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 3715 Number of elements = 7430 Number of tris = 7206 Number of quad = 0 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 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- 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. 3715 grid points. 7206 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). 78 boundary elements in index 3 (Marker = BC_5). 7206 triangles. 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 7206 TRIANGLE 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: 999.917. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 177.06. Mean K: 1.97231. Standard deviation K: 13.0434. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 63.4343| 90| | CV Face Area Aspect Ratio| 1| 5.23543| | CV Sub-Volume Ratio| 1| 3.11804| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 3715| 1/1.00| 10| | 1| 1048| 1/3.54| 7.96696| | 2| 298| 1/3.52| 6.37252| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.06136 m. Area projection in the x-plane = 0.178383 m, y-plane = 0.994925 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.138389 m. Min. coordinate in the x-direction = -0.000250564 m, y-direction = -0.0151999 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| 2.5576e-02| -0.385358| 2.453598| 1.625650| 5.369499| 0.360138| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.4625e-02| -0.512634| 2.087781| 1.374671| 4.973554| 1.183036| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.4397e-02| -0.792582| 1.733529| 1.142729| 4.657622| 3.896320| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.3771e-02| -0.880738| 1.486539| 1.023158| 4.334759| 14.592265| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.3775e-02| -0.987528| 1.351478| 0.932491| 4.191092| 111.166022| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 2.3772e-02| -1.104038| 1.188715| 0.874764| 3.951825| -483.924340| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 2.3625e-02| -1.178622| 1.124587| 0.844310| 3.820426| 127.331200| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 2.3443e-02| -1.243517| 1.097463| 0.824869| 3.768858| 40.162273| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 2.3468e-02| -1.287932| 1.075843| 0.810639| 3.733440| 25.154653| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 2.3221e-02| -1.300689| 1.046363| 0.775886| 3.684245| 21.097801| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.30069| < -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 352 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 = 0.650457 Cd = 0.030831 Cmz = 0.373226 Cx = 0.030831 Cy = 0.650457 Pressure Contribution Cl_p = 0.650457 Cd_p = 0.030831 Cmz_p = 0.373226 Cx_p = 0.030831 Cy_p = 0.650457 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m1.149s user 0m1.074s sys 0m0.536s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR2_NodeDist_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'su2_and_AFLR2_PyTest.py test;' su2_and_AFLR2_PyTest.py test; + python -u su2_and_AFLR2_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Saving geometry Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM 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 = 0.001 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 = 0.022 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 = 0.008 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 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- 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| 6.3291e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 6.2886e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 6.2476e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 6.2884e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 6.2724e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 6.2567e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 6.2170e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 6.1928e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 6.2088e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 6.2018e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.22124| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |CSV file |surface_flow_pyCAPS_su2_aflr2.csv | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary |flow_pyCAPS_su2_aflr2.szplt | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt| Error in tecFileWriterClose: Not all node map values for zone 1 have been written. Currently need 994 more values.0: Error finishing Tecplot file output. Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). +-----------------------------------------------------------------------+ --------------------------- Finalizing Solver --------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.072253 Cd = -0.01151 Cmz = 0.070975 Cx = -0.01151 Cy = 0.072253 Pressure Contribution Cl_p = 0.072253 Cd_p = -0.01151 Cmz_p = 0.070975 Cx_p = -0.01151 Cy_p = 0.072253 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m1.647s user 0m1.772s sys 0m0.552s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_AFLR4_AFLR3_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt su2_and_AFLR4_AFLR3_PyTest.py test; + python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 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 volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 38294 Number of elements = 220670 Number of triangles = 12448 Number of quadrilatarals = 0 Number of tetrahedrals = 208222 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wake 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...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.5901. Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 50 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 15.8114 m. Surface(s) where the force coefficients are evaluated and their reference origin for moment computation: - BC_1 (0, 0, 0). - BC_2 (0, 0, 0) m. Surface(s) plotted in the output file: BC_1, BC_2. Input mesh file name: ../aflr3/aflr3_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-8. 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| | PARAVIEW| 250| | SURFACE_PARAVIEW| 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_su2AFLRTest.dat. Surface file name: surface_flow_su2AFLRTest. Volume file name: flow_su2AFLRTest. Restart file name: restart_flow_su2AFLRTest.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| | | BC_2| +-----------------------------------------------------------------------+ | Far-field| BC_4| +-----------------------------------------------------------------------+ | Internal 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 ) ------------------- Three dimensional problem. 38294 grid points. 208222 volume elements. 4 surface markers. 6596 boundary elements in index 0 (Marker = BC_1). 5358 boundary elements in index 1 (Marker = BC_2). 74 boundary elements in index 2 (Marker = BC_3). 420 boundary elements in index 3 (Marker = BC_4). 208222 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.08667e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 4873.1. Mean K: 61.8586. Standard deviation K: 266.922. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 17.2334| 86.3276| | CV Face Area Aspect Ratio| 1.07899| 19318| | CV Sub-Volume Ratio| 1.06845| 686951| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 38294| 1/1.00| 10| | 1| 6362| 1/6.02| 8.24604| | 2| 1011| 1/6.29| 6.69971| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.90569 m. Wetted area = 118.038 m^2. Area projection in the x-plane = 11.1427 m^2, y-plane = 4.96714 m^2, z-plane = 55.4173 m^2. Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.582636 m. Min. coordinate in the x-direction = 0 m, y-direction = -7.90569 m, z-direction = -0.41192 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 226952| 1| m^2/s^2| 226952| | Velocity-X| 200.779| 1| m/s| 200.779| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 3.50461| 1| m/s| 3.50461| | Velocity Magnitude| 200.809| 1| m/s| 200.809| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.5901| +------------------------------------------------------------------------------+ 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| 7.1859e-01| -0.059021| 2.303387| 2.039067| 5.431874| 1.970398| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 7.1020e-01| 0.002899| 2.488448| 2.194491| 5.502382| 2.658900| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 7.0612e-01| 0.026727| 2.569164| 2.438598| 5.519932| 4.074903| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 7.0593e-01| -0.027928| 2.600852| 2.572666| 5.452520| 6.012667| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 7.0950e-01| -0.066798| 2.611567| 2.619922| 5.409363| 7.697173| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 7.0593e-01| -0.081876| 2.604321| 2.627463| 5.405669| 8.898085| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 7.0312e-01| -0.109417| 2.568028| 2.631615| 5.384249| 9.783851| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 7.0689e-01| -0.154243| 2.498102| 2.636523| 5.332167| 10.298250| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 7.0542e-01| -0.209194| 2.421734| 2.624341| 5.261991| 10.394140| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 7.0428e-01| -0.261272| 2.383246| 2.583148| 5.205405| 10.176655| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.261272| < -8| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_su2AFLRTest.dat | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |CSV file |surface_flow_su2AFLRTest.csv | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |Paraview |flow_su2AFLRTest.vtu | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |Paraview surface |surface_flow_su2AFLRTest.vtu | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.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 = 0.795414 Cd = 0.078161 Cmx = 0.000364 Cmy = -0.203015 Cmz = 0.000109 Cx = 0.064267 Cy = 0.000149 Cz = 0.796657 Pressure Contribution Cl_p = 0.795414 Cd_p = 0.078161 Cmx_p = 0.000364 Cmy_p = -0.203015 Cmz_p = 0.000109 Cx_p = 0.064267 Cy_p = 0.000149 Cz_p = 0.796657 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmx_v = 0.0 Cmy_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 Cz_v = 0.0 real 0m21.302s user 0m20.460s sys 0m0.548s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'su2_Morph_PyTest.py test;' su2_Morph_PyTest.py test; + python -u su2_Morph_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 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 volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 56425 Number of elements = 326721 Number of triangles = 15872 Number of quadrilatarals = 0 Number of tetrahedrals = 310849 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wake Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing SU2 surface file Writing SU2 Motion File - su2AFLRTest_motion.dat Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 15 - bcProps.surfaceProp[2].surfaceType = 1 - bcProps.surfaceProp[3].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...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.5901. Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 40 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 14.1421 m. Surface(s) where the force coefficients are evaluated and their reference origin for moment computation: - BC_1 (0, 0, 0). - BC_2 (0, 0, 0) m. Surface(s) plotted in the output file: BC_1, BC_2. Surface(s) affected by the design variables: BC_1, BC_2. Input mesh file name: ../volumeMesh/aflr3_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-8. 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| | PARAVIEW| 250| | SURFACE_PARAVIEW| 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_su2AFLRTest.dat. Surface file name: surface_flow_su2AFLRTest. Volume file name: flow_su2AFLRTest. Restart file name: restart_flow_su2AFLRTest.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| | | BC_2| +-----------------------------------------------------------------------+ | Far-field| BC_4| +-----------------------------------------------------------------------+ | Internal 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 ) ------------------- Three dimensional problem. 56425 grid points. 310849 volume elements. 4 surface markers. 9958 boundary elements in index 0 (Marker = BC_1). 5414 boundary elements in index 1 (Marker = BC_2). 80 boundary elements in index 2 (Marker = BC_3). 420 boundary elements in index 3 (Marker = BC_4). 310849 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.08667e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 5523.74. Mean K: 58.8177. Standard deviation K: 282.533. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 29.2241| 86.0517| | CV Face Area Aspect Ratio| 1.12536| 4445.2| | CV Sub-Volume Ratio| 1.02845| 57909.8| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 56425| 1/1.00| 10| | 1| 9299| 1/6.07| 8.22393| | 2| 1430| 1/6.5| 6.60902| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.07107 m. Wetted area = 96.2324 m^2. Area projection in the x-plane = 7.65774 m^2, y-plane = 4.21853 m^2, z-plane = 45.5887 m^2. Max. coordinate in the x-direction = 12.3872 m, y-direction = 7.07107 m, z-direction = 0.521791 m. Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.0650201 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 226952| 1| m^2/s^2| 226952| | Velocity-X| 200.779| 1| m/s| 200.779| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 3.50461| 1| m/s| 3.50461| | Velocity Magnitude| 200.809| 1| m/s| 200.809| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.5901| +------------------------------------------------------------------------------+ 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| 1.2503e+00| -0.459271| 1.871877| 1.655308| 5.031624| 0.762262| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.2168e+00| -0.456941| 2.040681| 1.747831| 5.043074| 1.447848| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.2125e+00| -0.398416| 2.120447| 1.970735| 5.091930| 3.304023| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.1986e+00| -0.382713| 2.165329| 2.106879| 5.096084| 7.146675| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.1960e+00| -0.387623| 2.192520| 2.179204| 5.084553| 12.977091| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.1981e+00| -0.395260| 2.209372| 2.208904| 5.080255| 20.307648| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.2023e+00| -0.386688| 2.193854| 2.231688| 5.091259| 28.440654| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.2028e+00| -0.387582| 2.150321| 2.255497| 5.085909| 33.542538| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.2040e+00| -0.424592| 2.094097| 2.270673| 5.038598| 31.887370| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.2029e+00| -0.488373| 2.035089| 2.263820| 4.964251| 26.644721| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.488373| < -8| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_su2AFLRTest.dat | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |CSV file |surface_flow_su2AFLRTest.csv | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |Paraview |flow_su2AFLRTest.vtu | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |Paraview surface |surface_flow_su2AFLRTest.vtu | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.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 = 0.522817 Cd = 0.019622 Projecting tessellation 1 (of 4) on to new body Projecting tessellation 2 (of 4) on to new body Projecting tessellation 3 (of 4) on to new body Projecting tessellation 4 (of 4) on to new body Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wake Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing SU2 surface file Writing SU2 Motion File - su2AFLRTest_motion.dat Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 15 - bcProps.surfaceProp[2].surfaceType = 1 - bcProps.surfaceProp[3].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Mesh Morphing...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, 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 . | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| | | BC_2| +-----------------------------------------------------------------------+ | Far-field| BC_4| +-----------------------------------------------------------------------+ | Internal boundary| BC_3| +-----------------------------------------------------------------------+ Three dimensional problem. 56425 grid points. 310849 volume elements. 4 surface markers. 9958 boundary elements in index 0 (Marker = BC_1). 5414 boundary elements in index 1 (Marker = BC_2). 80 boundary elements in index 2 (Marker = BC_3). 420 boundary elements in index 3 (Marker = BC_4). 310849 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. All volume elements are correctly orientend. All surface elements are correctly orientend. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 2.08667e+06. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Ignoring Convergence Field(s): RMS_DENSITY Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 5.669730 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Paraview |volume_deformed.vtu | |Paraview surface |surface_deformed.vtu | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.5901. Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 40 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 14.1421 m. Surface(s) where the force coefficients are evaluated and their reference origin for moment computation: - BC_1 (0, 0, 0). - BC_2 (0, 0, 0) m. Surface(s) plotted in the output file: BC_1, BC_2. Surface(s) affected by the design variables: BC_1, BC_2. Input mesh file name: aflr3_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-8. 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| | PARAVIEW| 250| | SURFACE_PARAVIEW| 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_su2AFLRTest.dat. Surface file name: surface_flow_su2AFLRTest. Volume file name: flow_su2AFLRTest. Restart file name: restart_flow_su2AFLRTest.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| | | BC_2| +-----------------------------------------------------------------------+ | Far-field| BC_4| +-----------------------------------------------------------------------+ | Internal 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 ) ------------------- Three dimensional problem. 56425 grid points. 310849 volume elements. 4 surface markers. 9958 boundary elements in index 0 (Marker = BC_1). 5414 boundary elements in index 1 (Marker = BC_2). 80 boundary elements in index 2 (Marker = BC_3). 420 boundary elements in index 3 (Marker = BC_4). 310849 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.08667e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 5523.56. Mean K: 58.7619. Standard deviation K: 282.437. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 26.9796| 85.7696| | CV Face Area Aspect Ratio| 1.13453| 4556.55| | CV Sub-Volume Ratio| 1.03232| 75345.6| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 56425| 1/1.00| 10| | 1| 9299| 1/6.07| 8.22393| | 2| 1430| 1/6.5| 6.60902| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.07107 m. Wetted area = 95.6308 m^2. Area projection in the x-plane = 9.17945 m^2, y-plane = 4.04295 m^2, z-plane = 44.962 m^2. Max. coordinate in the x-direction = 12.3585 m, y-direction = 7.07107 m, z-direction = 0.521791 m. Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.400127 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 226952| 1| m^2/s^2| 226952| | Velocity-X| 200.779| 1| m/s| 200.779| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 3.50461| 1| m/s| 3.50461| | Velocity Magnitude| 200.809| 1| m/s| 200.809| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.5901| +------------------------------------------------------------------------------+ 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| 1.0359e+00| -0.398750| 1.977474| 1.644084| 5.092145| 1.923782| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.0515e+00| -0.248975| 2.258948| 1.976579| 5.257848| 2.578720| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.0859e+00| -0.198142| 2.347683| 2.225644| 5.300689| 3.981171| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.1175e+00| -0.214514| 2.375555| 2.358260| 5.270011| 5.965906| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.1367e+00| -0.239435| 2.394864| 2.421022| 5.239901| 7.849147| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.1520e+00| -0.262371| 2.404237| 2.445537| 5.228001| 9.366346| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.1605e+00| -0.284513| 2.389017| 2.460376| 5.215548| 10.610658| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.1650e+00| -0.311476| 2.344163| 2.476241| 5.184871| 11.527148| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.1733e+00| -0.361259| 2.273271| 2.486137| 5.118277| 12.003369| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.1800e+00| -0.414971| 2.206048| 2.472056| 5.049690| 12.052158| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.414971| < -8| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_su2AFLRTest.dat | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |CSV file |surface_flow_su2AFLRTest.csv | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |Paraview |flow_su2AFLRTest.vtu | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |Paraview surface |surface_flow_su2AFLRTest.vtu | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.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 = 0.884977 Cd = 0.073429 real 0m52.825s user 0m51.042s sys 0m1.677s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_Morph_PyTest.py passed (as expected) ================================================= delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo ================================================= + echo 'su2_and_Delaundo_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt su2_and_Delaundo_PyTest.py test; + python -u su2_and_Delaundo_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 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 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 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 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 Warning: No boundary condition specified for capsGroup 2DSlice! 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 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- 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: ../delaundo/delaundo_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_su2_CAPS.dat. Surface file name: surface_flow_su2_CAPS. Volume file name: flow_su2_CAPS. Restart file name: restart_flow_su2_CAPS.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. 6317 grid points. 12340 volume elements. 5 surface markers. 24 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_2). 24 boundary elements in index 3 (Marker = BC_4). 198 boundary elements in index 4 (Marker = BC_5). 12340 triangles. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. There has been a re-orientation of 294 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 999.917. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 45.3524| 89.2595| | CV Face Area Aspect Ratio| 1.03245| 15.7138| | CV Sub-Volume Ratio| 1| 7.93643| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 6317| 1/1.00| 10| | 1| 1792| 1/3.53| 7.98923| | 2| 509| 1/3.52| 6.38684| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.07206 m. Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m. Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_5 is NOT a single straight. Boundary marker BC_2 is 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| 4.3858e-02| -1.163068| 1.073873| 1.341547| 4.312268| 0.062082| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.1182e-02| -1.558471| 0.813117| 0.969484| 3.926501| 0.143132| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.1802e-02| -1.599269| 0.950037| 1.012154| 3.879885| 0.386300| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.1790e-02| -1.661284| 1.005970| 1.023067| 3.797319| 0.981260| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.9851e-02| -1.658421| 1.009907| 0.965279| 3.792658| 2.399755| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 4.9582e-02| -1.630602| 0.996801| 0.859556| 3.833204| 6.390579| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 4.9344e-02| -1.628009| 1.002770| 0.822847| 3.846297| 27.872536| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 4.9188e-02| -1.646113| 1.024424| 0.882502| 3.830202| -48.293527| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 4.8755e-02| -1.672152| 1.033657| 0.939200| 3.797228| -22.113788| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 4.8694e-02| -1.695131| 1.018255| 0.944150| 3.765919| -19.281368| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.69513| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_su2_CAPS.dat | Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat). |CSV file |surface_flow_su2_CAPS.csv | Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat). |Tecplot binary |flow_su2_CAPS.szplt | Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat). |Tecplot binary surface |surface_flow_su2_CAPS.szplt | Error in tecFileWriterClose: Not all node map values for zone 1 have been written. Currently need 492 more values.0: Error finishing Tecplot file output. Writing the forces breakdown file (forces_breakdown_su2_CAPS.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 = 0.805707 Cd = -0.041787 Cmz = 0.408515 Cx = -0.041787 Cy = 0.805707 Pressure Contribution Cl_p = 0.805707 Cd_p = -0.041787 Cmz_p = 0.408515 Cx_p = -0.041787 Cy_p = 0.805707 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m1.583s user 0m1.515s sys 0m0.562s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_Tetgen_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt su2_and_Tetgen_PyTest.py test; + python -u su2_and_Tetgen_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 = 258 Number of elements = 512 Number of triangle elements = 512 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3130 Total number of elements = 6248 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 - 3130, elements - 6248 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.014526 Creating surface mesh ... Surface mesh seconds: 0.003903 Recovering boundaries... Boundary recovery seconds: 0.051689 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.003734 Suppressing Steiner points ... Steiner suppression seconds: 7e-06 Recovering Delaunayness... Delaunay recovery seconds: 0.007143 Refining mesh... 4180 insertions, added 2142 points, 134947 tetrahedra in queue. 1391 insertions, added 431 points, 139550 tetrahedra in queue. 1855 insertions, added 477 points, 138154 tetrahedra in queue. 2472 insertions, added 613 points, 122807 tetrahedra in queue. 3296 insertions, added 507 points, 67228 tetrahedra in queue. 4393 insertions, added 431 points, 1310 tetrahedra in queue. Refinement seconds: 0.393548 Smoothing vertices... Mesh smoothing seconds: 0.2719 Improving mesh... Mesh improvement seconds: 0.007729 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000798 Total running seconds: 0.755132 Statistics: Input points: 3130 Input facets: 6248 Input segments: 9372 Input holes: 2 Input regions: 0 Mesh points: 8227 Mesh tetrahedra: 40661 Mesh faces: 84447 Mesh faces on exterior boundary: 6250 Mesh faces on input facets: 6250 Mesh edges on input segments: 9373 Steiner points on input segments: 1 Steiner points inside domain: 5096 Done meshing using TetGen! Volume mesher did not preserve surface elements - data transfer will NOT be possible. 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...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.5901. Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 50 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 15.8114 m. Surface(s) where the force coefficients are evaluated and their reference origin for moment computation: - BC_1 (0, 0, 0). - BC_2 (0, 0, 0) m. Surface(s) plotted in the output file: BC_1, BC_2. Input mesh file name: ../myMesh/tetgen_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: 5. 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| | PARAVIEW| 250| | SURFACE_PARAVIEW| 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_Tetgen.dat. Surface file name: surface_flow_pyCAPS_SU2_Tetgen. Volume file name: flow_pyCAPS_SU2_Tetgen. Restart file name: restart_flow_pyCAPS_SU2_Tetgen.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| | | BC_2| +-----------------------------------------------------------------------+ | Far-field| 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 ) ------------------- Three dimensional problem. 8227 grid points. 40661 volume elements. 3 surface markers. 4468 boundary elements in index 0 (Marker = BC_1). 1270 boundary elements in index 1 (Marker = BC_2). 512 boundary elements in index 2 (Marker = BC_3). 40661 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.08741e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 414.134. Mean K: 30.6158. Standard deviation K: 37.5195. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 2.25569| 83.562| | CV Face Area Aspect Ratio| 1.40614| 7154.17| | CV Sub-Volume Ratio| 1.02596| 261709| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 8227| 1/1.00| 10| | 1| 1360| 1/6.05| 8.23235| | 2| 235| 1/5.79| 6.87793| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.90569 m. Wetted area = 120.046 m^2. Area projection in the x-plane = 10.7914 m^2, y-plane = 4.5843 m^2, z-plane = 57.287 m^2. Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m. Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 226952| 1| m^2/s^2| 226952| | Velocity-X| 200.779| 1| m/s| 200.779| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 3.50461| 1| m/s| 3.50461| | Velocity Magnitude| 200.809| 1| m/s| 200.809| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.5901| +------------------------------------------------------------------------------+ 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| 1.2550e-01| 0.614349| 3.046325| 2.089422| 6.105244| 1.831854| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.2494e-01| 0.764583| 3.258604| 2.974732| 6.265552| 2.165840| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.2399e-01| 0.642409| 3.278261| 3.214494| 6.139447| 3.169947| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.2384e-01| 0.541917| 3.250446| 3.272037| 6.028748| 4.533401| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.2373e-01| 0.535101| 3.187480| 3.218588| 6.011712| 5.728616| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 0.535101| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_pyCAPS_SU2_Tetgen.dat | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat). |CSV file |surface_flow_pyCAPS_SU2_Tetgen.csv | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat). |Paraview |flow_pyCAPS_SU2_Tetgen.vtu | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat). |Paraview surface |surface_flow_pyCAPS_SU2_Tetgen.vtu | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.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 = 0.763097 Cd = 0.133208 Cmx = -0.004493 Cmy = -0.215511 Cmz = 0.000816 Cx = 0.11987 Cy = 0.0005 Cz = 0.765306 real 0m3.380s user 0m3.406s sys 0m0.343s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_X43a_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt su2_X43a_PyTest.py test; + python -u su2_X43a_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = fuselage, index = 1 Name = verticalCS, index = 2 Name = fuselage_base, index = 3 Name = horizontalCS, index = 4 Name = inlet, index = 5 Name = hollowInlet, index = 6 Name = Farfield, index = 7 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 = 3808 Number of elements = 7616 Number of triangle elements = 7616 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 5678 Number of elements = 11352 Number of triangle elements = 11352 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9486 Total number of elements = 18968 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = fuselage, index = 1 Name = verticalCS, index = 2 Name = fuselage_base, index = 3 Name = horizontalCS, index = 4 Name = inlet, index = 5 Name = hollowInlet, index = 6 Name = Farfield, index = 7 Number of surface: nodes - 9486, elements - 18968 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.038681 Creating surface mesh ... Surface mesh seconds: 0.009625 Recovering boundaries... Warning: 2 segments are not recovered. Boundary recovery seconds: 0.144083 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.010911 Suppressing Steiner points ... Steiner suppression seconds: 8e-06 Recovering Delaunayness... Delaunay recovery seconds: 0.020629 Refining mesh... 12647 insertions, added 5230 points, 2965 tetrahedra in queue. Refinement seconds: 0.420143 Smoothing vertices... Mesh smoothing seconds: 0.341678 Improving mesh... Mesh improvement seconds: 0.012952 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.002731 Total running seconds: 1.00171 Statistics: Input points: 9486 Input facets: 18968 Input segments: 28452 Input holes: 6 Input regions: 0 Mesh points: 14837 Mesh tetrahedra: 61060 Mesh faces: 131604 Mesh faces on exterior boundary: 18968 Mesh faces on input facets: 18968 Mesh edges on input segments: 28452 Steiner points inside domain: 5351 Done meshing using TetGen! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - fuselage Boundary condition name - fuselage_base Boundary condition name - hollowInlet Boundary condition name - horizontalCS Boundary condition name - inlet Boundary condition name - verticalCS Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 - bcProps.surfaceProp[3].surfaceType = 1 - bcProps.surfaceProp[4].surfaceType = 1 - bcProps.surfaceProp[5].surfaceType = 1 - bcProps.surfaceProp[6].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...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 3.5. Angle of attack (AoA): 3 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. Surface(s) where the force coefficients are evaluated and their reference origin for moment computation: - BC_1 (0, 0, 0). - BC_3 (0, 0, 0). - BC_4 (0, 0, 0). - BC_2 (0, 0, 0). - BC_5 (0, 0, 0). - BC_6 (0, 0, 0) m. Surface(s) plotted in the output file: BC_1, BC_3, BC_6, BC_4, BC_5, BC_2. Input mesh file name: ../myMesh/tetgen_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: 5. 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| | PARAVIEW| 250| | SURFACE_PARAVIEW| 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_x43a_Test.dat. Surface file name: surface_flow_x43a_Test. Volume file name: flow_x43a_Test. Restart file name: restart_flow_x43a_Test.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| | | BC_3| | | BC_6| | | BC_4| | | BC_5| | | BC_2| +-----------------------------------------------------------------------+ | Far-field| BC_7| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 14837 grid points. 61060 volume elements. 7 surface markers. 4460 boundary elements in index 0 (Marker = BC_1). 1682 boundary elements in index 1 (Marker = BC_2). 92 boundary elements in index 2 (Marker = BC_3). 696 boundary elements in index 3 (Marker = BC_4). 434 boundary elements in index 4 (Marker = BC_5). 252 boundary elements in index 5 (Marker = BC_6). 11352 boundary elements in index 6 (Marker = BC_7). 61060 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.67745e+08. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 95.6599. Mean K: 0.6569. Standard deviation K: 2.74489. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.041314| 84.1309| | CV Face Area Aspect Ratio| 1.66509| 8739.77| | CV Sub-Volume Ratio| 1| 1.06812e+07| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 14837| 1/1.00| 10| | 1| 2949| 1/5.03| 8.75388| | 2| 771| 1/3.82| 8.39625| +-------------------------------------------+ Finding max control volume width. Semi-span length = 30 m. Wetted area = 13761 m^2. Area projection in the x-plane = 776.902 m^2, y-plane = 2106.32 m^2, z-plane = 5468.8 m^2. Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m. Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Boundary marker BC_3 is a single plane. Boundary marker BC_6 is NOT a single plane. Boundary marker BC_4 is NOT a single plane. Boundary marker BC_5 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 916077| 1| m^2/s^2| 916077| | Velocity-X| 1189.41| 1| m/s| 1189.41| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 62.3342| 1| m/s| 62.3342| | Velocity Magnitude| 1191.04| 1| m/s| 1191.04| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 3.5| +------------------------------------------------------------------------------+ 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| 2.7920e-01| 2.731580| 5.652568| 4.717779| 8.731055| -0.598944| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.7393e-01| 3.160279| 6.272701| 5.760915| 9.118543| -0.210439| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.7948e-01| 3.354228| 6.489942| 5.827928| 9.330964| -0.113496| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.8530e-01| 3.254338| 6.351828| 5.711746| 9.239524| -0.118542| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.8785e-01| 3.176424| 6.240821| 5.574708| 9.151588| -0.137089| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 3.17642| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_x43a_Test.dat | Writing the forces breakdown file (forces_breakdown_x43a_Test.dat). |CSV file |surface_flow_x43a_Test.csv | Writing the forces breakdown file (forces_breakdown_x43a_Test.dat). |Paraview |flow_x43a_Test.vtu | Writing the forces breakdown file (forces_breakdown_x43a_Test.dat). |Paraview surface |surface_flow_x43a_Test.vtu | Writing the forces breakdown file (forces_breakdown_x43a_Test.dat). +-----------------------------------------------------------------------+ Warning: there are 184 non-physical points in the solution. Warning: 87 reconstructed states for upwinding are non-physical. --------------------------- 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 = -13.538631 Cd = 98.758301 Cmx = 8.179386 Cmy = 10547.449834 Cmz = -80.129826 Cx = 99.331513 Cy = -1.05082 Cz = -8.351467 real 0m6.852s user 0m8.620s sys 0m0.974s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected) ================================================= ./execute_PyTestRegression.sh: line 413: ulimit: stack size: cannot modify limit: Operation not permitted flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC//flowCart ================================================= + echo 'cart3d_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt cart3d_PyTest.py test; + python -u cart3d_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Loading AIM Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.796888 Tessellating body 1 with MaxEdge = 0.094922 Sag = 0.003797 Angle = 15.000000 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9 > autoInputs.out Executing: ./aero.csh > aero.out C_A 0.023693377 C_Y -0.0012129281 C_N 0.065395002 C_D 0.025961197 C_S -0.0012129281 C_L 0.064528279 C_l 0.0510971 C_m 0.000248187 C_n -0.017525 C_M_x 0.0504544 C_M_y 0.000248187 C_M_z -0.0192976 real 0m16.203s user 0m28.146s sys 0m1.087s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected) ================================================= ================================================= + echo 'cart3d_OpenMDAO_3_alpha_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt cart3d_OpenMDAO_3_alpha_PyTest.py test; + python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt ---------------------------------------- >>> alpha [2.] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - alpha Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - CL2 Done getting CFD functional Body size = 3.625615 Tessellating body 1 with MaxEdge = 0.090640 Sag = 0.003626 Angle = 15.000000 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7 -mesh2d > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:15:08) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1 (00:15:12) aero.csh done o case M0.5901A2B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.01631562] CL 0.12773309 ---------------------------------------- ---------------------------------------- >>> alpha [2.] >>> CL2 [0.01631562] CL 0.12773309 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:15:13) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1 (00:15:16) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:15:17) Linearizing cut-cells (00:15:17) ... done o Number of simultaneous xsensit jobs: 1 (00:15:17) Computing gradients (00:15:21) ... done o case M0.5901A2B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[0.01572627]] ======================================== RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 1.63156D-02 |proj g|= 1.57263D-02 ---------------------------------------- >>> alpha [1.98427373] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:15:22) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1 (00:15:25) aero.csh done o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.01606724] CL 0.12675617 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:15:26) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1 (00:15:29) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:15:30) Linearizing cut-cells (00:15:30) ... done o Number of simultaneous xsensit jobs: 1 (00:15:30) Computing gradients (00:15:34) ... done o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[0.01560329]] ======================================== At iterate 1 f= 1.60672D-02 |proj g|= 1.56033D-02 ---------------------------------------- >>> alpha [-0.01099175] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:15:35) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1 (00:15:38) aero.csh done o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s) >>> CL2 [6.05653711e-06] CL 0.00246101 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:15:39) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1 (00:15:42) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:15:43) Linearizing cut-cells (00:15:43) ... done o Number of simultaneous xsensit jobs: 1 (00:15:43) Computing gradients (00:15:47) ... done o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[0.00031042]] ======================================== At iterate 2 f= 6.05654D-06 |proj g|= 3.10424D-04 ---------------------------------------- >>> alpha [-0.05149286] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:15:48) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1 (00:15:51) aero.csh done o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s) >>> CL2 [2.59817062e-10] CL 1.612e-05 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:15:51) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1 (00:15:55) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:15:55) Linearizing cut-cells (00:15:55) ... done o Number of simultaneous xsensit jobs: 1 (00:15:55) Computing gradients (00:15:59) ... done o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[2.03612433e-06]] ======================================== At iterate 3 f= 2.59817D-10 |proj g|= 2.03612D-06 ---------------------------------------- >>> alpha [-0.05176027] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:16:00) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1 (00:16:03) aero.csh done o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s) >>> CL2 [9.25766089e-15] CL 1e-07 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:16:04) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1 (00:16:08) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:16:08) Linearizing cut-cells (00:16:08) ... done o Number of simultaneous xsensit jobs: 1 (00:16:08) Computing gradients (00:16:12) ... done o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[1.21372408e-08]] ======================================== At iterate 4 f= 9.25766D-15 |proj g|= 1.21372D-08 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 4 5 4 0 0 1.214D-08 9.258D-15 F = 9.2576608860000000E-015 CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL Optimization Complete ----------------------------------- Optimized value: [-0.05176027] real 1m6.569s user 0m55.186s sys 0m9.777s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_alpha_PyTest.py passed (as expected) ================================================= ================================================= + echo 'cart3d_OpenMDAO_3_twist_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt cart3d_OpenMDAO_3_twist_PyTest.py test; + python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt ---------------------------------------- >>> twist [4.] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - CL2 Done getting CFD functional Body size = 3.630958 Tessellating body 1 with MaxEdge = 0.018155 Sag = 0.000908 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:16:16) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:16:30) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.00411365] CL 0.0641354 ---------------------------------------- ---------------------------------------- >>> twist [4.] >>> CL2 [0.00411365] CL 0.0641354 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:16:31) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:16:51) aero.csh done Max memory allowed: 32 GB Flow hexes: 37528 Estimated cutter memory: 0.003753 GB / DV Estimated xsensit memory: 0.071303 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:16:52) Linearizing cut-cells (00:16:54) ... done o Number of simultaneous xsensit jobs: 1 (00:16:54) Computing gradients (00:16:58) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[0.00210056]] ======================================== RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 4.11365D-03 |proj g|= 2.10056D-03 ---------------------------------------- >>> twist [3.99789944] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.630955 Tessellating body 1 with MaxEdge = 0.018155 Sag = 0.000908 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:17:00) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:17:10) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.0041123] CL 0.0641197 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:17:11) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:17:28) aero.csh done Max memory allowed: 32 GB Flow hexes: 37527 Estimated cutter memory: 0.003753 GB / DV Estimated xsensit memory: 0.071301 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:17:28) Linearizing cut-cells (00:17:30) ... done o Number of simultaneous xsensit jobs: 1 (00:17:30) Computing gradients (00:17:34) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[0.00210014]] ======================================== At iterate 1 f= 4.11230D-03 |proj g|= 2.10014D-03 ---------------------------------------- >>> twist [-6.51746279] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.635732 Tessellating body 1 with MaxEdge = 0.018179 Sag = 0.000909 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:17:36) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:17:51) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.00998113] CL -0.0999038 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:17:52) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:18:11) aero.csh done Max memory allowed: 32 GB Flow hexes: 37089 Estimated cutter memory: 0.003709 GB / DV Estimated xsensit memory: 0.070469 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:18:12) Linearizing cut-cells (00:18:14) ... done o Number of simultaneous xsensit jobs: 1 (00:18:14) Computing gradients (00:18:18) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[-0.00319688]] ======================================== ---------------------------------------- >>> twist [-0.14346249] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.625762 Tessellating body 1 with MaxEdge = 0.018129 Sag = 0.000906 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:18:20) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:18:34) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [4.79392927e-08] CL -0.00022338 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:18:35) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:18:54) aero.csh done Max memory allowed: 32 GB Flow hexes: 37755 Estimated cutter memory: 0.003776 GB / DV Estimated xsensit memory: 0.071735 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:18:54) Linearizing cut-cells (00:18:56) ... done o Number of simultaneous xsensit jobs: 1 (00:18:56) Computing gradients (00:19:01) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[-7.2473947e-06]] ======================================== At iterate 2 f= 4.79393D-08 |proj g|= 7.24739D-06 ---------------------------------------- >>> twist [-0.12922018] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.625747 Tessellating body 1 with MaxEdge = 0.018129 Sag = 0.000906 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:19:02) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:19:17) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [2.18169714e-08] CL 0.00015117 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:19:18) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:19:38) aero.csh done Max memory allowed: 32 GB Flow hexes: 37755 Estimated cutter memory: 0.003776 GB / DV Estimated xsensit memory: 0.071735 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:19:38) Linearizing cut-cells (00:19:40) ... done o Number of simultaneous xsensit jobs: 1 (00:19:40) Computing gradients (00:19:44) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[4.89190887e-06]] ======================================== At iterate 3 f= 2.18170D-08 |proj g|= 4.89191D-06 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 3 5 3 0 0 4.892D-06 2.182D-08 F = 2.1816971420000000E-008 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-0.12922018] real 3m32.014s user 5m10.137s sys 0m13.890s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py passed (as expected) ================================================= ================================================= + echo 'fun3d_Morph_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt fun3d_Morph_PyTest.py test; + python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 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 = 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 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 82829 Number of elements = 483649 Number of triangles = 15680 Number of quadrilatarals = 0 Number of tetrahedrals = 467969 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file 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 - 2 Design Variable name - Alpha Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Cd2 Objective name - Const Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha 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/fun3dAFLRTest_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_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 = 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/fun3dAFLRTest_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_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 real 0m8.449s user 0m8.066s sys 0m0.545s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case fun3d_Morph_PyTest.py passed (as expected) ================================================= Running.... STRUCTURE PyTests ================================================= + echo 'masstran_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 3.428666259749 Mass 5383.006027806 Centroid [1.222256036872, 0.1634981473779, -4.647736192456e-11] CG [1.222256036872, 0.1634981473779, -4.647907951721e-11] Ixx 22133.97306031 Iyy 23448.30046704 Izz 1389.213122564 Ixy 164.2055275655 Ixz -7.485782319314e-06 Iyz 1.710545499156e-06 I [22133.97306031, 23448.30046704, 1389.213122564, 164.2055275655, -7.485782319314e-06, 1.710545499156e-06] II [[22133.97306031, -164.2055275655, 7.485782319314e-06], [-164.2055275655, 23448.30046704, -1.710545499156e-06], [7.485782319314e-06, -1.710545499156e-06, 1389.213122564]] real 0m4.378s user 0m5.832s sys 0m12.199s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected) ================================================= ================================================= + echo 'masstran_AGARD445_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt masstran_AGARD445_PyTest.py test; + python -u masstran_AGARD445_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results mass properties..... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = constEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 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 = yatesPlate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 36 Number of elements = 25 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 25 Getting FEA materials....... Number of materials - 1 Material name - Mahogany Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - yatesPlate Done getting FEA properties Updating mesh element types based on properties input Area 547.7004 Mass 0.01605224431138 Centroid [20.03586282449, 14.01686746988, 0.0] CG [20.03586282449, 14.01686746988, 0.0] Ixx 1.140246300554 Iyy 0.919317482675 Izz 2.059563783229 Ixy 0.7352134614013 Ixz 0.0 Iyz 0.0 I [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0] II [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]] real 0m0.375s user 0m0.460s sys 0m0.119s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected) ================================================= ================================================= + echo 'hsm_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt hsm_SingleLoadCase_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u hsm_SingleLoadCase_PyTest.py -outLevel=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 = 1 Name = plateEdge, index = 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 0m0.496s user 0m0.724s sys 0m0.072s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo 'hsm_CantileverPlate_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt hsm_CantileverPlate_PyTest.py test; + python -u hsm_CantileverPlate_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = plate, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - plate Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plateTip, 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 = 40 Number of elements = 51 Elemental Tria3 = 0 Elemental Quad4 = 27 Getting FEA materials....... Number 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 - appliedLoad 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 = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 4 ->HSMSOL Matrix Non-zero Entries = 1313 Converging HSM equation system ... iter dr dd dp rlx max 1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00) 1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.03 0.00) 2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00) 3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00) 4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00) 5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.07 0.00) 6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.07 0.00) 7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00) 8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.00 0.00) 9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.10 0.00) 10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) iter dr dd dp rlx max 11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.00 0.00) 11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.00 0.00) 12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.07 0.00) 13* 0.336E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.10 0.00) 15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00) 16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.00 0.00) 17 0.148E-15 0.575E-15 0.104E-14 1.000 dps @ ( 1.00 0.10 0.00) Converging n vectors ... it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 ) it = 2 dn = 0.423E-15 rlx = 1.000 ( 31 ) Converging e1,e2 vectors ... it = 1 de = 0.285E+01 rlx = 0.351 ( 24 ) it = 2 de = 0.269E+01 rlx = 0.372 ( 14 ) it = 3 de = 0.202E+01 rlx = 0.494 ( 40 ) it = 4 de = 0.122E+01 rlx = 0.820 ( 40 ) it = 5 de = 0.378E+00 rlx = 1.000 ( 40 ) it = 6 de = 0.127E-01 rlx = 1.000 ( 14 ) it = 7 de = 0.524E-06 rlx = 1.000 ( 40 ) it = 8 de = 0.938E-16 rlx = 1.000 ( 22 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMCantileverPlate.dat real 0m0.403s user 0m0.585s sys 0m0.072s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected) ================================================= ASTROS_ROOT: /Users/jenkins/util/astros/Astros/Darwin-64bit ================================================= + echo 'astros_Aeroelastic_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_Aeroelastic_PyTest.py test; + python -u astros_Aeroelastic_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 1 Name = Rib_Root_Point, index = 1 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 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 366 Number of elements = 523 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 190 Elemental Quad4 = 333 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 = 367 Combined Number of elements = 524 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 190 Combined Elemental Quad4 = 333 Getting vortex lattice surface data VLM surface name - Skin_Top 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 Surface 1: Number of points found for aero-spline = 48 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Getting Aero Reference Parameters....... Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Ribs No "material" specified for Property tuple Ribs, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Property name - Spar1 No "material" specified for Property tuple Spar1, defaulting to an index of 1 Property name - Spar2 No "material" specified for Property tuple Spar2, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 43 automatic connections were made for capsConnect Rib_Root (node id 367) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m8.055s user 0m14.066s sys 0m6.279s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_AGARD445_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_AGARD445_PyTest.py test; + python -u astros_AGARD445_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results natural frequencies..... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = constEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = yatesPlate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 36 Number of elements = 25 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 25 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Mahogany Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - yatesPlate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 2 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Natural freq (Mode 1) = 5.78 (Hz) Natural freq (Mode 2) = 30.66 (Hz) real 0m0.569s user 0m0.678s sys 0m0.176s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_Composite_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_Composite_PyTest.py test; + python -u astros_Composite_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = plate, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - plate Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plateTip, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 15 Number of elements = 8 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 8 Aero_Reference value is NULL - No aero reference parameters set 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 - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - cantilever No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards real 0m0.665s user 0m0.773s sys 0m0.171s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_Composite_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_CompositeWingFreq_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_CompositeWingFreq_PyTest.py test; + python -u astros_CompositeWingFreq_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results for natural frequencies..... Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = wing, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - wing Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = wing, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = wing, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 443 Number of elements = 845 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 845 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Aluminum No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic" Material name - Graphite_epoxy Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - root No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Natural freq (Mode 1) = 5.90553 (Hz) Natural freq (Mode 2) = 29.72860 (Hz) Natural freq (Mode 3) = 39.11840 (Hz) Natural freq (Mode 4) = 77.46400 (Hz) Natural freq (Mode 5) = 99.53050 (Hz) Natural freq (Mode 6) = 146.35200 (Hz) Natural freq (Mode 7) = 178.74700 (Hz) Natural freq (Mode 8) = 234.29900 (Hz) Natural freq (Mode 9) = 278.97300 (Hz) Natural freq (Mode 10) = 313.52300 (Hz) Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 real 0m30.168s user 0m29.686s sys 0m0.622s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_CompositeWingFreq_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'astros_Flutter_15degree.py test;' astros_Flutter_15degree.py test; + python -u astros_Flutter_15degree.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 = Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Root_Point, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = WingSurface, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 96 Number of elements = 77 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 77 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 = 97 Combined Number of elements = 78 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 77 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 96 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - aluminum No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Body Property name - Edge Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - PointConstraint No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Getting FEA connections....... Number of connection tuples - 1 Connection name - Root No "groupName" specified for Connection tuple Root! Looking for automatic connections from the use of capsConnectLink for Root 8 automatic connections were made for capsConnect Root (node id 97) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Flutter Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aero card Writing analysis cards Writing constraint cards--each subcase individually Writing material cards Writing property cards Writing unsteady aeroelastic cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m0.970s user 0m0.983s sys 0m0.284s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected) ================================================= ================================================= + echo 'astros_MultipleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_MultipleLoadCase_PyTest.py test; + python -u astros_MultipleLoadCase_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 16 Number of elements = 9 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 9 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 5 Load name - load_0 Load name - load_1 Load name - load_2 Load name - load_3 Load name - load_4 Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 5 Analysis name - load_0 Analysis name - load_1 Analysis name - load_2 Analysis name - load_3 Analysis name - load_4 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case load_0, assuming all constraints are applied!!!! Warning: No constraints specified for case load_1, assuming all constraints are applied!!!! Warning: No constraints specified for case load_2, assuming all constraints are applied!!!! Warning: No constraints specified for case load_3, assuming all constraints are applied!!!! Warning: No constraints specified for case load_4, assuming all constraints are applied!!!! Writing analysis cards Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m0.805s user 0m0.847s sys 0m0.217s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_MultipleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_PyTest.py test; + python -u astros_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results for natural frequencies..... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 293 Number of elements = 217 Number of triangle elements = 0 Number of quadrilateral elements = 217 ---------------------------- Total number of nodes = 293 Total number of elements = 217 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Constraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 293 Number of elements = 217 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 217 Aero_Reference value is NULL - No aero reference parameters set 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 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Natural freq (Mode 1) = 0.02335 (Hz) Natural freq (Mode 2) = 0.02335 (Hz) Natural freq (Mode 3) = 0.11619 (Hz) Natural freq (Mode 4) = 0.11619 (Hz) Natural freq (Mode 5) = 0.14468 (Hz) Natural freq (Mode 6) = 0.14468 (Hz) Natural freq (Mode 7) = 0.23352 (Hz) Natural freq (Mode 8) = 0.23352 (Hz) Natural freq (Mode 9) = 0.30497 (Hz) Natural freq (Mode 10) = 0.30497 (Hz) real 0m11.045s user 0m12.180s sys 0m8.983s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_SingleLoadCase_PyTest.py test; + python -u astros_SingleLoadCase_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 6 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 6 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m0.668s user 0m0.772s sys 0m0.186s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_ThreeBarFreq_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_ThreeBarFreq_PyTest.py test; + python -u astros_ThreeBarFreq_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results for natural frequencies..... WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 2 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Natural freq (Mode 1) = 86.13400 (Hz) Natural freq (Mode 2) = 168.53300 (Hz) real 0m0.662s user 0m0.774s sys 0m0.172s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_ThreeBarLinkDesign_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_ThreeBarLinkDesign_PyTest.py test; + python -u astros_ThreeBarLinkDesign_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedForce Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Getting FEA design variables....... Number of design variables - 3 Design_Variable name - Bar1A Design_Variable name - Bar2A Design_Variable name - Bar3A Design_Variable_Relation name - Bar1A Design_Variable_Relation name - Bar2A Design_Variable_Relation name - Bar3A Number of design variable relations - 3 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 3 Design_Constraint name - stress1 Design_Constraint name - stress2 Design_Constraint name - stress3 Done getting FEA design constraints Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing design constraint cards Writing load cards Writing material cards Writing property cards Writing design variable cards Running Astros...... Done running Astros! real 0m0.783s user 0m0.863s sys 0m0.191s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_ThreeBarLinkDesign_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_ThreeBarMultiLoad_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_ThreeBarMultiLoad_PyTest.py test; + python -u astros_ThreeBarMultiLoad_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 2 Constraint name - conOne No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement" Constraint name - conTwo No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - loadOne Load name - loadTwo Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 2 Analysis name - analysisOne Analysis name - analysisTwo Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards real 0m0.696s user 0m0.776s sys 0m0.189s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_ThreeBar_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_ThreeBar_PyTest.py test; + python -u astros_ThreeBar_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedForce Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards real 0m0.641s user 0m0.772s sys 0m0.170s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_Trim_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_Trim_15degree.py test; + python -u astros_Trim_15degree.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 = Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Root_Point, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = WingSurface, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 96 Number of elements = 77 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 77 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 = 97 Combined Number of elements = 78 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 77 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 96 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - aluminum No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - Body Property name - Edge Property name - Root Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - PointConstraint No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - PointSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Root No "groupName" specified for Connection tuple Root! Looking for automatic connections from the use of capsConnectLink for Root 8 automatic connections were made for capsConnect Root (node id 97) Done getting FEA connections Getting FEA loads....... Number of loads - 2 Load name - GravityLoad No "groupName" specified for Load tuple GravityLoad, going to use load name Load name - PointLoad Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m0.963s user 0m0.981s sys 0m0.269s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected) ================================================= ================================================= + echo 'nastran_AGARD445_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_AGARD445_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u nastran_AGARD445_PyTest.py -outLevel=0 -noAnalysis Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = yatesPlate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 49 Number of elements = 36 Number of triangle elements = 0 Number of quadrilateral elements = 36 ---------------------------- Total number of nodes = 49 Total number of elements = 36 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = constEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = yatesPlate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 49 Number of elements = 36 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 36 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Mahogany Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - yatesPlate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Warning: No loads specified for case EigenAnalysis!!!! Writing mass increment cards Writing analysis cards, 0 Writing combined constraint cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! Getting results natural frequencies..... Reading Nastran FO6 file - extracting Eigen-Values! Number of Eigen-Values = 132 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Loading Eigen-Value = 11 Loading Eigen-Value = 12 Loading Eigen-Value = 13 Loading Eigen-Value = 14 Loading Eigen-Value = 15 Loading Eigen-Value = 16 Loading Eigen-Value = 17 Loading Eigen-Value = 18 Loading Eigen-Value = 19 Loading Eigen-Value = 20 Loading Eigen-Value = 21 Loading Eigen-Value = 22 Loading Eigen-Value = 23 Loading Eigen-Value = 24 Loading Eigen-Value = 25 Loading Eigen-Value = 26 Loading Eigen-Value = 27 Loading Eigen-Value = 28 Loading Eigen-Value = 29 Loading Eigen-Value = 30 Loading Eigen-Value = 31 Loading Eigen-Value = 32 Loading Eigen-Value = 33 Loading Eigen-Value = 34 Loading Eigen-Value = 35 Loading Eigen-Value = 36 Loading Eigen-Value = 37 Loading Eigen-Value = 38 Loading Eigen-Value = 39 Loading Eigen-Value = 40 Loading Eigen-Value = 41 Loading Eigen-Value = 42 Loading Eigen-Value = 43 Loading Eigen-Value = 44 Loading Eigen-Value = 45 Loading Eigen-Value = 46 Loading Eigen-Value = 47 Loading Eigen-Value = 48 Loading Eigen-Value = 49 Loading Eigen-Value = 50 Loading Eigen-Value = 51 Loading Eigen-Value = 52 Loading Eigen-Value = 53 Loading Eigen-Value = 54 Loading Eigen-Value = 55 Loading Eigen-Value = 56 Loading Eigen-Value = 57 Loading Eigen-Value = 58 Loading Eigen-Value = 59 Loading Eigen-Value = 60 Loading Eigen-Value = 61 Loading Eigen-Value = 62 Loading Eigen-Value = 63 Loading Eigen-Value = 64 Loading Eigen-Value = 65 Loading Eigen-Value = 66 Loading Eigen-Value = 67 Loading Eigen-Value = 68 Loading Eigen-Value = 69 Loading Eigen-Value = 70 Loading Eigen-Value = 71 Loading Eigen-Value = 72 Loading Eigen-Value = 73 Loading Eigen-Value = 74 Loading Eigen-Value = 75 Loading Eigen-Value = 76 Loading Eigen-Value = 77 Loading Eigen-Value = 78 Loading Eigen-Value = 79 Loading Eigen-Value = 80 Loading Eigen-Value = 81 Loading Eigen-Value = 82 Loading Eigen-Value = 83 Loading Eigen-Value = 84 Loading Eigen-Value = 85 Loading Eigen-Value = 86 Loading Eigen-Value = 87 Loading Eigen-Value = 88 Loading Eigen-Value = 89 Loading Eigen-Value = 90 Loading Eigen-Value = 91 Loading Eigen-Value = 92 Loading Eigen-Value = 93 Loading Eigen-Value = 94 Loading Eigen-Value = 95 Loading Eigen-Value = 96 Loading Eigen-Value = 97 Loading Eigen-Value = 98 Loading Eigen-Value = 99 Loading Eigen-Value = 100 Loading Eigen-Value = 101 Loading Eigen-Value = 102 Loading Eigen-Value = 103 Loading Eigen-Value = 104 Loading Eigen-Value = 105 Loading Eigen-Value = 106 Loading Eigen-Value = 107 Loading Eigen-Value = 108 Loading Eigen-Value = 109 Loading Eigen-Value = 110 Loading Eigen-Value = 111 Loading Eigen-Value = 112 Loading Eigen-Value = 113 Loading Eigen-Value = 114 Loading Eigen-Value = 115 Loading Eigen-Value = 116 Loading Eigen-Value = 117 Loading Eigen-Value = 118 Loading Eigen-Value = 119 Loading Eigen-Value = 120 Loading Eigen-Value = 121 Loading Eigen-Value = 122 Loading Eigen-Value = 123 Loading Eigen-Value = 124 Loading Eigen-Value = 125 Loading Eigen-Value = 126 Loading Eigen-Value = 127 Loading Eigen-Value = 128 Loading Eigen-Value = 129 Loading Eigen-Value = 130 Loading Eigen-Value = 131 Loading Eigen-Value = 132 Natural freq (Mode 0) = 9.44 (Hz) Natural freq (Mode 1) = 35.99 (Hz) Natural freq (Mode 2) = 50.58 (Hz) Natural freq (Mode 3) = 93.48 (Hz) Natural freq (Mode 4) = 122.58 (Hz) Natural freq (Mode 5) = 142.96 (Hz) Natural freq (Mode 6) = 153.81 (Hz) Natural freq (Mode 7) = 201.18 (Hz) Natural freq (Mode 8) = 203.69 (Hz) Natural freq (Mode 9) = 218.54 (Hz) Natural freq (Mode 10) = 244.49 (Hz) Natural freq (Mode 11) = 267.52 (Hz) Natural freq (Mode 12) = 282.33 (Hz) Natural freq (Mode 13) = 284.46 (Hz) Natural freq (Mode 14) = 311.84 (Hz) Natural freq (Mode 15) = 328.87 (Hz) Natural freq (Mode 16) = 334.68 (Hz) Natural freq (Mode 17) = 346.25 (Hz) Natural freq (Mode 18) = 362.24 (Hz) Natural freq (Mode 19) = 368.68 (Hz) Natural freq (Mode 20) = 377.76 (Hz) Natural freq (Mode 21) = 393.48 (Hz) Natural freq (Mode 22) = 403.01 (Hz) Natural freq (Mode 23) = 415.98 (Hz) Natural freq (Mode 24) = 430.66 (Hz) Natural freq (Mode 25) = 456.25 (Hz) Natural freq (Mode 26) = 460.70 (Hz) Natural freq (Mode 27) = 478.12 (Hz) Natural freq (Mode 28) = 500.39 (Hz) Natural freq (Mode 29) = 510.45 (Hz) Natural freq (Mode 30) = 514.48 (Hz) Natural freq (Mode 31) = 519.72 (Hz) Natural freq (Mode 32) = 531.28 (Hz) Natural freq (Mode 33) = 553.76 (Hz) Natural freq (Mode 34) = 566.65 (Hz) Natural freq (Mode 35) = 591.27 (Hz) Natural freq (Mode 36) = 611.71 (Hz) Natural freq (Mode 37) = 612.08 (Hz) Natural freq (Mode 38) = 624.35 (Hz) Natural freq (Mode 39) = 650.56 (Hz) Natural freq (Mode 40) = 670.08 (Hz) Natural freq (Mode 41) = 721.11 (Hz) Natural freq (Mode 42) = 732.49 (Hz) Natural freq (Mode 43) = 751.28 (Hz) Natural freq (Mode 44) = 814.54 (Hz) Natural freq (Mode 45) = 883.96 (Hz) Natural freq (Mode 46) = 951.75 (Hz) Natural freq (Mode 47) = 975.90 (Hz) Natural freq (Mode 48) = 1290.98 (Hz) Natural freq (Mode 49) = 1356.05 (Hz) Natural freq (Mode 50) = 1506.01 (Hz) Natural freq (Mode 51) = 1619.60 (Hz) Natural freq (Mode 52) = 1631.13 (Hz) Natural freq (Mode 53) = 1745.44 (Hz) Natural freq (Mode 54) = 1904.47 (Hz) Natural freq (Mode 55) = 2010.78 (Hz) Natural freq (Mode 56) = 2031.59 (Hz) Natural freq (Mode 57) = 2108.70 (Hz) Natural freq (Mode 58) = 2215.97 (Hz) Natural freq (Mode 59) = 2306.66 (Hz) Natural freq (Mode 60) = 2320.15 (Hz) Natural freq (Mode 61) = 2390.78 (Hz) Natural freq (Mode 62) = 2494.64 (Hz) Natural freq (Mode 63) = 2560.50 (Hz) Natural freq (Mode 64) = 2584.60 (Hz) Natural freq (Mode 65) = 2587.28 (Hz) Natural freq (Mode 66) = 2659.52 (Hz) Natural freq (Mode 67) = 2737.71 (Hz) Natural freq (Mode 68) = 2789.18 (Hz) Natural freq (Mode 69) = 2840.95 (Hz) Natural freq (Mode 70) = 2888.34 (Hz) Natural freq (Mode 71) = 2967.46 (Hz) Natural freq (Mode 72) = 3051.49 (Hz) Natural freq (Mode 73) = 3112.98 (Hz) Natural freq (Mode 74) = 3139.85 (Hz) Natural freq (Mode 75) = 3247.88 (Hz) Natural freq (Mode 76) = 3303.45 (Hz) Natural freq (Mode 77) = 3344.57 (Hz) Natural freq (Mode 78) = 3466.41 (Hz) Natural freq (Mode 79) = 3489.29 (Hz) Natural freq (Mode 80) = 3562.75 (Hz) Natural freq (Mode 81) = 3651.56 (Hz) Natural freq (Mode 82) = 3712.84 (Hz) Natural freq (Mode 83) = 3761.27 (Hz) Natural freq (Mode 84) = 3806.30 (Hz) Natural freq (Mode 85) = 3902.83 (Hz) Natural freq (Mode 86) = 3961.00 (Hz) Natural freq (Mode 87) = 4028.45 (Hz) Natural freq (Mode 88) = 4110.02 (Hz) Natural freq (Mode 89) = 4191.05 (Hz) Natural freq (Mode 90) = 4202.44 (Hz) Natural freq (Mode 91) = 4299.35 (Hz) Natural freq (Mode 92) = 4376.59 (Hz) Natural freq (Mode 93) = 4425.85 (Hz) Natural freq (Mode 94) = 4501.49 (Hz) Natural freq (Mode 95) = 4518.77 (Hz) Natural freq (Mode 96) = 4586.52 (Hz) Natural freq (Mode 97) = 4621.28 (Hz) Natural freq (Mode 98) = 4678.52 (Hz) Natural freq (Mode 99) = 4733.41 (Hz) Natural freq (Mode 100) = 4788.76 (Hz) Natural freq (Mode 101) = 4816.52 (Hz) Natural freq (Mode 102) = 4942.47 (Hz) Natural freq (Mode 103) = 4997.55 (Hz) Natural freq (Mode 104) = 5045.56 (Hz) Natural freq (Mode 105) = 5120.59 (Hz) Natural freq (Mode 106) = 5155.17 (Hz) Natural freq (Mode 107) = 5325.08 (Hz) Natural freq (Mode 108) = 5474.54 (Hz) Natural freq (Mode 109) = 5512.48 (Hz) Natural freq (Mode 110) = 5525.67 (Hz) Natural freq (Mode 111) = 5576.25 (Hz) Natural freq (Mode 112) = 5647.01 (Hz) Natural freq (Mode 113) = 5841.96 (Hz) Natural freq (Mode 114) = 6096.57 (Hz) Natural freq (Mode 115) = 6188.63 (Hz) Natural freq (Mode 116) = 6328.76 (Hz) Natural freq (Mode 117) = 6428.94 (Hz) Natural freq (Mode 118) = 6468.91 (Hz) Natural freq (Mode 119) = 6958.88 (Hz) Natural freq (Mode 120) = 7050.41 (Hz) Natural freq (Mode 121) = 7389.46 (Hz) Natural freq (Mode 122) = 7464.28 (Hz) Natural freq (Mode 123) = 7559.48 (Hz) Natural freq (Mode 124) = 8076.62 (Hz) Natural freq (Mode 125) = 8344.67 (Hz) Natural freq (Mode 126) = 8685.13 (Hz) Natural freq (Mode 127) = 9093.83 (Hz) Natural freq (Mode 128) = 9351.46 (Hz) Natural freq (Mode 129) = 10123.65 (Hz) Natural freq (Mode 130) = 10828.55 (Hz) Natural freq (Mode 131) = 11674.11 (Hz) real 0m0.514s user 0m0.585s sys 0m0.215s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_AGARD445_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_Aeroelastic_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_Aeroelastic_PyTest.py test; + python -u nastran_Aeroelastic_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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 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 = 1373 Number of elements = 1510 Number of triangle elements = 0 Number of quadrilateral elements = 1510 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 = 17 Number of elements = 10 Number of triangle elements = 0 Number of quadrilateral elements = 10 Body 4 (of 4) Number of nodes = 17 Number of elements = 10 Number of triangle elements = 0 Number of quadrilateral elements = 10 ---------------------------- Total number of nodes = 1408 Total number of elements = 1530 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 1 Name = Rib_Root_Point, index = 1 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 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1373 Number of elements = 1510 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 1510 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 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 17 Number of elements = 10 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 10 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 17 Number of elements = 10 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 10 Combining multiple FEA meshes! Combined Number of nodal coordinates = 1408 Combined Number of elements = 1531 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 1530 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 300 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Ribs No "material" specified for Property tuple Ribs, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Property name - Spar1 No "material" specified for Property tuple Spar1, defaulting to an index of 1 Property name - Spar2 No "material" specified for Property tuple Spar2, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 93 automatic connections were made for capsConnect Rib_Root (node id 1374) Done getting FEA connections Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No loads specified for case Trim1!!!! Writing mass increment cards Writing aeros card Writing aestat cards Writing analysis cards, 0 Writing constraint ADD cards Writing constraint cards Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m4.523s user 0m10.912s sys 0m5.530s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_Aeroelastic_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'nastran_CompositeWingDesign_PyTest.py test;' nastran_CompositeWingDesign_PyTest.py test; + python -u nastran_CompositeWingDesign_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, 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 = 323 Number of elements = 262 Number of triangle elements = 0 Number of quadrilateral elements = 262 ---------------------------- Total number of nodes = 323 Total number of elements = 262 Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = wing, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - wing Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = wing, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = wing, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 323 Number of elements = 262 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 262 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Aluminum No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic" Material name - Graphite_epoxy Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 8 Design_Variable name - L1 Design_Variable name - L2 Design_Variable name - L3 Design_Variable name - L4 Design_Variable name - L5 Design_Variable name - L6 Design_Variable name - L7 Design_Variable name - L8 Design_Variable_Relation name - L1R Design_Variable_Relation name - L2R Design_Variable_Relation name - L3R Design_Variable_Relation name - L4R Design_Variable_Relation name - L5R Design_Variable_Relation name - L6R Design_Variable_Relation name - L7R Design_Variable_Relation name - L8R Number of design variable relations - 8 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 8 Design_Constraint name - stress1 Design_Constraint name - stress2 Design_Constraint name - stress3 Design_Constraint name - stress4 Design_Constraint name - stress5 Design_Constraint name - stress6 Design_Constraint name - stress7 Design_Constraint name - stress8 Done getting FEA design constraints Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - StaticAnalysis Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing coordinate system cards Writing design variable cards Writing design variable relation cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.828s user 0m0.886s sys 0m0.207s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_CompositeWingDesign_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_CompositeWingFreq_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_CompositeWingFreq_PyTest.py test; + python -u nastran_CompositeWingFreq_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, 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 = 323 Number of elements = 262 Number of triangle elements = 0 Number of quadrilateral elements = 262 ---------------------------- Total number of nodes = 323 Total number of elements = 262 Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = wing, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - wing Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = wing, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = wing, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 323 Number of elements = 262 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 262 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Aluminum No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic" Material name - Graphite_epoxy Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - root No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Warning: No loads specified for case EigenAnalysis!!!! Writing mass increment cards Writing analysis cards, 0 Writing combined constraint cards Writing constraint cards Writing material cards Writing property cards Writing coordinate system cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! Getting results for natural frequencies..... Reading Nastran FO6 file - extracting Eigen-Values! Number of Eigen-Values = 1779 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Loading Eigen-Value = 11 Loading Eigen-Value = 12 Loading Eigen-Value = 13 Loading Eigen-Value = 14 Loading Eigen-Value = 15 Loading Eigen-Value = 16 Loading Eigen-Value = 17 Loading Eigen-Value = 18 Loading Eigen-Value = 19 Loading Eigen-Value = 20 Loading Eigen-Value = 21 Loading Eigen-Value = 22 Loading Eigen-Value = 23 Loading Eigen-Value = 24 Loading Eigen-Value = 25 Loading Eigen-Value = 26 Loading Eigen-Value = 27 Loading Eigen-Value = 28 Loading Eigen-Value = 29 Loading Eigen-Value = 30 Loading Eigen-Value = 31 Loading Eigen-Value = 32 Loading Eigen-Value = 33 Loading Eigen-Value = 34 Loading Eigen-Value = 35 Loading Eigen-Value = 36 Loading Eigen-Value = 37 Loading Eigen-Value = 38 Loading Eigen-Value = 39 Loading Eigen-Value = 40 Loading Eigen-Value = 41 Loading Eigen-Value = 42 Loading Eigen-Value = 43 Loading Eigen-Value = 44 Loading Eigen-Value = 45 Loading Eigen-Value = 46 Loading Eigen-Value = 47 Loading Eigen-Value = 48 Loading Eigen-Value = 49 Loading Eigen-Value = 50 Loading Eigen-Value = 51 Loading Eigen-Value = 52 Loading Eigen-Value = 53 Loading Eigen-Value = 54 Loading Eigen-Value = 55 Loading Eigen-Value = 56 Loading Eigen-Value = 57 Loading Eigen-Value = 58 Loading Eigen-Value = 59 Loading Eigen-Value = 60 Loading Eigen-Value = 61 Loading Eigen-Value = 62 Loading Eigen-Value = 63 Loading Eigen-Value = 64 Loading Eigen-Value = 65 Loading Eigen-Value = 66 Loading Eigen-Value = 67 Loading Eigen-Value = 68 Loading Eigen-Value = 69 Loading Eigen-Value = 70 Loading Eigen-Value = 71 Loading Eigen-Value = 72 Loading Eigen-Value = 73 Loading Eigen-Value = 74 Loading Eigen-Value = 75 Loading Eigen-Value = 76 Loading Eigen-Value = 77 Loading Eigen-Value = 78 Loading Eigen-Value = 79 Loading Eigen-Value = 80 Loading Eigen-Value = 81 Loading Eigen-Value = 82 Loading Eigen-Value = 83 Loading Eigen-Value = 84 Loading Eigen-Value = 85 Loading Eigen-Value = 86 Loading Eigen-Value = 87 Loading Eigen-Value = 88 Loading Eigen-Value = 89 Loading Eigen-Value = 90 Loading Eigen-Value = 91 Loading Eigen-Value = 92 Loading Eigen-Value = 93 Loading Eigen-Value = 94 Loading Eigen-Value = 95 Loading Eigen-Value = 96 Loading Eigen-Value = 97 Loading Eigen-Value = 98 Loading Eigen-Value = 99 Loading Eigen-Value = 100 Loading Eigen-Value = 101 Loading Eigen-Value = 102 Loading Eigen-Value = 103 Loading Eigen-Value = 104 Loading Eigen-Value = 105 Loading Eigen-Value = 106 Loading Eigen-Value = 107 Loading Eigen-Value = 108 Loading Eigen-Value = 109 Loading Eigen-Value = 110 Loading Eigen-Value = 111 Loading Eigen-Value = 112 Loading Eigen-Value = 113 Loading Eigen-Value = 114 Loading Eigen-Value = 115 Loading Eigen-Value = 116 Loading Eigen-Value = 117 Loading Eigen-Value = 118 Loading Eigen-Value = 119 Loading Eigen-Value = 120 Loading Eigen-Value = 121 Loading Eigen-Value = 122 Loading Eigen-Value = 123 Loading Eigen-Value = 124 Loading Eigen-Value = 125 Loading Eigen-Value = 126 Loading Eigen-Value = 127 Loading Eigen-Value = 128 Loading Eigen-Value = 129 Loading Eigen-Value = 130 Loading Eigen-Value = 131 Loading Eigen-Value = 132 Loading Eigen-Value = 133 Loading Eigen-Value = 134 Loading Eigen-Value = 135 Loading Eigen-Value = 136 Loading Eigen-Value = 137 Loading Eigen-Value = 138 Loading Eigen-Value = 139 Loading Eigen-Value = 140 Loading Eigen-Value = 141 Loading Eigen-Value = 142 Loading Eigen-Value = 143 Loading Eigen-Value = 144 Loading Eigen-Value = 145 Loading Eigen-Value = 146 Loading Eigen-Value = 147 Loading Eigen-Value = 148 Loading Eigen-Value = 149 Loading Eigen-Value = 150 Loading Eigen-Value = 151 Loading Eigen-Value = 152 Loading Eigen-Value = 153 Loading Eigen-Value = 154 Loading Eigen-Value = 155 Loading Eigen-Value = 156 Loading Eigen-Value = 157 Loading Eigen-Value = 158 Loading Eigen-Value = 159 Loading Eigen-Value = 160 Loading Eigen-Value = 161 Loading Eigen-Value = 162 Loading Eigen-Value = 163 Loading Eigen-Value = 164 Loading Eigen-Value = 165 Loading Eigen-Value = 166 Loading Eigen-Value = 167 Loading Eigen-Value = 168 Loading Eigen-Value = 169 Loading Eigen-Value = 170 Loading Eigen-Value = 171 Loading Eigen-Value = 172 Loading Eigen-Value = 173 Loading Eigen-Value = 174 Loading Eigen-Value = 175 Loading Eigen-Value = 176 Loading Eigen-Value = 177 Loading Eigen-Value = 178 Loading Eigen-Value = 179 Loading Eigen-Value = 180 Loading Eigen-Value = 181 Loading Eigen-Value = 182 Loading Eigen-Value = 183 Loading Eigen-Value = 184 Loading Eigen-Value = 185 Loading Eigen-Value = 186 Loading Eigen-Value = 187 Loading Eigen-Value = 188 Loading Eigen-Value = 189 Loading Eigen-Value = 190 Loading Eigen-Value = 191 Loading Eigen-Value = 192 Loading Eigen-Value = 193 Loading Eigen-Value = 194 Loading Eigen-Value = 195 Loading Eigen-Value = 196 Loading Eigen-Value = 197 Loading Eigen-Value = 198 Loading Eigen-Value = 199 Loading Eigen-Value = 200 Loading Eigen-Value = 201 Loading Eigen-Value = 202 Loading Eigen-Value = 203 Loading Eigen-Value = 204 Loading Eigen-Value = 205 Loading Eigen-Value = 206 Loading Eigen-Value = 207 Loading Eigen-Value = 208 Loading Eigen-Value = 209 Loading Eigen-Value = 210 Loading Eigen-Value = 211 Loading Eigen-Value = 212 Loading Eigen-Value = 213 Loading Eigen-Value = 214 Loading Eigen-Value = 215 Loading Eigen-Value = 216 Loading Eigen-Value = 217 Loading Eigen-Value = 218 Loading Eigen-Value = 219 Loading Eigen-Value = 220 Loading Eigen-Value = 221 Loading Eigen-Value = 222 Loading Eigen-Value = 223 Loading Eigen-Value = 224 Loading Eigen-Value = 225 Loading Eigen-Value = 226 Loading Eigen-Value = 227 Loading Eigen-Value = 228 Loading Eigen-Value = 229 Loading Eigen-Value = 230 Loading Eigen-Value = 231 Loading Eigen-Value = 232 Loading Eigen-Value = 233 Loading Eigen-Value = 234 Loading Eigen-Value = 235 Loading Eigen-Value = 236 Loading Eigen-Value = 237 Loading Eigen-Value = 238 Loading Eigen-Value = 239 Loading Eigen-Value = 240 Loading Eigen-Value = 241 Loading Eigen-Value = 242 Loading Eigen-Value = 243 Loading Eigen-Value = 244 Loading Eigen-Value = 245 Loading Eigen-Value = 246 Loading Eigen-Value = 247 Loading Eigen-Value = 248 Loading Eigen-Value = 249 Loading Eigen-Value = 250 Loading Eigen-Value = 251 Loading Eigen-Value = 252 Loading Eigen-Value = 253 Loading Eigen-Value = 254 Loading Eigen-Value = 255 Loading Eigen-Value = 256 Loading Eigen-Value = 257 Loading Eigen-Value = 258 Loading Eigen-Value = 259 Loading Eigen-Value = 260 Loading Eigen-Value = 261 Loading Eigen-Value = 262 Loading Eigen-Value = 263 Loading Eigen-Value = 264 Loading Eigen-Value = 265 Loading Eigen-Value = 266 Loading Eigen-Value = 267 Loading Eigen-Value = 268 Loading Eigen-Value = 269 Loading Eigen-Value = 270 Loading Eigen-Value = 271 Loading Eigen-Value = 272 Loading Eigen-Value = 273 Loading Eigen-Value = 274 Loading Eigen-Value = 275 Loading Eigen-Value = 276 Loading Eigen-Value = 277 Loading Eigen-Value = 278 Loading Eigen-Value = 279 Loading Eigen-Value = 280 Loading Eigen-Value = 281 Loading Eigen-Value = 282 Loading Eigen-Value = 283 Loading Eigen-Value = 284 Loading Eigen-Value = 285 Loading Eigen-Value = 286 Loading Eigen-Value = 287 Loading Eigen-Value = 288 Loading Eigen-Value = 289 Loading Eigen-Value = 290 Loading Eigen-Value = 291 Loading Eigen-Value = 292 Loading Eigen-Value = 293 Loading Eigen-Value = 294 Loading Eigen-Value = 295 Loading Eigen-Value = 296 Loading Eigen-Value = 297 Loading Eigen-Value = 298 Loading Eigen-Value = 299 Loading Eigen-Value = 300 Loading Eigen-Value = 301 Loading Eigen-Value = 302 Loading Eigen-Value = 303 Loading Eigen-Value = 304 Loading Eigen-Value = 305 Loading Eigen-Value = 306 Loading Eigen-Value = 307 Loading Eigen-Value = 308 Loading Eigen-Value = 309 Loading Eigen-Value = 310 Loading Eigen-Value = 311 Loading Eigen-Value = 312 Loading Eigen-Value = 313 Loading Eigen-Value = 314 Loading Eigen-Value = 315 Loading Eigen-Value = 316 Loading Eigen-Value = 317 Loading Eigen-Value = 318 Loading Eigen-Value = 319 Loading Eigen-Value = 320 Loading Eigen-Value = 321 Loading Eigen-Value = 322 Loading Eigen-Value = 323 Loading Eigen-Value = 324 Loading Eigen-Value = 325 Loading Eigen-Value = 326 Loading Eigen-Value = 327 Loading Eigen-Value = 328 Loading Eigen-Value = 329 Loading Eigen-Value = 330 Loading Eigen-Value = 331 Loading Eigen-Value = 332 Loading Eigen-Value = 333 Loading Eigen-Value = 334 Loading Eigen-Value = 335 Loading Eigen-Value = 336 Loading Eigen-Value = 337 Loading Eigen-Value = 338 Loading Eigen-Value = 339 Loading Eigen-Value = 340 Loading Eigen-Value = 341 Loading Eigen-Value = 342 Loading Eigen-Value = 343 Loading Eigen-Value = 344 Loading Eigen-Value = 345 Loading Eigen-Value = 346 Loading Eigen-Value = 347 Loading Eigen-Value = 348 Loading Eigen-Value = 349 Loading Eigen-Value = 350 Loading Eigen-Value = 351 Loading Eigen-Value = 352 Loading Eigen-Value = 353 Loading Eigen-Value = 354 Loading Eigen-Value = 355 Loading Eigen-Value = 356 Loading Eigen-Value = 357 Loading Eigen-Value = 358 Loading Eigen-Value = 359 Loading Eigen-Value = 360 Loading Eigen-Value = 361 Loading Eigen-Value = 362 Loading Eigen-Value = 363 Loading Eigen-Value = 364 Loading Eigen-Value = 365 Loading Eigen-Value = 366 Loading Eigen-Value = 367 Loading Eigen-Value = 368 Loading Eigen-Value = 369 Loading Eigen-Value = 370 Loading Eigen-Value = 371 Loading Eigen-Value = 372 Loading Eigen-Value = 373 Loading Eigen-Value = 374 Loading Eigen-Value = 375 Loading Eigen-Value = 376 Loading Eigen-Value = 377 Loading Eigen-Value = 378 Loading Eigen-Value = 379 Loading Eigen-Value = 380 Loading Eigen-Value = 381 Loading Eigen-Value = 382 Loading Eigen-Value = 383 Loading Eigen-Value = 384 Loading Eigen-Value = 385 Loading Eigen-Value = 386 Loading Eigen-Value = 387 Loading Eigen-Value = 388 Loading Eigen-Value = 389 Loading Eigen-Value = 390 Loading Eigen-Value = 391 Loading Eigen-Value = 392 Loading Eigen-Value = 393 Loading Eigen-Value = 394 Loading Eigen-Value = 395 Loading Eigen-Value = 396 Loading Eigen-Value = 397 Loading Eigen-Value = 398 Loading Eigen-Value = 399 Loading Eigen-Value = 400 Loading Eigen-Value = 401 Loading Eigen-Value = 402 Loading Eigen-Value = 403 Loading Eigen-Value = 404 Loading Eigen-Value = 405 Loading Eigen-Value = 406 Loading Eigen-Value = 407 Loading Eigen-Value = 408 Loading Eigen-Value = 409 Loading Eigen-Value = 410 Loading Eigen-Value = 411 Loading Eigen-Value = 412 Loading Eigen-Value = 413 Loading Eigen-Value = 414 Loading Eigen-Value = 415 Loading Eigen-Value = 416 Loading Eigen-Value = 417 Loading Eigen-Value = 418 Loading Eigen-Value = 419 Loading Eigen-Value = 420 Loading Eigen-Value = 421 Loading Eigen-Value = 422 Loading Eigen-Value = 423 Loading Eigen-Value = 424 Loading Eigen-Value = 425 Loading Eigen-Value = 426 Loading Eigen-Value = 427 Loading Eigen-Value = 428 Loading Eigen-Value = 429 Loading Eigen-Value = 430 Loading Eigen-Value = 431 Loading Eigen-Value = 432 Loading Eigen-Value = 433 Loading Eigen-Value = 434 Loading Eigen-Value = 435 Loading Eigen-Value = 436 Loading Eigen-Value = 437 Loading Eigen-Value = 438 Loading Eigen-Value = 439 Loading Eigen-Value = 440 Loading Eigen-Value = 441 Loading Eigen-Value = 442 Loading Eigen-Value = 443 Loading Eigen-Value = 444 Loading Eigen-Value = 445 Loading Eigen-Value = 446 Loading Eigen-Value = 447 Loading Eigen-Value = 448 Loading Eigen-Value = 449 Loading Eigen-Value = 450 Loading Eigen-Value = 451 Loading Eigen-Value = 452 Loading Eigen-Value = 453 Loading Eigen-Value = 454 Loading Eigen-Value = 455 Loading Eigen-Value = 456 Loading Eigen-Value = 457 Loading Eigen-Value = 458 Loading Eigen-Value = 459 Loading Eigen-Value = 460 Loading Eigen-Value = 461 Loading Eigen-Value = 462 Loading Eigen-Value = 463 Loading Eigen-Value = 464 Loading Eigen-Value = 465 Loading Eigen-Value = 466 Loading Eigen-Value = 467 Loading Eigen-Value = 468 Loading Eigen-Value = 469 Loading Eigen-Value = 470 Loading Eigen-Value = 471 Loading Eigen-Value = 472 Loading Eigen-Value = 473 Loading Eigen-Value = 474 Loading Eigen-Value = 475 Loading Eigen-Value = 476 Loading Eigen-Value = 477 Loading Eigen-Value = 478 Loading Eigen-Value = 479 Loading Eigen-Value = 480 Loading Eigen-Value = 481 Loading Eigen-Value = 482 Loading Eigen-Value = 483 Loading Eigen-Value = 484 Loading Eigen-Value = 485 Loading Eigen-Value = 486 Loading Eigen-Value = 487 Loading Eigen-Value = 488 Loading Eigen-Value = 489 Loading Eigen-Value = 490 Loading Eigen-Value = 491 Loading Eigen-Value = 492 Loading Eigen-Value = 493 Loading Eigen-Value = 494 Loading Eigen-Value = 495 Loading Eigen-Value = 496 Loading Eigen-Value = 497 Loading Eigen-Value = 498 Loading Eigen-Value = 499 Loading Eigen-Value = 500 Loading Eigen-Value = 501 Loading Eigen-Value = 502 Loading Eigen-Value = 503 Loading Eigen-Value = 504 Loading Eigen-Value = 505 Loading Eigen-Value = 506 Loading Eigen-Value = 507 Loading Eigen-Value = 508 Loading Eigen-Value = 509 Loading Eigen-Value = 510 Loading Eigen-Value = 511 Loading Eigen-Value = 512 Loading Eigen-Value = 513 Loading Eigen-Value = 514 Loading Eigen-Value = 515 Loading Eigen-Value = 516 Loading Eigen-Value = 517 Loading Eigen-Value = 518 Loading Eigen-Value = 519 Loading Eigen-Value = 520 Loading Eigen-Value = 521 Loading Eigen-Value = 522 Loading Eigen-Value = 523 Loading Eigen-Value = 524 Loading Eigen-Value = 525 Loading Eigen-Value = 526 Loading Eigen-Value = 527 Loading Eigen-Value = 528 Loading Eigen-Value = 529 Loading Eigen-Value = 530 Loading Eigen-Value = 531 Loading Eigen-Value = 532 Loading Eigen-Value = 533 Loading Eigen-Value = 534 Loading Eigen-Value = 535 Loading Eigen-Value = 536 Loading Eigen-Value = 537 Loading Eigen-Value = 538 Loading Eigen-Value = 539 Loading Eigen-Value = 540 Loading Eigen-Value = 541 Loading Eigen-Value = 542 Loading Eigen-Value = 543 Loading Eigen-Value = 544 Loading Eigen-Value = 545 Loading Eigen-Value = 546 Loading Eigen-Value = 547 Loading Eigen-Value = 548 Loading Eigen-Value = 549 Loading Eigen-Value = 550 Loading Eigen-Value = 551 Loading Eigen-Value = 552 Loading Eigen-Value = 553 Loading Eigen-Value = 554 Loading Eigen-Value = 555 Loading Eigen-Value = 556 Loading Eigen-Value = 557 Loading Eigen-Value = 558 Loading Eigen-Value = 559 Loading Eigen-Value = 560 Loading Eigen-Value = 561 Loading Eigen-Value = 562 Loading Eigen-Value = 563 Loading Eigen-Value = 564 Loading Eigen-Value = 565 Loading Eigen-Value = 566 Loading Eigen-Value = 567 Loading Eigen-Value = 568 Loading Eigen-Value = 569 Loading Eigen-Value = 570 Loading Eigen-Value = 571 Loading Eigen-Value = 572 Loading Eigen-Value = 573 Loading Eigen-Value = 574 Loading Eigen-Value = 575 Loading Eigen-Value = 576 Loading Eigen-Value = 577 Loading Eigen-Value = 578 Loading Eigen-Value = 579 Loading Eigen-Value = 580 Loading Eigen-Value = 581 Loading Eigen-Value = 582 Loading Eigen-Value = 583 Loading Eigen-Value = 584 Loading Eigen-Value = 585 Loading Eigen-Value = 586 Loading Eigen-Value = 587 Loading Eigen-Value = 588 Loading Eigen-Value = 589 Loading Eigen-Value = 590 Loading Eigen-Value = 591 Loading Eigen-Value = 592 Loading Eigen-Value = 593 Loading Eigen-Value = 594 Loading Eigen-Value = 595 Loading Eigen-Value = 596 Loading Eigen-Value = 597 Loading Eigen-Value = 598 Loading Eigen-Value = 599 Loading Eigen-Value = 600 Loading Eigen-Value = 601 Loading Eigen-Value = 602 Loading Eigen-Value = 603 Loading Eigen-Value = 604 Loading Eigen-Value = 605 Loading Eigen-Value = 606 Loading Eigen-Value = 607 Loading Eigen-Value = 608 Loading Eigen-Value = 609 Loading Eigen-Value = 610 Loading Eigen-Value = 611 Loading Eigen-Value = 612 Loading Eigen-Value = 613 Loading Eigen-Value = 614 Loading Eigen-Value = 615 Loading Eigen-Value = 616 Loading Eigen-Value = 617 Loading Eigen-Value = 618 Loading Eigen-Value = 619 Loading Eigen-Value = 620 Loading Eigen-Value = 621 Loading Eigen-Value = 622 Loading Eigen-Value = 623 Loading Eigen-Value = 624 Loading Eigen-Value = 625 Loading Eigen-Value = 626 Loading Eigen-Value = 627 Loading Eigen-Value = 628 Loading Eigen-Value = 629 Loading Eigen-Value = 630 Loading Eigen-Value = 631 Loading Eigen-Value = 632 Loading Eigen-Value = 633 Loading Eigen-Value = 634 Loading Eigen-Value = 635 Loading Eigen-Value = 636 Loading Eigen-Value = 637 Loading Eigen-Value = 638 Loading Eigen-Value = 639 Loading Eigen-Value = 640 Loading Eigen-Value = 641 Loading Eigen-Value = 642 Loading Eigen-Value = 643 Loading Eigen-Value = 644 Loading Eigen-Value = 645 Loading Eigen-Value = 646 Loading Eigen-Value = 647 Loading Eigen-Value = 648 Loading Eigen-Value = 649 Loading Eigen-Value = 650 Loading Eigen-Value = 651 Loading Eigen-Value = 652 Loading Eigen-Value = 653 Loading Eigen-Value = 654 Loading Eigen-Value = 655 Loading Eigen-Value = 656 Loading Eigen-Value = 657 Loading Eigen-Value = 658 Loading Eigen-Value = 659 Loading Eigen-Value = 660 Loading Eigen-Value = 661 Loading Eigen-Value = 662 Loading Eigen-Value = 663 Loading Eigen-Value = 664 Loading Eigen-Value = 665 Loading Eigen-Value = 666 Loading Eigen-Value = 667 Loading Eigen-Value = 668 Loading Eigen-Value = 669 Loading Eigen-Value = 670 Loading Eigen-Value = 671 Loading Eigen-Value = 672 Loading Eigen-Value = 673 Loading Eigen-Value = 674 Loading Eigen-Value = 675 Loading Eigen-Value = 676 Loading Eigen-Value = 677 Loading Eigen-Value = 678 Loading Eigen-Value = 679 Loading Eigen-Value = 680 Loading Eigen-Value = 681 Loading Eigen-Value = 682 Loading Eigen-Value = 683 Loading Eigen-Value = 684 Loading Eigen-Value = 685 Loading Eigen-Value = 686 Loading Eigen-Value = 687 Loading Eigen-Value = 688 Loading Eigen-Value = 689 Loading Eigen-Value = 690 Loading Eigen-Value = 691 Loading Eigen-Value = 692 Loading Eigen-Value = 693 Loading Eigen-Value = 694 Loading Eigen-Value = 695 Loading Eigen-Value = 696 Loading Eigen-Value = 697 Loading Eigen-Value = 698 Loading Eigen-Value = 699 Loading Eigen-Value = 700 Loading Eigen-Value = 701 Loading Eigen-Value = 702 Loading Eigen-Value = 703 Loading Eigen-Value = 704 Loading Eigen-Value = 705 Loading Eigen-Value = 706 Loading Eigen-Value = 707 Loading Eigen-Value = 708 Loading Eigen-Value = 709 Loading Eigen-Value = 710 Loading Eigen-Value = 711 Loading Eigen-Value = 712 Loading Eigen-Value = 713 Loading Eigen-Value = 714 Loading Eigen-Value = 715 Loading Eigen-Value = 716 Loading Eigen-Value = 717 Loading Eigen-Value = 718 Loading Eigen-Value = 719 Loading Eigen-Value = 720 Loading Eigen-Value = 721 Loading Eigen-Value = 722 Loading Eigen-Value = 723 Loading Eigen-Value = 724 Loading Eigen-Value = 725 Loading Eigen-Value = 726 Loading Eigen-Value = 727 Loading Eigen-Value = 728 Loading Eigen-Value = 729 Loading Eigen-Value = 730 Loading Eigen-Value = 731 Loading Eigen-Value = 732 Loading Eigen-Value = 733 Loading Eigen-Value = 734 Loading Eigen-Value = 735 Loading Eigen-Value = 736 Loading Eigen-Value = 737 Loading Eigen-Value = 738 Loading Eigen-Value = 739 Loading Eigen-Value = 740 Loading Eigen-Value = 741 Loading Eigen-Value = 742 Loading Eigen-Value = 743 Loading Eigen-Value = 744 Loading Eigen-Value = 745 Loading Eigen-Value = 746 Loading Eigen-Value = 747 Loading Eigen-Value = 748 Loading Eigen-Value = 749 Loading Eigen-Value = 750 Loading Eigen-Value = 751 Loading Eigen-Value = 752 Loading Eigen-Value = 753 Loading Eigen-Value = 754 Loading Eigen-Value = 755 Loading Eigen-Value = 756 Loading Eigen-Value = 757 Loading Eigen-Value = 758 Loading Eigen-Value = 759 Loading Eigen-Value = 760 Loading Eigen-Value = 761 Loading Eigen-Value = 762 Loading Eigen-Value = 763 Loading Eigen-Value = 764 Loading Eigen-Value = 765 Loading Eigen-Value = 766 Loading Eigen-Value = 767 Loading Eigen-Value = 768 Loading Eigen-Value = 769 Loading Eigen-Value = 770 Loading Eigen-Value = 771 Loading Eigen-Value = 772 Loading Eigen-Value = 773 Loading Eigen-Value = 774 Loading Eigen-Value = 775 Loading Eigen-Value = 776 Loading Eigen-Value = 777 Loading Eigen-Value = 778 Loading Eigen-Value = 779 Loading Eigen-Value = 780 Loading Eigen-Value = 781 Loading Eigen-Value = 782 Loading Eigen-Value = 783 Loading Eigen-Value = 784 Loading Eigen-Value = 785 Loading Eigen-Value = 786 Loading Eigen-Value = 787 Loading Eigen-Value = 788 Loading Eigen-Value = 789 Loading Eigen-Value = 790 Loading Eigen-Value = 791 Loading Eigen-Value = 792 Loading Eigen-Value = 793 Loading Eigen-Value = 794 Loading Eigen-Value = 795 Loading Eigen-Value = 796 Loading Eigen-Value = 797 Loading Eigen-Value = 798 Loading Eigen-Value = 799 Loading Eigen-Value = 800 Loading Eigen-Value = 801 Loading Eigen-Value = 802 Loading Eigen-Value = 803 Loading Eigen-Value = 804 Loading Eigen-Value = 805 Loading Eigen-Value = 806 Loading Eigen-Value = 807 Loading Eigen-Value = 808 Loading Eigen-Value = 809 Loading Eigen-Value = 810 Loading Eigen-Value = 811 Loading Eigen-Value = 812 Loading Eigen-Value = 813 Loading Eigen-Value = 814 Loading Eigen-Value = 815 Loading Eigen-Value = 816 Loading Eigen-Value = 817 Loading Eigen-Value = 818 Loading Eigen-Value = 819 Loading Eigen-Value = 820 Loading Eigen-Value = 821 Loading Eigen-Value = 822 Loading Eigen-Value = 823 Loading Eigen-Value = 824 Loading Eigen-Value = 825 Loading Eigen-Value = 826 Loading Eigen-Value = 827 Loading Eigen-Value = 828 Loading Eigen-Value = 829 Loading Eigen-Value = 830 Loading Eigen-Value = 831 Loading Eigen-Value = 832 Loading Eigen-Value = 833 Loading Eigen-Value = 834 Loading Eigen-Value = 835 Loading Eigen-Value = 836 Loading Eigen-Value = 837 Loading Eigen-Value = 838 Loading Eigen-Value = 839 Loading Eigen-Value = 840 Loading Eigen-Value = 841 Loading Eigen-Value = 842 Loading Eigen-Value = 843 Loading Eigen-Value = 844 Loading Eigen-Value = 845 Loading Eigen-Value = 846 Loading Eigen-Value = 847 Loading Eigen-Value = 848 Loading Eigen-Value = 849 Loading Eigen-Value = 850 Loading Eigen-Value = 851 Loading Eigen-Value = 852 Loading Eigen-Value = 853 Loading Eigen-Value = 854 Loading Eigen-Value = 855 Loading Eigen-Value = 856 Loading Eigen-Value = 857 Loading Eigen-Value = 858 Loading Eigen-Value = 859 Loading Eigen-Value = 860 Loading Eigen-Value = 861 Loading Eigen-Value = 862 Loading Eigen-Value = 863 Loading Eigen-Value = 864 Loading Eigen-Value = 865 Loading Eigen-Value = 866 Loading Eigen-Value = 867 Loading Eigen-Value = 868 Loading Eigen-Value = 869 Loading Eigen-Value = 870 Loading Eigen-Value = 871 Loading Eigen-Value = 872 Loading Eigen-Value = 873 Loading Eigen-Value = 874 Loading Eigen-Value = 875 Loading Eigen-Value = 876 Loading Eigen-Value = 877 Loading Eigen-Value = 878 Loading Eigen-Value = 879 Loading Eigen-Value = 880 Loading Eigen-Value = 881 Loading Eigen-Value = 882 Loading Eigen-Value = 883 Loading Eigen-Value = 884 Loading Eigen-Value = 885 Loading Eigen-Value = 886 Loading Eigen-Value = 887 Loading Eigen-Value = 888 Loading Eigen-Value = 889 Loading Eigen-Value = 890 Loading Eigen-Value = 891 Loading Eigen-Value = 892 Loading Eigen-Value = 893 Loading Eigen-Value = 894 Loading Eigen-Value = 895 Loading Eigen-Value = 896 Loading Eigen-Value = 897 Loading Eigen-Value = 898 Loading Eigen-Value = 899 Loading Eigen-Value = 900 Loading Eigen-Value = 901 Loading Eigen-Value = 902 Loading Eigen-Value = 903 Loading Eigen-Value = 904 Loading Eigen-Value = 905 Loading Eigen-Value = 906 Loading Eigen-Value = 907 Loading Eigen-Value = 908 Loading Eigen-Value = 909 Loading Eigen-Value = 910 Loading Eigen-Value = 911 Loading Eigen-Value = 912 Loading Eigen-Value = 913 Loading Eigen-Value = 914 Loading Eigen-Value = 915 Loading Eigen-Value = 916 Loading Eigen-Value = 917 Loading Eigen-Value = 918 Loading Eigen-Value = 919 Loading Eigen-Value = 920 Loading Eigen-Value = 921 Loading Eigen-Value = 922 Loading Eigen-Value = 923 Loading Eigen-Value = 924 Loading Eigen-Value = 925 Loading Eigen-Value = 926 Loading Eigen-Value = 927 Loading Eigen-Value = 928 Loading Eigen-Value = 929 Loading Eigen-Value = 930 Loading Eigen-Value = 931 Loading Eigen-Value = 932 Loading Eigen-Value = 933 Loading Eigen-Value = 934 Loading Eigen-Value = 935 Loading Eigen-Value = 936 Loading Eigen-Value = 937 Loading Eigen-Value = 938 Loading Eigen-Value = 939 Loading Eigen-Value = 940 Loading Eigen-Value = 941 Loading Eigen-Value = 942 Loading Eigen-Value = 943 Loading Eigen-Value = 944 Loading Eigen-Value = 945 Loading Eigen-Value = 946 Loading Eigen-Value = 947 Loading Eigen-Value = 948 Loading Eigen-Value = 949 Loading Eigen-Value = 950 Loading Eigen-Value = 951 Loading Eigen-Value = 952 Loading Eigen-Value = 953 Loading Eigen-Value = 954 Loading Eigen-Value = 955 Loading Eigen-Value = 956 Loading Eigen-Value = 957 Loading Eigen-Value = 958 Loading Eigen-Value = 959 Loading Eigen-Value = 960 Loading Eigen-Value = 961 Loading Eigen-Value = 962 Loading Eigen-Value = 963 Loading Eigen-Value = 964 Loading Eigen-Value = 965 Loading Eigen-Value = 966 Loading Eigen-Value = 967 Loading Eigen-Value = 968 Loading Eigen-Value = 969 Loading Eigen-Value = 970 Loading Eigen-Value = 971 Loading Eigen-Value = 972 Loading Eigen-Value = 973 Loading Eigen-Value = 974 Loading Eigen-Value = 975 Loading Eigen-Value = 976 Loading Eigen-Value = 977 Loading Eigen-Value = 978 Loading Eigen-Value = 979 Loading Eigen-Value = 980 Loading Eigen-Value = 981 Loading Eigen-Value = 982 Loading Eigen-Value = 983 Loading Eigen-Value = 984 Loading Eigen-Value = 985 Loading Eigen-Value = 986 Loading Eigen-Value = 987 Loading Eigen-Value = 988 Loading Eigen-Value = 989 Loading Eigen-Value = 990 Loading Eigen-Value = 991 Loading Eigen-Value = 992 Loading Eigen-Value = 993 Loading Eigen-Value = 994 Loading Eigen-Value = 995 Loading Eigen-Value = 996 Loading Eigen-Value = 997 Loading Eigen-Value = 998 Loading Eigen-Value = 999 Loading Eigen-Value = 1000 Loading Eigen-Value = 1001 Loading Eigen-Value = 1002 Loading Eigen-Value = 1003 Loading Eigen-Value = 1004 Loading Eigen-Value = 1005 Loading Eigen-Value = 1006 Loading Eigen-Value = 1007 Loading Eigen-Value = 1008 Loading Eigen-Value = 1009 Loading Eigen-Value = 1010 Loading Eigen-Value = 1011 Loading Eigen-Value = 1012 Loading Eigen-Value = 1013 Loading Eigen-Value = 1014 Loading Eigen-Value = 1015 Loading Eigen-Value = 1016 Loading Eigen-Value = 1017 Loading Eigen-Value = 1018 Loading Eigen-Value = 1019 Loading Eigen-Value = 1020 Loading Eigen-Value = 1021 Loading Eigen-Value = 1022 Loading Eigen-Value = 1023 Loading Eigen-Value = 1024 Loading Eigen-Value = 1025 Loading Eigen-Value = 1026 Loading Eigen-Value = 1027 Loading Eigen-Value = 1028 Loading Eigen-Value = 1029 Loading Eigen-Value = 1030 Loading Eigen-Value = 1031 Loading Eigen-Value = 1032 Loading Eigen-Value = 1033 Loading Eigen-Value = 1034 Loading Eigen-Value = 1035 Loading Eigen-Value = 1036 Loading Eigen-Value = 1037 Loading Eigen-Value = 1038 Loading Eigen-Value = 1039 Loading Eigen-Value = 1040 Loading Eigen-Value = 1041 Loading Eigen-Value = 1042 Loading Eigen-Value = 1043 Loading Eigen-Value = 1044 Loading Eigen-Value = 1045 Loading Eigen-Value = 1046 Loading Eigen-Value = 1047 Loading Eigen-Value = 1048 Loading Eigen-Value = 1049 Loading Eigen-Value = 1050 Loading Eigen-Value = 1051 Loading Eigen-Value = 1052 Loading Eigen-Value = 1053 Loading Eigen-Value = 1054 Loading Eigen-Value = 1055 Loading Eigen-Value = 1056 Loading Eigen-Value = 1057 Loading Eigen-Value = 1058 Loading Eigen-Value = 1059 Loading Eigen-Value = 1060 Loading Eigen-Value = 1061 Loading Eigen-Value = 1062 Loading Eigen-Value = 1063 Loading Eigen-Value = 1064 Loading Eigen-Value = 1065 Loading Eigen-Value = 1066 Loading Eigen-Value = 1067 Loading Eigen-Value = 1068 Loading Eigen-Value = 1069 Loading Eigen-Value = 1070 Loading Eigen-Value = 1071 Loading Eigen-Value = 1072 Loading Eigen-Value = 1073 Loading Eigen-Value = 1074 Loading Eigen-Value = 1075 Loading Eigen-Value = 1076 Loading Eigen-Value = 1077 Loading Eigen-Value = 1078 Loading Eigen-Value = 1079 Loading Eigen-Value = 1080 Loading Eigen-Value = 1081 Loading Eigen-Value = 1082 Loading Eigen-Value = 1083 Loading Eigen-Value = 1084 Loading Eigen-Value = 1085 Loading Eigen-Value = 1086 Loading Eigen-Value = 1087 Loading Eigen-Value = 1088 Loading Eigen-Value = 1089 Loading Eigen-Value = 1090 Loading Eigen-Value = 1091 Loading Eigen-Value = 1092 Loading Eigen-Value = 1093 Loading Eigen-Value = 1094 Loading Eigen-Value = 1095 Loading Eigen-Value = 1096 Loading Eigen-Value = 1097 Loading Eigen-Value = 1098 Loading Eigen-Value = 1099 Loading Eigen-Value = 1100 Loading Eigen-Value = 1101 Loading Eigen-Value = 1102 Loading Eigen-Value = 1103 Loading Eigen-Value = 1104 Loading Eigen-Value = 1105 Loading Eigen-Value = 1106 Loading Eigen-Value = 1107 Loading Eigen-Value = 1108 Loading Eigen-Value = 1109 Loading Eigen-Value = 1110 Loading Eigen-Value = 1111 Loading Eigen-Value = 1112 Loading Eigen-Value = 1113 Loading Eigen-Value = 1114 Loading Eigen-Value = 1115 Loading Eigen-Value = 1116 Loading Eigen-Value = 1117 Loading Eigen-Value = 1118 Loading Eigen-Value = 1119 Loading Eigen-Value = 1120 Loading Eigen-Value = 1121 Loading Eigen-Value = 1122 Loading Eigen-Value = 1123 Loading Eigen-Value = 1124 Loading Eigen-Value = 1125 Loading Eigen-Value = 1126 Loading Eigen-Value = 1127 Loading Eigen-Value = 1128 Loading Eigen-Value = 1129 Loading Eigen-Value = 1130 Loading Eigen-Value = 1131 Loading Eigen-Value = 1132 Loading Eigen-Value = 1133 Loading Eigen-Value = 1134 Loading Eigen-Value = 1135 Loading Eigen-Value = 1136 Loading Eigen-Value = 1137 Loading Eigen-Value = 1138 Loading Eigen-Value = 1139 Loading Eigen-Value = 1140 Loading Eigen-Value = 1141 Loading Eigen-Value = 1142 Loading Eigen-Value = 1143 Loading Eigen-Value = 1144 Loading Eigen-Value = 1145 Loading Eigen-Value = 1146 Loading Eigen-Value = 1147 Loading Eigen-Value = 1148 Loading Eigen-Value = 1149 Loading Eigen-Value = 1150 Loading Eigen-Value = 1151 Loading Eigen-Value = 1152 Loading Eigen-Value = 1153 Loading Eigen-Value = 1154 Loading Eigen-Value = 1155 Loading Eigen-Value = 1156 Loading Eigen-Value = 1157 Loading Eigen-Value = 1158 Loading Eigen-Value = 1159 Loading Eigen-Value = 1160 Loading Eigen-Value = 1161 Loading Eigen-Value = 1162 Loading Eigen-Value = 1163 Loading Eigen-Value = 1164 Loading Eigen-Value = 1165 Loading Eigen-Value = 1166 Loading Eigen-Value = 1167 Loading Eigen-Value = 1168 Loading Eigen-Value = 1169 Loading Eigen-Value = 1170 Loading Eigen-Value = 1171 Loading Eigen-Value = 1172 Loading Eigen-Value = 1173 Loading Eigen-Value = 1174 Loading Eigen-Value = 1175 Loading Eigen-Value = 1176 Loading Eigen-Value = 1177 Loading Eigen-Value = 1178 Loading Eigen-Value = 1179 Loading Eigen-Value = 1180 Loading Eigen-Value = 1181 Loading Eigen-Value = 1182 Loading Eigen-Value = 1183 Loading Eigen-Value = 1184 Loading Eigen-Value = 1185 Loading Eigen-Value = 1186 Loading Eigen-Value = 1187 Loading Eigen-Value = 1188 Loading Eigen-Value = 1189 Loading Eigen-Value = 1190 Loading Eigen-Value = 1191 Loading Eigen-Value = 1192 Loading Eigen-Value = 1193 Loading Eigen-Value = 1194 Loading Eigen-Value = 1195 Loading Eigen-Value = 1196 Loading Eigen-Value = 1197 Loading Eigen-Value = 1198 Loading Eigen-Value = 1199 Loading Eigen-Value = 1200 Loading Eigen-Value = 1201 Loading Eigen-Value = 1202 Loading Eigen-Value = 1203 Loading Eigen-Value = 1204 Loading Eigen-Value = 1205 Loading Eigen-Value = 1206 Loading Eigen-Value = 1207 Loading Eigen-Value = 1208 Loading Eigen-Value = 1209 Loading Eigen-Value = 1210 Loading Eigen-Value = 1211 Loading Eigen-Value = 1212 Loading Eigen-Value = 1213 Loading Eigen-Value = 1214 Loading Eigen-Value = 1215 Loading Eigen-Value = 1216 Loading Eigen-Value = 1217 Loading Eigen-Value = 1218 Loading Eigen-Value = 1219 Loading Eigen-Value = 1220 Loading Eigen-Value = 1221 Loading Eigen-Value = 1222 Loading Eigen-Value = 1223 Loading Eigen-Value = 1224 Loading Eigen-Value = 1225 Loading Eigen-Value = 1226 Loading Eigen-Value = 1227 Loading Eigen-Value = 1228 Loading Eigen-Value = 1229 Loading Eigen-Value = 1230 Loading Eigen-Value = 1231 Loading Eigen-Value = 1232 Loading Eigen-Value = 1233 Loading Eigen-Value = 1234 Loading Eigen-Value = 1235 Loading Eigen-Value = 1236 Loading Eigen-Value = 1237 Loading Eigen-Value = 1238 Loading Eigen-Value = 1239 Loading Eigen-Value = 1240 Loading Eigen-Value = 1241 Loading Eigen-Value = 1242 Loading Eigen-Value = 1243 Loading Eigen-Value = 1244 Loading Eigen-Value = 1245 Loading Eigen-Value = 1246 Loading Eigen-Value = 1247 Loading Eigen-Value = 1248 Loading Eigen-Value = 1249 Loading Eigen-Value = 1250 Loading Eigen-Value = 1251 Loading Eigen-Value = 1252 Loading Eigen-Value = 1253 Loading Eigen-Value = 1254 Loading Eigen-Value = 1255 Loading Eigen-Value = 1256 Loading Eigen-Value = 1257 Loading Eigen-Value = 1258 Loading Eigen-Value = 1259 Loading Eigen-Value = 1260 Loading Eigen-Value = 1261 Loading Eigen-Value = 1262 Loading Eigen-Value = 1263 Loading Eigen-Value = 1264 Loading Eigen-Value = 1265 Loading Eigen-Value = 1266 Loading Eigen-Value = 1267 Loading Eigen-Value = 1268 Loading Eigen-Value = 1269 Loading Eigen-Value = 1270 Loading Eigen-Value = 1271 Loading Eigen-Value = 1272 Loading Eigen-Value = 1273 Loading Eigen-Value = 1274 Loading Eigen-Value = 1275 Loading Eigen-Value = 1276 Loading Eigen-Value = 1277 Loading Eigen-Value = 1278 Loading Eigen-Value = 1279 Loading Eigen-Value = 1280 Loading Eigen-Value = 1281 Loading Eigen-Value = 1282 Loading Eigen-Value = 1283 Loading Eigen-Value = 1284 Loading Eigen-Value = 1285 Loading Eigen-Value = 1286 Loading Eigen-Value = 1287 Loading Eigen-Value = 1288 Loading Eigen-Value = 1289 Loading Eigen-Value = 1290 Loading Eigen-Value = 1291 Loading Eigen-Value = 1292 Loading Eigen-Value = 1293 Loading Eigen-Value = 1294 Loading Eigen-Value = 1295 Loading Eigen-Value = 1296 Loading Eigen-Value = 1297 Loading Eigen-Value = 1298 Loading Eigen-Value = 1299 Loading Eigen-Value = 1300 Loading Eigen-Value = 1301 Loading Eigen-Value = 1302 Loading Eigen-Value = 1303 Loading Eigen-Value = 1304 Loading Eigen-Value = 1305 Loading Eigen-Value = 1306 Loading Eigen-Value = 1307 Loading Eigen-Value = 1308 Loading Eigen-Value = 1309 Loading Eigen-Value = 1310 Loading Eigen-Value = 1311 Loading Eigen-Value = 1312 Loading Eigen-Value = 1313 Loading Eigen-Value = 1314 Loading Eigen-Value = 1315 Loading Eigen-Value = 1316 Loading Eigen-Value = 1317 Loading Eigen-Value = 1318 Loading Eigen-Value = 1319 Loading Eigen-Value = 1320 Loading Eigen-Value = 1321 Loading Eigen-Value = 1322 Loading Eigen-Value = 1323 Loading Eigen-Value = 1324 Loading Eigen-Value = 1325 Loading Eigen-Value = 1326 Loading Eigen-Value = 1327 Loading Eigen-Value = 1328 Loading Eigen-Value = 1329 Loading Eigen-Value = 1330 Loading Eigen-Value = 1331 Loading Eigen-Value = 1332 Loading Eigen-Value = 1333 Loading Eigen-Value = 1334 Loading Eigen-Value = 1335 Loading Eigen-Value = 1336 Loading Eigen-Value = 1337 Loading Eigen-Value = 1338 Loading Eigen-Value = 1339 Loading Eigen-Value = 1340 Loading Eigen-Value = 1341 Loading Eigen-Value = 1342 Loading Eigen-Value = 1343 Loading Eigen-Value = 1344 Loading Eigen-Value = 1345 Loading Eigen-Value = 1346 Loading Eigen-Value = 1347 Loading Eigen-Value = 1348 Loading Eigen-Value = 1349 Loading Eigen-Value = 1350 Loading Eigen-Value = 1351 Loading Eigen-Value = 1352 Loading Eigen-Value = 1353 Loading Eigen-Value = 1354 Loading Eigen-Value = 1355 Loading Eigen-Value = 1356 Loading Eigen-Value = 1357 Loading Eigen-Value = 1358 Loading Eigen-Value = 1359 Loading Eigen-Value = 1360 Loading Eigen-Value = 1361 Loading Eigen-Value = 1362 Loading Eigen-Value = 1363 Loading Eigen-Value = 1364 Loading Eigen-Value = 1365 Loading Eigen-Value = 1366 Loading Eigen-Value = 1367 Loading Eigen-Value = 1368 Loading Eigen-Value = 1369 Loading Eigen-Value = 1370 Loading Eigen-Value = 1371 Loading Eigen-Value = 1372 Loading Eigen-Value = 1373 Loading Eigen-Value = 1374 Loading Eigen-Value = 1375 Loading Eigen-Value = 1376 Loading Eigen-Value = 1377 Loading Eigen-Value = 1378 Loading Eigen-Value = 1379 Loading Eigen-Value = 1380 Loading Eigen-Value = 1381 Loading Eigen-Value = 1382 Loading Eigen-Value = 1383 Loading Eigen-Value = 1384 Loading Eigen-Value = 1385 Loading Eigen-Value = 1386 Loading Eigen-Value = 1387 Loading Eigen-Value = 1388 Loading Eigen-Value = 1389 Loading Eigen-Value = 1390 Loading Eigen-Value = 1391 Loading Eigen-Value = 1392 Loading Eigen-Value = 1393 Loading Eigen-Value = 1394 Loading Eigen-Value = 1395 Loading Eigen-Value = 1396 Loading Eigen-Value = 1397 Loading Eigen-Value = 1398 Loading Eigen-Value = 1399 Loading Eigen-Value = 1400 Loading Eigen-Value = 1401 Loading Eigen-Value = 1402 Loading Eigen-Value = 1403 Loading Eigen-Value = 1404 Loading Eigen-Value = 1405 Loading Eigen-Value = 1406 Loading Eigen-Value = 1407 Loading Eigen-Value = 1408 Loading Eigen-Value = 1409 Loading Eigen-Value = 1410 Loading Eigen-Value = 1411 Loading Eigen-Value = 1412 Loading Eigen-Value = 1413 Loading Eigen-Value = 1414 Loading Eigen-Value = 1415 Loading Eigen-Value = 1416 Loading Eigen-Value = 1417 Loading Eigen-Value = 1418 Loading Eigen-Value = 1419 Loading Eigen-Value = 1420 Loading Eigen-Value = 1421 Loading Eigen-Value = 1422 Loading Eigen-Value = 1423 Loading Eigen-Value = 1424 Loading Eigen-Value = 1425 Loading Eigen-Value = 1426 Loading Eigen-Value = 1427 Loading Eigen-Value = 1428 Loading Eigen-Value = 1429 Loading Eigen-Value = 1430 Loading Eigen-Value = 1431 Loading Eigen-Value = 1432 Loading Eigen-Value = 1433 Loading Eigen-Value = 1434 Loading Eigen-Value = 1435 Loading Eigen-Value = 1436 Loading Eigen-Value = 1437 Loading Eigen-Value = 1438 Loading Eigen-Value = 1439 Loading Eigen-Value = 1440 Loading Eigen-Value = 1441 Loading Eigen-Value = 1442 Loading Eigen-Value = 1443 Loading Eigen-Value = 1444 Loading Eigen-Value = 1445 Loading Eigen-Value = 1446 Loading Eigen-Value = 1447 Loading Eigen-Value = 1448 Loading Eigen-Value = 1449 Loading Eigen-Value = 1450 Loading Eigen-Value = 1451 Loading Eigen-Value = 1452 Loading Eigen-Value = 1453 Loading Eigen-Value = 1454 Loading Eigen-Value = 1455 Loading Eigen-Value = 1456 Loading Eigen-Value = 1457 Loading Eigen-Value = 1458 Loading Eigen-Value = 1459 Loading Eigen-Value = 1460 Loading Eigen-Value = 1461 Loading Eigen-Value = 1462 Loading Eigen-Value = 1463 Loading Eigen-Value = 1464 Loading Eigen-Value = 1465 Loading Eigen-Value = 1466 Loading Eigen-Value = 1467 Loading Eigen-Value = 1468 Loading Eigen-Value = 1469 Loading Eigen-Value = 1470 Loading Eigen-Value = 1471 Loading Eigen-Value = 1472 Loading Eigen-Value = 1473 Loading Eigen-Value = 1474 Loading Eigen-Value = 1475 Loading Eigen-Value = 1476 Loading Eigen-Value = 1477 Loading Eigen-Value = 1478 Loading Eigen-Value = 1479 Loading Eigen-Value = 1480 Loading Eigen-Value = 1481 Loading Eigen-Value = 1482 Loading Eigen-Value = 1483 Loading Eigen-Value = 1484 Loading Eigen-Value = 1485 Loading Eigen-Value = 1486 Loading Eigen-Value = 1487 Loading Eigen-Value = 1488 Loading Eigen-Value = 1489 Loading Eigen-Value = 1490 Loading Eigen-Value = 1491 Loading Eigen-Value = 1492 Loading Eigen-Value = 1493 Loading Eigen-Value = 1494 Loading Eigen-Value = 1495 Loading Eigen-Value = 1496 Loading Eigen-Value = 1497 Loading Eigen-Value = 1498 Loading Eigen-Value = 1499 Loading Eigen-Value = 1500 Loading Eigen-Value = 1501 Loading Eigen-Value = 1502 Loading Eigen-Value = 1503 Loading Eigen-Value = 1504 Loading Eigen-Value = 1505 Loading Eigen-Value = 1506 Loading Eigen-Value = 1507 Loading Eigen-Value = 1508 Loading Eigen-Value = 1509 Loading Eigen-Value = 1510 Loading Eigen-Value = 1511 Loading Eigen-Value = 1512 Loading Eigen-Value = 1513 Loading Eigen-Value = 1514 Loading Eigen-Value = 1515 Loading Eigen-Value = 1516 Loading Eigen-Value = 1517 Loading Eigen-Value = 1518 Loading Eigen-Value = 1519 Loading Eigen-Value = 1520 Loading Eigen-Value = 1521 Loading Eigen-Value = 1522 Loading Eigen-Value = 1523 Loading Eigen-Value = 1524 Loading Eigen-Value = 1525 Loading Eigen-Value = 1526 Loading Eigen-Value = 1527 Loading Eigen-Value = 1528 Loading Eigen-Value = 1529 Loading Eigen-Value = 1530 Loading Eigen-Value = 1531 Loading Eigen-Value = 1532 Loading Eigen-Value = 1533 Loading Eigen-Value = 1534 Loading Eigen-Value = 1535 Loading Eigen-Value = 1536 Loading Eigen-Value = 1537 Loading Eigen-Value = 1538 Loading Eigen-Value = 1539 Loading Eigen-Value = 1540 Loading Eigen-Value = 1541 Loading Eigen-Value = 1542 Loading Eigen-Value = 1543 Loading Eigen-Value = 1544 Loading Eigen-Value = 1545 Loading Eigen-Value = 1546 Loading Eigen-Value = 1547 Loading Eigen-Value = 1548 Loading Eigen-Value = 1549 Loading Eigen-Value = 1550 Loading Eigen-Value = 1551 Loading Eigen-Value = 1552 Loading Eigen-Value = 1553 Loading Eigen-Value = 1554 Loading Eigen-Value = 1555 Loading Eigen-Value = 1556 Loading Eigen-Value = 1557 Loading Eigen-Value = 1558 Loading Eigen-Value = 1559 Loading Eigen-Value = 1560 Loading Eigen-Value = 1561 Loading Eigen-Value = 1562 Loading Eigen-Value = 1563 Loading Eigen-Value = 1564 Loading Eigen-Value = 1565 Loading Eigen-Value = 1566 Loading Eigen-Value = 1567 Loading Eigen-Value = 1568 Loading Eigen-Value = 1569 Loading Eigen-Value = 1570 Loading Eigen-Value = 1571 Loading Eigen-Value = 1572 Loading Eigen-Value = 1573 Loading Eigen-Value = 1574 Loading Eigen-Value = 1575 Loading Eigen-Value = 1576 Loading Eigen-Value = 1577 Loading Eigen-Value = 1578 Loading Eigen-Value = 1579 Loading Eigen-Value = 1580 Loading Eigen-Value = 1581 Loading Eigen-Value = 1582 Loading Eigen-Value = 1583 Loading Eigen-Value = 1584 Loading Eigen-Value = 1585 Loading Eigen-Value = 1586 Loading Eigen-Value = 1587 Loading Eigen-Value = 1588 Loading Eigen-Value = 1589 Loading Eigen-Value = 1590 Loading Eigen-Value = 1591 Loading Eigen-Value = 1592 Loading Eigen-Value = 1593 Loading Eigen-Value = 1594 Loading Eigen-Value = 1595 Loading Eigen-Value = 1596 Loading Eigen-Value = 1597 Loading Eigen-Value = 1598 Loading Eigen-Value = 1599 Loading Eigen-Value = 1600 Loading Eigen-Value = 1601 Loading Eigen-Value = 1602 Loading Eigen-Value = 1603 Loading Eigen-Value = 1604 Loading Eigen-Value = 1605 Loading Eigen-Value = 1606 Loading Eigen-Value = 1607 Loading Eigen-Value = 1608 Loading Eigen-Value = 1609 Loading Eigen-Value = 1610 Loading Eigen-Value = 1611 Loading Eigen-Value = 1612 Loading Eigen-Value = 1613 Loading Eigen-Value = 1614 Loading Eigen-Value = 1615 Loading Eigen-Value = 1616 Loading Eigen-Value = 1617 Loading Eigen-Value = 1618 Loading Eigen-Value = 1619 Loading Eigen-Value = 1620 Loading Eigen-Value = 1621 Loading Eigen-Value = 1622 Loading Eigen-Value = 1623 Loading Eigen-Value = 1624 Loading Eigen-Value = 1625 Loading Eigen-Value = 1626 Loading Eigen-Value = 1627 Loading Eigen-Value = 1628 Loading Eigen-Value = 1629 Loading Eigen-Value = 1630 Loading Eigen-Value = 1631 Loading Eigen-Value = 1632 Loading Eigen-Value = 1633 Loading Eigen-Value = 1634 Loading Eigen-Value = 1635 Loading Eigen-Value = 1636 Loading Eigen-Value = 1637 Loading Eigen-Value = 1638 Loading Eigen-Value = 1639 Loading Eigen-Value = 1640 Loading Eigen-Value = 1641 Loading Eigen-Value = 1642 Loading Eigen-Value = 1643 Loading Eigen-Value = 1644 Loading Eigen-Value = 1645 Loading Eigen-Value = 1646 Loading Eigen-Value = 1647 Loading Eigen-Value = 1648 Loading Eigen-Value = 1649 Loading Eigen-Value = 1650 Loading Eigen-Value = 1651 Loading Eigen-Value = 1652 Loading Eigen-Value = 1653 Loading Eigen-Value = 1654 Loading Eigen-Value = 1655 Loading Eigen-Value = 1656 Loading Eigen-Value = 1657 Loading Eigen-Value = 1658 Loading Eigen-Value = 1659 Loading Eigen-Value = 1660 Loading Eigen-Value = 1661 Loading Eigen-Value = 1662 Loading Eigen-Value = 1663 Loading Eigen-Value = 1664 Loading Eigen-Value = 1665 Loading Eigen-Value = 1666 Loading Eigen-Value = 1667 Loading Eigen-Value = 1668 Loading Eigen-Value = 1669 Loading Eigen-Value = 1670 Loading Eigen-Value = 1671 Loading Eigen-Value = 1672 Loading Eigen-Value = 1673 Loading Eigen-Value = 1674 Loading Eigen-Value = 1675 Loading Eigen-Value = 1676 Loading Eigen-Value = 1677 Loading Eigen-Value = 1678 Loading Eigen-Value = 1679 Loading Eigen-Value = 1680 Loading Eigen-Value = 1681 Loading Eigen-Value = 1682 Loading Eigen-Value = 1683 Loading Eigen-Value = 1684 Loading Eigen-Value = 1685 Loading Eigen-Value = 1686 Loading Eigen-Value = 1687 Loading Eigen-Value = 1688 Loading Eigen-Value = 1689 Loading Eigen-Value = 1690 Loading Eigen-Value = 1691 Loading Eigen-Value = 1692 Loading Eigen-Value = 1693 Loading Eigen-Value = 1694 Loading Eigen-Value = 1695 Loading Eigen-Value = 1696 Loading Eigen-Value = 1697 Loading Eigen-Value = 1698 Loading Eigen-Value = 1699 Loading Eigen-Value = 1700 Loading Eigen-Value = 1701 Loading Eigen-Value = 1702 Loading Eigen-Value = 1703 Loading Eigen-Value = 1704 Loading Eigen-Value = 1705 Loading Eigen-Value = 1706 Loading Eigen-Value = 1707 Loading Eigen-Value = 1708 Loading Eigen-Value = 1709 Loading Eigen-Value = 1710 Loading Eigen-Value = 1711 Loading Eigen-Value = 1712 Loading Eigen-Value = 1713 Loading Eigen-Value = 1714 Loading Eigen-Value = 1715 Loading Eigen-Value = 1716 Loading Eigen-Value = 1717 Loading Eigen-Value = 1718 Loading Eigen-Value = 1719 Loading Eigen-Value = 1720 Loading Eigen-Value = 1721 Loading Eigen-Value = 1722 Loading Eigen-Value = 1723 Loading Eigen-Value = 1724 Loading Eigen-Value = 1725 Loading Eigen-Value = 1726 Loading Eigen-Value = 1727 Loading Eigen-Value = 1728 Loading Eigen-Value = 1729 Loading Eigen-Value = 1730 Loading Eigen-Value = 1731 Loading Eigen-Value = 1732 Loading Eigen-Value = 1733 Loading Eigen-Value = 1734 Loading Eigen-Value = 1735 Loading Eigen-Value = 1736 Loading Eigen-Value = 1737 Loading Eigen-Value = 1738 Loading Eigen-Value = 1739 Loading Eigen-Value = 1740 Loading Eigen-Value = 1741 Loading Eigen-Value = 1742 Loading Eigen-Value = 1743 Loading Eigen-Value = 1744 Loading Eigen-Value = 1745 Loading Eigen-Value = 1746 Loading Eigen-Value = 1747 Loading Eigen-Value = 1748 Loading Eigen-Value = 1749 Loading Eigen-Value = 1750 Loading Eigen-Value = 1751 Loading Eigen-Value = 1752 Loading Eigen-Value = 1753 Loading Eigen-Value = 1754 Loading Eigen-Value = 1755 Loading Eigen-Value = 1756 Loading Eigen-Value = 1757 Loading Eigen-Value = 1758 Loading Eigen-Value = 1759 Loading Eigen-Value = 1760 Loading Eigen-Value = 1761 Loading Eigen-Value = 1762 Loading Eigen-Value = 1763 Loading Eigen-Value = 1764 Loading Eigen-Value = 1765 Loading Eigen-Value = 1766 Loading Eigen-Value = 1767 Loading Eigen-Value = 1768 Loading Eigen-Value = 1769 Loading Eigen-Value = 1770 Loading Eigen-Value = 1771 Loading Eigen-Value = 1772 Loading Eigen-Value = 1773 Loading Eigen-Value = 1774 Loading Eigen-Value = 1775 Loading Eigen-Value = 1776 Loading Eigen-Value = 1777 Loading Eigen-Value = 1778 Loading Eigen-Value = 1779 Natural freq (Mode 1) = 5.91752 (Hz) Natural freq (Mode 2) = 29.92398 (Hz) Natural freq (Mode 3) = 40.01939 (Hz) Natural freq (Mode 4) = 78.26336 (Hz) Natural freq (Mode 5) = 102.48770 (Hz) Natural freq (Mode 6) = 148.28700 (Hz) Natural freq (Mode 7) = 182.97520 (Hz) Natural freq (Mode 8) = 238.39370 (Hz) Natural freq (Mode 9) = 285.36330 (Hz) Natural freq (Mode 10) = 321.90370 (Hz) Natural freq (Mode 11) = 338.36210 (Hz) Natural freq (Mode 12) = 347.87480 (Hz) Natural freq (Mode 13) = 412.76490 (Hz) Natural freq (Mode 14) = 446.89790 (Hz) Natural freq (Mode 15) = 477.26050 (Hz) Natural freq (Mode 16) = 556.73130 (Hz) Natural freq (Mode 17) = 582.55570 (Hz) Natural freq (Mode 18) = 627.20430 (Hz) Natural freq (Mode 19) = 696.67300 (Hz) Natural freq (Mode 20) = 750.94670 (Hz) Natural freq (Mode 21) = 757.10910 (Hz) Natural freq (Mode 22) = 797.86110 (Hz) Natural freq (Mode 23) = 847.03330 (Hz) Natural freq (Mode 24) = 944.72760 (Hz) Natural freq (Mode 25) = 956.33970 (Hz) Natural freq (Mode 26) = 978.56320 (Hz) Natural freq (Mode 27) = 1011.29500 (Hz) Natural freq (Mode 28) = 1121.40300 (Hz) Natural freq (Mode 29) = 1155.17800 (Hz) Natural freq (Mode 30) = 1174.22000 (Hz) Natural freq (Mode 31) = 1218.32400 (Hz) Natural freq (Mode 32) = 1289.59300 (Hz) Natural freq (Mode 33) = 1300.85200 (Hz) Natural freq (Mode 34) = 1332.20600 (Hz) Natural freq (Mode 35) = 1359.39700 (Hz) Natural freq (Mode 36) = 1412.35900 (Hz) Natural freq (Mode 37) = 1457.87000 (Hz) Natural freq (Mode 38) = 1504.80200 (Hz) Natural freq (Mode 39) = 1555.90000 (Hz) Natural freq (Mode 40) = 1607.07800 (Hz) Natural freq (Mode 41) = 1655.47400 (Hz) Natural freq (Mode 42) = 1717.08000 (Hz) Natural freq (Mode 43) = 1741.97300 (Hz) Natural freq (Mode 44) = 1801.38700 (Hz) Natural freq (Mode 45) = 1873.31100 (Hz) Natural freq (Mode 46) = 1913.09800 (Hz) Natural freq (Mode 47) = 1980.26900 (Hz) Natural freq (Mode 48) = 1991.99800 (Hz) Natural freq (Mode 49) = 2069.91300 (Hz) Natural freq (Mode 50) = 2113.76400 (Hz) Natural freq (Mode 51) = 2145.78500 (Hz) Natural freq (Mode 52) = 2175.50900 (Hz) Natural freq (Mode 53) = 2224.13400 (Hz) Natural freq (Mode 54) = 2298.75800 (Hz) Natural freq (Mode 55) = 2349.76500 (Hz) Natural freq (Mode 56) = 2413.31600 (Hz) Natural freq (Mode 57) = 2439.34000 (Hz) Natural freq (Mode 58) = 2497.21500 (Hz) Natural freq (Mode 59) = 2499.99000 (Hz) Natural freq (Mode 60) = 2549.47200 (Hz) Natural freq (Mode 61) = 2608.88800 (Hz) Natural freq (Mode 62) = 2632.75600 (Hz) Natural freq (Mode 63) = 2710.43000 (Hz) Natural freq (Mode 64) = 2747.45500 (Hz) Natural freq (Mode 65) = 2787.56600 (Hz) Natural freq (Mode 66) = 2804.88200 (Hz) Natural freq (Mode 67) = 2828.01000 (Hz) Natural freq (Mode 68) = 2891.33900 (Hz) Natural freq (Mode 69) = 2943.88700 (Hz) Natural freq (Mode 70) = 2996.34500 (Hz) Natural freq (Mode 71) = 3038.47900 (Hz) Natural freq (Mode 72) = 3110.97300 (Hz) Natural freq (Mode 73) = 3155.74800 (Hz) Natural freq (Mode 74) = 3171.54500 (Hz) Natural freq (Mode 75) = 3208.80000 (Hz) Natural freq (Mode 76) = 3270.76600 (Hz) Natural freq (Mode 77) = 3337.48000 (Hz) Natural freq (Mode 78) = 3397.62800 (Hz) Natural freq (Mode 79) = 3430.15700 (Hz) Natural freq (Mode 80) = 3486.27900 (Hz) Natural freq (Mode 81) = 3519.90500 (Hz) Natural freq (Mode 82) = 3582.41700 (Hz) Natural freq (Mode 83) = 3644.34000 (Hz) Natural freq (Mode 84) = 3690.50500 (Hz) Natural freq (Mode 85) = 3709.94700 (Hz) Natural freq (Mode 86) = 3751.86800 (Hz) Natural freq (Mode 87) = 3847.60300 (Hz) Natural freq (Mode 88) = 3881.69700 (Hz) Natural freq (Mode 89) = 3929.56900 (Hz) Natural freq (Mode 90) = 4030.33000 (Hz) Natural freq (Mode 91) = 4075.24600 (Hz) Natural freq (Mode 92) = 4112.23100 (Hz) Natural freq (Mode 93) = 4125.08800 (Hz) Natural freq (Mode 94) = 4175.94300 (Hz) Natural freq (Mode 95) = 4249.31900 (Hz) Natural freq (Mode 96) = 4326.93400 (Hz) Natural freq (Mode 97) = 4350.07800 (Hz) Natural freq (Mode 98) = 4422.66200 (Hz) Natural freq (Mode 99) = 4433.83300 (Hz) Natural freq (Mode 100) = 4490.80200 (Hz) Natural freq (Mode 101) = 4533.85600 (Hz) Natural freq (Mode 102) = 4575.81800 (Hz) Natural freq (Mode 103) = 4650.17200 (Hz) Natural freq (Mode 104) = 4653.01800 (Hz) Natural freq (Mode 105) = 4762.06400 (Hz) Natural freq (Mode 106) = 4783.26800 (Hz) Natural freq (Mode 107) = 4833.77500 (Hz) Natural freq (Mode 108) = 4859.19300 (Hz) Natural freq (Mode 109) = 4906.46000 (Hz) Natural freq (Mode 110) = 4983.49100 (Hz) Natural freq (Mode 111) = 5036.52400 (Hz) Natural freq (Mode 112) = 5088.89300 (Hz) Natural freq (Mode 113) = 5131.49800 (Hz) Natural freq (Mode 114) = 5189.45600 (Hz) Natural freq (Mode 115) = 5226.69000 (Hz) Natural freq (Mode 116) = 5312.39900 (Hz) Natural freq (Mode 117) = 5337.54300 (Hz) Natural freq (Mode 118) = 5412.15200 (Hz) Natural freq (Mode 119) = 5468.34800 (Hz) Natural freq (Mode 120) = 5515.48600 (Hz) Natural freq (Mode 121) = 5524.08000 (Hz) Natural freq (Mode 122) = 5619.29500 (Hz) Natural freq (Mode 123) = 5653.70400 (Hz) Natural freq (Mode 124) = 5733.63600 (Hz) Natural freq (Mode 125) = 5773.94900 (Hz) Natural freq (Mode 126) = 5844.35200 (Hz) Natural freq (Mode 127) = 5867.65000 (Hz) Natural freq (Mode 128) = 5906.70100 (Hz) Natural freq (Mode 129) = 5971.92900 (Hz) Natural freq (Mode 130) = 6009.02100 (Hz) Natural freq (Mode 131) = 6072.23100 (Hz) Natural freq (Mode 132) = 6114.32400 (Hz) Natural freq (Mode 133) = 6217.45300 (Hz) Natural freq (Mode 134) = 6258.33500 (Hz) Natural freq (Mode 135) = 6280.35900 (Hz) Natural freq (Mode 136) = 6328.06800 (Hz) Natural freq (Mode 137) = 6380.03600 (Hz) Natural freq (Mode 138) = 6420.51900 (Hz) Natural freq (Mode 139) = 6443.62300 (Hz) Natural freq (Mode 140) = 6482.95600 (Hz) Natural freq (Mode 141) = 6556.30700 (Hz) Natural freq (Mode 142) = 6581.93700 (Hz) Natural freq (Mode 143) = 6681.89000 (Hz) Natural freq (Mode 144) = 6710.49400 (Hz) Natural freq (Mode 145) = 6712.56300 (Hz) Natural freq (Mode 146) = 6757.85200 (Hz) Natural freq (Mode 147) = 6773.85300 (Hz) Natural freq (Mode 148) = 6855.24800 (Hz) Natural freq (Mode 149) = 6906.85000 (Hz) Natural freq (Mode 150) = 6964.86500 (Hz) Natural freq (Mode 151) = 7005.47200 (Hz) Natural freq (Mode 152) = 7093.12700 (Hz) Natural freq (Mode 153) = 7172.58500 (Hz) Natural freq (Mode 154) = 7235.36700 (Hz) Natural freq (Mode 155) = 7284.38800 (Hz) Natural freq (Mode 156) = 7339.50900 (Hz) Natural freq (Mode 157) = 7387.76000 (Hz) Natural freq (Mode 158) = 7432.07800 (Hz) Natural freq (Mode 159) = 7484.19100 (Hz) Natural freq (Mode 160) = 7505.65500 (Hz) Natural freq (Mode 161) = 7575.40800 (Hz) Natural freq (Mode 162) = 7619.31300 (Hz) Natural freq (Mode 163) = 7645.70400 (Hz) Natural freq (Mode 164) = 7763.99600 (Hz) Natural freq (Mode 165) = 7804.56500 (Hz) Natural freq (Mode 166) = 7847.62900 (Hz) Natural freq (Mode 167) = 7884.94000 (Hz) Natural freq (Mode 168) = 7971.14100 (Hz) Natural freq (Mode 169) = 7981.26000 (Hz) Natural freq (Mode 170) = 8018.25500 (Hz) Natural freq (Mode 171) = 8065.35200 (Hz) Natural freq (Mode 172) = 8190.58300 (Hz) Natural freq (Mode 173) = 8219.15300 (Hz) Natural freq (Mode 174) = 8242.49900 (Hz) Natural freq (Mode 175) = 8305.01600 (Hz) Natural freq (Mode 176) = 8338.74300 (Hz) Natural freq (Mode 177) = 8449.34200 (Hz) Natural freq (Mode 178) = 8515.47200 (Hz) Natural freq (Mode 179) = 8589.43700 (Hz) Natural freq (Mode 180) = 8616.56100 (Hz) Natural freq (Mode 181) = 8640.13700 (Hz) Natural freq (Mode 182) = 8712.28800 (Hz) Natural freq (Mode 183) = 8716.81500 (Hz) Natural freq (Mode 184) = 8787.58300 (Hz) Natural freq (Mode 185) = 8846.56900 (Hz) Natural freq (Mode 186) = 8875.50500 (Hz) Natural freq (Mode 187) = 8964.94700 (Hz) Natural freq (Mode 188) = 8992.86500 (Hz) Natural freq (Mode 189) = 9077.22400 (Hz) Natural freq (Mode 190) = 9096.26100 (Hz) Natural freq (Mode 191) = 9145.99500 (Hz) Natural freq (Mode 192) = 9199.71100 (Hz) Natural freq (Mode 193) = 9239.19700 (Hz) Natural freq (Mode 194) = 9335.28900 (Hz) Natural freq (Mode 195) = 9367.16700 (Hz) Natural freq (Mode 196) = 9496.20700 (Hz) Natural freq (Mode 197) = 9506.20900 (Hz) Natural freq (Mode 198) = 9530.04800 (Hz) Natural freq (Mode 199) = 9569.59000 (Hz) Natural freq (Mode 200) = 9612.48400 (Hz) Natural freq (Mode 201) = 9670.18300 (Hz) Natural freq (Mode 202) = 9702.23300 (Hz) Natural freq (Mode 203) = 9772.30000 (Hz) Natural freq (Mode 204) = 9825.17600 (Hz) Natural freq (Mode 205) = 9883.47700 (Hz) Natural freq (Mode 206) = 9901.35100 (Hz) Natural freq (Mode 207) = 9952.14500 (Hz) Natural freq (Mode 208) = 10096.61000 (Hz) Natural freq (Mode 209) = 10117.51000 (Hz) Natural freq (Mode 210) = 10152.60000 (Hz) Natural freq (Mode 211) = 10241.89000 (Hz) Natural freq (Mode 212) = 10283.19000 (Hz) Natural freq (Mode 213) = 10290.01000 (Hz) Natural freq (Mode 214) = 10313.76000 (Hz) Natural freq (Mode 215) = 10380.63000 (Hz) Natural freq (Mode 216) = 10423.29000 (Hz) Natural freq (Mode 217) = 10489.16000 (Hz) Natural freq (Mode 218) = 10534.94000 (Hz) Natural freq (Mode 219) = 10617.34000 (Hz) Natural freq (Mode 220) = 10692.66000 (Hz) Natural freq (Mode 221) = 10724.57000 (Hz) Natural freq (Mode 222) = 10783.30000 (Hz) Natural freq (Mode 223) = 10796.14000 (Hz) Natural freq (Mode 224) = 10837.42000 (Hz) Natural freq (Mode 225) = 10917.22000 (Hz) Natural freq (Mode 226) = 10990.39000 (Hz) Natural freq (Mode 227) = 11032.01000 (Hz) Natural freq (Mode 228) = 11066.56000 (Hz) Natural freq (Mode 229) = 11107.64000 (Hz) Natural freq (Mode 230) = 11181.18000 (Hz) Natural freq (Mode 231) = 11203.75000 (Hz) Natural freq (Mode 232) = 11301.06000 (Hz) Natural freq (Mode 233) = 11368.84000 (Hz) Natural freq (Mode 234) = 11405.65000 (Hz) Natural freq (Mode 235) = 11479.89000 (Hz) Natural freq (Mode 236) = 11556.38000 (Hz) Natural freq (Mode 237) = 11582.24000 (Hz) Natural freq (Mode 238) = 11608.71000 (Hz) Natural freq (Mode 239) = 11663.11000 (Hz) Natural freq (Mode 240) = 11767.24000 (Hz) Natural freq (Mode 241) = 11809.88000 (Hz) Natural freq (Mode 242) = 11869.78000 (Hz) Natural freq (Mode 243) = 11968.82000 (Hz) Natural freq (Mode 244) = 11983.42000 (Hz) Natural freq (Mode 245) = 12042.58000 (Hz) Natural freq (Mode 246) = 12116.63000 (Hz) Natural freq (Mode 247) = 12143.37000 (Hz) Natural freq (Mode 248) = 12143.61000 (Hz) Natural freq (Mode 249) = 12189.26000 (Hz) Natural freq (Mode 250) = 12256.66000 (Hz) Natural freq (Mode 251) = 12310.75000 (Hz) Natural freq (Mode 252) = 12364.03000 (Hz) Natural freq (Mode 253) = 12370.65000 (Hz) Natural freq (Mode 254) = 12548.26000 (Hz) Natural freq (Mode 255) = 12565.68000 (Hz) Natural freq (Mode 256) = 12594.88000 (Hz) Natural freq (Mode 257) = 12712.07000 (Hz) Natural freq (Mode 258) = 12770.17000 (Hz) Natural freq (Mode 259) = 12775.62000 (Hz) Natural freq (Mode 260) = 12825.19000 (Hz) Natural freq (Mode 261) = 12905.15000 (Hz) Natural freq (Mode 262) = 12955.70000 (Hz) Natural freq (Mode 263) = 13036.73000 (Hz) Natural freq (Mode 264) = 13054.72000 (Hz) Natural freq (Mode 265) = 13161.42000 (Hz) Natural freq (Mode 266) = 13192.61000 (Hz) Natural freq (Mode 267) = 13239.57000 (Hz) Natural freq (Mode 268) = 13284.37000 (Hz) Natural freq (Mode 269) = 13384.14000 (Hz) Natural freq (Mode 270) = 13408.39000 (Hz) Natural freq (Mode 271) = 13456.16000 (Hz) Natural freq (Mode 272) = 13472.22000 (Hz) Natural freq (Mode 273) = 13530.73000 (Hz) Natural freq (Mode 274) = 13593.85000 (Hz) Natural freq (Mode 275) = 13760.49000 (Hz) Natural freq (Mode 276) = 13785.68000 (Hz) Natural freq (Mode 277) = 13876.39000 (Hz) Natural freq (Mode 278) = 13897.87000 (Hz) Natural freq (Mode 279) = 13949.89000 (Hz) Natural freq (Mode 280) = 13982.83000 (Hz) Natural freq (Mode 281) = 14036.06000 (Hz) Natural freq (Mode 282) = 14061.26000 (Hz) Natural freq (Mode 283) = 14126.31000 (Hz) Natural freq (Mode 284) = 14289.37000 (Hz) Natural freq (Mode 285) = 14326.99000 (Hz) Natural freq (Mode 286) = 14398.55000 (Hz) Natural freq (Mode 287) = 14484.76000 (Hz) Natural freq (Mode 288) = 14489.28000 (Hz) Natural freq (Mode 289) = 14522.37000 (Hz) Natural freq (Mode 290) = 14565.89000 (Hz) Natural freq (Mode 291) = 14606.46000 (Hz) Natural freq (Mode 292) = 14649.44000 (Hz) Natural freq (Mode 293) = 14786.59000 (Hz) Natural freq (Mode 294) = 14893.02000 (Hz) Natural freq (Mode 295) = 14975.89000 (Hz) Natural freq (Mode 296) = 14990.37000 (Hz) Natural freq (Mode 297) = 15048.04000 (Hz) Natural freq (Mode 298) = 15137.92000 (Hz) Natural freq (Mode 299) = 15180.15000 (Hz) Natural freq (Mode 300) = 15208.71000 (Hz) Natural freq (Mode 301) = 15324.33000 (Hz) Natural freq (Mode 302) = 15358.41000 (Hz) Natural freq (Mode 303) = 15371.80000 (Hz) Natural freq (Mode 304) = 15469.29000 (Hz) Natural freq (Mode 305) = 15502.22000 (Hz) Natural freq (Mode 306) = 15582.06000 (Hz) Natural freq (Mode 307) = 15697.16000 (Hz) Natural freq (Mode 308) = 15716.81000 (Hz) Natural freq (Mode 309) = 15838.63000 (Hz) Natural freq (Mode 310) = 15881.20000 (Hz) Natural freq (Mode 311) = 15983.89000 (Hz) Natural freq (Mode 312) = 15994.51000 (Hz) Natural freq (Mode 313) = 16002.53000 (Hz) Natural freq (Mode 314) = 16137.48000 (Hz) Natural freq (Mode 315) = 16143.49000 (Hz) Natural freq (Mode 316) = 16191.25000 (Hz) Natural freq (Mode 317) = 16444.55000 (Hz) Natural freq (Mode 318) = 16465.20000 (Hz) Natural freq (Mode 319) = 16540.14000 (Hz) Natural freq (Mode 320) = 16545.05000 (Hz) Natural freq (Mode 321) = 16607.63000 (Hz) Natural freq (Mode 322) = 16787.41000 (Hz) Natural freq (Mode 323) = 16809.01000 (Hz) Natural freq (Mode 324) = 16854.44000 (Hz) Natural freq (Mode 325) = 16898.50000 (Hz) Natural freq (Mode 326) = 16931.53000 (Hz) Natural freq (Mode 327) = 16952.62000 (Hz) Natural freq (Mode 328) = 17074.71000 (Hz) Natural freq (Mode 329) = 17099.57000 (Hz) Natural freq (Mode 330) = 17119.86000 (Hz) Natural freq (Mode 331) = 17222.80000 (Hz) Natural freq (Mode 332) = 17266.61000 (Hz) Natural freq (Mode 333) = 17383.30000 (Hz) Natural freq (Mode 334) = 17418.65000 (Hz) Natural freq (Mode 335) = 17488.28000 (Hz) Natural freq (Mode 336) = 17541.06000 (Hz) Natural freq (Mode 337) = 17694.88000 (Hz) Natural freq (Mode 338) = 17700.81000 (Hz) Natural freq (Mode 339) = 17741.71000 (Hz) Natural freq (Mode 340) = 17800.10000 (Hz) Natural freq (Mode 341) = 17816.33000 (Hz) Natural freq (Mode 342) = 17925.23000 (Hz) Natural freq (Mode 343) = 17964.70000 (Hz) Natural freq (Mode 344) = 18050.17000 (Hz) Natural freq (Mode 345) = 18098.53000 (Hz) Natural freq (Mode 346) = 18131.22000 (Hz) Natural freq (Mode 347) = 18183.38000 (Hz) Natural freq (Mode 348) = 18215.32000 (Hz) Natural freq (Mode 349) = 18334.29000 (Hz) Natural freq (Mode 350) = 18362.53000 (Hz) Natural freq (Mode 351) = 18486.87000 (Hz) Natural freq (Mode 352) = 18591.83000 (Hz) Natural freq (Mode 353) = 18709.08000 (Hz) Natural freq (Mode 354) = 18712.34000 (Hz) Natural freq (Mode 355) = 18799.42000 (Hz) Natural freq (Mode 356) = 18829.22000 (Hz) Natural freq (Mode 357) = 18853.39000 (Hz) Natural freq (Mode 358) = 18976.00000 (Hz) Natural freq (Mode 359) = 19059.20000 (Hz) Natural freq (Mode 360) = 19125.02000 (Hz) Natural freq (Mode 361) = 19157.08000 (Hz) Natural freq (Mode 362) = 19255.37000 (Hz) Natural freq (Mode 363) = 19304.60000 (Hz) Natural freq (Mode 364) = 19419.35000 (Hz) Natural freq (Mode 365) = 19455.45000 (Hz) Natural freq (Mode 366) = 19511.95000 (Hz) Natural freq (Mode 367) = 19591.56000 (Hz) Natural freq (Mode 368) = 19646.65000 (Hz) Natural freq (Mode 369) = 19757.04000 (Hz) Natural freq (Mode 370) = 19782.00000 (Hz) Natural freq (Mode 371) = 19921.47000 (Hz) Natural freq (Mode 372) = 20038.24000 (Hz) Natural freq (Mode 373) = 20087.59000 (Hz) Natural freq (Mode 374) = 20247.26000 (Hz) Natural freq (Mode 375) = 20314.55000 (Hz) Natural freq (Mode 376) = 20347.61000 (Hz) Natural freq (Mode 377) = 20409.15000 (Hz) Natural freq (Mode 378) = 20555.38000 (Hz) Natural freq (Mode 379) = 20745.27000 (Hz) Natural freq (Mode 380) = 20826.08000 (Hz) Natural freq (Mode 381) = 20926.47000 (Hz) Natural freq (Mode 382) = 20927.93000 (Hz) Natural freq (Mode 383) = 20961.74000 (Hz) Natural freq (Mode 384) = 21049.74000 (Hz) Natural freq (Mode 385) = 21086.09000 (Hz) Natural freq (Mode 386) = 21226.15000 (Hz) Natural freq (Mode 387) = 21285.19000 (Hz) Natural freq (Mode 388) = 21322.08000 (Hz) Natural freq (Mode 389) = 21443.02000 (Hz) Natural freq (Mode 390) = 21485.59000 (Hz) Natural freq (Mode 391) = 21498.71000 (Hz) Natural freq (Mode 392) = 21600.59000 (Hz) Natural freq (Mode 393) = 21699.40000 (Hz) Natural freq (Mode 394) = 21749.01000 (Hz) Natural freq (Mode 395) = 21760.19000 (Hz) Natural freq (Mode 396) = 21871.83000 (Hz) Natural freq (Mode 397) = 21968.82000 (Hz) Natural freq (Mode 398) = 22004.93000 (Hz) Natural freq (Mode 399) = 22037.06000 (Hz) Natural freq (Mode 400) = 22132.05000 (Hz) Natural freq (Mode 401) = 22272.75000 (Hz) Natural freq (Mode 402) = 22284.71000 (Hz) Natural freq (Mode 403) = 22343.19000 (Hz) Natural freq (Mode 404) = 22492.85000 (Hz) Natural freq (Mode 405) = 22675.22000 (Hz) Natural freq (Mode 406) = 22726.67000 (Hz) Natural freq (Mode 407) = 22795.38000 (Hz) Natural freq (Mode 408) = 22847.12000 (Hz) Natural freq (Mode 409) = 23027.21000 (Hz) Natural freq (Mode 410) = 23066.16000 (Hz) Natural freq (Mode 411) = 23111.55000 (Hz) Natural freq (Mode 412) = 23264.07000 (Hz) Natural freq (Mode 413) = 23277.39000 (Hz) Natural freq (Mode 414) = 23280.87000 (Hz) Natural freq (Mode 415) = 23489.27000 (Hz) Natural freq (Mode 416) = 23508.29000 (Hz) Natural freq (Mode 417) = 23538.90000 (Hz) Natural freq (Mode 418) = 23734.87000 (Hz) Natural freq (Mode 419) = 23748.21000 (Hz) Natural freq (Mode 420) = 23776.47000 (Hz) Natural freq (Mode 421) = 23836.88000 (Hz) Natural freq (Mode 422) = 23851.33000 (Hz) Natural freq (Mode 423) = 23996.21000 (Hz) Natural freq (Mode 424) = 24072.71000 (Hz) Natural freq (Mode 425) = 24231.38000 (Hz) Natural freq (Mode 426) = 24326.89000 (Hz) Natural freq (Mode 427) = 24335.46000 (Hz) Natural freq (Mode 428) = 24378.13000 (Hz) Natural freq (Mode 429) = 24422.91000 (Hz) Natural freq (Mode 430) = 24535.55000 (Hz) Natural freq (Mode 431) = 24612.28000 (Hz) Natural freq (Mode 432) = 24749.69000 (Hz) Natural freq (Mode 433) = 24864.25000 (Hz) Natural freq (Mode 434) = 25020.23000 (Hz) Natural freq (Mode 435) = 25036.26000 (Hz) Natural freq (Mode 436) = 25255.07000 (Hz) Natural freq (Mode 437) = 25348.07000 (Hz) Natural freq (Mode 438) = 25376.09000 (Hz) Natural freq (Mode 439) = 25408.28000 (Hz) Natural freq (Mode 440) = 25484.80000 (Hz) Natural freq (Mode 441) = 25615.76000 (Hz) Natural freq (Mode 442) = 25669.87000 (Hz) Natural freq (Mode 443) = 25819.13000 (Hz) Natural freq (Mode 444) = 25981.25000 (Hz) Natural freq (Mode 445) = 25999.63000 (Hz) Natural freq (Mode 446) = 26070.56000 (Hz) Natural freq (Mode 447) = 26145.77000 (Hz) Natural freq (Mode 448) = 26279.59000 (Hz) Natural freq (Mode 449) = 26351.51000 (Hz) Natural freq (Mode 450) = 26395.38000 (Hz) Natural freq (Mode 451) = 26502.02000 (Hz) Natural freq (Mode 452) = 26532.53000 (Hz) Natural freq (Mode 453) = 26637.85000 (Hz) Natural freq (Mode 454) = 26643.48000 (Hz) Natural freq (Mode 455) = 26745.91000 (Hz) Natural freq (Mode 456) = 26934.27000 (Hz) Natural freq (Mode 457) = 27070.38000 (Hz) Natural freq (Mode 458) = 27164.86000 (Hz) Natural freq (Mode 459) = 27237.99000 (Hz) Natural freq (Mode 460) = 27380.39000 (Hz) Natural freq (Mode 461) = 27500.71000 (Hz) Natural freq (Mode 462) = 27556.49000 (Hz) Natural freq (Mode 463) = 27702.19000 (Hz) Natural freq (Mode 464) = 27702.94000 (Hz) Natural freq (Mode 465) = 27916.39000 (Hz) Natural freq (Mode 466) = 28012.95000 (Hz) Natural freq (Mode 467) = 28161.58000 (Hz) Natural freq (Mode 468) = 28179.12000 (Hz) Natural freq (Mode 469) = 28422.62000 (Hz) Natural freq (Mode 470) = 28474.77000 (Hz) Natural freq (Mode 471) = 28560.92000 (Hz) Natural freq (Mode 472) = 28566.15000 (Hz) Natural freq (Mode 473) = 28710.87000 (Hz) Natural freq (Mode 474) = 28781.45000 (Hz) Natural freq (Mode 475) = 28999.03000 (Hz) Natural freq (Mode 476) = 29078.86000 (Hz) Natural freq (Mode 477) = 29154.48000 (Hz) Natural freq (Mode 478) = 29296.92000 (Hz) Natural freq (Mode 479) = 29356.81000 (Hz) Natural freq (Mode 480) = 29380.71000 (Hz) Natural freq (Mode 481) = 29478.38000 (Hz) Natural freq (Mode 482) = 29553.13000 (Hz) Natural freq (Mode 483) = 29622.04000 (Hz) Natural freq (Mode 484) = 29712.53000 (Hz) Natural freq (Mode 485) = 30011.06000 (Hz) Natural freq (Mode 486) = 30035.66000 (Hz) Natural freq (Mode 487) = 30102.46000 (Hz) Natural freq (Mode 488) = 30209.47000 (Hz) Natural freq (Mode 489) = 30280.31000 (Hz) Natural freq (Mode 490) = 30323.96000 (Hz) Natural freq (Mode 491) = 30365.31000 (Hz) Natural freq (Mode 492) = 30520.68000 (Hz) Natural freq (Mode 493) = 30541.57000 (Hz) Natural freq (Mode 494) = 30606.26000 (Hz) Natural freq (Mode 495) = 30742.72000 (Hz) Natural freq (Mode 496) = 30869.45000 (Hz) Natural freq (Mode 497) = 30969.95000 (Hz) Natural freq (Mode 498) = 31100.58000 (Hz) Natural freq (Mode 499) = 31169.65000 (Hz) Natural freq (Mode 500) = 31244.07000 (Hz) Natural freq (Mode 501) = 31425.86000 (Hz) Natural freq (Mode 502) = 31537.51000 (Hz) Natural freq (Mode 503) = 31639.96000 (Hz) Natural freq (Mode 504) = 31754.34000 (Hz) Natural freq (Mode 505) = 31760.84000 (Hz) Natural freq (Mode 506) = 31883.20000 (Hz) Natural freq (Mode 507) = 32002.92000 (Hz) Natural freq (Mode 508) = 32220.74000 (Hz) Natural freq (Mode 509) = 32290.88000 (Hz) Natural freq (Mode 510) = 32391.40000 (Hz) Natural freq (Mode 511) = 32608.03000 (Hz) Natural freq (Mode 512) = 32647.91000 (Hz) Natural freq (Mode 513) = 32720.89000 (Hz) Natural freq (Mode 514) = 32949.41000 (Hz) Natural freq (Mode 515) = 32988.75000 (Hz) Natural freq (Mode 516) = 33115.60000 (Hz) Natural freq (Mode 517) = 33200.03000 (Hz) Natural freq (Mode 518) = 33318.92000 (Hz) Natural freq (Mode 519) = 33330.25000 (Hz) Natural freq (Mode 520) = 33333.78000 (Hz) Natural freq (Mode 521) = 33486.56000 (Hz) Natural freq (Mode 522) = 33531.17000 (Hz) Natural freq (Mode 523) = 33683.28000 (Hz) Natural freq (Mode 524) = 33797.57000 (Hz) Natural freq (Mode 525) = 33906.94000 (Hz) Natural freq (Mode 526) = 33914.80000 (Hz) Natural freq (Mode 527) = 33989.41000 (Hz) Natural freq (Mode 528) = 34210.63000 (Hz) Natural freq (Mode 529) = 34378.73000 (Hz) Natural freq (Mode 530) = 34494.40000 (Hz) Natural freq (Mode 531) = 34582.28000 (Hz) Natural freq (Mode 532) = 34836.82000 (Hz) Natural freq (Mode 533) = 34902.17000 (Hz) Natural freq (Mode 534) = 34987.61000 (Hz) Natural freq (Mode 535) = 35067.79000 (Hz) Natural freq (Mode 536) = 35153.96000 (Hz) Natural freq (Mode 537) = 35173.18000 (Hz) Natural freq (Mode 538) = 35315.79000 (Hz) Natural freq (Mode 539) = 35452.04000 (Hz) Natural freq (Mode 540) = 35564.39000 (Hz) Natural freq (Mode 541) = 35577.60000 (Hz) Natural freq (Mode 542) = 35671.63000 (Hz) Natural freq (Mode 543) = 35764.36000 (Hz) Natural freq (Mode 544) = 35817.39000 (Hz) Natural freq (Mode 545) = 35987.39000 (Hz) Natural freq (Mode 546) = 35988.65000 (Hz) Natural freq (Mode 547) = 36149.87000 (Hz) Natural freq (Mode 548) = 36216.11000 (Hz) Natural freq (Mode 549) = 36374.59000 (Hz) Natural freq (Mode 550) = 36456.40000 (Hz) Natural freq (Mode 551) = 36643.81000 (Hz) Natural freq (Mode 552) = 36841.90000 (Hz) Natural freq (Mode 553) = 36898.49000 (Hz) Natural freq (Mode 554) = 36940.48000 (Hz) Natural freq (Mode 555) = 37109.42000 (Hz) Natural freq (Mode 556) = 37109.45000 (Hz) Natural freq (Mode 557) = 37157.88000 (Hz) Natural freq (Mode 558) = 37177.07000 (Hz) Natural freq (Mode 559) = 37287.62000 (Hz) Natural freq (Mode 560) = 37387.53000 (Hz) Natural freq (Mode 561) = 37522.76000 (Hz) Natural freq (Mode 562) = 37628.77000 (Hz) Natural freq (Mode 563) = 37734.15000 (Hz) Natural freq (Mode 564) = 37824.32000 (Hz) Natural freq (Mode 565) = 37936.66000 (Hz) Natural freq (Mode 566) = 38054.42000 (Hz) Natural freq (Mode 567) = 38287.95000 (Hz) Natural freq (Mode 568) = 38432.25000 (Hz) Natural freq (Mode 569) = 38489.84000 (Hz) Natural freq (Mode 570) = 38652.49000 (Hz) Natural freq (Mode 571) = 38702.59000 (Hz) Natural freq (Mode 572) = 38877.29000 (Hz) Natural freq (Mode 573) = 39004.32000 (Hz) Natural freq (Mode 574) = 39191.21000 (Hz) Natural freq (Mode 575) = 39286.07000 (Hz) Natural freq (Mode 576) = 39329.37000 (Hz) Natural freq (Mode 577) = 39574.73000 (Hz) Natural freq (Mode 578) = 39720.89000 (Hz) Natural freq (Mode 579) = 40162.23000 (Hz) Natural freq (Mode 580) = 40253.22000 (Hz) Natural freq (Mode 581) = 40293.79000 (Hz) Natural freq (Mode 582) = 40337.32000 (Hz) Natural freq (Mode 583) = 40474.10000 (Hz) Natural freq (Mode 584) = 40602.31000 (Hz) Natural freq (Mode 585) = 40635.95000 (Hz) Natural freq (Mode 586) = 40660.85000 (Hz) Natural freq (Mode 587) = 40743.75000 (Hz) Natural freq (Mode 588) = 40756.84000 (Hz) Natural freq (Mode 589) = 40949.57000 (Hz) Natural freq (Mode 590) = 40995.24000 (Hz) Natural freq (Mode 591) = 41223.55000 (Hz) Natural freq (Mode 592) = 41359.39000 (Hz) Natural freq (Mode 593) = 41528.88000 (Hz) Natural freq (Mode 594) = 41791.72000 (Hz) Natural freq (Mode 595) = 41887.48000 (Hz) Natural freq (Mode 596) = 42118.45000 (Hz) Natural freq (Mode 597) = 42198.64000 (Hz) Natural freq (Mode 598) = 42348.55000 (Hz) Natural freq (Mode 599) = 42370.13000 (Hz) Natural freq (Mode 600) = 42416.97000 (Hz) Natural freq (Mode 601) = 42462.20000 (Hz) Natural freq (Mode 602) = 42642.21000 (Hz) Natural freq (Mode 603) = 42726.17000 (Hz) Natural freq (Mode 604) = 42854.97000 (Hz) Natural freq (Mode 605) = 42962.25000 (Hz) Natural freq (Mode 606) = 43123.13000 (Hz) Natural freq (Mode 607) = 43203.68000 (Hz) Natural freq (Mode 608) = 43400.77000 (Hz) Natural freq (Mode 609) = 43508.95000 (Hz) Natural freq (Mode 610) = 43597.38000 (Hz) Natural freq (Mode 611) = 43700.77000 (Hz) Natural freq (Mode 612) = 43704.76000 (Hz) Natural freq (Mode 613) = 43877.68000 (Hz) Natural freq (Mode 614) = 44012.25000 (Hz) Natural freq (Mode 615) = 44106.74000 (Hz) Natural freq (Mode 616) = 44292.90000 (Hz) Natural freq (Mode 617) = 44314.06000 (Hz) Natural freq (Mode 618) = 44374.05000 (Hz) Natural freq (Mode 619) = 44397.46000 (Hz) Natural freq (Mode 620) = 44586.68000 (Hz) Natural freq (Mode 621) = 44696.46000 (Hz) Natural freq (Mode 622) = 44741.60000 (Hz) Natural freq (Mode 623) = 45054.47000 (Hz) Natural freq (Mode 624) = 45140.14000 (Hz) Natural freq (Mode 625) = 45249.72000 (Hz) Natural freq (Mode 626) = 45385.59000 (Hz) Natural freq (Mode 627) = 45567.35000 (Hz) Natural freq (Mode 628) = 45605.37000 (Hz) Natural freq (Mode 629) = 45735.81000 (Hz) Natural freq (Mode 630) = 45752.43000 (Hz) Natural freq (Mode 631) = 46051.15000 (Hz) Natural freq (Mode 632) = 46420.19000 (Hz) Natural freq (Mode 633) = 46488.60000 (Hz) Natural freq (Mode 634) = 46552.35000 (Hz) Natural freq (Mode 635) = 46577.11000 (Hz) Natural freq (Mode 636) = 46578.90000 (Hz) Natural freq (Mode 637) = 46694.76000 (Hz) Natural freq (Mode 638) = 46912.64000 (Hz) Natural freq (Mode 639) = 46981.14000 (Hz) Natural freq (Mode 640) = 47193.58000 (Hz) Natural freq (Mode 641) = 47238.25000 (Hz) Natural freq (Mode 642) = 47338.20000 (Hz) Natural freq (Mode 643) = 47429.59000 (Hz) Natural freq (Mode 644) = 47576.44000 (Hz) Natural freq (Mode 645) = 47611.71000 (Hz) Natural freq (Mode 646) = 47691.93000 (Hz) Natural freq (Mode 647) = 47807.08000 (Hz) Natural freq (Mode 648) = 47890.22000 (Hz) Natural freq (Mode 649) = 47917.94000 (Hz) Natural freq (Mode 650) = 48003.06000 (Hz) Natural freq (Mode 651) = 48405.16000 (Hz) Natural freq (Mode 652) = 48501.56000 (Hz) Natural freq (Mode 653) = 48589.31000 (Hz) Natural freq (Mode 654) = 48598.45000 (Hz) Natural freq (Mode 655) = 48779.29000 (Hz) Natural freq (Mode 656) = 48883.09000 (Hz) Natural freq (Mode 657) = 48930.20000 (Hz) Natural freq (Mode 658) = 49088.71000 (Hz) Natural freq (Mode 659) = 49207.57000 (Hz) Natural freq (Mode 660) = 49256.51000 (Hz) Natural freq (Mode 661) = 49376.35000 (Hz) Natural freq (Mode 662) = 49480.93000 (Hz) Natural freq (Mode 663) = 49565.85000 (Hz) Natural freq (Mode 664) = 49718.37000 (Hz) Natural freq (Mode 665) = 49722.37000 (Hz) Natural freq (Mode 666) = 49790.09000 (Hz) Natural freq (Mode 667) = 49897.80000 (Hz) Natural freq (Mode 668) = 50054.08000 (Hz) Natural freq (Mode 669) = 50090.88000 (Hz) Natural freq (Mode 670) = 50160.08000 (Hz) Natural freq (Mode 671) = 50228.52000 (Hz) Natural freq (Mode 672) = 50465.21000 (Hz) Natural freq (Mode 673) = 50484.11000 (Hz) Natural freq (Mode 674) = 50692.21000 (Hz) Natural freq (Mode 675) = 50853.68000 (Hz) Natural freq (Mode 676) = 50857.21000 (Hz) Natural freq (Mode 677) = 50936.92000 (Hz) Natural freq (Mode 678) = 51135.05000 (Hz) Natural freq (Mode 679) = 51171.95000 (Hz) Natural freq (Mode 680) = 51382.60000 (Hz) Natural freq (Mode 681) = 51500.84000 (Hz) Natural freq (Mode 682) = 51551.45000 (Hz) Natural freq (Mode 683) = 51604.40000 (Hz) Natural freq (Mode 684) = 51794.87000 (Hz) Natural freq (Mode 685) = 51921.50000 (Hz) Natural freq (Mode 686) = 52077.61000 (Hz) Natural freq (Mode 687) = 52106.14000 (Hz) Natural freq (Mode 688) = 52156.48000 (Hz) Natural freq (Mode 689) = 52196.38000 (Hz) Natural freq (Mode 690) = 52375.95000 (Hz) Natural freq (Mode 691) = 52511.88000 (Hz) Natural freq (Mode 692) = 52690.02000 (Hz) Natural freq (Mode 693) = 52760.29000 (Hz) Natural freq (Mode 694) = 52983.51000 (Hz) Natural freq (Mode 695) = 53151.14000 (Hz) Natural freq (Mode 696) = 53168.78000 (Hz) Natural freq (Mode 697) = 53351.66000 (Hz) Natural freq (Mode 698) = 53457.94000 (Hz) Natural freq (Mode 699) = 53501.50000 (Hz) Natural freq (Mode 700) = 53568.66000 (Hz) Natural freq (Mode 701) = 53771.08000 (Hz) Natural freq (Mode 702) = 53815.28000 (Hz) Natural freq (Mode 703) = 53819.51000 (Hz) Natural freq (Mode 704) = 54018.69000 (Hz) Natural freq (Mode 705) = 54206.11000 (Hz) Natural freq (Mode 706) = 54242.44000 (Hz) Natural freq (Mode 707) = 54451.73000 (Hz) Natural freq (Mode 708) = 54504.73000 (Hz) Natural freq (Mode 709) = 54515.07000 (Hz) Natural freq (Mode 710) = 54603.34000 (Hz) Natural freq (Mode 711) = 54798.02000 (Hz) Natural freq (Mode 712) = 54826.34000 (Hz) Natural freq (Mode 713) = 54976.60000 (Hz) Natural freq (Mode 714) = 55099.90000 (Hz) Natural freq (Mode 715) = 55233.76000 (Hz) Natural freq (Mode 716) = 55312.55000 (Hz) Natural freq (Mode 717) = 55359.35000 (Hz) Natural freq (Mode 718) = 55622.14000 (Hz) Natural freq (Mode 719) = 55794.26000 (Hz) Natural freq (Mode 720) = 55892.18000 (Hz) Natural freq (Mode 721) = 56015.41000 (Hz) Natural freq (Mode 722) = 56088.41000 (Hz) Natural freq (Mode 723) = 56115.56000 (Hz) Natural freq (Mode 724) = 56334.32000 (Hz) Natural freq (Mode 725) = 56351.92000 (Hz) Natural freq (Mode 726) = 56609.43000 (Hz) Natural freq (Mode 727) = 56690.62000 (Hz) Natural freq (Mode 728) = 56781.62000 (Hz) Natural freq (Mode 729) = 56865.87000 (Hz) Natural freq (Mode 730) = 56948.31000 (Hz) Natural freq (Mode 731) = 57119.90000 (Hz) Natural freq (Mode 732) = 57228.48000 (Hz) Natural freq (Mode 733) = 57330.72000 (Hz) Natural freq (Mode 734) = 57473.44000 (Hz) Natural freq (Mode 735) = 57547.01000 (Hz) Natural freq (Mode 736) = 57627.58000 (Hz) Natural freq (Mode 737) = 57732.92000 (Hz) Natural freq (Mode 738) = 57822.45000 (Hz) Natural freq (Mode 739) = 57992.67000 (Hz) Natural freq (Mode 740) = 58178.70000 (Hz) Natural freq (Mode 741) = 58235.37000 (Hz) Natural freq (Mode 742) = 58342.95000 (Hz) Natural freq (Mode 743) = 58393.04000 (Hz) Natural freq (Mode 744) = 58548.01000 (Hz) Natural freq (Mode 745) = 58743.37000 (Hz) Natural freq (Mode 746) = 58747.77000 (Hz) Natural freq (Mode 747) = 58763.92000 (Hz) Natural freq (Mode 748) = 58967.43000 (Hz) Natural freq (Mode 749) = 59096.52000 (Hz) Natural freq (Mode 750) = 59102.65000 (Hz) Natural freq (Mode 751) = 59219.30000 (Hz) Natural freq (Mode 752) = 59386.15000 (Hz) Natural freq (Mode 753) = 59562.50000 (Hz) Natural freq (Mode 754) = 59631.56000 (Hz) Natural freq (Mode 755) = 59639.75000 (Hz) Natural freq (Mode 756) = 59712.64000 (Hz) Natural freq (Mode 757) = 59838.64000 (Hz) Natural freq (Mode 758) = 59903.59000 (Hz) Natural freq (Mode 759) = 60006.47000 (Hz) Natural freq (Mode 760) = 60127.36000 (Hz) Natural freq (Mode 761) = 60224.49000 (Hz) Natural freq (Mode 762) = 60294.48000 (Hz) Natural freq (Mode 763) = 60324.69000 (Hz) Natural freq (Mode 764) = 60396.43000 (Hz) Natural freq (Mode 765) = 60515.33000 (Hz) Natural freq (Mode 766) = 60559.32000 (Hz) Natural freq (Mode 767) = 60678.05000 (Hz) Natural freq (Mode 768) = 60828.19000 (Hz) Natural freq (Mode 769) = 60907.92000 (Hz) Natural freq (Mode 770) = 61254.36000 (Hz) Natural freq (Mode 771) = 61307.17000 (Hz) Natural freq (Mode 772) = 61381.37000 (Hz) Natural freq (Mode 773) = 61481.29000 (Hz) Natural freq (Mode 774) = 61562.68000 (Hz) Natural freq (Mode 775) = 61716.24000 (Hz) Natural freq (Mode 776) = 61781.28000 (Hz) Natural freq (Mode 777) = 61795.57000 (Hz) Natural freq (Mode 778) = 61994.89000 (Hz) Natural freq (Mode 779) = 62094.15000 (Hz) Natural freq (Mode 780) = 62113.02000 (Hz) Natural freq (Mode 781) = 62222.04000 (Hz) Natural freq (Mode 782) = 62288.52000 (Hz) Natural freq (Mode 783) = 62385.94000 (Hz) Natural freq (Mode 784) = 62396.24000 (Hz) Natural freq (Mode 785) = 62527.74000 (Hz) Natural freq (Mode 786) = 62579.81000 (Hz) Natural freq (Mode 787) = 62721.25000 (Hz) Natural freq (Mode 788) = 62738.94000 (Hz) Natural freq (Mode 789) = 62865.63000 (Hz) Natural freq (Mode 790) = 62948.16000 (Hz) Natural freq (Mode 791) = 63042.76000 (Hz) Natural freq (Mode 792) = 63143.53000 (Hz) Natural freq (Mode 793) = 63170.49000 (Hz) Natural freq (Mode 794) = 63233.18000 (Hz) Natural freq (Mode 795) = 63391.41000 (Hz) Natural freq (Mode 796) = 63540.32000 (Hz) Natural freq (Mode 797) = 63602.34000 (Hz) Natural freq (Mode 798) = 63750.55000 (Hz) Natural freq (Mode 799) = 63885.63000 (Hz) Natural freq (Mode 800) = 63965.49000 (Hz) Natural freq (Mode 801) = 64042.26000 (Hz) Natural freq (Mode 802) = 64146.40000 (Hz) Natural freq (Mode 803) = 64163.32000 (Hz) Natural freq (Mode 804) = 64321.53000 (Hz) Natural freq (Mode 805) = 64416.47000 (Hz) Natural freq (Mode 806) = 64596.16000 (Hz) Natural freq (Mode 807) = 64668.98000 (Hz) Natural freq (Mode 808) = 64816.43000 (Hz) Natural freq (Mode 809) = 64962.29000 (Hz) Natural freq (Mode 810) = 65109.30000 (Hz) Natural freq (Mode 811) = 65160.50000 (Hz) Natural freq (Mode 812) = 65187.46000 (Hz) Natural freq (Mode 813) = 65332.37000 (Hz) Natural freq (Mode 814) = 65388.61000 (Hz) Natural freq (Mode 815) = 65410.63000 (Hz) Natural freq (Mode 816) = 65475.19000 (Hz) Natural freq (Mode 817) = 65597.51000 (Hz) Natural freq (Mode 818) = 65661.34000 (Hz) Natural freq (Mode 819) = 65720.16000 (Hz) Natural freq (Mode 820) = 65867.98000 (Hz) Natural freq (Mode 821) = 66059.62000 (Hz) Natural freq (Mode 822) = 66131.58000 (Hz) Natural freq (Mode 823) = 66322.35000 (Hz) Natural freq (Mode 824) = 66464.03000 (Hz) Natural freq (Mode 825) = 66530.87000 (Hz) Natural freq (Mode 826) = 66564.12000 (Hz) Natural freq (Mode 827) = 66605.34000 (Hz) Natural freq (Mode 828) = 66789.47000 (Hz) Natural freq (Mode 829) = 66945.90000 (Hz) Natural freq (Mode 830) = 66998.07000 (Hz) Natural freq (Mode 831) = 67080.26000 (Hz) Natural freq (Mode 832) = 67189.01000 (Hz) Natural freq (Mode 833) = 67243.66000 (Hz) Natural freq (Mode 834) = 67296.74000 (Hz) Natural freq (Mode 835) = 67376.41000 (Hz) Natural freq (Mode 836) = 67513.82000 (Hz) Natural freq (Mode 837) = 67567.81000 (Hz) Natural freq (Mode 838) = 67666.32000 (Hz) Natural freq (Mode 839) = 67841.24000 (Hz) Natural freq (Mode 840) = 67908.45000 (Hz) Natural freq (Mode 841) = 68016.58000 (Hz) Natural freq (Mode 842) = 68079.98000 (Hz) Natural freq (Mode 843) = 68176.81000 (Hz) Natural freq (Mode 844) = 68460.19000 (Hz) Natural freq (Mode 845) = 68554.47000 (Hz) Natural freq (Mode 846) = 68590.22000 (Hz) Natural freq (Mode 847) = 68651.88000 (Hz) Natural freq (Mode 848) = 68687.21000 (Hz) Natural freq (Mode 849) = 68786.12000 (Hz) Natural freq (Mode 850) = 68856.07000 (Hz) Natural freq (Mode 851) = 68911.45000 (Hz) Natural freq (Mode 852) = 68921.30000 (Hz) Natural freq (Mode 853) = 69021.59000 (Hz) Natural freq (Mode 854) = 69065.40000 (Hz) Natural freq (Mode 855) = 69205.85000 (Hz) Natural freq (Mode 856) = 69252.89000 (Hz) Natural freq (Mode 857) = 69340.47000 (Hz) Natural freq (Mode 858) = 69375.84000 (Hz) Natural freq (Mode 859) = 69440.12000 (Hz) Natural freq (Mode 860) = 69512.06000 (Hz) Natural freq (Mode 861) = 69654.96000 (Hz) Natural freq (Mode 862) = 69777.94000 (Hz) Natural freq (Mode 863) = 69802.79000 (Hz) Natural freq (Mode 864) = 69841.16000 (Hz) Natural freq (Mode 865) = 69862.84000 (Hz) Natural freq (Mode 866) = 70097.50000 (Hz) Natural freq (Mode 867) = 70162.36000 (Hz) Natural freq (Mode 868) = 70263.24000 (Hz) Natural freq (Mode 869) = 70382.94000 (Hz) Natural freq (Mode 870) = 70458.26000 (Hz) Natural freq (Mode 871) = 70518.42000 (Hz) Natural freq (Mode 872) = 70586.77000 (Hz) Natural freq (Mode 873) = 70696.01000 (Hz) Natural freq (Mode 874) = 70815.79000 (Hz) Natural freq (Mode 875) = 70909.97000 (Hz) Natural freq (Mode 876) = 70983.21000 (Hz) Natural freq (Mode 877) = 71056.86000 (Hz) Natural freq (Mode 878) = 71154.90000 (Hz) Natural freq (Mode 879) = 71186.77000 (Hz) Natural freq (Mode 880) = 71297.27000 (Hz) Natural freq (Mode 881) = 71311.62000 (Hz) Natural freq (Mode 882) = 71367.08000 (Hz) Natural freq (Mode 883) = 71546.12000 (Hz) Natural freq (Mode 884) = 71616.69000 (Hz) Natural freq (Mode 885) = 71716.84000 (Hz) Natural freq (Mode 886) = 71918.26000 (Hz) Natural freq (Mode 887) = 72018.71000 (Hz) Natural freq (Mode 888) = 72140.89000 (Hz) Natural freq (Mode 889) = 72189.70000 (Hz) Natural freq (Mode 890) = 72303.92000 (Hz) Natural freq (Mode 891) = 72392.19000 (Hz) Natural freq (Mode 892) = 72479.59000 (Hz) Natural freq (Mode 893) = 72685.64000 (Hz) Natural freq (Mode 894) = 72758.08000 (Hz) Natural freq (Mode 895) = 72772.19000 (Hz) Natural freq (Mode 896) = 72899.19000 (Hz) Natural freq (Mode 897) = 73060.15000 (Hz) Natural freq (Mode 898) = 73133.38000 (Hz) Natural freq (Mode 899) = 73302.51000 (Hz) Natural freq (Mode 900) = 73340.19000 (Hz) Natural freq (Mode 901) = 73393.19000 (Hz) Natural freq (Mode 902) = 73522.47000 (Hz) Natural freq (Mode 903) = 73626.04000 (Hz) Natural freq (Mode 904) = 73721.49000 (Hz) Natural freq (Mode 905) = 73739.77000 (Hz) Natural freq (Mode 906) = 73766.51000 (Hz) Natural freq (Mode 907) = 73944.32000 (Hz) Natural freq (Mode 908) = 74006.82000 (Hz) Natural freq (Mode 909) = 74121.25000 (Hz) Natural freq (Mode 910) = 74153.07000 (Hz) Natural freq (Mode 911) = 74175.30000 (Hz) Natural freq (Mode 912) = 74249.00000 (Hz) Natural freq (Mode 913) = 74364.63000 (Hz) Natural freq (Mode 914) = 74494.14000 (Hz) Natural freq (Mode 915) = 74538.38000 (Hz) Natural freq (Mode 916) = 74634.16000 (Hz) Natural freq (Mode 917) = 74679.94000 (Hz) Natural freq (Mode 918) = 74739.85000 (Hz) Natural freq (Mode 919) = 74803.58000 (Hz) Natural freq (Mode 920) = 74993.28000 (Hz) Natural freq (Mode 921) = 75053.98000 (Hz) Natural freq (Mode 922) = 75093.93000 (Hz) Natural freq (Mode 923) = 75299.71000 (Hz) Natural freq (Mode 924) = 75358.80000 (Hz) Natural freq (Mode 925) = 75425.58000 (Hz) Natural freq (Mode 926) = 75536.12000 (Hz) Natural freq (Mode 927) = 75713.14000 (Hz) Natural freq (Mode 928) = 75834.39000 (Hz) Natural freq (Mode 929) = 75884.56000 (Hz) Natural freq (Mode 930) = 76007.14000 (Hz) Natural freq (Mode 931) = 76120.42000 (Hz) Natural freq (Mode 932) = 76225.74000 (Hz) Natural freq (Mode 933) = 76255.57000 (Hz) Natural freq (Mode 934) = 76430.79000 (Hz) Natural freq (Mode 935) = 76638.92000 (Hz) Natural freq (Mode 936) = 76687.01000 (Hz) Natural freq (Mode 937) = 76810.80000 (Hz) Natural freq (Mode 938) = 76828.09000 (Hz) Natural freq (Mode 939) = 76925.01000 (Hz) Natural freq (Mode 940) = 77008.94000 (Hz) Natural freq (Mode 941) = 77102.92000 (Hz) Natural freq (Mode 942) = 77151.28000 (Hz) Natural freq (Mode 943) = 77289.38000 (Hz) Natural freq (Mode 944) = 77372.04000 (Hz) Natural freq (Mode 945) = 77376.51000 (Hz) Natural freq (Mode 946) = 77440.76000 (Hz) Natural freq (Mode 947) = 77523.43000 (Hz) Natural freq (Mode 948) = 77561.89000 (Hz) Natural freq (Mode 949) = 77587.38000 (Hz) Natural freq (Mode 950) = 77748.95000 (Hz) Natural freq (Mode 951) = 77853.38000 (Hz) Natural freq (Mode 952) = 77858.82000 (Hz) Natural freq (Mode 953) = 77953.25000 (Hz) Natural freq (Mode 954) = 78000.41000 (Hz) Natural freq (Mode 955) = 78099.35000 (Hz) Natural freq (Mode 956) = 78253.68000 (Hz) Natural freq (Mode 957) = 78382.22000 (Hz) Natural freq (Mode 958) = 78418.48000 (Hz) Natural freq (Mode 959) = 78515.48000 (Hz) Natural freq (Mode 960) = 78610.92000 (Hz) Natural freq (Mode 961) = 78645.10000 (Hz) Natural freq (Mode 962) = 78727.57000 (Hz) Natural freq (Mode 963) = 78863.91000 (Hz) Natural freq (Mode 964) = 78937.32000 (Hz) Natural freq (Mode 965) = 79053.58000 (Hz) Natural freq (Mode 966) = 79077.26000 (Hz) Natural freq (Mode 967) = 79215.24000 (Hz) Natural freq (Mode 968) = 79294.12000 (Hz) Natural freq (Mode 969) = 79324.82000 (Hz) Natural freq (Mode 970) = 79362.91000 (Hz) Natural freq (Mode 971) = 79527.23000 (Hz) Natural freq (Mode 972) = 79611.69000 (Hz) Natural freq (Mode 973) = 79647.10000 (Hz) Natural freq (Mode 974) = 79832.89000 (Hz) Natural freq (Mode 975) = 79866.64000 (Hz) Natural freq (Mode 976) = 79970.43000 (Hz) Natural freq (Mode 977) = 80030.32000 (Hz) Natural freq (Mode 978) = 80104.74000 (Hz) Natural freq (Mode 979) = 80123.64000 (Hz) Natural freq (Mode 980) = 80182.67000 (Hz) Natural freq (Mode 981) = 80321.53000 (Hz) Natural freq (Mode 982) = 80385.61000 (Hz) Natural freq (Mode 983) = 80444.38000 (Hz) Natural freq (Mode 984) = 80581.53000 (Hz) Natural freq (Mode 985) = 80665.28000 (Hz) Natural freq (Mode 986) = 80757.29000 (Hz) Natural freq (Mode 987) = 80846.96000 (Hz) Natural freq (Mode 988) = 81004.13000 (Hz) Natural freq (Mode 989) = 81044.79000 (Hz) Natural freq (Mode 990) = 81140.53000 (Hz) Natural freq (Mode 991) = 81244.66000 (Hz) Natural freq (Mode 992) = 81434.94000 (Hz) Natural freq (Mode 993) = 81460.92000 (Hz) Natural freq (Mode 994) = 81502.50000 (Hz) Natural freq (Mode 995) = 81572.23000 (Hz) Natural freq (Mode 996) = 81703.12000 (Hz) Natural freq (Mode 997) = 81809.87000 (Hz) Natural freq (Mode 998) = 81917.77000 (Hz) Natural freq (Mode 999) = 81922.97000 (Hz) Natural freq (Mode 1000) = 82100.35000 (Hz) Natural freq (Mode 1001) = 82120.03000 (Hz) Natural freq (Mode 1002) = 82160.63000 (Hz) Natural freq (Mode 1003) = 82272.67000 (Hz) Natural freq (Mode 1004) = 82375.92000 (Hz) Natural freq (Mode 1005) = 82426.08000 (Hz) Natural freq (Mode 1006) = 82607.53000 (Hz) Natural freq (Mode 1007) = 82667.54000 (Hz) Natural freq (Mode 1008) = 82795.73000 (Hz) Natural freq (Mode 1009) = 82830.25000 (Hz) Natural freq (Mode 1010) = 82913.56000 (Hz) Natural freq (Mode 1011) = 83117.39000 (Hz) Natural freq (Mode 1012) = 83264.48000 (Hz) Natural freq (Mode 1013) = 83303.87000 (Hz) Natural freq (Mode 1014) = 83383.77000 (Hz) Natural freq (Mode 1015) = 83474.57000 (Hz) Natural freq (Mode 1016) = 83564.55000 (Hz) Natural freq (Mode 1017) = 83612.36000 (Hz) Natural freq (Mode 1018) = 83635.59000 (Hz) Natural freq (Mode 1019) = 83660.44000 (Hz) Natural freq (Mode 1020) = 83784.58000 (Hz) Natural freq (Mode 1021) = 83861.33000 (Hz) Natural freq (Mode 1022) = 83937.67000 (Hz) Natural freq (Mode 1023) = 84023.90000 (Hz) Natural freq (Mode 1024) = 84139.57000 (Hz) Natural freq (Mode 1025) = 84188.86000 (Hz) Natural freq (Mode 1026) = 84266.69000 (Hz) Natural freq (Mode 1027) = 84269.75000 (Hz) Natural freq (Mode 1028) = 84309.34000 (Hz) Natural freq (Mode 1029) = 84427.03000 (Hz) Natural freq (Mode 1030) = 84673.20000 (Hz) Natural freq (Mode 1031) = 84725.60000 (Hz) Natural freq (Mode 1032) = 84802.77000 (Hz) Natural freq (Mode 1033) = 84921.77000 (Hz) Natural freq (Mode 1034) = 84960.34000 (Hz) Natural freq (Mode 1035) = 85091.32000 (Hz) Natural freq (Mode 1036) = 85116.43000 (Hz) Natural freq (Mode 1037) = 85264.96000 (Hz) Natural freq (Mode 1038) = 85286.54000 (Hz) Natural freq (Mode 1039) = 85306.32000 (Hz) Natural freq (Mode 1040) = 85421.91000 (Hz) Natural freq (Mode 1041) = 85547.09000 (Hz) Natural freq (Mode 1042) = 85661.92000 (Hz) Natural freq (Mode 1043) = 85719.86000 (Hz) Natural freq (Mode 1044) = 85749.15000 (Hz) Natural freq (Mode 1045) = 85924.99000 (Hz) Natural freq (Mode 1046) = 86089.57000 (Hz) Natural freq (Mode 1047) = 86148.53000 (Hz) Natural freq (Mode 1048) = 86302.17000 (Hz) Natural freq (Mode 1049) = 86373.30000 (Hz) Natural freq (Mode 1050) = 86491.27000 (Hz) Natural freq (Mode 1051) = 86624.46000 (Hz) Natural freq (Mode 1052) = 86658.50000 (Hz) Natural freq (Mode 1053) = 86688.69000 (Hz) Natural freq (Mode 1054) = 86846.44000 (Hz) Natural freq (Mode 1055) = 86952.64000 (Hz) Natural freq (Mode 1056) = 87074.96000 (Hz) Natural freq (Mode 1057) = 87237.35000 (Hz) Natural freq (Mode 1058) = 87398.33000 (Hz) Natural freq (Mode 1059) = 87464.73000 (Hz) Natural freq (Mode 1060) = 87561.27000 (Hz) Natural freq (Mode 1061) = 87628.88000 (Hz) Natural freq (Mode 1062) = 87672.54000 (Hz) Natural freq (Mode 1063) = 87868.90000 (Hz) Natural freq (Mode 1064) = 87909.61000 (Hz) Natural freq (Mode 1065) = 87948.39000 (Hz) Natural freq (Mode 1066) = 88031.61000 (Hz) Natural freq (Mode 1067) = 88056.46000 (Hz) Natural freq (Mode 1068) = 88172.09000 (Hz) Natural freq (Mode 1069) = 88206.87000 (Hz) Natural freq (Mode 1070) = 88308.04000 (Hz) Natural freq (Mode 1071) = 88352.02000 (Hz) Natural freq (Mode 1072) = 88465.10000 (Hz) Natural freq (Mode 1073) = 88565.23000 (Hz) Natural freq (Mode 1074) = 88657.34000 (Hz) Natural freq (Mode 1075) = 88700.26000 (Hz) Natural freq (Mode 1076) = 88709.47000 (Hz) Natural freq (Mode 1077) = 88724.85000 (Hz) Natural freq (Mode 1078) = 88816.78000 (Hz) Natural freq (Mode 1079) = 88873.34000 (Hz) Natural freq (Mode 1080) = 89020.17000 (Hz) Natural freq (Mode 1081) = 89078.82000 (Hz) Natural freq (Mode 1082) = 89146.32000 (Hz) Natural freq (Mode 1083) = 89216.51000 (Hz) Natural freq (Mode 1084) = 89285.04000 (Hz) Natural freq (Mode 1085) = 89306.96000 (Hz) Natural freq (Mode 1086) = 89439.18000 (Hz) Natural freq (Mode 1087) = 89528.18000 (Hz) Natural freq (Mode 1088) = 89620.32000 (Hz) Natural freq (Mode 1089) = 89716.06000 (Hz) Natural freq (Mode 1090) = 89813.61000 (Hz) Natural freq (Mode 1091) = 89915.21000 (Hz) Natural freq (Mode 1092) = 89957.09000 (Hz) Natural freq (Mode 1093) = 90076.36000 (Hz) Natural freq (Mode 1094) = 90217.64000 (Hz) Natural freq (Mode 1095) = 90281.78000 (Hz) Natural freq (Mode 1096) = 90337.50000 (Hz) Natural freq (Mode 1097) = 90383.03000 (Hz) Natural freq (Mode 1098) = 90467.45000 (Hz) Natural freq (Mode 1099) = 90504.77000 (Hz) Natural freq (Mode 1100) = 90625.35000 (Hz) Natural freq (Mode 1101) = 90713.12000 (Hz) Natural freq (Mode 1102) = 90740.85000 (Hz) Natural freq (Mode 1103) = 90752.30000 (Hz) Natural freq (Mode 1104) = 90845.66000 (Hz) Natural freq (Mode 1105) = 90901.66000 (Hz) Natural freq (Mode 1106) = 91071.76000 (Hz) Natural freq (Mode 1107) = 91110.43000 (Hz) Natural freq (Mode 1108) = 91256.23000 (Hz) Natural freq (Mode 1109) = 91418.58000 (Hz) Natural freq (Mode 1110) = 91547.07000 (Hz) Natural freq (Mode 1111) = 91607.19000 (Hz) Natural freq (Mode 1112) = 91650.98000 (Hz) Natural freq (Mode 1113) = 91713.15000 (Hz) Natural freq (Mode 1114) = 91833.30000 (Hz) Natural freq (Mode 1115) = 91977.28000 (Hz) Natural freq (Mode 1116) = 92097.01000 (Hz) Natural freq (Mode 1117) = 92197.90000 (Hz) Natural freq (Mode 1118) = 92227.72000 (Hz) Natural freq (Mode 1119) = 92254.49000 (Hz) Natural freq (Mode 1120) = 92434.76000 (Hz) Natural freq (Mode 1121) = 92530.93000 (Hz) Natural freq (Mode 1122) = 92547.32000 (Hz) Natural freq (Mode 1123) = 92617.38000 (Hz) Natural freq (Mode 1124) = 92860.10000 (Hz) Natural freq (Mode 1125) = 92989.60000 (Hz) Natural freq (Mode 1126) = 93070.57000 (Hz) Natural freq (Mode 1127) = 93135.01000 (Hz) Natural freq (Mode 1128) = 93268.29000 (Hz) Natural freq (Mode 1129) = 93358.34000 (Hz) Natural freq (Mode 1130) = 93369.00000 (Hz) Natural freq (Mode 1131) = 93384.06000 (Hz) Natural freq (Mode 1132) = 93491.51000 (Hz) Natural freq (Mode 1133) = 93537.09000 (Hz) Natural freq (Mode 1134) = 93562.33000 (Hz) Natural freq (Mode 1135) = 93754.73000 (Hz) Natural freq (Mode 1136) = 93814.21000 (Hz) Natural freq (Mode 1137) = 93871.80000 (Hz) Natural freq (Mode 1138) = 93938.57000 (Hz) Natural freq (Mode 1139) = 94024.20000 (Hz) Natural freq (Mode 1140) = 94128.21000 (Hz) Natural freq (Mode 1141) = 94232.26000 (Hz) Natural freq (Mode 1142) = 94351.51000 (Hz) Natural freq (Mode 1143) = 94409.17000 (Hz) Natural freq (Mode 1144) = 94558.20000 (Hz) Natural freq (Mode 1145) = 94631.15000 (Hz) Natural freq (Mode 1146) = 94732.62000 (Hz) Natural freq (Mode 1147) = 94826.06000 (Hz) Natural freq (Mode 1148) = 94976.99000 (Hz) Natural freq (Mode 1149) = 95048.56000 (Hz) Natural freq (Mode 1150) = 95181.86000 (Hz) Natural freq (Mode 1151) = 95192.30000 (Hz) Natural freq (Mode 1152) = 95297.16000 (Hz) Natural freq (Mode 1153) = 95436.33000 (Hz) Natural freq (Mode 1154) = 95618.01000 (Hz) Natural freq (Mode 1155) = 95702.23000 (Hz) Natural freq (Mode 1156) = 95750.83000 (Hz) Natural freq (Mode 1157) = 95867.23000 (Hz) Natural freq (Mode 1158) = 95962.79000 (Hz) Natural freq (Mode 1159) = 96041.91000 (Hz) Natural freq (Mode 1160) = 96091.17000 (Hz) Natural freq (Mode 1161) = 96284.30000 (Hz) Natural freq (Mode 1162) = 96348.77000 (Hz) Natural freq (Mode 1163) = 96411.30000 (Hz) Natural freq (Mode 1164) = 96457.12000 (Hz) Natural freq (Mode 1165) = 96570.81000 (Hz) Natural freq (Mode 1166) = 96623.90000 (Hz) Natural freq (Mode 1167) = 96696.38000 (Hz) Natural freq (Mode 1168) = 96737.32000 (Hz) Natural freq (Mode 1169) = 96846.65000 (Hz) Natural freq (Mode 1170) = 97008.36000 (Hz) Natural freq (Mode 1171) = 97119.42000 (Hz) Natural freq (Mode 1172) = 97233.69000 (Hz) Natural freq (Mode 1173) = 97270.07000 (Hz) Natural freq (Mode 1174) = 97447.92000 (Hz) Natural freq (Mode 1175) = 97506.07000 (Hz) Natural freq (Mode 1176) = 97594.28000 (Hz) Natural freq (Mode 1177) = 97805.04000 (Hz) Natural freq (Mode 1178) = 97894.72000 (Hz) Natural freq (Mode 1179) = 97928.87000 (Hz) Natural freq (Mode 1180) = 97981.40000 (Hz) Natural freq (Mode 1181) = 98086.96000 (Hz) Natural freq (Mode 1182) = 98117.62000 (Hz) Natural freq (Mode 1183) = 98245.71000 (Hz) Natural freq (Mode 1184) = 98360.74000 (Hz) Natural freq (Mode 1185) = 98519.72000 (Hz) Natural freq (Mode 1186) = 98691.42000 (Hz) Natural freq (Mode 1187) = 98754.68000 (Hz) Natural freq (Mode 1188) = 98877.99000 (Hz) Natural freq (Mode 1189) = 98986.09000 (Hz) Natural freq (Mode 1190) = 99067.69000 (Hz) Natural freq (Mode 1191) = 99222.21000 (Hz) Natural freq (Mode 1192) = 99324.10000 (Hz) Natural freq (Mode 1193) = 99363.49000 (Hz) Natural freq (Mode 1194) = 99552.85000 (Hz) Natural freq (Mode 1195) = 99565.86000 (Hz) Natural freq (Mode 1196) = 99651.71000 (Hz) Natural freq (Mode 1197) = 99914.16000 (Hz) Natural freq (Mode 1198) = 99997.05000 (Hz) Natural freq (Mode 1199) = 100086.10000 (Hz) Natural freq (Mode 1200) = 100112.50000 (Hz) Natural freq (Mode 1201) = 100320.50000 (Hz) Natural freq (Mode 1202) = 100334.10000 (Hz) Natural freq (Mode 1203) = 100410.10000 (Hz) Natural freq (Mode 1204) = 100520.60000 (Hz) Natural freq (Mode 1205) = 100611.10000 (Hz) Natural freq (Mode 1206) = 100756.50000 (Hz) Natural freq (Mode 1207) = 100857.90000 (Hz) Natural freq (Mode 1208) = 100906.60000 (Hz) Natural freq (Mode 1209) = 101024.70000 (Hz) Natural freq (Mode 1210) = 101217.30000 (Hz) Natural freq (Mode 1211) = 101378.20000 (Hz) Natural freq (Mode 1212) = 101425.90000 (Hz) Natural freq (Mode 1213) = 101568.40000 (Hz) Natural freq (Mode 1214) = 101649.20000 (Hz) Natural freq (Mode 1215) = 101854.50000 (Hz) Natural freq (Mode 1216) = 101859.60000 (Hz) Natural freq (Mode 1217) = 102032.30000 (Hz) Natural freq (Mode 1218) = 102118.70000 (Hz) Natural freq (Mode 1219) = 102163.20000 (Hz) Natural freq (Mode 1220) = 102309.80000 (Hz) Natural freq (Mode 1221) = 102376.90000 (Hz) Natural freq (Mode 1222) = 102475.10000 (Hz) Natural freq (Mode 1223) = 102587.10000 (Hz) Natural freq (Mode 1224) = 102626.40000 (Hz) Natural freq (Mode 1225) = 102808.10000 (Hz) Natural freq (Mode 1226) = 102999.10000 (Hz) Natural freq (Mode 1227) = 103055.40000 (Hz) Natural freq (Mode 1228) = 103153.30000 (Hz) Natural freq (Mode 1229) = 103210.50000 (Hz) Natural freq (Mode 1230) = 103389.80000 (Hz) Natural freq (Mode 1231) = 103567.90000 (Hz) Natural freq (Mode 1232) = 103741.10000 (Hz) Natural freq (Mode 1233) = 103800.40000 (Hz) Natural freq (Mode 1234) = 103844.10000 (Hz) Natural freq (Mode 1235) = 103957.40000 (Hz) Natural freq (Mode 1236) = 104142.80000 (Hz) Natural freq (Mode 1237) = 104186.80000 (Hz) Natural freq (Mode 1238) = 104368.90000 (Hz) Natural freq (Mode 1239) = 104521.90000 (Hz) Natural freq (Mode 1240) = 104605.60000 (Hz) Natural freq (Mode 1241) = 104640.40000 (Hz) Natural freq (Mode 1242) = 104752.90000 (Hz) Natural freq (Mode 1243) = 104877.60000 (Hz) Natural freq (Mode 1244) = 104974.20000 (Hz) Natural freq (Mode 1245) = 105069.10000 (Hz) Natural freq (Mode 1246) = 105261.70000 (Hz) Natural freq (Mode 1247) = 105316.40000 (Hz) Natural freq (Mode 1248) = 105535.40000 (Hz) Natural freq (Mode 1249) = 105616.20000 (Hz) Natural freq (Mode 1250) = 105792.20000 (Hz) Natural freq (Mode 1251) = 105817.40000 (Hz) Natural freq (Mode 1252) = 105974.60000 (Hz) Natural freq (Mode 1253) = 106104.30000 (Hz) Natural freq (Mode 1254) = 106143.00000 (Hz) Natural freq (Mode 1255) = 106291.00000 (Hz) Natural freq (Mode 1256) = 106393.00000 (Hz) Natural freq (Mode 1257) = 106517.20000 (Hz) Natural freq (Mode 1258) = 106601.60000 (Hz) Natural freq (Mode 1259) = 106776.20000 (Hz) Natural freq (Mode 1260) = 106847.60000 (Hz) Natural freq (Mode 1261) = 106928.10000 (Hz) Natural freq (Mode 1262) = 107010.40000 (Hz) Natural freq (Mode 1263) = 107146.40000 (Hz) Natural freq (Mode 1264) = 107311.10000 (Hz) Natural freq (Mode 1265) = 107361.80000 (Hz) Natural freq (Mode 1266) = 107415.20000 (Hz) Natural freq (Mode 1267) = 107609.10000 (Hz) Natural freq (Mode 1268) = 107719.30000 (Hz) Natural freq (Mode 1269) = 108001.00000 (Hz) Natural freq (Mode 1270) = 108061.80000 (Hz) Natural freq (Mode 1271) = 108076.50000 (Hz) Natural freq (Mode 1272) = 108252.70000 (Hz) Natural freq (Mode 1273) = 108325.20000 (Hz) Natural freq (Mode 1274) = 108375.60000 (Hz) Natural freq (Mode 1275) = 108506.50000 (Hz) Natural freq (Mode 1276) = 108549.10000 (Hz) Natural freq (Mode 1277) = 108709.70000 (Hz) Natural freq (Mode 1278) = 108776.70000 (Hz) Natural freq (Mode 1279) = 108840.10000 (Hz) Natural freq (Mode 1280) = 109176.60000 (Hz) Natural freq (Mode 1281) = 109253.60000 (Hz) Natural freq (Mode 1282) = 109305.80000 (Hz) Natural freq (Mode 1283) = 109383.00000 (Hz) Natural freq (Mode 1284) = 109470.60000 (Hz) Natural freq (Mode 1285) = 109580.90000 (Hz) Natural freq (Mode 1286) = 109637.50000 (Hz) Natural freq (Mode 1287) = 109903.10000 (Hz) Natural freq (Mode 1288) = 109941.40000 (Hz) Natural freq (Mode 1289) = 109970.10000 (Hz) Natural freq (Mode 1290) = 110176.20000 (Hz) Natural freq (Mode 1291) = 110262.20000 (Hz) Natural freq (Mode 1292) = 110397.60000 (Hz) Natural freq (Mode 1293) = 110469.50000 (Hz) Natural freq (Mode 1294) = 110498.80000 (Hz) Natural freq (Mode 1295) = 110660.80000 (Hz) Natural freq (Mode 1296) = 110709.90000 (Hz) Natural freq (Mode 1297) = 110855.40000 (Hz) Natural freq (Mode 1298) = 111003.50000 (Hz) Natural freq (Mode 1299) = 111108.40000 (Hz) Natural freq (Mode 1300) = 111239.20000 (Hz) Natural freq (Mode 1301) = 111263.50000 (Hz) Natural freq (Mode 1302) = 111446.80000 (Hz) Natural freq (Mode 1303) = 111644.50000 (Hz) Natural freq (Mode 1304) = 111765.20000 (Hz) Natural freq (Mode 1305) = 111843.10000 (Hz) Natural freq (Mode 1306) = 111987.60000 (Hz) Natural freq (Mode 1307) = 112035.40000 (Hz) Natural freq (Mode 1308) = 112128.30000 (Hz) Natural freq (Mode 1309) = 112392.30000 (Hz) Natural freq (Mode 1310) = 112433.70000 (Hz) Natural freq (Mode 1311) = 112461.80000 (Hz) Natural freq (Mode 1312) = 112598.60000 (Hz) Natural freq (Mode 1313) = 112674.70000 (Hz) Natural freq (Mode 1314) = 112785.90000 (Hz) Natural freq (Mode 1315) = 112877.40000 (Hz) Natural freq (Mode 1316) = 112951.70000 (Hz) Natural freq (Mode 1317) = 113078.10000 (Hz) Natural freq (Mode 1318) = 113182.60000 (Hz) Natural freq (Mode 1319) = 113251.80000 (Hz) Natural freq (Mode 1320) = 113572.60000 (Hz) Natural freq (Mode 1321) = 113614.80000 (Hz) Natural freq (Mode 1322) = 113655.60000 (Hz) Natural freq (Mode 1323) = 114032.30000 (Hz) Natural freq (Mode 1324) = 114186.80000 (Hz) Natural freq (Mode 1325) = 114294.00000 (Hz) Natural freq (Mode 1326) = 114354.20000 (Hz) Natural freq (Mode 1327) = 114521.20000 (Hz) Natural freq (Mode 1328) = 114551.30000 (Hz) Natural freq (Mode 1329) = 114600.10000 (Hz) Natural freq (Mode 1330) = 114716.60000 (Hz) Natural freq (Mode 1331) = 114808.50000 (Hz) Natural freq (Mode 1332) = 114961.50000 (Hz) Natural freq (Mode 1333) = 115052.60000 (Hz) Natural freq (Mode 1334) = 115156.20000 (Hz) Natural freq (Mode 1335) = 115377.20000 (Hz) Natural freq (Mode 1336) = 115484.80000 (Hz) Natural freq (Mode 1337) = 115597.90000 (Hz) Natural freq (Mode 1338) = 115718.90000 (Hz) Natural freq (Mode 1339) = 115960.20000 (Hz) Natural freq (Mode 1340) = 116114.10000 (Hz) Natural freq (Mode 1341) = 116243.00000 (Hz) Natural freq (Mode 1342) = 116262.40000 (Hz) Natural freq (Mode 1343) = 116413.40000 (Hz) Natural freq (Mode 1344) = 116477.70000 (Hz) Natural freq (Mode 1345) = 116555.20000 (Hz) Natural freq (Mode 1346) = 116672.70000 (Hz) Natural freq (Mode 1347) = 116713.00000 (Hz) Natural freq (Mode 1348) = 116874.30000 (Hz) Natural freq (Mode 1349) = 117031.80000 (Hz) Natural freq (Mode 1350) = 117183.70000 (Hz) Natural freq (Mode 1351) = 117264.80000 (Hz) Natural freq (Mode 1352) = 117412.80000 (Hz) Natural freq (Mode 1353) = 117527.50000 (Hz) Natural freq (Mode 1354) = 117697.90000 (Hz) Natural freq (Mode 1355) = 117771.70000 (Hz) Natural freq (Mode 1356) = 117868.10000 (Hz) Natural freq (Mode 1357) = 117969.50000 (Hz) Natural freq (Mode 1358) = 118129.50000 (Hz) Natural freq (Mode 1359) = 118302.40000 (Hz) Natural freq (Mode 1360) = 118370.90000 (Hz) Natural freq (Mode 1361) = 118419.00000 (Hz) Natural freq (Mode 1362) = 118571.50000 (Hz) Natural freq (Mode 1363) = 118877.20000 (Hz) Natural freq (Mode 1364) = 118947.70000 (Hz) Natural freq (Mode 1365) = 118997.70000 (Hz) Natural freq (Mode 1366) = 119126.20000 (Hz) Natural freq (Mode 1367) = 119270.50000 (Hz) Natural freq (Mode 1368) = 119406.20000 (Hz) Natural freq (Mode 1369) = 119511.30000 (Hz) Natural freq (Mode 1370) = 119574.30000 (Hz) Natural freq (Mode 1371) = 119781.00000 (Hz) Natural freq (Mode 1372) = 119933.60000 (Hz) Natural freq (Mode 1373) = 120145.60000 (Hz) Natural freq (Mode 1374) = 120190.00000 (Hz) Natural freq (Mode 1375) = 120321.80000 (Hz) Natural freq (Mode 1376) = 120353.10000 (Hz) Natural freq (Mode 1377) = 120597.80000 (Hz) Natural freq (Mode 1378) = 120644.50000 (Hz) Natural freq (Mode 1379) = 120725.60000 (Hz) Natural freq (Mode 1380) = 120837.90000 (Hz) Natural freq (Mode 1381) = 120870.10000 (Hz) Natural freq (Mode 1382) = 121080.50000 (Hz) Natural freq (Mode 1383) = 121177.30000 (Hz) Natural freq (Mode 1384) = 121278.30000 (Hz) Natural freq (Mode 1385) = 121504.70000 (Hz) Natural freq (Mode 1386) = 121567.70000 (Hz) Natural freq (Mode 1387) = 121628.50000 (Hz) Natural freq (Mode 1388) = 121743.40000 (Hz) Natural freq (Mode 1389) = 121787.00000 (Hz) Natural freq (Mode 1390) = 122020.70000 (Hz) Natural freq (Mode 1391) = 122085.30000 (Hz) Natural freq (Mode 1392) = 122227.70000 (Hz) Natural freq (Mode 1393) = 122430.00000 (Hz) Natural freq (Mode 1394) = 122517.90000 (Hz) Natural freq (Mode 1395) = 122566.40000 (Hz) Natural freq (Mode 1396) = 122794.80000 (Hz) Natural freq (Mode 1397) = 122905.20000 (Hz) Natural freq (Mode 1398) = 123064.90000 (Hz) Natural freq (Mode 1399) = 123171.70000 (Hz) Natural freq (Mode 1400) = 123264.40000 (Hz) Natural freq (Mode 1401) = 123359.30000 (Hz) Natural freq (Mode 1402) = 123494.90000 (Hz) Natural freq (Mode 1403) = 123758.80000 (Hz) Natural freq (Mode 1404) = 123897.70000 (Hz) Natural freq (Mode 1405) = 124106.20000 (Hz) Natural freq (Mode 1406) = 124163.70000 (Hz) Natural freq (Mode 1407) = 124297.60000 (Hz) Natural freq (Mode 1408) = 124377.30000 (Hz) Natural freq (Mode 1409) = 124544.60000 (Hz) Natural freq (Mode 1410) = 124658.30000 (Hz) Natural freq (Mode 1411) = 124674.60000 (Hz) Natural freq (Mode 1412) = 124969.70000 (Hz) Natural freq (Mode 1413) = 125010.20000 (Hz) Natural freq (Mode 1414) = 125106.50000 (Hz) Natural freq (Mode 1415) = 125287.30000 (Hz) Natural freq (Mode 1416) = 125364.30000 (Hz) Natural freq (Mode 1417) = 125496.00000 (Hz) Natural freq (Mode 1418) = 125668.20000 (Hz) Natural freq (Mode 1419) = 125806.90000 (Hz) Natural freq (Mode 1420) = 125859.20000 (Hz) Natural freq (Mode 1421) = 126124.10000 (Hz) Natural freq (Mode 1422) = 126336.10000 (Hz) Natural freq (Mode 1423) = 126512.70000 (Hz) Natural freq (Mode 1424) = 126539.10000 (Hz) Natural freq (Mode 1425) = 126620.50000 (Hz) Natural freq (Mode 1426) = 126877.60000 (Hz) Natural freq (Mode 1427) = 126962.30000 (Hz) Natural freq (Mode 1428) = 127132.20000 (Hz) Natural freq (Mode 1429) = 127254.70000 (Hz) Natural freq (Mode 1430) = 127477.10000 (Hz) Natural freq (Mode 1431) = 127659.30000 (Hz) Natural freq (Mode 1432) = 127893.90000 (Hz) Natural freq (Mode 1433) = 127957.60000 (Hz) Natural freq (Mode 1434) = 128099.20000 (Hz) Natural freq (Mode 1435) = 128180.30000 (Hz) Natural freq (Mode 1436) = 128320.40000 (Hz) Natural freq (Mode 1437) = 128363.50000 (Hz) Natural freq (Mode 1438) = 128546.60000 (Hz) Natural freq (Mode 1439) = 128764.90000 (Hz) Natural freq (Mode 1440) = 128804.00000 (Hz) Natural freq (Mode 1441) = 128925.30000 (Hz) Natural freq (Mode 1442) = 128959.00000 (Hz) Natural freq (Mode 1443) = 128969.90000 (Hz) Natural freq (Mode 1444) = 129220.00000 (Hz) Natural freq (Mode 1445) = 129323.20000 (Hz) Natural freq (Mode 1446) = 129474.70000 (Hz) Natural freq (Mode 1447) = 129675.90000 (Hz) Natural freq (Mode 1448) = 129703.10000 (Hz) Natural freq (Mode 1449) = 130113.10000 (Hz) Natural freq (Mode 1450) = 130185.80000 (Hz) Natural freq (Mode 1451) = 130348.10000 (Hz) Natural freq (Mode 1452) = 130578.30000 (Hz) Natural freq (Mode 1453) = 130708.50000 (Hz) Natural freq (Mode 1454) = 130869.20000 (Hz) Natural freq (Mode 1455) = 130922.50000 (Hz) Natural freq (Mode 1456) = 131020.90000 (Hz) Natural freq (Mode 1457) = 131122.90000 (Hz) Natural freq (Mode 1458) = 131424.50000 (Hz) Natural freq (Mode 1459) = 131584.80000 (Hz) Natural freq (Mode 1460) = 131684.30000 (Hz) Natural freq (Mode 1461) = 131809.90000 (Hz) Natural freq (Mode 1462) = 131858.60000 (Hz) Natural freq (Mode 1463) = 131958.50000 (Hz) Natural freq (Mode 1464) = 132233.70000 (Hz) Natural freq (Mode 1465) = 132449.40000 (Hz) Natural freq (Mode 1466) = 132607.40000 (Hz) Natural freq (Mode 1467) = 132729.70000 (Hz) Natural freq (Mode 1468) = 132880.40000 (Hz) Natural freq (Mode 1469) = 133046.80000 (Hz) Natural freq (Mode 1470) = 133201.30000 (Hz) Natural freq (Mode 1471) = 133234.10000 (Hz) Natural freq (Mode 1472) = 133629.50000 (Hz) Natural freq (Mode 1473) = 133796.90000 (Hz) Natural freq (Mode 1474) = 133948.40000 (Hz) Natural freq (Mode 1475) = 134006.30000 (Hz) Natural freq (Mode 1476) = 134324.40000 (Hz) Natural freq (Mode 1477) = 134507.70000 (Hz) Natural freq (Mode 1478) = 134620.10000 (Hz) Natural freq (Mode 1479) = 134837.70000 (Hz) Natural freq (Mode 1480) = 134916.50000 (Hz) Natural freq (Mode 1481) = 135097.00000 (Hz) Natural freq (Mode 1482) = 135137.40000 (Hz) Natural freq (Mode 1483) = 135476.30000 (Hz) Natural freq (Mode 1484) = 135553.40000 (Hz) Natural freq (Mode 1485) = 135680.90000 (Hz) Natural freq (Mode 1486) = 135723.70000 (Hz) Natural freq (Mode 1487) = 136137.20000 (Hz) Natural freq (Mode 1488) = 136254.00000 (Hz) Natural freq (Mode 1489) = 136531.70000 (Hz) Natural freq (Mode 1490) = 136629.60000 (Hz) Natural freq (Mode 1491) = 136739.30000 (Hz) Natural freq (Mode 1492) = 136927.00000 (Hz) Natural freq (Mode 1493) = 136989.70000 (Hz) Natural freq (Mode 1494) = 137183.70000 (Hz) Natural freq (Mode 1495) = 137230.00000 (Hz) Natural freq (Mode 1496) = 137313.30000 (Hz) Natural freq (Mode 1497) = 137520.90000 (Hz) Natural freq (Mode 1498) = 137639.00000 (Hz) Natural freq (Mode 1499) = 138090.60000 (Hz) Natural freq (Mode 1500) = 138387.40000 (Hz) Natural freq (Mode 1501) = 138465.10000 (Hz) Natural freq (Mode 1502) = 138815.80000 (Hz) Natural freq (Mode 1503) = 138915.10000 (Hz) Natural freq (Mode 1504) = 138942.60000 (Hz) Natural freq (Mode 1505) = 139174.70000 (Hz) Natural freq (Mode 1506) = 139199.90000 (Hz) Natural freq (Mode 1507) = 139357.90000 (Hz) Natural freq (Mode 1508) = 139425.70000 (Hz) Natural freq (Mode 1509) = 139577.30000 (Hz) Natural freq (Mode 1510) = 139690.00000 (Hz) Natural freq (Mode 1511) = 139888.50000 (Hz) Natural freq (Mode 1512) = 140098.70000 (Hz) Natural freq (Mode 1513) = 140249.80000 (Hz) Natural freq (Mode 1514) = 140367.30000 (Hz) Natural freq (Mode 1515) = 140657.00000 (Hz) Natural freq (Mode 1516) = 140786.00000 (Hz) Natural freq (Mode 1517) = 141026.50000 (Hz) Natural freq (Mode 1518) = 141186.20000 (Hz) Natural freq (Mode 1519) = 141405.70000 (Hz) Natural freq (Mode 1520) = 141619.60000 (Hz) Natural freq (Mode 1521) = 141793.30000 (Hz) Natural freq (Mode 1522) = 142003.20000 (Hz) Natural freq (Mode 1523) = 142060.70000 (Hz) Natural freq (Mode 1524) = 142212.40000 (Hz) Natural freq (Mode 1525) = 142235.00000 (Hz) Natural freq (Mode 1526) = 142422.80000 (Hz) Natural freq (Mode 1527) = 142663.20000 (Hz) Natural freq (Mode 1528) = 143052.20000 (Hz) Natural freq (Mode 1529) = 143084.90000 (Hz) Natural freq (Mode 1530) = 143132.30000 (Hz) Natural freq (Mode 1531) = 143274.40000 (Hz) Natural freq (Mode 1532) = 143396.20000 (Hz) Natural freq (Mode 1533) = 143756.70000 (Hz) Natural freq (Mode 1534) = 143943.30000 (Hz) Natural freq (Mode 1535) = 144127.80000 (Hz) Natural freq (Mode 1536) = 144235.40000 (Hz) Natural freq (Mode 1537) = 144542.10000 (Hz) Natural freq (Mode 1538) = 144662.30000 (Hz) Natural freq (Mode 1539) = 144690.70000 (Hz) Natural freq (Mode 1540) = 144771.30000 (Hz) Natural freq (Mode 1541) = 145039.90000 (Hz) Natural freq (Mode 1542) = 145151.10000 (Hz) Natural freq (Mode 1543) = 145284.10000 (Hz) Natural freq (Mode 1544) = 145642.50000 (Hz) Natural freq (Mode 1545) = 146249.40000 (Hz) Natural freq (Mode 1546) = 146402.00000 (Hz) Natural freq (Mode 1547) = 146685.30000 (Hz) Natural freq (Mode 1548) = 146725.90000 (Hz) Natural freq (Mode 1549) = 146784.20000 (Hz) Natural freq (Mode 1550) = 146916.60000 (Hz) Natural freq (Mode 1551) = 147213.30000 (Hz) Natural freq (Mode 1552) = 147379.50000 (Hz) Natural freq (Mode 1553) = 147702.80000 (Hz) Natural freq (Mode 1554) = 148135.00000 (Hz) Natural freq (Mode 1555) = 148211.80000 (Hz) Natural freq (Mode 1556) = 148385.40000 (Hz) Natural freq (Mode 1557) = 148579.80000 (Hz) Natural freq (Mode 1558) = 148840.20000 (Hz) Natural freq (Mode 1559) = 148989.20000 (Hz) Natural freq (Mode 1560) = 149117.70000 (Hz) Natural freq (Mode 1561) = 149384.50000 (Hz) Natural freq (Mode 1562) = 149901.10000 (Hz) Natural freq (Mode 1563) = 150012.00000 (Hz) Natural freq (Mode 1564) = 150026.60000 (Hz) Natural freq (Mode 1565) = 150123.80000 (Hz) Natural freq (Mode 1566) = 150212.80000 (Hz) Natural freq (Mode 1567) = 150535.40000 (Hz) Natural freq (Mode 1568) = 150791.90000 (Hz) Natural freq (Mode 1569) = 151291.00000 (Hz) Natural freq (Mode 1570) = 151469.60000 (Hz) Natural freq (Mode 1571) = 151604.60000 (Hz) Natural freq (Mode 1572) = 151672.40000 (Hz) Natural freq (Mode 1573) = 151822.30000 (Hz) Natural freq (Mode 1574) = 152226.20000 (Hz) Natural freq (Mode 1575) = 152338.60000 (Hz) Natural freq (Mode 1576) = 152687.80000 (Hz) Natural freq (Mode 1577) = 152820.80000 (Hz) Natural freq (Mode 1578) = 153515.50000 (Hz) Natural freq (Mode 1579) = 153649.70000 (Hz) Natural freq (Mode 1580) = 153716.80000 (Hz) Natural freq (Mode 1581) = 154080.40000 (Hz) Natural freq (Mode 1582) = 154227.00000 (Hz) Natural freq (Mode 1583) = 154281.30000 (Hz) Natural freq (Mode 1584) = 154350.30000 (Hz) Natural freq (Mode 1585) = 154510.10000 (Hz) Natural freq (Mode 1586) = 154829.60000 (Hz) Natural freq (Mode 1587) = 155355.80000 (Hz) Natural freq (Mode 1588) = 155436.70000 (Hz) Natural freq (Mode 1589) = 155641.50000 (Hz) Natural freq (Mode 1590) = 155881.40000 (Hz) Natural freq (Mode 1591) = 155898.70000 (Hz) Natural freq (Mode 1592) = 156045.80000 (Hz) Natural freq (Mode 1593) = 156632.20000 (Hz) Natural freq (Mode 1594) = 156715.70000 (Hz) Natural freq (Mode 1595) = 156944.30000 (Hz) Natural freq (Mode 1596) = 156959.70000 (Hz) Natural freq (Mode 1597) = 157074.30000 (Hz) Natural freq (Mode 1598) = 157281.40000 (Hz) Natural freq (Mode 1599) = 157509.00000 (Hz) Natural freq (Mode 1600) = 157672.90000 (Hz) Natural freq (Mode 1601) = 157765.50000 (Hz) Natural freq (Mode 1602) = 157847.60000 (Hz) Natural freq (Mode 1603) = 157987.50000 (Hz) Natural freq (Mode 1604) = 158062.80000 (Hz) Natural freq (Mode 1605) = 158390.60000 (Hz) Natural freq (Mode 1606) = 158600.10000 (Hz) Natural freq (Mode 1607) = 158957.10000 (Hz) Natural freq (Mode 1608) = 159008.80000 (Hz) Natural freq (Mode 1609) = 159347.70000 (Hz) Natural freq (Mode 1610) = 159448.00000 (Hz) Natural freq (Mode 1611) = 160017.90000 (Hz) Natural freq (Mode 1612) = 160125.80000 (Hz) Natural freq (Mode 1613) = 160197.70000 (Hz) Natural freq (Mode 1614) = 160403.10000 (Hz) Natural freq (Mode 1615) = 160624.50000 (Hz) Natural freq (Mode 1616) = 160755.70000 (Hz) Natural freq (Mode 1617) = 160803.50000 (Hz) Natural freq (Mode 1618) = 160976.60000 (Hz) Natural freq (Mode 1619) = 161448.10000 (Hz) Natural freq (Mode 1620) = 161586.90000 (Hz) Natural freq (Mode 1621) = 161815.20000 (Hz) Natural freq (Mode 1622) = 161986.90000 (Hz) Natural freq (Mode 1623) = 162466.80000 (Hz) Natural freq (Mode 1624) = 162566.50000 (Hz) Natural freq (Mode 1625) = 162608.40000 (Hz) Natural freq (Mode 1626) = 162717.60000 (Hz) Natural freq (Mode 1627) = 162844.00000 (Hz) Natural freq (Mode 1628) = 163278.60000 (Hz) Natural freq (Mode 1629) = 163309.40000 (Hz) Natural freq (Mode 1630) = 163964.70000 (Hz) Natural freq (Mode 1631) = 164005.10000 (Hz) Natural freq (Mode 1632) = 164261.60000 (Hz) Natural freq (Mode 1633) = 164326.10000 (Hz) Natural freq (Mode 1634) = 164590.90000 (Hz) Natural freq (Mode 1635) = 164656.90000 (Hz) Natural freq (Mode 1636) = 165096.90000 (Hz) Natural freq (Mode 1637) = 165297.50000 (Hz) Natural freq (Mode 1638) = 165804.30000 (Hz) Natural freq (Mode 1639) = 166068.20000 (Hz) Natural freq (Mode 1640) = 166457.30000 (Hz) Natural freq (Mode 1641) = 166514.40000 (Hz) Natural freq (Mode 1642) = 166618.00000 (Hz) Natural freq (Mode 1643) = 167181.10000 (Hz) Natural freq (Mode 1644) = 167769.30000 (Hz) Natural freq (Mode 1645) = 167803.40000 (Hz) Natural freq (Mode 1646) = 167887.70000 (Hz) Natural freq (Mode 1647) = 167937.00000 (Hz) Natural freq (Mode 1648) = 168171.80000 (Hz) Natural freq (Mode 1649) = 168637.70000 (Hz) Natural freq (Mode 1650) = 168827.00000 (Hz) Natural freq (Mode 1651) = 168918.90000 (Hz) Natural freq (Mode 1652) = 169013.80000 (Hz) Natural freq (Mode 1653) = 169143.70000 (Hz) Natural freq (Mode 1654) = 169595.50000 (Hz) Natural freq (Mode 1655) = 169874.10000 (Hz) Natural freq (Mode 1656) = 169886.40000 (Hz) Natural freq (Mode 1657) = 169891.20000 (Hz) Natural freq (Mode 1658) = 169934.80000 (Hz) Natural freq (Mode 1659) = 170188.10000 (Hz) Natural freq (Mode 1660) = 170651.40000 (Hz) Natural freq (Mode 1661) = 170659.80000 (Hz) Natural freq (Mode 1662) = 171236.50000 (Hz) Natural freq (Mode 1663) = 171387.80000 (Hz) Natural freq (Mode 1664) = 171667.50000 (Hz) Natural freq (Mode 1665) = 171785.20000 (Hz) Natural freq (Mode 1666) = 172104.00000 (Hz) Natural freq (Mode 1667) = 172379.30000 (Hz) Natural freq (Mode 1668) = 172531.20000 (Hz) Natural freq (Mode 1669) = 173061.80000 (Hz) Natural freq (Mode 1670) = 173218.80000 (Hz) Natural freq (Mode 1671) = 173992.60000 (Hz) Natural freq (Mode 1672) = 174199.60000 (Hz) Natural freq (Mode 1673) = 174311.20000 (Hz) Natural freq (Mode 1674) = 174609.30000 (Hz) Natural freq (Mode 1675) = 174851.40000 (Hz) Natural freq (Mode 1676) = 175088.40000 (Hz) Natural freq (Mode 1677) = 175104.80000 (Hz) Natural freq (Mode 1678) = 175240.60000 (Hz) Natural freq (Mode 1679) = 175725.80000 (Hz) Natural freq (Mode 1680) = 175958.00000 (Hz) Natural freq (Mode 1681) = 176785.50000 (Hz) Natural freq (Mode 1682) = 176887.90000 (Hz) Natural freq (Mode 1683) = 176960.70000 (Hz) Natural freq (Mode 1684) = 177004.30000 (Hz) Natural freq (Mode 1685) = 177410.10000 (Hz) Natural freq (Mode 1686) = 177613.00000 (Hz) Natural freq (Mode 1687) = 177999.40000 (Hz) Natural freq (Mode 1688) = 178203.10000 (Hz) Natural freq (Mode 1689) = 178443.20000 (Hz) Natural freq (Mode 1690) = 179265.20000 (Hz) Natural freq (Mode 1691) = 179577.40000 (Hz) Natural freq (Mode 1692) = 179735.20000 (Hz) Natural freq (Mode 1693) = 179903.20000 (Hz) Natural freq (Mode 1694) = 180130.10000 (Hz) Natural freq (Mode 1695) = 180359.50000 (Hz) Natural freq (Mode 1696) = 180434.90000 (Hz) Natural freq (Mode 1697) = 181385.00000 (Hz) Natural freq (Mode 1698) = 181992.60000 (Hz) Natural freq (Mode 1699) = 182050.10000 (Hz) Natural freq (Mode 1700) = 182062.40000 (Hz) Natural freq (Mode 1701) = 183019.60000 (Hz) Natural freq (Mode 1702) = 183208.80000 (Hz) Natural freq (Mode 1703) = 183609.70000 (Hz) Natural freq (Mode 1704) = 184158.80000 (Hz) Natural freq (Mode 1705) = 184251.30000 (Hz) Natural freq (Mode 1706) = 184789.50000 (Hz) Natural freq (Mode 1707) = 184832.80000 (Hz) Natural freq (Mode 1708) = 185132.10000 (Hz) Natural freq (Mode 1709) = 185327.30000 (Hz) Natural freq (Mode 1710) = 185472.20000 (Hz) Natural freq (Mode 1711) = 185901.70000 (Hz) Natural freq (Mode 1712) = 186622.70000 (Hz) Natural freq (Mode 1713) = 187198.40000 (Hz) Natural freq (Mode 1714) = 187443.40000 (Hz) Natural freq (Mode 1715) = 187507.80000 (Hz) Natural freq (Mode 1716) = 187872.30000 (Hz) Natural freq (Mode 1717) = 188187.00000 (Hz) Natural freq (Mode 1718) = 188741.90000 (Hz) Natural freq (Mode 1719) = 188959.60000 (Hz) Natural freq (Mode 1720) = 189275.20000 (Hz) Natural freq (Mode 1721) = 190410.90000 (Hz) Natural freq (Mode 1722) = 190828.60000 (Hz) Natural freq (Mode 1723) = 191294.90000 (Hz) Natural freq (Mode 1724) = 191352.10000 (Hz) Natural freq (Mode 1725) = 191490.70000 (Hz) Natural freq (Mode 1726) = 191801.40000 (Hz) Natural freq (Mode 1727) = 192067.80000 (Hz) Natural freq (Mode 1728) = 192128.50000 (Hz) Natural freq (Mode 1729) = 192910.30000 (Hz) Natural freq (Mode 1730) = 193493.10000 (Hz) Natural freq (Mode 1731) = 193667.50000 (Hz) Natural freq (Mode 1732) = 193707.10000 (Hz) Natural freq (Mode 1733) = 194562.50000 (Hz) Natural freq (Mode 1734) = 194671.90000 (Hz) Natural freq (Mode 1735) = 194895.90000 (Hz) Natural freq (Mode 1736) = 195986.20000 (Hz) Natural freq (Mode 1737) = 196046.40000 (Hz) Natural freq (Mode 1738) = 196164.80000 (Hz) Natural freq (Mode 1739) = 196916.80000 (Hz) Natural freq (Mode 1740) = 196945.90000 (Hz) Natural freq (Mode 1741) = 196963.30000 (Hz) Natural freq (Mode 1742) = 198742.00000 (Hz) Natural freq (Mode 1743) = 198832.90000 (Hz) Natural freq (Mode 1744) = 199305.40000 (Hz) Natural freq (Mode 1745) = 200294.70000 (Hz) Natural freq (Mode 1746) = 200419.80000 (Hz) Natural freq (Mode 1747) = 201244.20000 (Hz) Natural freq (Mode 1748) = 201284.70000 (Hz) Natural freq (Mode 1749) = 201362.20000 (Hz) Natural freq (Mode 1750) = 201875.70000 (Hz) Natural freq (Mode 1751) = 202090.90000 (Hz) Natural freq (Mode 1752) = 202691.80000 (Hz) Natural freq (Mode 1753) = 203016.30000 (Hz) Natural freq (Mode 1754) = 204512.00000 (Hz) Natural freq (Mode 1755) = 205046.80000 (Hz) Natural freq (Mode 1756) = 205539.70000 (Hz) Natural freq (Mode 1757) = 206255.10000 (Hz) Natural freq (Mode 1758) = 209931.40000 (Hz) Natural freq (Mode 1759) = 210310.70000 (Hz) Natural freq (Mode 1760) = 211454.20000 (Hz) Natural freq (Mode 1761) = 211898.10000 (Hz) Natural freq (Mode 1762) = 212483.80000 (Hz) Natural freq (Mode 1763) = 213805.00000 (Hz) Natural freq (Mode 1764) = 215284.00000 (Hz) Natural freq (Mode 1765) = 216529.80000 (Hz) Natural freq (Mode 1766) = 217898.60000 (Hz) Natural freq (Mode 1767) = 219200.70000 (Hz) Natural freq (Mode 1768) = 220852.30000 (Hz) Natural freq (Mode 1769) = 222877.80000 (Hz) Natural freq (Mode 1770) = 223804.40000 (Hz) Natural freq (Mode 1771) = 230522.70000 (Hz) Natural freq (Mode 1772) = 231395.10000 (Hz) Natural freq (Mode 1773) = 234055.50000 (Hz) Natural freq (Mode 1774) = 237433.60000 (Hz) Natural freq (Mode 1775) = 240144.30000 (Hz) Natural freq (Mode 1776) = 240535.30000 (Hz) Natural freq (Mode 1777) = 243767.00000 (Hz) Natural freq (Mode 1778) = 253575.70000 (Hz) Natural freq (Mode 1779) = 267124.30000 (Hz) real 0m0.877s user 0m0.914s sys 0m0.218s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_CompositeWingFreq_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_Composite_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_Composite_PyTest.py test; + python -u nastran_Composite_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 49 Number of elements = 36 Number of triangle elements = 0 Number of quadrilateral elements = 36 ---------------------------- Total number of nodes = 49 Total number of elements = 36 Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = plate, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - plate Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plateTip, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 49 Number of elements = 36 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 36 Aero_Reference value is NULL - No aero reference parameters set 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 - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - cantilever No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Warning: No loads specified for case EigenAnalysis!!!! Writing mass increment cards Writing analysis cards, 0 Writing combined constraint cards Writing constraint cards Writing material cards Writing property cards Writing coordinate system cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.555s user 0m0.563s sys 0m0.231s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_Composite_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_Flutter_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_Flutter_15degree.py test; + python -u nastran_Flutter_15degree.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 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 = 133 Number of elements = 108 Number of triangle elements = 0 Number of quadrilateral elements = 108 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 = 134 Total number of elements = 108 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Root_Point, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = WingSurface, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 133 Number of elements = 108 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 108 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 = 134 Combined Number of elements = 109 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 108 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 133 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - aluminum No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Body Property name - Edge Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - PointConstraint No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Getting FEA connections....... Number of connection tuples - 1 Connection name - Root No "groupName" specified for Connection tuple Root! Looking for automatic connections from the use of capsConnectLink for Root 7 automatic connections were made for capsConnect Root (node id 134) Done getting FEA connections Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Flutter Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No loads specified for case Flutter!!!! Writing mass increment cards Writing aero card Writing analysis cards, 0 Writing constraint ADD cards Writing constraint cards Writing material cards Writing property cards Writing aeroelastic cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.519s user 0m0.606s sys 0m0.196s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_Flutter_15degree.py passed (as expected) ================================================= ================================================= + echo 'nastran_MultiLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_MultiLoadCase_PyTest.py test; + python -u nastran_MultiLoadCase_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 49 Number of elements = 36 Number of triangle elements = 0 Number of quadrilateral elements = 36 ---------------------------- Total number of nodes = 49 Total number of elements = 36 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 49 Number of elements = 36 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 36 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 5 Load name - load_0 Load name - load_1 Load name - load_2 Load name - load_3 Load name - load_4 Done getting FEA loads Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 5 Analysis name - load_0 Analysis name - load_1 Analysis name - load_2 Analysis name - load_3 Analysis name - load_4 Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case load_0, assuming all constraints are applied!!!! Warning: No constraints specified for case load_1, assuming all constraints are applied!!!! Warning: No constraints specified for case load_2, assuming all constraints are applied!!!! Warning: No constraints specified for case load_3, assuming all constraints are applied!!!! Warning: No constraints specified for case load_4, assuming all constraints are applied!!!! Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing combined constraint cards Writing load ADD cards Writing combined constraint cards Writing load ADD cards Writing combined constraint cards Writing load ADD cards Writing combined constraint cards Writing load ADD cards Writing combined constraint cards Writing load cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.539s user 0m0.606s sys 0m0.215s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_MultiLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_OptimizationMultiLoad_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_OptimizationMultiLoad_PyTest.py test; + python -u nastran_OptimizationMultiLoad_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 49 Number of elements = 36 Number of triangle elements = 0 Number of quadrilateral elements = 36 ---------------------------- Total number of nodes = 49 Total number of elements = 36 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 49 Number of elements = 36 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 36 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - load_0 Load name - load_1 Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - materialDV Design_Variable name - propertyDV Design_Variable_Relation name - materialDVR Name madeupium not found in attribute map!!!! Design_Variable_Relation name - propertyDVR Number of design variable relations - 2 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 2 Design_Constraint name - stress1 Design_Constraint name - stress2 Done getting FEA design constraints Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 2 Analysis name - load_0 Analysis name - load_1 Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case load_0, assuming all constraints are applied!!!! Warning: No constraints specified for case load_1, assuming all constraints are applied!!!! Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing combined constraint cards Writing design constraint ADD cards Writing load ADD cards Writing combined constraint cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running NASTRAN! real 0m0.517s user 0m0.574s sys 0m0.215s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_OptimizationMultiLoad_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_PlateMisc_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_PlateMisc_PyTest.py test; + python -u nastran_PlateMisc_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 49 Number of elements = 36 Number of triangle elements = 0 Number of quadrilateral elements = 36 ---------------------------- Total number of nodes = 49 Total number of elements = 36 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 49 Number of elements = 36 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 36 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 3 Load name - moment Load name - pressure Load name - thermal Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - pltvar Number of design variable relations - 0 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 1 Design_Constraint name - pltcon Done getting FEA design constraints Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.464s user 0m0.538s sys 0m0.179s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_PlateMisc_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u nastran_PyTest.py -outLevel=0 -noAnalysis 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 = 2099 Number of elements = 1853 Number of triangle elements = 0 Number of quadrilateral elements = 1853 ---------------------------- Total number of nodes = 2099 Total number of elements = 1853 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA 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 capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference 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 = 2099 Number of elements = 1853 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 1853 Aero_Reference value is NULL - No aero reference parameters set 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 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Warning: No loads specified for case EigenAnalysis!!!! Writing mass increment cards Writing analysis cards, 0 Writing combined constraint cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! Getting results for natural frequencies..... Reading Nastran FO6 file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Natural freq (Mode 1) = 0.02165 (Hz) Natural freq (Mode 2) = 0.02165 (Hz) Natural freq (Mode 3) = 0.10665 (Hz) Natural freq (Mode 4) = 0.10665 (Hz) Natural freq (Mode 5) = 0.13547 (Hz) Natural freq (Mode 6) = 0.13547 (Hz) Natural freq (Mode 7) = 0.23092 (Hz) Natural freq (Mode 8) = 0.23092 (Hz) Natural freq (Mode 9) = 0.27609 (Hz) Natural freq (Mode 10) = 0.27609 (Hz) real 0m4.338s user 0m5.654s sys 0m9.992s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_SingleLoadCase_PyTest.py test; + python -u nastran_SingleLoadCase_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.525s user 0m0.567s sys 0m0.219s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBarDesign_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_ThreeBarDesign_PyTest.py test; + python -u nastran_ThreeBarDesign_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 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 = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedForce Done getting FEA loads Getting FEA design variables....... Number of design variables - 3 Design_Variable name - Bar1A Design_Variable name - Bar2A Design_Variable name - Bar3A Design_Variable_Relation name - Bar1A Design_Variable_Relation name - Bar2A Design_Variable_Relation name - Bar3A Number of design variable relations - 3 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 3 Design_Constraint name - stress1 Design_Constraint name - stress2 Design_Constraint name - stress3 Done getting FEA design constraints Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.562s user 0m0.600s sys 0m0.214s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBarDesign_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBarFreq_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_ThreeBarFreq_PyTest.py test; + python -u nastran_ThreeBarFreq_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 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 = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Warning: No loads specified for case EigenAnalysis!!!! Writing mass increment cards Writing analysis cards, 0 Writing combined constraint cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.503s user 0m0.582s sys 0m0.196s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBarFreq_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBarLinkDesign_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_ThreeBarLinkDesign_PyTest.py test; + python -u nastran_ThreeBarLinkDesign_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 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 = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedForce Done getting FEA loads Getting FEA design variables....... Number of design variables - 3 Design_Variable name - Bar1A Design_Variable name - Bar2A Design_Variable name - Bar3A Design_Variable_Relation name - Bar1A Design_Variable_Relation name - Bar2A Design_Variable_Relation name - Bar3A Number of design variable relations - 3 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 3 Design_Constraint name - stress1 Design_Constraint name - stress2 Design_Constraint name - stress3 Done getting FEA design constraints Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.558s user 0m0.589s sys 0m0.227s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBarLinkDesign_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBarMultiLoad_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_ThreeBarMultiLoad_PyTest.py test; + python -u nastran_ThreeBarMultiLoad_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 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 = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 2 Constraint name - conOne No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement" Constraint name - conTwo No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - loadOne Load name - loadTwo Done getting FEA loads Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 2 Analysis name - caseOne Analysis name - caseTwo Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.557s user 0m0.588s sys 0m0.225s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBarMultiLoad_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBar_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_ThreeBar_PyTest.py test; + python -u nastran_ThreeBar_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 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 = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedForce Done getting FEA loads Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.528s user 0m0.599s sys 0m0.221s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBar_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_Trim_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nastran_Trim_15degree.py test; + python -u nastran_Trim_15degree.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 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 = 117 Number of elements = 96 Number of triangle elements = 0 Number of quadrilateral elements = 96 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 = 118 Total number of elements = 96 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Root_Point, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = WingSurface, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 117 Number of elements = 96 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 96 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 = 118 Combined Number of elements = 97 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 96 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 117 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - aluminum No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - Body Property name - Edge Property name - Root Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - PointConstraint No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - PointSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Root No "groupName" specified for Connection tuple Root! Looking for automatic connections from the use of capsConnectLink for Root 9 automatic connections were made for capsConnect Root (node id 118) Done getting FEA connections Getting FEA loads....... Number of loads - 2 Load name - GravityLoad No "groupName" specified for Load tuple GravityLoad, going to use load name Load name - PointLoad Done getting FEA loads Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No loads specified for case Trim, assuming all loads are applied!!!! Writing mass increment cards Writing aeros card Writing aestat cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m0.544s user 0m0.585s sys 0m0.209s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_Trim_15degree.py passed (as expected) ================================================= Running.... AEROELASTIC PyTests ================================================= + echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aeroelasticSimple_Pressure_SU2_and_Astros.py test; + python -u aeroelasticSimple_Pressure_SU2_and_Astros.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1293 2452 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1298 2462 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3418 6687 0 AFLR4 : Nodes, Trias,Quads= 3008 5867 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1316 2498 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1319 2504 0 AFLR4 : Nodes, Trias,Quads= 1294 2454 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 200 344 0 AFLR4 : Nodes, Trias,Quads= 160 264 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 193 330 0 AFLR4 : Nodes, Trias,Quads= 155 254 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17 21 0 AFLR4 : Nodes, Trias,Quads= 11 9 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9343 18682 928 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 9343 18682 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1337 2540 0 AFLR4 : Nodes, Trias,Quads= 1321 2508 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1339 2544 0 AFLR4 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3782 7410 0 AFLR4 : Nodes, Trias,Quads= 2950 5746 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1339 2544 0 AFLR4 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1338 2542 0 AFLR4 : Nodes, Trias,Quads= 1322 2510 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1340 2546 0 AFLR4 : Nodes, Trias,Quads= 1321 2508 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 233 404 0 AFLR4 : Nodes, Trias,Quads= 210 358 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 224 386 0 AFLR4 : Nodes, Trias,Quads= 196 330 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 18 22 0 AFLR4 : Nodes, Trias,Quads= 12 10 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9489 18974 946 OVERALL : CPU Time = 0.163 seconds Body 1 (of 1) Number of nodes = 9489 Number of elements = 18974 Number of triangle elements = 18974 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9489 Total number of elements = 18974 Total number of triangle elements = 18974 Total number of quadrilateral elements = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 60093 Number of elements = 345939 Number of triangles = 18974 Number of quadrilatarals = 0 Number of tetrahedrals = 326965 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 - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Info: No recognized data transfer names found. Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelasticSimple_Pressure_SA.dat. Surface file name: surface_flow_aeroelasticSimple_Pressure_SA. Volume file name: flow_aeroelasticSimple_Pressure_SA. Restart file name: restart_flow_aeroelasticSimple_Pressure_SA.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 60093 grid points. 326965 volume elements. 3 surface markers. 12530 boundary elements in index 0 (Marker = BC_1). 5746 boundary elements in index 1 (Marker = BC_2). 698 boundary elements in index 2 (Marker = BC_3). 326965 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 83.4538. Mean K: 0.86237. Standard deviation K: 5.00385. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 54.7348| 86.8035| | CV Face Area Aspect Ratio| 1.06478| 21.5651| | CV Sub-Volume Ratio| 1| 8.64744| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 60093| 1/1.00| 10| | 1| 10214| 1/5.88| 8.309| | 2| 1799| 1/5.68| 6.98637| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 9.2451 m^2. Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m. Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 1.4064e+00| -1.355330| 0.925001| 0.586785| 4.113776| -0.972828| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.4108e+00| -1.745808| 0.767133| 0.413608| 3.711112| -0.534020| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.3978e+00| -1.758263| 0.583631| 0.231030| 3.699433| 1.633106| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.75826| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Pressure_SA.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat). |CSV file |surface_flow_aeroelasticSimple_Pressure_SA.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat). |Tecplot binary |flow_aeroelasticSimple_Pressure_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Pressure_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.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) ------------------------ Running PostAnalysis ...... su2 Running ...... astros Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA 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, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 180 Number of elements = 194 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 32 Elemental Quad4 = 162 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv Number of variables = 16 Number of data points = 361 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 3.101730e+09, tgt = 3.101730e+09, diff = 3.131247e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv Number of variables = 16 Number of data points = 361 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 3.017948e+09, tgt = 3.017948e+09, diff = 2.034838e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv Number of variables = 16 Number of data points = 361 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 4.372770e+07, tgt = 4.372770e+07, diff = 1.404514e-02 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m16.192s user 0m16.283s sys 0m1.377s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aeroelasticSimple_Displacement_SU2_and_Astros.py test; + python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... astros Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA 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, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 180 Number of elements = 194 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 32 Elemental Quad4 = 162 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureInternal Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Running PostAnalysis ...... astros Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1293 2452 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1298 2462 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3418 6687 0 AFLR4 : Nodes, Trias,Quads= 3008 5867 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1316 2498 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1319 2504 0 AFLR4 : Nodes, Trias,Quads= 1294 2454 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 200 344 0 AFLR4 : Nodes, Trias,Quads= 160 264 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 193 330 0 AFLR4 : Nodes, Trias,Quads= 155 254 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17 21 0 AFLR4 : Nodes, Trias,Quads= 11 9 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9343 18682 928 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 9343 18682 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1337 2540 0 AFLR4 : Nodes, Trias,Quads= 1321 2508 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1339 2544 0 AFLR4 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3782 7410 0 AFLR4 : Nodes, Trias,Quads= 2950 5746 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1339 2544 0 AFLR4 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1338 2542 0 AFLR4 : Nodes, Trias,Quads= 1322 2510 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1340 2546 0 AFLR4 : Nodes, Trias,Quads= 1321 2508 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 233 404 0 AFLR4 : Nodes, Trias,Quads= 210 358 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 224 386 0 AFLR4 : Nodes, Trias,Quads= 196 330 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 18 22 0 AFLR4 : Nodes, Trias,Quads= 12 10 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9489 18974 946 OVERALL : CPU Time = 0.161 seconds Body 1 (of 1) Number of nodes = 9489 Number of elements = 18974 Number of triangle elements = 18974 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9489 Total number of elements = 18974 Total number of triangle elements = 18974 Total number of quadrilateral elements = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 60093 Number of elements = 345939 Number of triangles = 18974 Number of quadrilatarals = 0 Number of tetrahedrals = 326965 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 - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Displacement_SA_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, 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 . | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 60093 grid points. 326965 volume elements. 3 surface markers. 12530 boundary elements in index 0 (Marker = BC_1). 5746 boundary elements in index 1 (Marker = BC_2). 698 boundary elements in index 2 (Marker = BC_3). 326965 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. All volume elements are correctly orientend. All surface elements are correctly orientend. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 63999.5. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 13.245034 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelasticSimple_Displacement_SA.dat. Surface file name: surface_flow_aeroelasticSimple_Displacement_SA. Volume file name: flow_aeroelasticSimple_Displacement_SA. Restart file name: restart_flow_aeroelasticSimple_Displacement_SA.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 60093 grid points. 326965 volume elements. 3 surface markers. 12530 boundary elements in index 0 (Marker = BC_1). 5746 boundary elements in index 1 (Marker = BC_2). 698 boundary elements in index 2 (Marker = BC_3). 326965 tetrahedra. 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 3 TETRAHEDRON volume elements. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 63997.8. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 83.9101. Mean K: 0.902367. Standard deviation K: 4.47382. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 42.5942| 86.8036| | CV Face Area Aspect Ratio| 1.05478| 23.5105| | CV Sub-Volume Ratio| 1| 134.901| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 60093| 1/1.00| 10| | 1| 10214| 1/5.88| 8.309| | 2| 1799| 1/5.68| 6.98637| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.89892 m. Wetted area = 11.6151 m^2. Area projection in the x-plane = 2.90002 m^2, y-plane = 1.28883 m^2, z-plane = 4.27937 m^2. Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89892 m, z-direction = 0.526515 m. Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86329e-18 m, z-direction = -0.706552 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 1.4117e+00| -0.685108| 1.753422| 1.256019| 4.783998| 0.049188| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.3876e+00| -1.120721| 1.479573| 1.113372| 4.351408| 0.028658| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.3940e+00| -1.141622| 1.261036| 0.931565| 4.324727| 0.031964| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.14162| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Displacement_SA.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). |CSV file |surface_flow_aeroelasticSimple_Displacement_SA.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). |Tecplot binary |flow_aeroelasticSimple_Displacement_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Displacement_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.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) ------------------------ Running PostAnalysis ...... su2 real 0m34.998s user 0m34.421s sys 0m2.226s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelasticSimple_Displacement_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + echo 'aeroelasticSimple_Iterative_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aeroelasticSimple_Iterative_SU2_and_Astros.py test; + python -u aeroelasticSimple_Iterative_SU2_and_Astros.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 2 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 381 692 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 374 678 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 927 1777 0 AFLR4 : Nodes, Trias,Quads= 821 1565 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 374 678 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 378 686 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 63 96 0 AFLR4 : Nodes, Trias,Quads= 55 80 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 64 96 0 AFLR4 : Nodes, Trias,Quads= 57 82 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 7 5 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 2592 5180 482 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 2592 5180 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 385 700 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 385 700 0 AFLR4 : Nodes, Trias,Quads= 381 692 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 1009 1939 0 AFLR4 : Nodes, Trias,Quads= 953 1827 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 383 696 0 AFLR4 : Nodes, Trias,Quads= 378 686 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 383 696 0 AFLR4 : Nodes, Trias,Quads= 382 694 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 381 692 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 74 115 0 AFLR4 : Nodes, Trias,Quads= 65 97 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 75 116 0 AFLR4 : Nodes, Trias,Quads= 63 92 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 2739 5474 490 OVERALL : CPU Time = 0.066 seconds Body 1 (of 1) Number of nodes = 2739 Number of elements = 5474 Number of triangle elements = 5474 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2739 Total number of elements = 5474 Total number of triangle elements = 5474 Total number of quadrilateral elements = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 11301 Number of elements = 64025 Number of triangles = 5474 Number of quadrilatarals = 0 Number of tetrahedrals = 58551 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 - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 47.1143. Mean K: 0.755059. Standard deviation K: 3.51124. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 54.7348| 85.4032| | CV Face Area Aspect Ratio| 1.05389| 21.5536| | CV Sub-Volume Ratio| 1| 13.9349| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11301| 1/1.00| 10| | 1| 2021| 1/5.59| 8.45099| | 2| 414| 1/4.88| 7.47269| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 8.08979 m^2. Area projection in the x-plane = 0.572014 m^2, y-plane = 0.261888 m^2, z-plane = 3.84035 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380358 m. Min. coordinate in the x-direction = 0 m, y-direction = -2.8602e-18 m, z-direction = -0.0467106 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.3569e-01| -0.790402| 1.509543| 1.185099| 4.678704| -1.072828| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.2750e-01| -1.125423| 1.402824| 1.016209| 4.328795| -0.842279| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.2642e-01| -1.188494| 1.266186| 0.868459| 4.264282| -0.355290| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.18849| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA 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, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 180 Number of elements = 194 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 32 Elemental Quad4 = 162 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 3.095468e+09, tgt = 3.095467e+09, diff = 1.346687e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 3.008438e+09, tgt = 3.008438e+09, diff = 1.930931e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 4.099882e+07, tgt = 4.099882e+07, diff = 3.402070e-02 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, 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 . | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. All volume elements are correctly orientend. All surface elements are correctly orientend. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 63999.5. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 0.906648 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. 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 1059 TETRAHEDRON volume elements. There has been a re-orientation of 43 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 64515. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 33.5988. Mean K: 0.526022. Standard deviation K: 1.77961. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 3.57195| 85.5935| | CV Face Area Aspect Ratio| 1.16408| 159.268| | CV Sub-Volume Ratio| 1| 6410.87| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11301| 1/1.00| 10| | 1| 2022| 1/5.59| 8.45239| | 2| 415| 1/4.87| 7.4787| +-------------------------------------------+ Finding max control volume width. Semi-span length = 4.34904 m. Wetted area = 166.087 m^2. Area projection in the x-plane = 64.7975 m^2, y-plane = 37.3137 m^2, z-plane = 5.27348 m^2. Max. coordinate in the x-direction = 2.74566 m, y-direction = 4.34904 m, z-direction = 19.6307 m. Min. coordinate in the x-direction = -0.647511 m, y-direction = -0.0653684 m, z-direction = -18.9106 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.4223e-01| 1.834424| 4.789528| 4.866267| 7.303530| -0.031030| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.4667e-01| 2.279632| 4.832406| 4.888836| 7.690003| -0.045547| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.5139e-01| 2.326325| 4.844282| 4.900460| 7.711785| -0.025198| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 2.32633| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 59 non-physical points in the solution. Warning: 2 reconstructed states for upwinding are non-physical. --------------------------- 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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 1.889013e+09, tgt = 1.889013e+09, diff = 1.783712e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 1.356764e+09, tgt = 1.356764e+09, diff = 2.847698e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 1.544678e+07, tgt = 1.544678e+07, diff = 5.994724e-02 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, 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 . | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. There has been a re-orientation of 1059 TETRAHEDRON volume elements. There has been a re-orientation of 43 TRIANGLE surface elements. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 64515. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 4.367542 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. 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 27048 TETRAHEDRON volume elements. There has been a re-orientation of 1531 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 567481. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 105.217. Mean K: 1.32211. Standard deviation K: 5.15455. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.800934| 81.1446| | CV Face Area Aspect Ratio| 1.53152| 961.841| | CV Sub-Volume Ratio| 1| 103390| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11301| 1/1.00| 10| | 1| 2018| 1/5.6| 8.44681| | 2| 413| 1/4.89| 7.46667| +-------------------------------------------+ Finding max control volume width. Semi-span length = 1.38253 m. Wetted area = 1283.54 m^2. Area projection in the x-plane = 312.855 m^2, y-plane = 448.481 m^2, z-plane = 63.5159 m^2. Max. coordinate in the x-direction = 13.9358 m, y-direction = 1.38253 m, z-direction = 228.447 m. Min. coordinate in the x-direction = 0.0404474 m, y-direction = -18.09 m, z-direction = -0.0756566 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.4447e-01| 3.680103| 6.645738| 6.490933| 9.149209| -0.074394| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.5446e-01| 3.953727| 6.601837| 6.531704| 9.385408| -0.068059| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.5869e-01| 4.102420| 6.694617| 6.667295| 9.479603| -0.082163| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 4.10242| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 411 non-physical points in the solution. Warning: 28 reconstructed states for upwinding are non-physical. --------------------------- 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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 1.300681e+09, tgt = 1.300681e+09, diff = 5.065727e+01 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 1.188523e+09, tgt = 1.188523e+09, diff = 5.800187e+01 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 1.304642e+07, tgt = 1.304642e+07, diff = 7.784819e-03 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, 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 . | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. There has been a re-orientation of 27048 TETRAHEDRON volume elements. There has been a re-orientation of 1531 TRIANGLE surface elements. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 567481. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 27.779394 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. 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 27100 TETRAHEDRON volume elements. There has been a re-orientation of 3235 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 4.1102e+09. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 42.3079. Mean K: 0.547697. Standard deviation K: 2.0063. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.627985| 85.0642| | CV Face Area Aspect Ratio| 1.44985| 34677| | CV Sub-Volume Ratio| 1| 5.46302e+06| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11301| 1/1.00| 10| | 1| 1998| 1/5.66| 8.41881| | 2| 411| 1/4.86| 7.4546| +-------------------------------------------+ Finding max control volume width. Semi-span length = 1.89763 m. Wetted area = 5762.5 m^2. Area projection in the x-plane = 1473.21 m^2, y-plane = 1717.92 m^2, z-plane = 123.508 m^2. Max. coordinate in the x-direction = 6.80902 m, y-direction = 1.89763 m, z-direction = 474.436 m. Min. coordinate in the x-direction = 0.0324872 m, y-direction = -32.3124 m, z-direction = -1.31748 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.4254e-01| 5.976390| 8.943243| 8.907682| 11.445496| -0.033796| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.4463e-01| 6.427253| 8.962699| 8.955813| 11.829598| -0.032181| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.4717e-01| 6.584833| 9.029467| 9.074330| 11.957314| -0.030968| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 6.58483| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 598 non-physical points in the solution. Warning: 38 reconstructed states for upwinding are non-physical. --------------------------- 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) ------------------------ Running PostAnalysis ...... su2 Cl = -751.30915 Cd = 24260.68865 real 0m48.345s user 0m46.756s sys 0m2.714s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelasticSimple_Iterative_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + echo 'aeroelastic_Iterative_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aeroelastic_Iterative_SU2_and_Astros.py test; + python -u aeroelastic_Iterative_SU2_and_Astros.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 2 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 381 692 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 374 678 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 927 1777 0 AFLR4 : Nodes, Trias,Quads= 821 1565 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 374 678 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 378 686 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 63 96 0 AFLR4 : Nodes, Trias,Quads= 55 80 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 64 96 0 AFLR4 : Nodes, Trias,Quads= 57 82 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 7 5 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 2592 5180 482 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 2592 5180 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 385 700 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 385 700 0 AFLR4 : Nodes, Trias,Quads= 381 692 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 1009 1939 0 AFLR4 : Nodes, Trias,Quads= 953 1827 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 383 696 0 AFLR4 : Nodes, Trias,Quads= 378 686 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 383 696 0 AFLR4 : Nodes, Trias,Quads= 382 694 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 381 692 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 74 115 0 AFLR4 : Nodes, Trias,Quads= 65 97 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 75 116 0 AFLR4 : Nodes, Trias,Quads= 63 92 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 2739 5474 490 OVERALL : CPU Time = 0.070 seconds Body 1 (of 1) Number of nodes = 2739 Number of elements = 5474 Number of triangle elements = 5474 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2739 Total number of elements = 5474 Total number of triangle elements = 5474 Total number of quadrilateral elements = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 11301 Number of elements = 64025 Number of triangles = 5474 Number of quadrilatarals = 0 Number of tetrahedrals = 58551 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 - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 47.1143. Mean K: 0.755059. Standard deviation K: 3.51124. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 54.7348| 85.4032| | CV Face Area Aspect Ratio| 1.05389| 21.5536| | CV Sub-Volume Ratio| 1| 13.9349| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11301| 1/1.00| 10| | 1| 2021| 1/5.59| 8.45099| | 2| 414| 1/4.88| 7.47269| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 8.08979 m^2. Area projection in the x-plane = 0.572014 m^2, y-plane = 0.261888 m^2, z-plane = 3.84035 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380358 m. Min. coordinate in the x-direction = 0 m, y-direction = -2.8602e-18 m, z-direction = -0.0467106 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.2915e-01| -0.790402| 1.509543| 1.185099| 4.678704| -1.072828| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.3419e-01| -1.125423| 1.402824| 1.016209| 4.328795| -0.842279| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.3087e-01| -1.188494| 1.266186| 0.868459| 4.264282| -0.355290| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.18849| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA 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, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Ribs_and_Spars, index = 1 Name = Skin, index = 2 Name = Rib_Root, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 746 Number of elements = 898 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 120 Elemental Quad4 = 778 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - Rib_Root Property name - Ribs_and_Spars Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 3.095468e+09, tgt = 3.095468e+09, diff = 6.724647e+01 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 3.008438e+09, tgt = 3.008438e+09, diff = 7.140274e+01 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 4.099882e+07, tgt = 4.099881e+07, diff = 2.658112e+00 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 330 (total = 330) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 330 (total = 660) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 30 (total = 690) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, 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 . | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. All volume elements are correctly orientend. All surface elements are correctly orientend. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 63999.5. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 1.138566 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. 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 14459 TETRAHEDRON volume elements. There has been a re-orientation of 682 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 111778. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 331.173. Mean K: 2.9916. Standard deviation K: 14.8257. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 3.40837| 84.3565| | CV Face Area Aspect Ratio| 1.28265| 2842.4| | CV Sub-Volume Ratio| 1| 163626| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11301| 1/1.00| 10| | 1| 2017| 1/5.6| 8.44541| | 2| 417| 1/4.84| 7.4907| +-------------------------------------------+ Finding max control volume width. Semi-span length = 11.7588 m. Wetted area = 1396.25 m^2. Area projection in the x-plane = 460.266 m^2, y-plane = 458.805 m^2, z-plane = 57.6887 m^2. Max. coordinate in the x-direction = 3.70785 m, y-direction = 11.7588 m, z-direction = 39.9754 m. Min. coordinate in the x-direction = -12.9853 m, y-direction = -0.927282 m, z-direction = -70.3501 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.1972e-01| 2.914707| 5.875636| 6.265734| 8.383813| 0.209002| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.2583e-01| 3.316493| 5.858698| 6.095228| 8.744846| 0.234611| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.2753e-01| 3.407997| 5.867221| 6.069520| 8.809945| 0.177305| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 3.408| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 199 non-physical points in the solution. Warning: 20 reconstructed states for upwinding are non-physical. --------------------------- 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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 8.819257e+08, tgt = 8.819253e+08, diff = 3.923236e+02 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 1.207830e+09, tgt = 1.207830e+09, diff = 2.597151e+02 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 1.219268e+07, tgt = 1.219271e+07, diff = 2.880687e+01 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 330 (total = 330) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 330 (total = 660) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 30 (total = 690) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, 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 . | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. There has been a re-orientation of 14459 TETRAHEDRON volume elements. There has been a re-orientation of 682 TRIANGLE surface elements. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 111778. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 18.246992 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. 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 31311 TETRAHEDRON volume elements. There has been a re-orientation of 3369 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 1.16776e+11. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 21.0169. Mean K: 0.354492. Standard deviation K: 1.30595. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.453746| 85.8506| | CV Face Area Aspect Ratio| 1.5343| 899846| | CV Sub-Volume Ratio| 1| 6.31279e+06| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11301| 1/1.00| 10| | 1| 1992| 1/5.67| 8.41038| | 2| 421| 1/4.73| 7.51457| +-------------------------------------------+ Finding max control volume width. Semi-span length = 397.143 m. Wetted area = 881016 m^2. Area projection in the x-plane = 445045 m^2, y-plane = 151377 m^2, z-plane = 8426.75 m^2. Max. coordinate in the x-direction = 50.0167 m, y-direction = 397.143 m, z-direction = 0.159487 m. Min. coordinate in the x-direction = -18.3734 m, y-direction = -10.3349 m, z-direction = -5468.94 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.4143e-01| 7.276733| 10.242971| 10.238844| 12.745838| 0.089051| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.5440e-01| 7.638465| 10.267040| 10.181291| 13.033584| 0.027721| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.5817e-01| 7.779909| 10.393368| 10.306450| 13.183336| -0.089022| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 7.77991| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 552 non-physical points in the solution. Warning: 55 reconstructed states for upwinding are non-physical. --------------------------- 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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 1.076975e+09, tgt = 1.076975e+09, diff = 3.649154e+02 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 1.571003e+09, tgt = 1.571004e+09, diff = 1.719102e+02 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 104 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 1.913889e+07, tgt = 1.913886e+07, diff = 2.267927e+01 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 330 (total = 330) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 330 (total = 660) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 30 (total = 690) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, 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 . | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. There has been a re-orientation of 31311 TETRAHEDRON volume elements. There has been a re-orientation of 3369 TRIANGLE surface elements. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 1.16776e+11. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 28.378696 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 11301 grid points. 58551 volume elements. 3 surface markers. 3452 boundary elements in index 0 (Marker = BC_1). 1827 boundary elements in index 1 (Marker = BC_2). 195 boundary elements in index 2 (Marker = BC_3). 58551 tetrahedra. 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 12469 TETRAHEDRON volume elements. There has been a re-orientation of 3032 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 1.4591e+13. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 17.5858. Mean K: 0.217072. Standard deviation K: 0.879795. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.577466| 85.1191| | CV Face Area Aspect Ratio| 1.70706| 2.96442e+07| | CV Sub-Volume Ratio| 1| 1.37716e+09| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11301| 1/1.00| 10| | 1| 1992| 1/5.67| 8.41038| | 2| 413| 1/4.82| 7.46667| +-------------------------------------------+ Finding max control volume width. Semi-span length = 993.177 m. Wetted area = 4.88018e+06 m^2. Area projection in the x-plane = 1.61503e+06 m^2, y-plane = 1.25948e+06 m^2, z-plane = 71304.9 m^2. Max. coordinate in the x-direction = 127.282 m, y-direction = 993.177 m, z-direction = 0.159487 m. Min. coordinate in the x-direction = -60.3931 m, y-direction = -24.6094 m, z-direction = -13719 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.1414e-01| 8.373383| 11.340190| 11.408519| 13.842489| 0.034826| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.1938e-01| 8.825382| 11.415919| 11.390647| 14.294942| -0.015998| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.2293e-01| 8.879168| 11.426477| 11.408611| 14.320373| -0.006719| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 8.87917| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 476 non-physical points in the solution. Warning: 51 reconstructed states for upwinding are non-physical. --------------------------- 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) ------------------------ Running PostAnalysis ...... su2 real 1m27.889s user 1m31.741s sys 0m8.404s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelastic_Iterative_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + echo 'aeroelasticSimple_Temperature_SU2_and_TACS.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aeroelasticSimple_Temperature_SU2_and_TACS.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u aeroelasticSimple_Temperature_SU2_and_TACS.py -outLevel=0 -noPlotData Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1293 2452 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1298 2462 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3418 6687 0 AFLR4 : Nodes, Trias,Quads= 3008 5867 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1316 2498 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1319 2504 0 AFLR4 : Nodes, Trias,Quads= 1294 2454 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 200 344 0 AFLR4 : Nodes, Trias,Quads= 160 264 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 193 330 0 AFLR4 : Nodes, Trias,Quads= 155 254 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17 21 0 AFLR4 : Nodes, Trias,Quads= 11 9 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9343 18682 928 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 9343 18682 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1337 2540 0 AFLR4 : Nodes, Trias,Quads= 1321 2508 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1339 2544 0 AFLR4 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3782 7410 0 AFLR4 : Nodes, Trias,Quads= 2950 5746 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1339 2544 0 AFLR4 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1338 2542 0 AFLR4 : Nodes, Trias,Quads= 1322 2510 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1340 2546 0 AFLR4 : Nodes, Trias,Quads= 1321 2508 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 233 404 0 AFLR4 : Nodes, Trias,Quads= 210 358 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 224 386 0 AFLR4 : Nodes, Trias,Quads= 196 330 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 18 22 0 AFLR4 : Nodes, Trias,Quads= 12 10 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9489 18974 946 OVERALL : CPU Time = 0.167 seconds Body 1 (of 1) Number of nodes = 9489 Number of elements = 18974 Number of triangle elements = 18974 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9489 Total number of elements = 18974 Total number of triangle elements = 18974 Total number of quadrilateral elements = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- Volume mesh: Number of nodes = 60093 Number of elements = 345939 Number of triangles = 18974 Number of quadrilatarals = 0 Number of tetrahedrals = 326965 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 - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Info: No recognized data transfer names found. Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_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: 3. 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_aeroelasticSimple_Temperature_SM.dat. Surface file name: surface_flow_aeroelasticSimple_Temperature_SM. Volume file name: flow_aeroelasticSimple_Temperature_SM. Restart file name: restart_flow_aeroelasticSimple_Temperature_SM.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 60093 grid points. 326965 volume elements. 3 surface markers. 12530 boundary elements in index 0 (Marker = BC_1). 5746 boundary elements in index 1 (Marker = BC_2). 698 boundary elements in index 2 (Marker = BC_3). 326965 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 83.4538. Mean K: 0.86237. Standard deviation K: 5.00385. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 54.7348| 86.8035| | CV Face Area Aspect Ratio| 1.06478| 21.5651| | CV Sub-Volume Ratio| 1| 8.64744| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 60093| 1/1.00| 10| | 1| 10214| 1/5.88| 8.309| | 2| 1799| 1/5.68| 6.98637| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 9.2451 m^2. Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m. Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 1.3789e+00| -1.355330| 0.925001| 0.586785| 4.113776| -0.972828| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.3861e+00| -1.745808| 0.767133| 0.413608| 3.711112| -0.534020| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.3723e+00| -1.758263| 0.583631| 0.231030| 3.699433| 1.633106| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.75826| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Temperature_SM.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat). |CSV file |surface_flow_aeroelasticSimple_Temperature_SM.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat). |Tecplot binary |flow_aeroelasticSimple_Temperature_SM.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Temperature_SM.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... tacs Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 12 Number of elements = 12 Number of triangle elements = 4 Number of quadrilateral elements = 8 ---------------------------- Total number of nodes = 12 Total number of elements = 12 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA 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, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 12 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4 Elemental Quad4 = 8 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - Skin No "groupName" specified for Load tuple Skin, going to use load name Done getting FEA loads Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA 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, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 12 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4 Elemental Quad4 = 8 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv Number of variables = 16 Number of data points = 361 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature' Rank 0: src = 1.497275e+03, tgt = 1.497275e+03, diff = 8.156515e-06 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA 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, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 12 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4 Elemental Quad4 = 8 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv Number of variables = 16 Number of data points = 361 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature' Rank 0: src = 1.453270e+03, tgt = 1.453270e+03, diff = 4.021617e-06 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA 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, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 12 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4 Elemental Quad4 = 8 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv Number of variables = 16 Number of data points = 361 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature' Rank 0: src = 2.098244e+01, tgt = 2.098244e+01, diff = 1.101341e-13 Extracting external thermal loads from data transfer.... TransferName = Skin_Top Number of Nodes = 9 (total = 9) Extracting external thermal loads from data transfer.... TransferName = Skin_Bottom Number of Nodes = 9 (total = 18) Extracting external thermal loads from data transfer.... TransferName = Skin_Tip Number of Nodes = 4 (total = 16) Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Running PostAnalysis ...... tacs real 0m15.447s user 0m15.626s sys 0m1.283s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelasticSimple_Temperature_SU2_and_TACS.py passed (as expected) ================================================= Running.... CORSAIRLITE PyTests ================================================= + echo 'gp.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt gp.py test; + python -u gp.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Objective --------- 0.00713 dimensionless Variables --------- x : 3.00000 [-] The X variable y : 81.00008 [-] The Y variable z : 0.19245 [-] The Z variable Sensitivities ------------- No Constants in the Formulation Solve Report ------------ Solve Method : Geometric Program Classification : Convex Solver : cvxopt real 0m5.051s user 0m1.503s sys 0m0.124s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case gp.py passed (as expected) ================================================= ================================================= + echo 'qp.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt qp.py test; + python -u qp.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Objective --------- -21.56250 dimensionless Variables --------- x : 1.62500 [-] The X variable y : 1.37500 [-] The Y variable Constants --------- c : 3 [-] A constant c2 : 2 [-] A constant Sensitivities ------------- c : + 0.46957 A constant c2 : - 0.22338 A constant Solve Report ------------ Solve Method : Quadratic Program Classification : Convex Solver : cvxopt real 0m1.053s user 0m1.553s sys 0m0.082s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case qp.py passed (as expected) ================================================= ================================================= + echo 'sp.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt sp.py test; + python -u sp.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Objective --------- 0.45721 dimensionless Variables --------- x : 2.56155 [-] The X variable y : 6.56155 [-] The Y variable z : 1.17116 [-] The Z variable Constants --------- c : 2 [-] A constant Sensitivities ------------- Sensitivities not computed Solve Report ------------ Solve Method : Signomial Program--Standard Classification : Iterative Solver : cvxopt Number of Iterations : 3 Termination Status : Converged, relative error (3.15e-04) is less than specified tolerance (1.00e-03) real 0m1.039s user 0m1.535s sys 0m0.088s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case sp.py passed (as expected) ================================================= ================================================= + echo 'boydBox.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt boydBox.py test; + python -u boydBox.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Objective --------- 0.00520 1 / meter ** 3 Variables --------- d : 11.26658 meter The Z variable h : 2.92246 meter The Y variable w : 5.84486 meter The X variable Constants --------- Aflr : 1000 meter ** 2 Area of floor Awall : 100 meter ** 2 Area of wall alpha : 0.50000 [-] Aspect Ratio Constraint beta : 2 [-] Aspect Ratio Constraint delta : 2 [-] Aspect Ratio Constraint gamma : 0.50000 [-] Aspect Ratio Constraint Sensitivities ------------- Sensitivities not computed Solve Report ------------ Solve Method : Geometric Program Classification : Convex Solver : cvxopt real 0m0.932s user 0m1.434s sys 0m0.087s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case boydBox.py passed (as expected) ================================================= ================================================= + echo 'hoburg_gp.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt hoburg_gp.py test; + python -u hoburg_gp.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Objective --------- 5905.58568 newton Variables --------- AR : 20.36983 [-] aspect ratio C_D_0 : 0.01271 [-] Drag Coefficient, segment 0 C_D_1 : 0.01273 [-] Drag Coefficient, segment 1 C_D_2 : 0.00778 [-] Drag Coefficient, segment 2 C_Dfuse_0 : 0.00180 [-] Fuselage Drag Coefficient, segment 0 C_Dfuse_1 : 0.00180 [-] Fuselage Drag Coefficient, segment 1 C_Dfuse_2 : 0.00180 [-] Fuselage Drag Coefficient, segment 2 C_Di_0 : 0.00542 [-] Induced Drag Coefficient, segment 0 C_Di_1 : 0.00542 [-] Induced Drag Coefficient, segment 1 C_Di_2 : 0.00023 [-] Induced Drag Coefficient, segment 2 C_Dp_0 : 0.00549 [-] Wing Profile Drag Coefficient, segment 0 C_Dp_1 : 0.00551 [-] Wing Profile Drag Coefficient, segment 1 C_Dp_2 : 0.00575 [-] Wing Profile Drag Coefficient, segment 2 C_L_0 : 0.57420 [-] Lift Coefficient, segment 0 C_L_1 : 0.57421 [-] Lift Coefficient, segment 1 C_L_2 : 0.11881 [-] Lift Coefficient, segment 2 I_cap_bar : 0.00002 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4 M_r_bar : 36139.20785 newton Root Bending unit per unit chord P_max : 1185884.98442 watt Maximum Engine Power R : 4999.98983 kilometer Single Segment range Re_0 : 4232645.50367 [-] Reynolds Number, segment 0 Re_1 : 4051247.93913 [-] Reynolds Number, segment 1 Re_2 : 9305153.26607 [-] Reynolds Number, segment 2 S : 27.73109 meter ** 2 total wing area T_0 : 746.21338 newton Thrust, segment 0 T_1 : 684.51827 newton Thrust, segment 1 T_2 : 2208.51611 newton Thrust, segment 2 V_0 : 68.23357 meter / second Velocity, segment 0 V_1 : 65.30930 meter / second Velocity, segment 1 V_2 : 150.00638 meter / second Velocity, segment 2 V_stall : 37.99896 meter / second stall speed W_0 : 33698.97702 newton Weight, segment 0 W_1 : 30873.13301 newton Weight, segment 1 W_2 : 33698.96566 newton Weight, segment 2 W_MTO : 36788.13387 newton Maximum Takeoff Weight W_cap : 4091.65066 newton Weight of Wing Spar Cap W_eng : 2806.10727 newton Engine Weight W_fuel_out : 3079.86524 newton Weight of fuel, outbound W_fuel_ret : 2825.71897 newton Weight of fuel, return W_pay : 4905.15902 newton Payload Weight W_tilde : 22409.98513 newton Dry Weight, no wing W_web : 139.91823 newton Weight of Wing Spar Shear Web W_wing : 8462.91404 newton wing weight W_zfw : 30872.92436 newton Zero Fuel Weight eta_0_0 : 0.26999 [-] Overall Efficiency, segment 0 eta_0_1 : 0.26996 [-] Overall Efficiency, segment 1 eta_0_2 : 0.27945 [-] Overall Efficiency, segment 2 eta_i_0 : 0.90752 [-] Inviscid Propeller Efficiency, segment 0 eta_i_1 : 0.90742 [-] Inviscid Propeller Efficiency, segment 1 eta_i_2 : 0.93932 [-] Inviscid Propeller Efficiency, segment 2 eta_prop_0 : 0.77139 [-] Propeller Efficiency, segment 0 eta_prop_1 : 0.77131 [-] Propeller Efficiency, segment 1 eta_prop_2 : 0.79842 [-] Propeller Efficiency, segment 2 nu : 0.78603 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2 p : 1.90003 [-] Dummy Variable (1+2*lam_w) q : 1.45002 [-] Dummy Variable (1+lam_w) t_cap_bar : 0.00456 [-] Spar cap thickness per unit chord t_web_bar : 0.00069 [-] Spar web thickness per unit chord tau : 0.15000 [-] airfoil thickness to chord ratio z_bre_0 : 0.08745 [-] Breguet Range Factor, segment 0 z_bre_1 : 0.08758 [-] Breguet Range Factor, segment 1 Constants --------- A_prop : 0.78500 meter ** 2 Disk area of propeller CDA0 : 0.05000 meter ** 2 fuselage drag area C_Lmax : 1.50000 [-] max CL with flaps down N_lift : 6 [-] Ultimate Load Factor W_fixed : 14700 newton fixed weight e : 0.95000 [-] Oswald efficiency factor eta_eng : 0.35000 [-] Engine Efficiency eta_v : 0.85000 [-] Propeller Viscous Efficiency f_wadd : 2 [-] Added Weight Fraction g : 9.81000 meter / second ** 2 Gravitational constant h_fuel : 46000000 joule / kilogram Fuel Specific energy density k_ew : 0.03720 newton / watt ** 0.803 Constant for engine weight mu : 0.00002 kilogram / meter / second viscosity of air r_h : 0.75000 [-] Ratio of height at rear spar to maximum wing height rho : 0.90912 kilogram / meter ** 3 density of air rho_SL : 1.22500 kilogram / meter ** 3 density of air, sea level rho_cap : 2700 kilogram / meter ** 3 Density of wing cap material (aluminum) rho_web : 2700 kilogram / meter ** 3 Density of wing web material (aluminum) sigma_max : 310 megapascal Allowable tensile stress of aluminum sigma_max_shear : 167 megapascal Allowable shear stress of aluminum w_bar : 0.50000 [-] Ratio of spar box width to chord length Sensitivities ------------- Sensitivities not computed Solve Report ------------ Solve Method : Geometric Program Classification : Convex Solver : cvxopt real 0m6.178s user 0m6.609s sys 0m0.094s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case hoburg_gp.py passed (as expected) ================================================= ================================================= + echo 'hoburg_blackbox.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt hoburg_blackbox.py test; + python -u hoburg_blackbox.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Objective --------- 5905.2294 newton Variables --------- AR : 20.3737 [-] aspect ratio C_D_0 : 0.0127 [-] Drag Coefficient, segment 0 C_D_1 : 0.0127 [-] Drag Coefficient, segment 1 C_D_2 : 0.0078 [-] Drag Coefficient, segment 2 C_Dfuse_0 : 0.0018 [-] Fuselage Drag Coefficient, segment 0 C_Dfuse_1 : 0.0018 [-] Fuselage Drag Coefficient, segment 1 C_Dfuse_2 : 0.0018 [-] Fuselage Drag Coefficient, segment 2 C_Di_0 : 0.0054 [-] Induced Drag Coefficient, segment 0 C_Di_1 : 0.0054 [-] Induced Drag Coefficient, segment 1 C_Di_2 : 0.0002 [-] Induced Drag Coefficient, segment 2 C_Dp_0 : 0.0055 [-] Wing Profile Drag Coefficient, segment 0 C_Dp_1 : 0.0055 [-] Wing Profile Drag Coefficient, segment 1 C_Dp_2 : 0.0057 [-] Wing Profile Drag Coefficient, segment 2 C_L_0 : 0.5743 [-] Lift Coefficient, segment 0 C_L_1 : 0.5743 [-] Lift Coefficient, segment 1 C_L_2 : 0.1189 [-] Lift Coefficient, segment 2 I_cap_bar : 0.0000 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4 M_r_bar : 36141.5015 newton Root Bending unit per unit chord P_max : 1184357.7686 watt Maximum Engine Power R : 5000.0000 kilometer Single Segment range Re_0 : 4231748.4657 [-] Reynolds Number, segment 0 Re_1 : 4050340.4368 [-] Reynolds Number, segment 1 Re_2 : 9301869.2068 [-] Reynolds Number, segment 2 S : 27.7189 meter ** 2 total wing area T_0 : 746.1648 newton Thrust, segment 0 T_1 : 684.5072 newton Thrust, segment 1 T_2 : 2206.5587 newton Thrust, segment 2 V_0 : 68.2403 meter / second Velocity, segment 0 V_1 : 65.3149 meter / second Velocity, segment 1 V_2 : 150.0000 meter / second Velocity, segment 2 V_stall : 38.0000 meter / second stall speed W_0 : 33694.3546 newton Weight, segment 0 W_1 : 30868.7209 newton Weight, segment 1 W_2 : 33694.3546 newton Weight, segment 2 W_MTO : 36773.9503 newton Maximum Takeoff Weight W_cap : 4091.0280 newton Weight of Wing Spar Cap W_eng : 2802.5264 newton Engine Weight W_fuel_out : 3079.5957 newton Weight of fuel, outbound W_fuel_ret : 2825.6337 newton Weight of fuel, return W_pay : 4905.0000 newton Payload Weight W_tilde : 22407.5264 newton Dry Weight, no wing W_web : 139.5692 newton Weight of Wing Spar Shear Web W_wing : 8461.1945 newton wing weight W_zfw : 30868.7209 newton Zero Fuel Weight eta_0_0 : 0.2700 [-] Overall Efficiency, segment 0 eta_0_1 : 0.2700 [-] Overall Efficiency, segment 1 eta_0_2 : 0.2795 [-] Overall Efficiency, segment 2 eta_i_0 : 0.9075 [-] Inviscid Propeller Efficiency, segment 0 eta_i_1 : 0.9074 [-] Inviscid Propeller Efficiency, segment 1 eta_i_2 : 0.9394 [-] Inviscid Propeller Efficiency, segment 2 eta_prop_0 : 0.7714 [-] Propeller Efficiency, segment 0 eta_prop_1 : 0.7713 [-] Propeller Efficiency, segment 1 eta_prop_2 : 0.7985 [-] Propeller Efficiency, segment 2 nu : 0.7860 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2 p : 1.9000 [-] Dummy Variable (1+2*lam_w) q : 1.4500 [-] Dummy Variable (1+lam_w) t_cap_bar : 0.0046 [-] Spar cap thickness per unit chord t_web_bar : 0.0007 [-] Spar web thickness per unit chord tau : 0.1500 [-] airfoil thickness to chord ratio z_bre_0 : 0.0875 [-] Breguet Range Factor, segment 0 z_bre_1 : 0.0876 [-] Breguet Range Factor, segment 1 Constants --------- A_prop : 0.7850 meter ** 2 Disk area of propeller CDA0 : 0.0500 meter ** 2 fuselage drag area C_Lmax : 1.5000 [-] max CL with flaps down N_lift : 6 [-] Ultimate Load Factor W_fixed : 14700 newton fixed weight e : 0.9500 [-] Oswald efficiency factor eta_eng : 0.3500 [-] Engine Efficiency eta_v : 0.8500 [-] Propeller Viscous Efficiency f_wadd : 2 [-] Added Weight Fraction g : 9.8100 meter / second ** 2 Gravitational constant h_fuel : 46000000 joule / kilogram Fuel Specific energy density k_ew : 0.0372 newton / watt ** 0.803 Constant for engine weight mu : 0.0000 kilogram / meter / second viscosity of air r_h : 0.7500 [-] Ratio of height at rear spar to maximum wing height rho : 0.9091 kilogram / meter ** 3 density of air rho_SL : 1.2250 kilogram / meter ** 3 density of air, sea level rho_cap : 2700 kilogram / meter ** 3 Density of wing cap material (aluminum) rho_web : 2700 kilogram / meter ** 3 Density of wing web material (aluminum) sigma_max : 310 megapascal Ultimate tensile stress of aluminum sigma_max_shear : 167 megapascal Ultimate shear stress of aluminum w_bar : 0.5000 [-] Ratio of spar box width to chord length Sensitivities ------------- Sensitivities not currently implemented for optimization type Logspace Sequential Quadratic Program Solve Report ------------ Solve Method : Logspace Sequential Quadratic Program Classification : Iterative Solver : cvxopt Number of Iterations : 7 Termination Status : Converged, gradient of Lagrangian (9.636631e-07) within tolerance (1.000000e-06) Messages -------- 1. Wolfe Condition 1 failed at iteration 5 (Step 5). Watchdog counter is 1 2. Wolfe Condition 1 failed at iteration 6 (Step 6). Watchdog counter is 2 real 0m23.991s user 0m24.299s sys 0m0.158s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case hoburg_blackbox.py passed (as expected) ================================================= ================================================= + echo 'pyCAPS/sizeWing.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt pyCAPS/sizeWing.py test; + python -u pyCAPS/sizeWing.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nrock 2 Objective --------- 0.075 dimensionless Variables --------- AR : 10.000 [-] Wing aspect ratio CD : 0.075 [-] Drag Coefficient CL : 0.999 [-] Lift Coefficient S : 2.642 meter ** 2 Wing area V : 2.722 meter / second Airspeed W : 11.979 newton Aircraft weight Wwing : 1.598 newton Wing weight Constants --------- ARmax : 10 [-] Max AR CD0 : 0.040 [-] Profile drag CLmax : 1 [-] Max CL E0 : 10 joule Maximum elastic potential energy in rubber band Wfixed : 0.100 newton Weight of fixed components Wrock : 2 newton Weight of each rock e : 0.900 [-] Oswawld efficiency factor g : 9.810 meter / second ** 2 Gravitational constant nrock : 2 [-] Number of rocks to carry rho : 1.225 kilogram / meter ** 3 Density of air rho_wing : 1 kilogram / meter ** 3 Weight density of wing tau : 0.120 [-] Airfoil thickness as t/c Sensitivities ------------- Sensitivities not computed Solve Report ------------ Solve Method : Geometric Program Classification : Convex Solver : cvxopt Optimized L/D: 13.267784561972137 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! real 0m1.301s user 0m1.749s sys 0m0.132s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case pyCAPS/sizeWing.py passed (as expected) ================================================= avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/avl ================================================= + echo 'pyCAPS/optTaperAvl.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt pyCAPS/optTaperAvl.py test; + python -u pyCAPS/optTaperAvl.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Objective --------- 1.00805 dimensionless Variables --------- e : 0.99202 [-] Oswald efficiency factor lam : 0.39881 [-] Wing taper ratio Sensitivities ------------- Sensitivities not available for optimizations of type Sequential Log Convex Program Solve Report ------------ Solve Method : Sequential Log Convex Program Classification : Iterative Solver : cvxopt Number of Iterations : 6 Termination Status : Converged, gradient of Lagrangian (5.888774e-08) within tolerance (1.000000e-06) Messages -------- 1. Wolfe Condition 1 failed at iteration 5 (Step 5). Watchdog counter is 1 real 0m5.183s user 0m3.368s sys 0m1.853s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case pyCAPS/optTaperAvl.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'pyCAPS/optWingAvl.py test;' pyCAPS/optWingAvl.py test; + python -u pyCAPS/optWingAvl.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt nrock 2 Starting iteration 0 at 0.1766 seconds AR : 9.0 dimensionless CD : 0.1 dimensionless CL : 1.0 dimensionless S : 1.0 meter ** 2 V : 1.0 meter / second W : 10.0 newton Wwing : 0.1 newton e : 1.0 dimensionless lam : 0.3 dimensionless AVL run case - lam, AR: 0.3 9.0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) y: 0.990550414371373 dimensionless dydx: [, ] Calling cvxopt.solvers.cp at 1.1715 seconds Got sol from cvxopt at 1.1920 seconds status optimal x [ 1.05e-01] [-3.26e-01] [-1.49e-11] [-4.10e-01] [ 1.28e+00] [-6.40e-01] [ 7.00e-01] [-1.08e-02] [ 5.73e-03] [-3.20e-16] [ 3.50e-16] [ 1.56e-16] [ 5.20e-16] [ 2.70e-16] [ 4.16e-27] [ 3.37e-16] [ 2.07e-23] y [-6.40e-01] [ 7.00e-01] [ 3.11e-01] znl [ 6.74e-01] [ 4.14e-08] zl [ 1.04e+00] [ 5.41e-01] [ 8.31e-12] snl [ 8.55e-11] [ 2.03e-01] sl [ 1.49e-11] [ 4.30e-10] [ 8.74e-01] gap 8.743959706200045e-09 relative gap 7.1941976174589016e-09 primal objective -1.2154183372694929 dual objective -1.2154183416834794 primal slack 1.3843122277340912e-11 dual slack 8.310943825855639e-12 primal infeasibility 1.13903462789848e-09 dual infeasibility 2.3823418495103618e-11 AVL run case - lam, AR: 0.3017253411787602 9.999999995701312 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) y: 0.9892210301573232 dimensionless dydx: [, ] logspace stuff at 2.1207 seconds Starting iteration 1 at 2.1374 seconds AR : 9.999999995701312 dimensionless CD : 0.07217671497330859 dimensionless CL : 0.9999999999851361 dimensionless S : 0.6639217992634345 meter ** 2 V : 3.600068783658014 meter / second W : 5.270412635736404 newton Wwing : 0.20138431695627712 newton e : 0.9892553874046033 dimensionless lam : 0.3017253411787602 dimensionless Calling cvxopt.solvers.cp at 2.1421 seconds Got sol from cvxopt at 2.1614 seconds status optimal x [ 3.90e-10] [-5.94e-05] [-1.96e-07] [ 1.14e-08] [ 7.38e-08] [-3.68e-08] [ 1.70e-08] [ 1.33e-04] [ 8.64e-03] [ 6.35e-21] [-6.95e-21] [ 2.23e-16] [ 5.42e-17] [ 2.20e-16] [ 1.27e-26] [ 5.00e-16] [ 6.63e-26] y [ 1.27e-05] [-1.39e-05] [ 4.46e-01] znl [ 1.00e+00] [ 1.33e-10] zl [ 1.08e-01] [ 4.39e-01] [ 2.53e-11] snl [ 2.06e-11] [ 2.03e-01] sl [ 1.96e-07] [ 4.02e-11] [ 8.74e-01] gap 2.1363031593454878e-08 relative gap 8.126967446080017e-09 primal objective -2.628659673511942 dual objective -2.628659684337833 primal slack 2.0577846480825846e-11 dual slack 2.53050406780468e-11 primal infeasibility 3.085803284597273e-09 dual infeasibility 3.13391320011975e-09 AVL run case - lam, AR: 0.30434464835769004 9.99999999959832 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) y: 0.9893844569300133 dimensionless dydx: [, ] logspace stuff at 3.0470 seconds Starting iteration 2 at 3.0680 seconds AR : 9.99999999959832 dimensionless CD : 0.07217242517886707 dimensionless CL : 0.9999998041107226 dimensionless S : 0.6639218068635588 meter ** 2 V : 3.6000690493939635 meter / second W : 5.270412441791246 newton Wwing : 0.20138432037500312 newton e : 0.9893868959019062 dimensionless lam : 0.30434464835769004 dimensionless Calling cvxopt.solvers.cp at 3.0724 seconds Got sol from cvxopt at 3.0904 seconds status optimal x [ 7.75e-13] [-3.52e-04] [ 4.29e-09] [-2.11e-10] [-1.42e-09] [ 1.25e-09] [-3.17e-10] [ 7.91e-04] [ 4.20e-02] [ 7.26e-21] [-7.89e-21] [ 2.23e-16] [ 5.45e-17] [ 2.20e-16] [ 1.24e-26] [ 5.00e-16] [ 6.65e-26] y [ 1.45e-05] [-1.58e-05] [ 4.45e-01] znl [ 1.00e+00] [ 1.33e-10] zl [ 1.09e-01] [ 4.39e-01] [ 2.49e-11] snl [ 2.02e-11] [ 2.03e-01] sl [ 1.92e-07] [ 3.94e-11] [ 8.74e-01] gap 2.097954193386208e-08 relative gap 7.980432613224019e-09 primal objective -2.628872763000068 dual objective -2.628872773631917 primal slack 2.0226195523752228e-11 dual slack 2.4870270238975127e-11 primal infeasibility 3.030673275151341e-09 dual infeasibility 3.0769326689078285e-09 AVL run case - lam, AR: 0.3174093513141515 9.999999999606068 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) y: 0.9901147289476044 dimensionless dydx: [, ] logspace stuff at 4.0210 seconds Starting iteration 3 at 4.0404 seconds AR : 9.999999999606068 dimensionless CD : 0.07214699157334123 dimensionless CL : 0.9999998084033913 dimensionless S : 0.6639218067235316 meter ** 2 V : 3.6000690442960233 meter / second W : 5.270412448377285 newton Wwing : 0.20138432031121437 newton e : 0.9901696737885595 dimensionless lam : 0.3174093513141515 dimensionless Calling cvxopt.solvers.cp at 4.0456 seconds Got sol from cvxopt at 4.0634 seconds status optimal x [ 2.14e-12] [-1.28e-03] [ 1.17e-08] [-5.10e-10] [-3.51e-09] [ 4.16e-09] [-7.67e-10] [ 2.88e-03] [ 1.81e-01] [-4.10e-21] [ 4.49e-21] [ 2.23e-16] [ 5.51e-17] [ 2.20e-16] [ 1.18e-26] [ 5.00e-16] [ 6.61e-26] y [-8.19e-06] [ 8.98e-06] [ 4.45e-01] znl [ 1.00e+00] [ 1.32e-10] zl [ 1.10e-01] [ 4.40e-01] [ 2.37e-11] snl [ 1.92e-11] [ 2.03e-01] sl [ 1.80e-07] [ 3.73e-11] [ 8.74e-01] gap 1.9913348949433526e-08 relative gap 7.57253767423933e-09 primal objective -2.629679746219796 dual objective -2.629679756312171 primal slack 1.9233234440857094e-11 dual slack 2.3654666051747643e-11 primal infeasibility 2.8765759057609882e-09 dual infeasibility 2.9202707353765115e-09 AVL run case - lam, AR: 0.38029905717662316 9.999999999627487 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) y: 0.9919295458295864 dimensionless dydx: [, ] logspace stuff at 4.9677 seconds Starting iteration 4 at 4.9917 seconds AR : 9.999999999627487 dimensionless CD : 0.0720544031114864 dimensionless CL : 0.9999998201037487 dimensionless S : 0.6639218063847038 meter ** 2 V : 3.600069031643119 meter / second W : 5.270412470306208 newton Wwing : 0.20138432015683602 newton e : 0.993029781490428 dimensionless lam : 0.38029905717662316 dimensionless Calling cvxopt.solvers.cp at 5.0025 seconds Got sol from cvxopt at 5.0208 seconds status optimal x [-1.57e-12] [ 4.08e-04] [-8.59e-09] [ 5.53e-10] [ 3.53e-09] [-9.72e-10] [ 8.30e-10] [-9.18e-04] [ 5.19e-02] [-2.12e-20] [ 2.32e-20] [ 2.24e-16] [ 5.46e-17] [ 2.20e-16] [ 1.23e-26] [ 5.00e-16] [ 6.59e-26] y [-4.25e-05] [ 4.64e-05] [ 4.47e-01] znl [ 1.00e+00] [ 1.32e-10] zl [ 1.09e-01] [ 4.39e-01] [ 2.45e-11] snl [ 1.99e-11] [ 2.03e-01] sl [ 1.88e-07] [ 3.88e-11] [ 8.74e-01] gap 2.0688403479344937e-08 relative gap 7.866667127626345e-09 primal objective -2.629881644119772 dual objective -2.629881654604473 primal slack 1.9944303018503003e-11 dual slack 2.4539201182220112e-11 primal infeasibility 2.9853825022328838e-09 dual infeasibility 3.036428971722002e-09 AVL run case - lam, AR: 0.4005573159778744 9.999999999611775 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) y: 0.9920150584836487 dimensionless dydx: [, ] logspace stuff at 5.7477 seconds Starting iteration 5 at 5.7664 seconds AR : 9.999999999611775 dimensionless CD : 0.07208383829260301 dimensionless CL : 0.9999998115160276 dimensionless S : 0.6639218067517705 meter ** 2 V : 3.600069044356998 meter / second W : 5.270412465184867 newton Wwing : 0.20138432032400524 newton e : 0.9921187131764504 dimensionless lam : 0.4005573159778744 dimensionless Calling cvxopt.solvers.cp at 5.7704 seconds Got sol from cvxopt at 5.7777 seconds status optimal x [ 8.00e-13] [ 4.58e-05] [ 4.24e-09] [-2.43e-10] [-1.58e-09] [ 8.36e-10] [-3.65e-10] [-1.03e-04] [-4.33e-03] [-2.09e-21] [ 2.29e-21] [ 2.23e-16] [ 5.49e-17] [ 2.19e-16] [ 1.20e-26] [ 5.00e-16] [ 6.74e-26] y [-4.18e-06] [ 4.57e-06] [ 4.45e-01] znl [ 1.00e+00] [ 1.35e-10] zl [ 1.10e-01] [ 4.39e-01] [ 2.41e-11] snl [ 1.96e-11] [ 2.03e-01] sl [ 1.84e-07] [ 3.80e-11] [ 8.74e-01] gap 2.031955843004712e-08 relative gap 7.726423169498243e-09 primal objective -2.6298790506664265 dual objective -2.629879060964246 primal slack 1.961702717405949e-11 dual slack 2.4096853737212874e-11 primal infeasibility 2.93236429442893e-09 dual infeasibility 2.967263152169171e-09 AVL run case - lam, AR: 0.39882645454912435 9.999999999619773 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) y: 0.9920158805953975 dimensionless dydx: [, ] logspace stuff at 6.5225 seconds Starting iteration 6 at 6.5419 seconds AR : 9.999999999619773 dimensionless CD : 0.07208714305299402 dimensionless CL : 0.9999998157581855 dimensionless S : 0.6639218065905538 meter ** 2 V : 3.6000690386621352 meter / second W : 5.270412469588729 newton Wwing : 0.20138432025057307 newton e : 0.9920165401543579 dimensionless lam : 0.39882645454912435 dimensionless Calling cvxopt.solvers.cp at 6.5462 seconds Got sol from cvxopt at 6.5544 seconds status optimal x [ 2.35e-13] [ 2.97e-07] [ 1.09e-09] [-5.55e-11] [-3.69e-10] [ 2.96e-10] [-8.34e-11] [-6.65e-07] [-3.26e-05] [ 1.22e-24] [-1.28e-24] [ 2.23e-16] [ 5.49e-17] [ 2.19e-16] [ 1.20e-26] [ 5.00e-16] [ 6.76e-26] y [ 2.45e-09] [-2.57e-09] [ 4.45e-01] znl [ 1.00e+00] [ 1.35e-10] zl [ 1.10e-01] [ 4.39e-01] [ 2.40e-11] snl [ 1.95e-11] [ 2.03e-01] sl [ 1.83e-07] [ 3.78e-11] [ 8.74e-01] gap 2.0211071384287106e-08 relative gap 7.685171306970461e-09 primal objective -2.6298790979396434 dual objective -2.629879108182298 primal slack 1.9527381359129242e-11 dual slack 2.395834706018389e-11 primal infeasibility 2.9156313147459703e-09 dual infeasibility 2.9337884446774703e-09 AVL run case - lam, AR: 0.39881343719465984 9.999999999622123 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Getting vortex lattice surface data VLM surface name - wing 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 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) y: 0.9920158812322912 dimensionless dydx: [, ] logspace stuff at 7.1977 seconds Objective --------- 0.072 dimensionless Variables --------- AR : 10.000 [-] Wing aspect ratio CD : 0.072 [-] Drag Coefficient CL : 1.000 [-] Lift Coefficient S : 0.664 meter ** 2 Wing area V : 3.600 meter / second Airspeed W : 5.270 newton Aircraft weight Wwing : 0.201 newton Wing weight e : 0.992 [-] Oswald efficiency factor lam : 0.399 [-] Wing taper ratio Sensitivities ------------- Sensitivities not available for optimizations of type Sequential Log Convex Program Solve Report ------------ Solve Method : Sequential Log Convex Program Classification : Iterative Solver : cvxopt Number of Iterations : 7 Termination Status : Converged, gradient of Lagrangian (1.043842e-07) within tolerance (1.000000e-06) Messages -------- 1. Wolfe Condition 1 failed at iteration 3 (Step 3). Watchdog counter is 1 13.872092548132818 real 0m8.520s user 0m5.358s sys 0m2.959s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case pyCAPS/optWingAvl.py passed (as expected) ================================================= ================================================= + echo 'pyCAPS/GPSize.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt pyCAPS/GPSize.py test; + python -u pyCAPS/GPSize.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Objective --------- 6339.9402476213 newton Variables --------- AR : 18.0583068591 [-] aspect ratio C_D_0 : 0.0127966186 [-] Drag Coefficient, segment 0 C_D_1 : 0.0128135534 [-] Drag Coefficient, segment 1 C_D_2 : 0.0077622395 [-] Drag Coefficient, segment 2 C_Dfuse_0 : 0.0017626506 [-] Fuselage Drag Coefficient, segment 0 C_Dfuse_1 : 0.0017626506 [-] Fuselage Drag Coefficient, segment 1 C_Dfuse_2 : 0.0017626510 [-] Fuselage Drag Coefficient, segment 2 C_Di_0 : 0.0056016002 [-] Induced Drag Coefficient, segment 0 C_Di_1 : 0.0056028716 [-] Induced Drag Coefficient, segment 1 C_Di_2 : 0.0002594009 [-] Induced Drag Coefficient, segment 2 C_Dp_0 : 0.0054327043 [-] Wing Profile Drag Coefficient, segment 0 C_Dp_1 : 0.0054483614 [-] Wing Profile Drag Coefficient, segment 1 C_Dp_2 : 0.0057382717 [-] Wing Profile Drag Coefficient, segment 2 C_L_0 : 0.5494535783 [-] Lift Coefficient, segment 0 C_L_1 : 0.5495159270 [-] Lift Coefficient, segment 1 C_L_2 : 0.1182390122 [-] Lift Coefficient, segment 2 I_cap_bar : 0.0000193397 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4 M_r_bar : 32106.9717613474 newton Root Bending unit per unit chord P_max : 1211155.7559680410 watt Maximum Engine Power R : 4999.9816129528 kilometer Single Segment range Re_0 : 4636790.3991634697 [-] Reynolds Number, segment 0 Re_1 : 4427330.4209076529 [-] Reynolds Number, segment 1 Re_2 : 9995446.9239517339 [-] Reynolds Number, segment 2 S : 28.3664420021 meter ** 2 total wing area T_0 : 799.0178645705 newton Thrust, segment 0 T_1 : 729.4239244544 newton Thrust, segment 1 T_2 : 2252.7493855701 newton Thrust, segment 2 V_0 : 69.5874592840 meter / second Velocity, segment 0 V_1 : 66.4439512429 meter / second Velocity, segment 1 V_2 : 150.0084591036 meter / second Velocity, segment 2 V_stall : 37.9986643205 meter / second stall speed W_0 : 34307.5807516552 newton Weight, segment 0 W_1 : 31281.5531631160 newton Weight, segment 1 W_2 : 34307.5610637156 newton Weight, segment 2 W_MTO : 37630.4011124297 newton Maximum Takeoff Weight W_cap : 4278.1047592241 newton Weight of Wing Spar Cap W_eng : 2854.2361754189 newton Engine Weight W_fuel_out : 3314.0247993997 newton Weight of fuel, outbound W_fuel_ret : 3025.9122892774 newton Weight of fuel, return W_pay : 4905.2326701420 newton Payload Weight W_tilde : 22457.8594632444 newton Dry Weight, no wing W_web : 133.6940460361 newton Weight of Wing Spar Shear Web W_wing : 8823.3040844200 newton wing weight W_zfw : 31281.2018350684 newton Zero Fuel Weight eta_0_0 : 0.2693167459 [-] Overall Efficiency, segment 0 eta_0_1 : 0.2692858916 [-] Overall Efficiency, segment 1 eta_0_2 : 0.2791280518 [-] Overall Efficiency, segment 2 eta_i_0 : 0.9052651192 [-] Inviscid Propeller Efficiency, segment 0 eta_i_1 : 0.9051614203 [-] Inviscid Propeller Efficiency, segment 1 eta_i_2 : 0.9382448822 [-] Inviscid Propeller Efficiency, segment 2 eta_prop_0 : 0.7694756986 [-] Propeller Efficiency, segment 0 eta_prop_1 : 0.7693875506 [-] Propeller Efficiency, segment 1 eta_prop_2 : 0.7975082496 [-] Propeller Efficiency, segment 2 nu : 0.7860410805 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2 p : 1.9000448519 [-] Dummy Variable (1+2*lam_w) q : 1.4500404597 [-] Dummy Variable (1+lam_w) t_cap_bar : 0.0043345438 [-] Spar cap thickness per unit chord t_web_bar : 0.0006000270 [-] Spar web thickness per unit chord tau : 0.1499996279 [-] airfoil thickness to chord ratio z_bre_0 : 0.0922115805 [-] Breguet Range Factor, segment 0 z_bre_1 : 0.0923337617 [-] Breguet Range Factor, segment 1 Constants --------- A_prop : 0.7850000000 meter ** 2 Disk area of propeller CDA0 : 0.0500000000 meter ** 2 fuselage drag area C_Lmax : 1.5000000000 [-] max CL with flaps down N_lift : 6 [-] Ultimate Load Factor W_fixed : 14700 newton fixed weight e : 0.9500000000 [-] Oswald efficiency factor eta_eng : 0.3500000000 [-] Engine Efficiency eta_v : 0.8500000000 [-] Propeller Viscous Efficiency f_wadd : 2 [-] Added Weight Fraction g : 9.8100000000 meter / second ** 2 Gravitational constant h_fuel : 46000000 joule / kilogram Fuel Specific energy density k_ew : 0.0372000000 newton / watt ** 0.803 Constant for engine weight mu : 0.0000171000 kilogram / meter / second viscosity of air r_h : 0.7500000000 [-] Ratio of height at rear spar to maximum wing height rho : 0.9091220000 kilogram / meter ** 3 density of air rho_SL : 1.2250000000 kilogram / meter ** 3 density of air, sea level rho_cap : 2700 kilogram / meter ** 3 Density of wing cap material (aluminum) rho_web : 2700 kilogram / meter ** 3 Density of wing web material (aluminum) sigma_max : 250 megapascal Allowable tensile stress of aluminum sigma_max_shear : 167 megapascal Allowable shear stress of aluminum w_bar : 0.5000000000 [-] Ratio of spar box width to chord length Sensitivities ------------- Sensitivities not computed Solve Report ------------ Solve Method : Geometric Program Classification : Convex Solver : cvxopt EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! real 0m5.424s user 0m5.831s sys 0m0.158s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case pyCAPS/GPSize.py passed (as expected) ================================================= mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/mses ================================================= + echo 'pyCAPS/MSES.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt pyCAPS/MSES.py test; + python -u pyCAPS/MSES.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Objective --------- 6436.9111747642 newton Variables --------- AR : 17.8847143703 [-] aspect ratio Alpha_p20_MSES_0 : 22.6676624733 degree Angle of Attack + 20deg from MSES, segment 0 Alpha_p20_MSES_1 : 22.7725605594 degree Angle of Attack + 20deg from MSES, segment 1 Alpha_p20_MSES_2 : 18.8664426951 degree Angle of Attack + 20deg from MSES, segment 2 C_D_0 : 0.0127680026 [-] Drag Coefficient, segment 0 C_D_1 : 0.0130143941 [-] Drag Coefficient, segment 1 C_D_2 : 0.0074765087 [-] Drag Coefficient, segment 2 C_Dfuse_0 : 0.0017731859 [-] Fuselage Drag Coefficient, segment 0 C_Dfuse_1 : 0.0017731859 [-] Fuselage Drag Coefficient, segment 1 C_Dfuse_2 : 0.0017731859 [-] Fuselage Drag Coefficient, segment 2 C_Di_0 : 0.0053689965 [-] Induced Drag Coefficient, segment 0 C_Di_1 : 0.0055861389 [-] Induced Drag Coefficient, segment 1 C_Di_2 : 0.0002610120 [-] Induced Drag Coefficient, segment 2 C_Dp_0 : 0.0056258204 [-] Wing Profile Drag Coefficient, segment 0 C_Dp_1 : 0.0056550700 [-] Wing Profile Drag Coefficient, segment 1 C_Dp_2 : 0.0054423095 [-] Wing Profile Drag Coefficient, segment 2 C_L_0 : 0.5353228067 [-] Lift Coefficient, segment 0 C_L_1 : 0.5460488610 [-] Lift Coefficient, segment 1 C_L_2 : 0.1180337615 [-] Lift Coefficient, segment 2 C_L_MSES_0 : 0.5353228067 [-] Lift Coefficient from MSES, segment 0 C_L_MSES_1 : 0.5460488610 [-] Lift Coefficient from MSES, segment 1 C_L_MSES_2 : 0.1180337615 [-] Lift Coefficient from MSES, segment 2 I_cap_bar : 0.0000189923 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4 M_r_bar : 31649.2629256045 newton Root Bending unit per unit chord P_max : 1155819.0983774771 watt Maximum Engine Power R : 5000.0000010210 kilometer Single Segment range Re_0 : 4702125.2746726070 [-] Reynolds Number, segment 0 Re_1 : 4440814.5793337049 [-] Reynolds Number, segment 1 Re_2 : 10013489.5565969180 [-] Reynolds Number, segment 2 S : 28.1978812745 meter ** 2 total wing area T_0 : 811.9144361127 newton Thrust, segment 0 T_1 : 738.1899382843 newton Thrust, segment 1 T_2 : 2156.2042613309 newton Thrust, segment 2 V_0 : 70.4366540784 meter / second Velocity, segment 0 V_1 : 66.5224856090 meter / second Velocity, segment 1 V_2 : 150.0000049409 meter / second Velocity, segment 2 V_stall : 37.9999998304 meter / second stall speed W_0 : 34040.6240956632 newton Weight, segment 0 W_1 : 30972.5122439076 newton Weight, segment 1 W_2 : 34040.6240956631 newton Weight, segment 2 W_MTO : 37409.4238057056 newton Maximum Takeoff Weight W_cap : 4178.0707911956 newton Weight of Wing Spar Cap W_eng : 2748.1693321190 newton Engine Weight W_fuel_out : 3368.7993606073 newton Weight of fuel, outbound W_fuel_ret : 3068.1118141569 newton Weight of fuel, return W_pay : 4905.0000238714 newton Payload Weight W_tilde : 22353.1693245709 newton Dry Weight, no wing W_web : 131.6008887574 newton Weight of Wing Spar Shear Web W_wing : 8619.3429955669 newton wing weight W_zfw : 30972.5122296163 newton Zero Fuel Weight eta_0_0 : 0.2695063546 [-] Overall Efficiency, segment 0 eta_0_1 : 0.2690604520 [-] Overall Efficiency, segment 1 eta_0_2 : 0.2798281448 [-] Overall Efficiency, segment 2 eta_i_0 : 0.9059037131 [-] Inviscid Propeller Efficiency, segment 0 eta_i_1 : 0.9044048805 [-] Inviscid Propeller Efficiency, segment 1 eta_i_2 : 0.9405988059 [-] Inviscid Propeller Efficiency, segment 2 eta_prop_0 : 0.7700181561 [-] Propeller Efficiency, segment 0 eta_prop_1 : 0.7687441484 [-] Propeller Efficiency, segment 1 eta_prop_2 : 0.7995089850 [-] Propeller Efficiency, segment 2 nu : 0.7859963973 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2 p : 1.9000000011 [-] Dummy Variable (1+2*lam_w) q : 1.4500000023 [-] Dummy Variable (1+lam_w) t_cap_bar : 0.0042510724 [-] Spar cap thickness per unit chord t_web_bar : 0.0005949804 [-] Spar web thickness per unit chord tau : 0.1499998017 [-] airfoil thickness to chord ratio z_bre_0 : 0.0943682262 [-] Breguet Range Factor, segment 0 z_bre_1 : 0.0944547882 [-] Breguet Range Factor, segment 1 Sensitivities ------------- Sensitivities not available for optimizations of type Sequential Log Convex Program Solve Report ------------ Solve Method : Sequential Log Convex Program Classification : Iterative Solver : cvxopt Number of Iterations : 31 Termination Status : Converged, relative change in the objective function (8.48e-06) is witin specified tolerance (1.00e-05) Messages -------- 1. Attempted step of size 1.00e+00 at iteration 2 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 2. Attempted step of size 9.00e-01 at iteration 2 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 3. Wolfe Condition 1 failed at iteration 4 (Step 4). Watchdog counter is 1 4. Wolfe Condition 1 failed at iteration 7 (Step 7). Watchdog counter is 1 5. Wolfe Condition 1 failed at iteration 8 (Step 8). Watchdog counter is 2 6. Wolfe Condition 1 failed at iteration 11 (Step 11). Watchdog counter is 1 7. Wolfe Condition 1 failed at iteration 12 (Step 12). Watchdog counter is 2 8. Wolfe Condition 1 failed at iteration 13 (Step 13). Watchdog counter is 3 9. Attempted step of size 1.00e+00 at iteration 14 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 10. Wolfe Condition 1 failed at iteration 14 (Step 14). Watchdog counter is 4 11. Wolfe Condition 1 failed at iteration 16 (Step 16). Watchdog counter is 1 12. Wolfe Condition 1 failed at iteration 17 (Step 17). Watchdog counter is 2 real 4m20.889s user 4m12.239s sys 0m6.700s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case pyCAPS/MSES.py passed (as expected) ================================================= ================================================= + echo 'pyCAPS/Camber.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt pyCAPS/Camber.py test; + python -u pyCAPS/Camber.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Objective --------- 5491.4359225133 newton Variables --------- AR : 16.4147174429 [-] aspect ratio Alpha_p20_MSES_0 : 18.0126155823 degree Angle of Attack + 20deg from MSES, segment 0 Alpha_p20_MSES_1 : 18.1754881520 degree Angle of Attack + 20deg from MSES, segment 1 Alpha_p20_MSES_2 : 14.5292099988 degree Angle of Attack + 20deg from MSES, segment 2 C_D_0 : 0.0102948117 [-] Drag Coefficient, segment 0 C_D_1 : 0.0107150833 [-] Drag Coefficient, segment 1 C_D_2 : 0.0069659104 [-] Drag Coefficient, segment 2 C_Dfuse_0 : 0.0019058054 [-] Fuselage Drag Coefficient, segment 0 C_Dfuse_1 : 0.0019058054 [-] Fuselage Drag Coefficient, segment 1 C_Dfuse_2 : 0.0019058054 [-] Fuselage Drag Coefficient, segment 2 C_Di_0 : 0.0044487314 [-] Induced Drag Coefficient, segment 0 C_Di_1 : 0.0048480057 [-] Induced Drag Coefficient, segment 1 C_Di_2 : 0.0002903621 [-] Induced Drag Coefficient, segment 2 C_Dp_0 : 0.0039402749 [-] Wing Profile Drag Coefficient, segment 0 C_Dp_1 : 0.0039612726 [-] Wing Profile Drag Coefficient, segment 1 C_Dp_2 : 0.0047697411 [-] Wing Profile Drag Coefficient, segment 2 C_L_0 : 0.4642555300 [-] Lift Coefficient, segment 0 C_L_1 : 0.4845048407 [-] Lift Coefficient, segment 1 C_L_2 : 0.1187898747 [-] Lift Coefficient, segment 2 C_L_MSES_0 : 0.4642555300 [-] Lift Coefficient from MSES, segment 0 C_L_MSES_1 : 0.4845048407 [-] Lift Coefficient from MSES, segment 1 C_L_MSES_2 : 0.1187898747 [-] Lift Coefficient from MSES, segment 2 I_cap_bar : 0.0000169655 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4 M_r_bar : 28632.8148697486 newton Root Bending unit per unit chord P_max : 995317.3030262130 watt Maximum Engine Power R : 5000.0000150914 kilometer Single Segment range Re_0 : 5146611.2342969924 [-] Reynolds Number, segment 0 Re_1 : 4834919.6517840819 [-] Reynolds Number, segment 1 Re_2 : 10114462.7451584097 [-] Reynolds Number, segment 2 S : 26.2686333615 meter ** 2 total wing area T_0 : 708.1364694815 newton Thrust, segment 0 T_1 : 647.1687649939 newton Thrust, segment 1 T_2 : 1869.9310318896 newton Thrust, segment 2 V_0 : 76.2664901710 meter / second Velocity, segment 0 V_1 : 71.6311268476 meter / second Velocity, segment 1 V_2 : 150.0000569370 meter / second Velocity, segment 2 V_stall : 37.9862969911 meter / second stall speed W_0 : 31915.7596170390 newton Weight, segment 0 W_1 : 29289.9561426453 newton Weight, segment 1 W_2 : 31915.7596170390 newton Weight, segment 2 W_MTO : 34825.3028076972 newton Maximum Takeoff Weight W_cap : 3504.9733685113 newton Weight of Wing Spar Cap W_eng : 2435.1503729458 newton Engine Weight W_fuel_out : 2865.6326794429 newton Weight of fuel, outbound W_fuel_ret : 2625.8032430704 newton Weight of fuel, return W_pay : 4905.0001242919 newton Payload Weight W_tilde : 22040.1505203108 newton Dry Weight, no wing W_web : 119.9293311624 newton Weight of Wing Spar Shear Web W_wing : 7249.8053469954 newton wing weight W_zfw : 29289.9559483835 newton Zero Fuel Weight camberLocation : 0.7087509688 [-] location of maximum airfoil camber scaled by chord eta_0_0 : 0.2755554590 [-] Overall Efficiency, segment 0 eta_0_1 : 0.2747888706 [-] Overall Efficiency, segment 1 eta_0_2 : 0.2819554372 [-] Overall Efficiency, segment 2 eta_i_0 : 0.9262368370 [-] Inviscid Propeller Efficiency, segment 0 eta_i_1 : 0.9236600693 [-] Inviscid Propeller Efficiency, segment 1 eta_i_2 : 0.9477493688 [-] Inviscid Propeller Efficiency, segment 2 eta_prop_0 : 0.7873013115 [-] Propeller Efficiency, segment 0 eta_prop_1 : 0.7851110589 [-] Propeller Efficiency, segment 1 eta_prop_2 : 0.8055869634 [-] Propeller Efficiency, segment 2 maxCamber : 0.0491463515 [-] maximum airfoil camber scaled by chord nu : 0.7859964213 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2 p : 1.9000000162 [-] Dummy Variable (1+2*lam_w) q : 1.4500000250 [-] Dummy Variable (1+lam_w) t_cap_bar : 0.0037976551 [-] Spar cap thickness per unit chord t_web_bar : 0.0005785209 [-] Spar web thickness per unit chord tau : 0.1495748504 [-] airfoil thickness to chord ratio z_bre_0 : 0.0860294936 [-] Breguet Range Factor, segment 0 z_bre_1 : 0.0859477878 [-] Breguet Range Factor, segment 1 Sensitivities ------------- Sensitivities not available for optimizations of type Sequential Log Convex Program Solve Report ------------ Solve Method : Sequential Log Convex Program Classification : Iterative Solver : cvxopt Number of Iterations : 99 Termination Status : Converged, relative change in the objective function (7.65e-06) is witin specified tolerance (1.00e-05) Messages -------- 1. Attempted step of size 1.00e+00 at iteration 1 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 2. Attempted step of size 1.00e+00 at iteration 3 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 3. Attempted step of size 1.00e+00 at iteration 7 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 4. Wolfe Condition 1 failed at iteration 8 (Step 8). Watchdog counter is 1 5. Attempted step of size 1.00e+00 at iteration 10 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 6. Wolfe Condition 1 failed at iteration 11 (Step 11). Watchdog counter is 1 7. Attempted step of size 1.00e+00 at iteration 12 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 8. Wolfe Condition 1 failed at iteration 14 (Step 14). Watchdog counter is 1 9. Attempted step of size 1.00e+00 at iteration 15 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 10. Wolfe Condition 1 failed at iteration 18 (Step 18). Watchdog counter is 1 11. Wolfe Condition 1 failed at iteration 21 (Step 21). Watchdog counter is 1 12. Attempted step of size 2.15e-01 at iteration 27 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 13. Attempted step of size 1.77e-01 at iteration 32 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 14. Attempted step of size 1.57e-01 at iteration 36 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 15. Wolfe Condition 1 failed at iteration 37 (Step 37). Watchdog counter is 1 16. Attempted step of size 1.42e-01 at iteration 40 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 17. Wolfe Condition 1 failed at iteration 43 (Step 43). Watchdog counter is 1 18. Attempted step of size 1.30e-01 at iteration 44 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 19. Wolfe Condition 1 failed at iteration 49 (Step 49). Watchdog counter is 1 20. Wolfe Condition 1 failed at iteration 50 (Step 50). Watchdog counter is 2 21. Attempted step of size 1.13e-01 at iteration 52 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 22. Attempted step of size 1.09e-01 at iteration 54 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 23. Attempted step of size 3.28e-02 at iteration 54 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 24. Wolfe Condition 1 failed at iteration 59 (Step 59). Watchdog counter is 1 25. Wolfe Condition 1 failed at iteration 60 (Step 60). Watchdog counter is 2 26. Wolfe Condition 1 failed at iteration 62 (Step 62). Watchdog counter is 1 27. Wolfe Condition 1 failed at iteration 67 (Step 67). Watchdog counter is 1 28. Wolfe Condition 1 failed at iteration 68 (Step 68). Watchdog counter is 2 29. Attempted step of size 8.84e-02 at iteration 71 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 30. Wolfe Condition 1 failed at iteration 72 (Step 72). Watchdog counter is 1 31. Wolfe Condition 1 failed at iteration 73 (Step 73). Watchdog counter is 2 32. Wolfe Condition 1 failed at iteration 74 (Step 74). Watchdog counter is 3 33. Wolfe Condition 1 failed at iteration 75 (Step 75). Watchdog counter is 4 34. Wolfe Condition 1 failed at iteration 95 (Step 95). Watchdog counter is 1 real 13m48.832s user 13m21.988s sys 0m20.410s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case pyCAPS/Camber.py passed (as expected) ================================================= ================================================= + echo 'pyCAPS/CMConstraint.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt pyCAPS/CMConstraint.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u pyCAPS/CMConstraint.py -outLevel=0 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Getting CFD design variables....... Number of design variables - 3 Design Variable name - camber Design Variable name - maxloc Design Variable name - thickness 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 Objective --------- 6389.1599788872 newton Variables --------- AR : 18.1246600755 [-] aspect ratio Alpha_p20_MSES_0 : 22.7354842586 degree Angle of Attack + 20deg from MSES, segment 0 Alpha_p20_MSES_1 : 22.7563511509 degree Angle of Attack + 20deg from MSES, segment 1 Alpha_p20_MSES_2 : 18.6841775414 degree Angle of Attack + 20deg from MSES, segment 2 C_D_0 : 0.0132149995 [-] Drag Coefficient, segment 0 C_D_1 : 0.0132499519 [-] Drag Coefficient, segment 1 C_D_2 : 0.0075834110 [-] Drag Coefficient, segment 2 C_Dfuse_0 : 0.0017623324 [-] Fuselage Drag Coefficient, segment 0 C_Dfuse_1 : 0.0017623324 [-] Fuselage Drag Coefficient, segment 1 C_Dfuse_2 : 0.0017623324 [-] Fuselage Drag Coefficient, segment 2 C_Di_0 : 0.0058797215 [-] Induced Drag Coefficient, segment 0 C_Di_1 : 0.0059269314 [-] Induced Drag Coefficient, segment 1 C_Di_2 : 0.0002582450 [-] Induced Drag Coefficient, segment 2 C_Dp_0 : 0.0055729459 [-] Wing Profile Drag Coefficient, segment 0 C_Dp_1 : 0.0055606884 [-] Wing Profile Drag Coefficient, segment 1 C_Dp_2 : 0.0055628314 [-] Wing Profile Drag Coefficient, segment 2 C_L_0 : 0.5638905478 [-] Lift Coefficient, segment 0 C_L_1 : 0.5661550132 [-] Lift Coefficient, segment 1 C_L_2 : 0.1181879141 [-] Lift Coefficient, segment 2 C_L_MSES_0 : 0.5638905478 [-] Lift Coefficient from MSES, segment 0 C_L_MSES_1 : 0.5661550132 [-] Lift Coefficient from MSES, segment 1 C_L_MSES_2 : 0.1181879141 [-] Lift Coefficient from MSES, segment 2 I_cap_bar : 0.0000194277 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4 M_r_bar : 32142.4766677387 newton Root Bending unit per unit chord P_max : 1180922.1189759877 watt Maximum Engine Power R : 5000.0000115189 kilometer Single Segment range Re_0 : 4569113.0350051858 [-] Reynolds Number, segment 0 Re_1 : 4352777.0943119153 [-] Reynolds Number, segment 1 Re_2 : 9977785.5636399947 [-] Reynolds Number, segment 2 S : 28.3718598326 meter ** 2 total wing area T_0 : 803.8161139074 newton Thrust, segment 0 T_1 : 731.4741552257 newton Thrust, segment 1 T_2 : 2200.5003332610 newton Thrust, segment 2 V_0 : 68.6872633568 meter / second Velocity, segment 0 V_1 : 65.4352286761 meter / second Velocity, segment 1 V_2 : 150.0000174706 meter / second Velocity, segment 2 V_stall : 37.9999992819 meter / second stall speed W_0 : 34295.4186254629 newton Weight, segment 0 W_1 : 31251.0744708949 newton Weight, segment 1 W_2 : 34295.4186254629 newton Weight, segment 2 W_MTO : 37640.2357223150 newton Maximum Takeoff Weight W_cap : 4291.8687051105 newton Weight of Wing Spar Cap W_eng : 2795.9949775438 newton Engine Weight W_fuel_out : 3344.8158627813 newton Weight of fuel, outbound W_fuel_ret : 3044.3441161059 newton Weight of fuel, return W_pay : 4905.0002866763 newton Payload Weight W_tilde : 22400.9952205062 newton Dry Weight, no wing W_web : 133.1707762079 newton Weight of Wing Spar Shear Web W_wing : 8850.0789606646 newton wing weight W_zfw : 31251.0742320470 newton Zero Fuel Weight camberLocation : 0.3743117570 [-] location of maximum airfoil camber scaled by chord eta_0_0 : 0.2685537422 [-] Overall Efficiency, segment 0 eta_0_1 : 0.2684906678 [-] Overall Efficiency, segment 1 eta_0_2 : 0.2795064938 [-] Overall Efficiency, segment 2 eta_i_0 : 0.9027016546 [-] Inviscid Propeller Efficiency, segment 0 eta_i_1 : 0.9024896397 [-] Inviscid Propeller Efficiency, segment 1 eta_i_2 : 0.9395176263 [-] Inviscid Propeller Efficiency, segment 2 eta_prop_0 : 0.7672964064 [-] Propeller Efficiency, segment 0 eta_prop_1 : 0.7671161938 [-] Propeller Efficiency, segment 1 eta_prop_2 : 0.7985899824 [-] Propeller Efficiency, segment 2 maxCamber : 0.0222539259 [-] maximum airfoil camber scaled by chord negCMp1_0 : 1.0554550403 [-] Negative CM about 0.25c + 1, segment 0 negCMp1_1 : 1.0551745498 [-] Negative CM about 0.25c + 1, segment 1 negCMp1_2 : 1.0580510080 [-] Negative CM about 0.25c + 1, segment 2 nu : 0.7859964727 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2 p : 1.9000000085 [-] Dummy Variable (1+2*lam_w) q : 1.4500000156 [-] Dummy Variable (1+lam_w) t_cap_bar : 0.0043555913 [-] Spar cap thickness per unit chord t_web_bar : 0.0006005377 [-] Spar web thickness per unit chord tau : 0.1499999234 [-] airfoil thickness to chord ratio z_bre_0 : 0.0930629119 [-] Breguet Range Factor, segment 0 z_bre_1 : 0.0929596776 [-] Breguet Range Factor, segment 1 Sensitivities ------------- Sensitivities not available for optimizations of type Sequential Log Convex Program Solve Report ------------ Solve Method : Sequential Log Convex Program Classification : Iterative Solver : cvxopt Number of Iterations : 26 Termination Status : Converged, relative change in the objective function (3.87e-06) is witin specified tolerance (1.00e-05) Messages -------- 1. Wolfe Condition 1 failed at iteration 3 (Step 3). Watchdog counter is 1 2. Attempted step of size 1.00e+00 at iteration 6 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 3. Wolfe Condition 1 failed at iteration 7 (Step 7). Watchdog counter is 1 4. Wolfe Condition 1 failed at iteration 9 (Step 9). Watchdog counter is 1 5. Wolfe Condition 1 failed at iteration 12 (Step 12). Watchdog counter is 1 6. Wolfe Condition 1 failed at iteration 13 (Step 13). Watchdog counter is 2 7. Attempted step of size 1.00e+00 at iteration 14 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 8. Attempted step of size 1.00e+00 at iteration 15 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 9. Wolfe Condition 1 failed at iteration 21 (Step 21). Watchdog counter is 1 10. Attempted step of size 2.87e-01 at iteration 22 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 11. Attempted step of size 2.37e-01 at iteration 25 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 12. Attempted step of size 7.12e-02 at iteration 25 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 13. Attempted step of size 2.14e-02 at iteration 25 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. 14. Attempted step of size 6.41e-03 at iteration 25 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule. real 4m1.143s user 3m54.116s sys 0m4.855s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case pyCAPS/CMConstraint.py passed (as expected) ================================================= Traceback (most recent call last): File "", line 1, in ModuleNotFoundError: No module named 'torch' ************************************************* ************************************************* ================================================= Did not run examples for: awave autoLink Pointwise Fun3D abaqus Nastran Mystran Plato Mystran ================================================= All tests pass! ================================================= ================================================= + cd /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023 + bash -e execute_Training.sh ================================================= Using python : /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python ================================================= ================================================= + echo 'transport.csm test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log transport.csm test; + /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 transport.csm + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log WARNING:: cannot open "./verify_7.8.1/transport.vfy", so verification is being skipped MESSAGE:: Building wingOml MESSAGE:: Building wingWaffle MESSAGE:: Building wingHinges MESSAGE:: Building nacelleOml MESSAGE:: Building htailOml MESSAGE:: Building htailWaffle MESSAGE:: Building htailHinges MESSAGE:: Building vtailOml MESSAGE:: Building vtailWaffle MESSAGE:: Building vtailHinges MESSAGE:: Building fuseOml MESSAGE:: Building fuseWaffle MESSAGE:: Building fuseIml MESSAGE:: Building payload ==> serveESP completed successfully with 5 warnings and no verification data real 0m11.021s user 0m12.306s sys 0m10.651s + status=0 + set +x ================================================= data/ESP/transport passed (as expected) ================================================= execute_Training.sh: line 157: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/test/template_avl: No such file or directory ================================================= template_avl.py test; + python template_avl.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... ==> Setting Build Variables and Geometry Values... ==> Creating AVL aim... {'wingHinge1': {'deflectionAngle': -10.0}, 'wingHinge2': {'deflectionAngle': 10.0}, 'wingHinge3': {'deflectionAngle': 15.0}, 'wingHinge4': {'deflectionAngle': 15.0}, 'wingHinge5': {'deflectionAngle': 10.0}, 'wingHinge6': {'deflectionAngle': 10.0}, 'htailHinge1': {'deflectionAngle': 5.0}, 'htailHinge2': {'deflectionAngle': 5.0}} ==> Running AVL... MESSAGE:: Building wingOml MESSAGE:: Building wingHinges MESSAGE:: Building htailOml MESSAGE:: Building htailHinges MESSAGE:: Building vtailOml MESSAGE:: Building vtailHinges Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing, index = 1 Name = Htail, index = 2 Name = Vtail, index = 3 Getting vortex lattice control surface data VLM control surface name - htailHinge1 VLM control surface name - htailHinge2 VLM control surface name - wingHinge1 VLM control surface name - wingHinge2 VLM control surface name - wingHinge3 VLM control surface name - wingHinge4 VLM control surface name - wingHinge5 VLM control surface name - wingHinge6 Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Htail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Warning: Control htailControl1 not found in controls tuple! Only defaults will be used. Warning: Control htailControl1 not found in controls tuple! Only defaults will be used. Warning: Control htailControl1 not found in controls tuple! Only defaults will be used. Warning: Control htailControl1 not found in controls tuple! Only defaults will be used. Warning: Control WingControl1 not found in controls tuple! Only defaults will be used. Warning: Control WingControl1 not found in controls tuple! Only defaults will be used. Warning: Control WingControl2 not found in controls tuple! Only defaults will be used. Warning: Control WingControl2 not found in controls tuple! Only defaults will be used. Warning: Control WingControl3 not found in controls tuple! Only defaults will be used. Warning: Control WingControl3 not found in controls tuple! Only defaults will be used. Warning: Control WingControl3 not found in controls tuple! Only defaults will be used. Warning: Control WingControl3 not found in controls tuple! Only defaults will be used. Warning: Control WingControl2 not found in controls tuple! Only defaults will be used. Warning: Control WingControl2 not found in controls tuple! Only defaults will be used. Warning: Control WingControl4 not found in controls tuple! Only defaults will be used. Warning: Control WingControl4 not found in controls tuple! Only defaults will be used. Writing surface - Htail (ID = 0) Section 1 of 7 (ID = 0) Section 2 of 7 (ID = 3) Control surface 1 of 1 Section 3 of 7 (ID = 4) Control surface 1 of 1 Section 4 of 7 (ID = 1) Section 5 of 7 (ID = 5) Control surface 1 of 1 Section 6 of 7 (ID = 6) Control surface 1 of 1 Section 7 of 7 (ID = 2) Writing surface - Wing (ID = 1) Section 1 of 17 (ID = 0) Section 2 of 17 (ID = 5) Control surface 1 of 1 Section 3 of 17 (ID = 6) Control surface 1 of 1 Section 4 of 17 (ID = 7) Control surface 1 of 1 Section 5 of 17 (ID = 8) Control surface 1 of 1 Section 6 of 17 (ID = 4) Section 7 of 17 (ID = 9) Control surface 1 of 1 Section 8 of 17 (ID = 10) Control surface 1 of 1 Section 9 of 17 (ID = 1) Section 10 of 17 (ID = 11) Control surface 1 of 1 Section 11 of 17 (ID = 12) Control surface 1 of 1 Section 12 of 17 (ID = 3) Section 13 of 17 (ID = 13) Control surface 1 of 1 Section 14 of 17 (ID = 14) Control surface 1 of 1 Section 15 of 17 (ID = 15) Control surface 1 of 1 Section 16 of 17 (ID = 16) Control surface 1 of 1 Section 17 of 17 (ID = 2) ================ run_avl.py complete ================== Force/moment coefficients: CXtot : 0.1440096030964816 CYtot : -3.53511379732127e-11 CZtot : -1.170781090342353 Cltot : -3.063862377222321e-10 Cmtot : -1.825893600985071 Cntot : 2.402339104754559e-10 CLtot : 1.178001299993477 CDtot : 0.06148222914722529 e : 0.7858931265075788 real 0m14.787s user 0m12.780s sys 0m20.030s + status=0 + set +x ================================================= data/session01/template_avl.py passed (as expected) ================================================= ================================================= + echo 'f118-A.csm test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log f118-A.csm test; + /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-A.csm + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log WARNING:: cannot open "./verify_7.8.1/f118-A.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.115s user 0m0.113s sys 0m0.008s + status=0 + set +x ================================================= data/session02/f118-A passed (as expected) ================================================= ================================================= 1_f118_Geom.py test; + python 1_f118_Geom.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-A.csm"... ==> Bulding and viewing geometry... real 0m0.279s user 0m0.333s sys 0m0.066s + status=0 + set +x ================================================= data/session02/1_f118_Geom.py passed (as expected) ================================================= ================================================= 2_f118_DESPMTR.py test; + python 2_f118_DESPMTR.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-A.csm"... --> old htail:area = 1210.0 --> new htail:area = 2420.0 ==> Bulding and viewing Wide Body geometry... ==> Bulding and viewing Canard geometry... ==> All design parameters --> wing:area = 1210.0 --> wing:aspect = 9.0 --> wing:thick = 0.1 --> wing:xroot = 54.0 --> wing:zroot = -5.0 --> htail:area = 4240.0 --> htail:aspect = 4.15 --> htail:thick = 0.08 --> htail:xroot = 145.0 --> htail:zroot = 5.0 --> vtail = [[1220.0, 1.8, 0.08, 150.0, -8.0, 9.0], [1220.0, 1.8, 0.08, 150.0, 8.0, 9.0]] --> fuse:length = 180.0 --> fuse:width = 20.0 --> fuse:height = 20.0 real 0m0.357s user 0m0.419s sys 0m0.083s + status=0 + set +x ================================================= data/session02/2_f118_DESPMTR.py passed (as expected) ================================================= ================================================= 3_f118_Save.py test; + python 3_f118_Save.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-A.csm"... --> old htail:area = 1210.0 --> new htail:area = 2420.0 ==> Bulding and saving Wide Body geometry... ==> Bulding and saving Canard geometry... ==> All design parameters --> wing:area = 1210.0 --> wing:aspect = 9.0 --> wing:thick = 0.1 --> wing:xroot = 54.0 --> wing:zroot = -5.0 --> htail:area = 4240.0 --> htail:aspect = 4.15 --> htail:thick = 0.08 --> htail:xroot = 145.0 --> htail:zroot = 5.0 --> vtail = [[1220.0, 1.8, 0.08, 150.0, -8.0, 9.0], [1220.0, 1.8, 0.08, 150.0, 8.0, 9.0]] --> fuse:length = 180.0 --> fuse:width = 20.0 --> fuse:height = 20.0 real 0m0.341s user 0m0.402s sys 0m0.085s + status=0 + set +x ================================================= data/session02/3_f118_Save.py passed (as expected) ================================================= ================================================= 4_f118_Shortcut.py test; + python 4_f118_Shortcut.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-A.csm"... --> old htail:area = 1210.0 --> new htail:area = 2420.0 ==> Bulding and viewing Wide Body geometry... ==> Bulding and viewing Canard geometry... ==> Grouped parameters --> fuse fuse:length = 180.0 fuse:width = 20.0 fuse:height = 20.0 --> wing wing:area = 1210.0 wing:aspect = 9.0 wing:thick = 0.1 wing:xroot = 54.0 wing:zroot = -5.0 --> htail htail:area = 4240.0 htail:aspect = 4.15 htail:thick = 0.08 htail:xroot = 145.0 htail:zroot = 5.0 real 0m0.317s user 0m0.379s sys 0m0.083s + status=0 + set +x ================================================= data/session02/4_f118_Shortcut.py passed (as expected) ================================================= ================================================= 5_f118_writeParameters.py test; + python 5_f118_writeParameters.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-A.csm"... ==> Saving parameters to "f118_4.params"... ==> Loading 2nd geometry from file "f118-A.csm"... ==> Reading parameters from "f118_4.params"... --> Opening DESPMTR file "f118_4.params" updating CFGPMTR nrow [ 1, 1] = 1.000000 updating DESPMTR wing:area [ 1, 1] = 4240.000000 updating DESPMTR wing:aspect [ 1, 1] = 9.000000 updating DESPMTR wing:thick [ 1, 1] = 0.100000 updating DESPMTR wing:xroot [ 1, 1] = 54.000000 updating DESPMTR wing:zroot [ 1, 1] = -5.000000 updating DESPMTR htail:area [ 1, 1] = 2420.000000 updating DESPMTR htail:aspect [ 1, 1] = 4.150000 updating DESPMTR htail:thick [ 1, 1] = 0.080000 updating DESPMTR htail:xroot [ 1, 1] = 145.000000 updating DESPMTR htail:zroot [ 1, 1] = 5.000000 updating DESPMTR vtail [ 1, 1] = 1220.000000 updating DESPMTR vtail [ 1, 2] = 1.800000 updating DESPMTR vtail [ 1, 3] = 0.080000 updating DESPMTR vtail [ 1, 4] = 150.000000 updating DESPMTR vtail [ 1, 5] = 0.000000 updating DESPMTR vtail [ 1, 6] = 9.000000 updating DESPMTR fuse:length [ 1, 1] = 180.000000 updating DESPMTR fuse:width [ 1, 1] = 60.000000 updating DESPMTR fuse:height [ 1, 1] = 20.000000 ==> Building and viewing the geometry... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! real 0m0.321s user 0m0.380s sys 0m0.109s + status=0 + set +x ================================================= data/session02/5_f118_writeParameters.py passed (as expected) ================================================= ================================================= 6_f118_bodies.py test; + python 6_f118_bodies.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-A.csm"... ==> pyEGADS egos... Wing Htail Vtail1 Fuselage real 0m0.264s user 0m0.316s sys 0m0.066s + status=0 + set +x ================================================= data/session02/6_f118_bodies.py passed (as expected) ================================================= ================================================= + echo '7_f118_OUTPMTR.py test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log 7_f118_OUTPMTR.py test; + python 7_f118_OUTPMTR.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-A.csm"... --> wing:wet = 9422.222222222223 --> wing:volume = 9202.959910328365 --> htail:prop[0] = 2660.2506024096383 --> htail:prop[1] = 1652.8901595442062 --> vtail:prop = [1371.822222222222, None] --> fuse:wet = None Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session02/7_f118_OUTPMTR.py", line 34, in print ("--> wing:span =", f118.outpmtr.wing.span ) ^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/pyCAPS/problem.py", line 1954, in __getattr__ --> fuse:volume = None raise AttributeError("No Out Value: {!r}".format(name)) AttributeError: No Out Value: 'span' real 0m0.274s user 0m0.330s sys 0m0.068s + status=1 + set +x ================================================= data/session02/7_f118_OUTPMTR.py failed (as expected) ================================================= ================================================= 8_f118_Phasing.py test; + python 8_f118_Phasing.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-A.csm"... --> old htail:area = 1210.0 --> new htail:area = 2420.0 ==> Bulding and viewing Wide Body geometry... ==> Bulding and viewing geometry from WideBody phase... ==> Bulding and viewing Canard geometry... real 0m0.420s user 0m0.505s sys 0m0.154s + status=0 + set +x ================================================= data/session02/8_f118_Phasing.py passed (as expected) ================================================= ================================================= f118_Custom.py test; + python f118_Custom.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../../data/session02/f118-A.csm"... ==> Bulding and viewing geometry... real 0m0.291s user 0m0.349s sys 0m0.072s + status=0 + set +x ================================================= solutions/session02/f118_Custom.py passed (as expected) ================================================= ================================================= + echo 'f118-B.csm test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log f118-B.csm test; + /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-B.csm + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log WARNING:: cannot open "./verify_7.8.1/f118-B.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.127s user 0m0.116s sys 0m0.009s + status=0 + set +x ================================================= data/session03/f118-B passed (as expected) ================================================= ================================================= + echo 'f118-C.csm test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log f118-C.csm test; + /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-C.csm + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log WARNING:: cannot open "./verify_7.8.1/f118-C.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.125s user 0m0.118s sys 0m0.009s + status=0 + set +x ================================================= data/session03/f118-C passed (as expected) ================================================= ================================================= + echo 'naca.csm test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log naca.csm test; + /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 naca.csm + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log WARNING:: cannot open "./verify_7.8.1/naca.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.135s user 0m0.122s sys 0m0.009s + status=0 + set +x ================================================= data/session03/naca passed (as expected) ================================================= ================================================= 01_xfoil_input.py test; + python 01_xfoil_input.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... ==> Creating xfoilAIM ==> Modified Mach = 0.5 ==> Default Alpha = None ==> Modified Alpha = 2.5 ==> Modified Alpha = [0.0, 3.0, 5.0, 7.0, 8.0] ==> Unset Alpha = None EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! real 0m0.304s user 0m0.347s sys 0m0.062s + status=0 + set +x ================================================= data/session03/01_xfoil_input.py passed (as expected) ================================================= ================================================= 02_xfoil_Analysis.py test; + python 02_xfoil_Analysis.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... ==> Creating xfoilAIM ==> Setting analysis values ==> Running preAnalysis ==> Running xFoil...... ==> Running postAnalysis ==> Retrieve analysis results --> Alpha = [0.0, 3.0, 5.0, 7.0, 8.0] --> Cl = [-3.53757125655385e-07, 0.377437462009099, 0.642259371967833, 0.955175653138806, 1.00909750957761] --> Cd = [0.00617285380994127, 0.00729426778019113, 0.0100194565543501, 0.0148710807063523, 0.0185150448281103] real 0m0.790s user 0m0.921s sys 0m0.093s + status=0 + set +x ================================================= data/session03/02_xfoil_Analysis.py passed (as expected) ================================================= ================================================= 03_xfoil_AutoExec.py test; + python 03_xfoil_AutoExec.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... ==> Creating xfoilAIM ==> Setting analysis values ==> Retrieve analysis results --> Alpha = [0.0, 3.0, 5.0, 7.0, 8.0] --> Cl = [-3.53757125655385e-07, 0.377437462009099, 0.642259371967833, 0.955175653138806, 1.00909750957761] --> Cd = [0.00617285380994127, 0.00729426778019113, 0.0100194565543501, 0.0148710807063523, 0.0185150448281103] real 0m0.729s user 0m0.910s sys 0m0.086s + status=0 + set +x ================================================= data/session03/03_xfoil_AutoExec.py passed (as expected) ================================================= ================================================= 04_xfoil_MultiAnalysis.py test; + python 04_xfoil_MultiAnalysis.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... ==> Creating xfoilAIM ==> Setting analysis values ==> Retrieve analysis results --> Alpha = [0.0, 3.0, 5.0, 7.0, 8.0] --> Cl = [-3.53757125655385e-07, 0.377437462009099, 0.642259371967833, 0.955175653138806, 1.00909750957761] --> Cd = [0.00617285380994127, 0.00729426778019113, 0.0100194565543501, 0.0148710807063523, 0.0185150448281103] ==> Retrieve analysis results --> Alpha = [2.87619228202795e-06, 0.789686474041505, 1.18477801663719, 2.37671255179738, 3.18364393502637] --> Cl = [-1.68829566253184e-16, 0.1, 0.150000000000232, 0.300000000000164, 0.4] --> Cd = [0.00617285381076772, 0.00623021348481478, 0.00630554753827162, 0.00680929883615774, 0.00747424244863518] real 0m1.298s user 0m1.172s sys 0m0.135s + status=0 + set +x ================================================= data/session03/04_xfoil_MultiAnalysis.py passed (as expected) ================================================= ================================================= 05_xfoil_Camber_Plot.py test; + python 05_xfoil_Camber_Plot.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... ==> Creating xfoilAIM ==> Setting analysis values ==> Retrieve analysis results. camber = 0.0 ==> Retrieve analysis results. camber = 0.01 ==> Retrieve analysis results. camber = 0.04 ==> Retrieve analysis results. camber = 0.07 ==> Plotting analysis results (close plot window to finish Python script /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session03/05_xfoil_Camber_Plot.py:65: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown plt.show() real 0m4.280s user 0m3.909s sys 0m0.214s + status=0 + set +x ================================================= data/session03/05_xfoil_Camber_Plot.py passed (as expected) ================================================= ================================================= 05_xfoil_Camber.py test; + python 05_xfoil_Camber.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... ==> Creating xfoilAIM ==> Setting analysis values ==> Retrieve analysis results. camber = 0.0 ==> Retrieve analysis results. camber = 0.01 ==> Retrieve analysis results. camber = 0.04 ==> Retrieve analysis results. camber = 0.07 --> Cambers = [0.0, 0.01, 0.04, 0.07] --> Alpha = [[0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0]] --> Cl = [[-3.53757125655385e-07, 0.126697477361167, 0.377437462181223], [0.140339949737382, 0.266469023977517, 0.514670926888889], [0.554542727545724, 0.680708956698588, 0.940291957324874], [0.919771481559598, 1.03861131519228]] --> Cd = [[0.00617285380994127, 0.00627268560115845, 0.00729426778762296], [0.00625861871528683, 0.00622635244563391, 0.00706717658622291], [0.00787687247022521, 0.00739456756394117, 0.00782133651724681], [0.00972065010479203, 0.0101041953398598]] real 0m1.958s user 0m2.010s sys 0m0.151s + status=0 + set +x ================================================= data/session03/05_xfoil_Camber.py passed (as expected) ================================================= ================================================= 06_xfoil_CleanDirty.py test; + python 06_xfoil_CleanDirty.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... ==> Creating xfoilAIM 1. No Errors -------------------------------------------------------------------------------- ==> Setting alpha sequence ==> Running preAnalysis ==> Running xFoil...... ==> Running postAnalysis --> Cl = [-3.53757125655385e-07, 0.377437462009099, 0.642259371967833, 0.955175653138806, 1.00909750957761] 2. DIRTY AnalysisVal Error -------------------------------------------------------------------------------- ==> Setting new alpha sequence ==> Attempting to get Cl ==> CAPSError = CAPS_DIRTY: ================================================================================ ================================================================================ ==> Running preAnalysis ==> Running xFoil...... ==> Running postAnalysis ==> Attempting to get Cl --> Cl = 0.252764696628542 3. DIRTY GeometryVal Error -------------------------------------------------------------------------------- ==> Modifying camber ==> Attempting to get Cl ==> CAPSError = CAPS_DIRTY: ================================================================================ ================================================================================ ==> Running preAnalysis ==> Running xFoil...... ==> Running postAnalysis ==> Attempting to get Cl --> Cl = [1.03861130997329, 1.15325582947796] 4. DIRTY pre- but no postAnalysis Error -------------------------------------------------------------------------------- ==> Modifying Mach ==> Running preAnalysis but not running postAnalysis ==> Attempting to get Cl ==> CAPSError = CAPS_DIRTY: ================================================================================ ================================================================================ ==> Running xFoil...... ==> Running postAnalysis ==> Attempting to get Cl --> Cl = [0.967203918355951, 1.07899610948977] 5. CLEAN Error -------------------------------------------------------------------------------- ==> Running preAnalysis ==> CAPSError = CAPS_CLEAN: ================================================================================ ================================================================================ real 0m1.884s user 0m1.848s sys 0m0.159s + status=0 + set +x ================================================= data/session03/06_xfoil_CleanDirty.py passed (as expected) ================================================= ================================================= 07_masstran_f118_AIM.py test; + python 07_masstran_f118_AIM.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-B.csm"... ==> Geometry used by masstranAll instance with no capsIntent ==> Geometry used by Wing instance with capsIntent='wing' ==> Geometry used by Tail instance with capsIntent='tail' ==> Geometry used by WingFuse instance with capsIntent=['wing','fuse'] real 0m0.710s user 0m0.519s sys 0m0.305s + status=0 + set +x ================================================= data/session03/07_masstran_f118_AIM.py passed (as expected) ================================================= ================================================= 08_masstran_f118_Wing.py test; + python 08_masstran_f118_Wing.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-C.csm"... Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = wing:faces, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing:faces Done getting FEA properties Updating mesh element types based on properties input --> Mass = 14792888.88889 --> CG = [64.85254706407, 3.3674366504e-14, -3.914745293593] real 0m0.520s user 0m0.524s sys 0m0.155s + status=0 + set +x ================================================= data/session03/08_masstran_f118_Wing.py passed (as expected) ================================================= ================================================= 09_masstran_f118.py test; + python 09_masstran_f118.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-C.csm"... Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 6 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - Madeupium No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic" Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 6 Property name - fuse:nose Property name - fuse:side Property name - fuse:tail Property name - htail:faces Property name - vtail:faces Property name - wing:faces Done getting FEA properties Updating mesh element types based on properties input -->Mass = 52825838.86801 -->CG = [91.69615213878, 5.294802100603e-15, 0.7254947287442] real 0m0.407s user 0m0.475s sys 0m0.152s + status=0 + set +x ================================================= data/session03/09_masstran_f118.py passed (as expected) ================================================= ================================================= 10_masstran_f118_journal.py test; + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log + python 10_masstran_f118_journal.py ################################################################################ ==> First execution ==> Loading geometry from file "f118-C.csm"... ================================================================================ ==> Computing mass 1 Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = wing:faces, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 488 Number of elements = 972 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 972 Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing:faces Done getting FEA properties Updating mesh element types based on properties input --> 14792888.88889 Something went wrong! ################################################################################ ==> Second execution ==> Loading geometry from file "f118-C.csm"... ================================================================================ ==> Computing mass 1 --> 14792888.88889 CAPS Info: Hit last success -- going live! ================================================================================ ==> Computing mass 2 Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = wing:faces, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 488 Number of elements = 972 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 972 Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing:faces Done getting FEA properties Updating mesh element types based on properties input --> 1479288.888889 Something went wrong! ################################################################################ ==> Third execution ==> Loading geometry from file "f118-C.csm"... ================================================================================ ==> Computing mass 1 --> 14792888.88889 ================================================================================ ==> Computing mass 2 --> 1479288.888889 CAPS Info: Hit last success -- going live! ================================================================================ ==> Computing mass 3 Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = wing:faces, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 488 Number of elements = 972 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 972 Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing:faces Done getting FEA properties Updating mesh element types based on properties input --> 147928.8888889 ################################################################################ ==> Fourth execution ==> Loading geometry from file "f118-C.csm"... ================================================================================ ==> Computing mass 1 --> 14792888.88889 ================================================================================ ==> Computing mass 2 --> 1479288.888889 ================================================================================ ==> Computing mass 3 --> 147928.8888889 real 0m0.535s user 0m0.527s sys 0m0.190s + status=0 + set +x ================================================= data/session03/10_masstran_f118_journal.py passed (as expected) ================================================= ================================================= + echo 'f118-C.csm test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log f118-C.csm test; + /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-C.csm + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log WARNING:: cannot open "./verify_7.8.1/f118-C.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.130s user 0m0.116s sys 0m0.009s + status=0 + set +x ================================================= solutions/session03/f118-C passed (as expected) ================================================= ================================================= xfoil_thickness.py test; + python xfoil_thickness.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../../data/session03/naca.csm"... ==> Create xfoilAIM ==> Setting analysis values ==> Retrieve analysis results ==> Retrieve analysis results ==> Retrieve analysis results ==> Retrieve analysis results --> Thickness = [0.08, 0.1, 0.12, 0.16] --> Alpha = [[0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0, 3.0]] --> Cl = [[4.33419461234289e-07, 0.118003705247125, 0.4078230913009], [3.88197275319707e-07, 0.12399312361356, 0.371340021267165], [-3.53757125655385e-07, 0.126697477361167, 0.377437462181223], [2.73507879809025e-07, 0.127624319978928, 0.380868543480744]] --> Cd = [[0.00449613835213978, 0.00482192214520964, 0.00769709940290085], [0.00540044826496585, 0.0055477373653873, 0.00718424709040834], [0.00617285380994127, 0.00627268560115845, 0.00729426778762296], [0.00752780925536514, 0.0075937493874947, 0.00822813502005816]] real 0m1.209s user 0m1.288s sys 0m0.153s + status=0 + set +x ================================================= solutions/session03/xfoil_thickness.py passed (as expected) ================================================= ================================================= f118_masstran.py test; + python f118_masstran.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../../data/session03/f118-B.csm"... ==> Geometry with capsIntent=['wing','fuse', 'htail'] real 0m0.522s user 0m0.520s sys 0m0.135s + status=0 + set +x ================================================= solutions/session03/f118_masstran.py passed (as expected) ================================================= ================================================= masstran_topbot.py test; + python masstran_topbot.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-C.csm"... Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - Madeupium No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic" Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 8 Property name - fuse:bottom Property name - fuse:nose Property name - fuse:side Property name - fuse:tail Property name - fuse:top Property name - htail:faces Property name - vtail:faces Property name - wing:faces Done getting FEA properties Updating mesh element types based on properties input -->Mass = 52073438.86801 -->CG = [91.72065954403, 0.04009689171826, 0.1932821772294] real 0m0.421s user 0m0.497s sys 0m0.166s + status=0 + set +x ================================================= solutions/session03/masstran_topbot.py passed (as expected) ================================================= ================================================= masstran_CG.py test; + python masstran_CG.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "f118-C.csm"... Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - Madeupium No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic" Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 8 Property name - fuse:bottom Property name - fuse:nose Property name - fuse:side Property name - fuse:tail Property name - fuse:top Property name - htail:faces Property name - vtail:faces Property name - wing:faces 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined 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 = 8 Name = wing:faces, index = 1 Name = htail:faces, index = 2 Name = vtail:faces, index = 3 Name = fuse:nose, index = 4 Name = fuse:tail, index = 5 Name = fuse:side, index = 6 Name = fuse:bottom, index = 7 Name = fuse:top, index = 8 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 900 Number of elements = 1796 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1796 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 170 Number of elements = 336 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 336 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 90 Number of elements = 176 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 176 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 1698 Number of elements = 3392 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3392 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 2858 Combined Number of elements = 5700 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 5700 Combined Elemental Quad4 = 0 Updating mesh element types based on properties input -->Oringal CG = 91.72065954403 -->CG sweep = [84.05056882825, 85.58458697141, 87.11860511456, 88.65262325772, 90.18664140087, 91.72065954403, 93.25467768718, 94.78869583034, 96.32271397349, 97.85673211665, 99.3907502598] real 0m0.833s user 0m0.652s sys 0m0.343s + status=0 + set +x ================================================= solutions/session03/masstran_CG.py passed (as expected) ================================================= ================================================= + echo 'f118-D.csm test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log f118-D.csm test; + /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-D.csm + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log WARNING:: cannot open "./verify_7.8.1/f118-D.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.122s user 0m0.115s sys 0m0.009s + status=0 + set +x ================================================= data/session04/f118-D passed (as expected) ================================================= ================================================= + echo 'naca.csm test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log naca.csm test; + /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 naca.csm + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log WARNING:: cannot open "./verify_7.8.1/naca.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.129s user 0m0.123s sys 0m0.009s + status=0 + set +x ================================================= data/session04/naca passed (as expected) ================================================= ================================================= 1_mses_Deriv.py test; + python 1_mses_Deriv.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... ==> Area and Area derivatives... --> Area 0.082218968985062 --> dArea/dthick 0.6847211877073472 ==> Drag and Drag derivatives... Getting CFD design variables....... Number of design variables - 2 Design Variable name - camber Design Variable name - thick Done getting CFD design variables --> CD = 0.005288407930235986 --> dCD/dAlpha = -2.872255740855454e-07 --> dCD/dMach = 0.0012453366375636868 --> dCD/dcamber = -3.202096592002027e-05 --> dCD/dthick = 0.01572066789258299 ==> All Drag derivatives... --> CD derivs = {'Alpha': -2.872255740855454e-07, 'Mach': 0.0012453366375636868, 'Re': -3.6387727030798095e-11, 'camber': -3.202096592002027e-05, 'thick': 0.01572066789258299} real 0m2.155s user 0m2.200s sys 0m0.134s + status=0 + set +x ================================================= data/session04/1_mses_Deriv.py passed (as expected) ================================================= ================================================= 2_mses_DerivPlot_CD_Alpha.py test; + python 2_mses_DerivPlot_CD_Alpha.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... --> Alpha -3.0 --> Alpha -2.5714285714285716 --> Alpha -2.142857142857143 --> Alpha -1.7142857142857144 --> Alpha -1.2857142857142858 --> Alpha -0.8571428571428572 --> Alpha -0.4285714285714288 --> Alpha 0.0 --> Alpha 0.4285714285714284 --> Alpha 0.8571428571428568 --> Alpha 1.2857142857142856 --> Alpha 1.7142857142857144 --> Alpha 2.1428571428571423 --> Alpha 2.571428571428571 --> Alpha 3.0 /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/2_mses_DerivPlot_CD_Alpha.py:77: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown plt.show() real 0m28.509s user 0m25.773s sys 0m0.779s + status=0 + set +x ================================================= data/session04/2_mses_DerivPlot_CD_Alpha.py passed (as expected) ================================================= ================================================= 3_mses_OpenMDAO_CD_Alpha.py test; + python 3_mses_OpenMDAO_CD_Alpha.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:38983] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/2802712576/sm_segment.VIGGEN.502.a70e0000.0 could be created. ==> Starting Optimization... --> Alpha [3.] --> CD [0.00803595] --> Alpha [3.] --> CD [0.00803595] --> Alpha [3.] --> CD_alpha [[0.00014124]] RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 8.03595D-03 |proj g|= 1.41235D-04 --> Alpha [2.99985876] --> CD [0.00803593] --> Alpha [2.99985876] --> CD_alpha [[0.00014123]] At iterate 1 f= 8.03593D-03 |proj g|= 1.41231D-04 --> Alpha [-1.95855368] --> CD [0.0079199] --> Alpha [-1.95855368] --> CD_alpha [[-8.82237932e-05]] At iterate 2 f= 7.91990D-03 |proj g|= 8.82238D-05 --> Alpha [-0.05208071] --> CD [0.00783467] --> Alpha [-0.05208071] --> CD_alpha [[-2.58066379e-06]] At iterate 3 f= 7.83467D-03 |proj g|= 2.58066D-06 --> Alpha [0.00536658] --> CD [0.0078346] --> Alpha [0.00536658] --> CD_alpha [[1.71380689e-08]] At iterate 4 f= 7.83460D-03 |proj g|= 1.71381D-08 --> Alpha [0.00498759] --> CD [0.0078346] --> Alpha [0.00498759] --> CD_alpha [[-2.03931178e-09]] At iterate 5 f= 7.83460D-03 |proj g|= 2.03931D-09 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 5 6 5 0 0 2.039D-09 7.835D-03 F = 7.8346014199255319E-003 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- --> Optimized value: [0.00498759] real 0m13.906s user 0m12.432s sys 0m0.619s + status=0 + set +x ================================================= data/session04/3_mses_OpenMDAO_CD_Alpha.py passed (as expected) ================================================= ================================================= 4_mses_DerivPlot_CD_camber.py test; + python 4_mses_DerivPlot_CD_camber.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... --> camber -0.1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - camber Done getting CFD design variables --> camber -0.08571428571428572 --> camber -0.07142857142857142 --> camber -0.05714285714285715 --> camber -0.04285714285714286 --> camber -0.028571428571428567 --> camber -0.01428571428571429 --> camber 0.0 --> camber 0.01428571428571429 --> camber 0.02857142857142858 --> camber 0.04285714285714287 --> camber 0.05714285714285716 --> camber 0.07142857142857142 --> camber 0.08571428571428572 --> camber 0.1 /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/4_mses_DerivPlot_CD_camber.py:80: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown plt.show() real 0m28.849s user 0m27.559s sys 0m0.673s + status=0 + set +x ================================================= data/session04/4_mses_DerivPlot_CD_camber.py passed (as expected) ================================================= ================================================= 5_mses_OpenMDAO_CD_camber.py test; + python 5_mses_OpenMDAO_CD_camber.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:39190] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/773128192/sm_segment.VIGGEN.502.2e150000.0 could be created. ==> Starting Optimization... --> camber [0.1] Getting CFD design variables....... Number of design variables - 1 Design Variable name - camber Done getting CFD design variables --> CD [0.01370215] --> camber [0.1] --> CD [0.01370215] --> camber [0.1] --> CD_camber [[0.17593485]] RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 1 variables are exactly at the bounds At iterate 0 f= 1.37022D-02 |proj g|= 1.75935D-01 --> camber [-0.07593485] --> CD [0.01053684] --> camber [-0.07593485] --> CD_camber [[-0.07712924]] At iterate 1 f= 1.05368D-02 |proj g|= 7.71292D-02 --> camber [-0.02231317] --> CD [0.00803517] --> camber [-0.02231317] --> CD_camber [[-0.0171107]] At iterate 2 f= 8.03517D-03 |proj g|= 1.71107D-02 --> camber [-0.00702616] --> CD [0.0078537] --> camber [-0.00702616] --> CD_camber [[-0.00523687]] At iterate 3 f= 7.85370D-03 |proj g|= 5.23687D-03 --> camber [-0.00028392] --> CD [0.00783468] --> camber [-0.00028392] --> CD_camber [[-0.00015053]] At iterate 4 f= 7.83468D-03 |proj g|= 1.50527D-04 --> camber [-8.43924833e-05] --> CD [0.00783469] --> camber [-8.43924833e-05] --> CD_camber [[-4.75268316e-07]] --> camber [-0.00023422] --> CD [0.00783469] --> camber [-0.00023422] --> CD_camber [[-0.00011282]] --> camber [-0.00027527] --> CD [0.00783469] --> camber [-0.00027527] --> CD_camber [[-0.00014369]] --> camber [-0.00028357] --> CD [0.00783468] --> camber [-0.00028357] --> CD_camber [[-0.00015009]] --> camber [-0.00028392] --> CD [0.00783469] --> camber [-0.00028392] --> CD_camber [[-0.00015045]] --> camber [-0.00028392] --> CD [0.00783468] --> camber [-0.00028392] --> CD_camber [[-0.00015053]] --> camber [-0.00028392] --> CD [0.00783468] --> camber [-0.00028392] --> CD_camber [[-0.00015048]] --> camber [-0.00028392] --> CD [0.00783468] --> camber [-0.00028392] --> CD_camber [[-0.00015048]] --> camber [-0.00028392] --> CD [0.00783468] --> camber [-0.00028392] --> CD_camber [[-0.00015048]] At iterate 5 f= 7.83468D-03 |proj g|= 1.50476D-04 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 5 14 5 0 0 1.505D-04 7.835D-03 F = 7.8346831540125825E-003 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- --> Optimized value: [-0.00028392] real 0m25.988s user 0m25.417s sys 0m0.605s + status=0 + set +x ================================================= data/session04/5_mses_OpenMDAO_CD_camber.py passed (as expected) ================================================= ================================================= 6_mses_DerivPlot_CL2_camber.py test; + python 6_mses_DerivPlot_CL2_camber.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "naca.csm"... --> camber -0.1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - camber Done getting CFD design variables --> camber -0.08571428571428572 --> camber -0.07142857142857142 --> camber -0.05714285714285715 --> camber -0.04285714285714286 --> camber -0.028571428571428567 --> camber -0.01428571428571429 --> camber 0.0 --> camber 0.01428571428571429 --> camber 0.02857142857142858 --> camber 0.04285714285714287 --> camber 0.05714285714285716 --> camber 0.07142857142857142 --> camber 0.08571428571428572 --> camber 0.1 /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/6_mses_DerivPlot_CL2_camber.py:82: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown plt.show() real 0m30.671s user 0m28.397s sys 0m0.767s + status=0 + set +x ================================================= data/session04/6_mses_DerivPlot_CL2_camber.py passed (as expected) ================================================= ================================================= 7_mses_OpenMDAO_CL2_camber.py test; + python 7_mses_OpenMDAO_CL2_camber.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:39445] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/708771840/sm_segment.VIGGEN.502.2a3f0000.0 could be created. ==> Starting Optimization... --> camber [0.1] Getting CFD design variables....... Number of design variables - 1 Design Variable name - camber Done getting CFD design variables --> CL2 [1.23492174] --> camber [0.1] --> CL2 [1.23492174] --> camber [0.1] --> CL2_camber [[14.37217996]] RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 1 variables are exactly at the bounds At iterate 0 f= 1.23492D+00 |proj g|= 2.00000D-01 --> camber [-0.1] --> CL2 [1.23490353] --> camber [-0.1] --> CL2_camber [[-14.37225246]] --> camber [9.91451295e-05] --> CL2 [1.68377899e-06] --> camber [9.91451295e-05] --> CL2_camber [[0.03419212]] At iterate 1 f= 1.68378D-06 |proj g|= 3.41921D-02 --> camber [-0.00013909] --> CL2 [3.35149206e-06] --> camber [-0.00013909] --> CL2_camber [[-0.04823952]] --> camber [2.48992281e-07] --> CL2 [1.02478314e-12] --> camber [2.48992281e-07] --> CL2_camber [[-2.66746531e-05]] At iterate 2 f= 1.02478D-12 |proj g|= 2.66747D-05 --> camber [3.26085013e-07] --> CL2 [1.67189956e-13] --> camber [3.26085013e-07] --> CL2_camber [[1.07742885e-05]] At iterate 3 f= 1.67190D-13 |proj g|= 1.07743D-05 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 3 6 3 0 0 1.077D-05 1.672D-13 F = 1.6718995645907989E-013 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- --> Optimized value: [3.26085013e-07] real 0m12.564s user 0m12.392s sys 0m0.395s + status=0 + set +x ================================================= data/session04/7_mses_OpenMDAO_CL2_camber.py passed (as expected) ================================================= ================================================= 8_mses_OpenMDAO_CDCL.py test; + python 8_mses_OpenMDAO_CDCL.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:39527] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/682754048/sm_segment.VIGGEN.502.28b20000.0 could be created. ==> Starting Optimization... --> Alpha [0.] --> camber [0.1] Getting CFD design variables....... Number of design variables - 1 Design Variable name - camber Done getting CFD design variables --> CD [0.01370215] --> CL [1.11127033] --> Alpha [0.] --> camber [0.1] --> CD [0.01370215] --> CL [1.11127033] --> Alpha [0.] --> camber [0.1] --> CD_Alpha [[0.00105841]] --> CL_Alpha [[0.09897622]] --> CD_camber [[0.17593485]] --> CL_camber [[6.46655435]] --> Alpha [0.00077914] --> camber [0.04412056] --> CD [0.00864294] --> CL [0.57036568] --> Alpha [0.00077914] --> camber [0.04412056] --> CD_Alpha [[0.00023873]] --> CL_Alpha [[0.12984106]] --> CD_camber [[0.03642485]] --> CL_camber [[12.533991]] --> Alpha [0.00103084] --> camber [0.05844972] --> CD [0.0093022] --> CL [0.7443929] --> Alpha [0.00103084] --> camber [0.05844972] --> CD_Alpha [[0.00033987]] --> CL_Alpha [[0.12673046]] --> CD_camber [[0.05177195]] --> CL_camber [[11.83406756]] --> Alpha [0.00125705] --> camber [0.05892111] --> CD [0.00932813] --> CL [0.74994779] Optimization terminated successfully (Exit mode 0) Current function value: 0.009328127623067835 Iterations: 3 Function evaluations: 4 Gradient evaluations: 3 Optimization Complete ----------------------------------- --> Optimized value: [0.05892111] real 0m10.242s user 0m9.470s sys 0m0.377s + status=0 + set +x ================================================= data/session04/8_mses_OpenMDAO_CDCL.py passed (as expected) ================================================= ================================================= 9_masstran_OpenMDAO_thick.py test; + python 9_masstran_OpenMDAO_thick.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:39578] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/2254962688/sm_segment.VIGGEN.502.86680000.0 could be created. ==> Starting Optimization... /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages/openmdao/core/driver.py:619: DriverWarning:The following design variable initial conditions are out of their specified bounds: masstranSystem.x2 val: [0.] lower: 0.01 upper: 10.0 Set the initial value of the design variable to a valid value or set the driver option['invalid_desvar_behavior'] to 'ignore'. --> x1 [0.1] --> x2 [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 = 4 Name = wing, index = 1 Name = htail, index = 2 Name = vtail, index = 3 Name = fuse, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Combining multiple FEA meshes! Combined Number of nodal coordinates = 8672 Combined Number of elements = 8664 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 8664 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 4 Property name - fuse Property name - htail Property name - vtail Property name - wing Done getting FEA properties Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [2.75695334] --> x1 [0.1] --> x2 [0.01] /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/9_masstran_OpenMDAO_thick.py:52: DeprecationWarning: Conversion of an array with ndim > 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.) "x1": {"initialValue":float(inputs['x1'])}, /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/9_masstran_OpenMDAO_thick.py:53: DeprecationWarning: Conversion of an array with ndim > 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.) "x2": {"initialValue":float(inputs['x2'])}, Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [2.70119648] --> x1 [0.1] --> x2 [0.01] --> dCGx_x1 [[-68.82272937]] --> dCGx_x2 [[-5.53091882]] RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 2 M = 10 At X0 1 variables are exactly at the bounds At iterate 0 f= 2.70120D+00 |proj g|= 9.90000D+00 --> x1 [10.] --> x2 [5.54091882] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [10.16370853] --> x1 [10.] --> x2 [5.54091882] --> dCGx_x1 [[0.04843981]] --> dCGx_x2 [[0.03754845]] --> x1 [3.33378327] --> x2 [1.81664573] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [8.85443326] --> x1 [3.33378327] --> x2 [1.81664573] --> dCGx_x1 [[0.48418692]] --> dCGx_x2 [[0.1268106]] --> x1 [1.12760341] --> x2 [0.5841001] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [5.7972651] --> x1 [1.12760341] --> x2 [0.5841001] --> dCGx_x1 [[3.182136]] --> dCGx_x2 [[0.42790152]] --> x1 [0.42334159] --> x2 [0.19064405] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [1.60230885] --> x1 [0.42334159] --> x2 [0.19064405] --> dCGx_x1 [[8.88674345]] --> dCGx_x2 [[0.86253194]] At iterate 1 f= 1.60231D+00 |proj g|= 4.13342D-01 --> x1 [0.38612876] --> x2 [0.16914154] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [1.24954556] --> x1 [0.38612876] --> x2 [0.16914154] --> dCGx_x1 [[9.04121089]] --> dCGx_x2 [[0.8599867]] --> x1 [0.23727742] --> x2 [0.08313149] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [0.04927766] --> x1 [0.23727742] --> x2 [0.08313149] --> dCGx_x1 [[3.58807069]] --> dCGx_x2 [[0.31359947]] At iterate 2 f= 4.92777D-02 |proj g|= 2.27277D-01 --> x1 [0.11213433] --> x2 [0.01347811] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [1.95060563] --> x1 [0.11213433] --> x2 [0.01347811] --> dCGx_x1 [[-52.76118222]] --> dCGx_x2 [[-4.27221829]] --> x1 [0.21361795] --> x2 [0.06996287] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [5.61440048e-05] --> x1 [0.21361795] --> x2 [0.06996287] --> dCGx_x1 [[0.13868009]] --> dCGx_x2 [[0.01195172]] At iterate 3 f= 5.61440D-05 |proj g|= 1.38680D-01 --> x1 [0.21266725] --> x2 [0.06943529] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [3.06804662e-06] --> x1 [0.21266725] --> x2 [0.06943529] --> dCGx_x1 [[-0.03260179]] --> dCGx_x2 [[-0.00280809]] At iterate 4 f= 3.06805D-06 |proj g|= 3.26018D-02 --> x1 [0.2128482] --> x2 [0.0695357] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [1.43517357e-10] --> x1 [0.2128482] --> x2 [0.0695357] --> dCGx_x1 [[0.00022274]] --> dCGx_x2 [[1.91872578e-05]] At iterate 5 f= 1.43517D-10 |proj g|= 2.22739D-04 --> x1 [0.21284697] --> x2 [0.06953502] Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - x1 Design_Variable name - x2 Design_Variable_Relation name - fuseRel Design_Variable_Relation name - wingRel Number of design variable relations - 2 Done getting FEA design variables --> dCGx [3.63550505e-16] --> x1 [0.21284697] --> x2 [0.06953502] --> dCGx_x1 [[3.54510824e-07]] --> dCGx_x2 [[3.05383747e-08]] At iterate 6 f= 3.63551D-16 |proj g|= 3.54511D-07 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 2 6 12 7 0 0 3.545D-07 3.636D-16 F = 3.6355050512987024E-016 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- ==> Optimized value: --> x1 [0.21284697] --> x2 [0.06953502] real 0m1.448s user 0m1.815s sys 0m0.370s + status=0 + set +x ================================================= data/session04/9_masstran_OpenMDAO_thick.py passed (as expected) ================================================= ================================================= masstran_OpenMDAO_geom.py test; + python masstran_OpenMDAO_geom.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:39623] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/3767926784/sm_segment.VIGGEN.502.e0960000.0 could be created. ==> Initial values: htail:lh 5.0 wing:xroot 4.0 ==> Starting Optimization... --> htail:lh [5.] --> wing:xroot [4.] Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wing, index = 1 Name = htail, index = 2 Name = vtail, index = 3 Name = fuse, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Combining multiple FEA meshes! Combined Number of nodal coordinates = 8672 Combined Number of elements = 8664 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 8664 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 4 Property name - fuse Property name - htail Property name - vtail Property name - wing Done getting FEA properties Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - htail:lh Design_Variable name - wing:xroot Number of design variable relations - 0 Done getting FEA design variables --> dCGx [2.10539929] --> htail:lh [5.] --> wing:xroot [4.] --> dCGx [2.10539929] --> htail:lh [5.] --> wing:xroot [4.] --> dCGx_htail:lh [[-0.40374365]] --> dCGx_wing:xroot [[-1.15229479]] RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 2 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 2.10540D+00 |proj g|= 1.15229D+00 --> htail:lh [5.40374365] --> wing:xroot [5.15229479] Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wing, index = 1 Name = htail, index = 2 Name = vtail, index = 3 Name = fuse, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Combining multiple FEA meshes! Combined Number of nodal coordinates = 8672 Combined Number of elements = 8664 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 8664 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - htail:lh Design_Variable name - wing:xroot Number of design variable relations - 0 Done getting FEA design variables --> dCGx [0.86918465] --> htail:lh [5.40374365] --> wing:xroot [5.15229479] --> dCGx_htail:lh [[-0.30002756]] --> dCGx_wing:xroot [[-0.74124931]] At iterate 1 f= 8.69185D-01 |proj g|= 7.41249D-01 --> htail:lh [6.474753] --> wing:xroot [7.25471671] Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wing, index = 1 Name = htail, index = 2 Name = vtail, index = 3 Name = fuse, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Combining multiple FEA meshes! Combined Number of nodal coordinates = 8672 Combined Number of elements = 8664 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 8664 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - htail:lh Design_Variable name - wing:xroot Number of design variable relations - 0 Done getting FEA design variables --> dCGx [0.00905292] --> htail:lh [6.474753] --> wing:xroot [7.25471671] --> dCGx_htail:lh [[0.03711399]] --> dCGx_wing:xroot [[0.07531706]] At iterate 2 f= 9.05292D-03 |proj g|= 7.53171D-02 --> htail:lh [6.35917671] --> wing:xroot [7.05983716] Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wing, index = 1 Name = htail, index = 2 Name = vtail, index = 3 Name = fuse, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Combining multiple FEA meshes! Combined Number of nodal coordinates = 8672 Combined Number of elements = 8664 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 8664 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - htail:lh Design_Variable name - wing:xroot Number of design variable relations - 0 Done getting FEA design variables --> dCGx [1.94377289e-05] --> htail:lh [6.35917671] --> wing:xroot [7.05983716] --> dCGx_htail:lh [[-0.00169617]] --> dCGx_wing:xroot [[-0.00349307]] At iterate 3 f= 1.94377D-05 |proj g|= 3.49307D-03 --> htail:lh [6.3642348] --> wing:xroot [7.06847132] Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wing, index = 1 Name = htail, index = 2 Name = vtail, index = 3 Name = fuse, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Combining multiple FEA meshes! Combined Number of nodal coordinates = 8672 Combined Number of elements = 8664 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 8664 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - htail:lh Design_Variable name - wing:xroot Number of design variable relations - 0 Done getting FEA design variables --> dCGx [2.31615861e-10] --> htail:lh [6.3642348] --> wing:xroot [7.06847132] --> dCGx_htail:lh [[-5.85873617e-06]] --> dCGx_wing:xroot [[-1.20573655e-05]] At iterate 4 f= 2.31616D-10 |proj g|= 1.20574D-05 --> htail:lh [6.36425233] --> wing:xroot [7.06850123] Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wing, index = 1 Name = htail, index = 2 Name = vtail, index = 3 Name = fuse, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Combining multiple FEA meshes! Combined Number of nodal coordinates = 8672 Combined Number of elements = 8664 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 8664 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 2 Design_Variable name - htail:lh Design_Variable name - wing:xroot Number of design variable relations - 0 Done getting FEA design variables --> dCGx [6.3756283e-18] --> htail:lh [6.36425233] --> wing:xroot [7.06850123] --> dCGx_htail:lh [[9.72035735e-10]] --> dCGx_wing:xroot [[2.00045928e-09]] At iterate 5 f= 6.37563D-18 |proj g|= 2.00046D-09 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 2 5 6 5 0 0 2.000D-09 6.376D-18 F = 6.3756282976940919E-018 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- ==> Optimized values: --> htail:lh 6.3642523342704855 --> wing:xroot 7.068501228645885 real 0m1.419s user 0m1.899s sys 0m0.293s + status=0 + set +x ================================================= solutions/session04/masstran_OpenMDAO_geom.py passed (as expected) ================================================= ================================================= + echo 'avlPlaneVanilla.csm test;' + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log avlPlaneVanilla.csm test; + /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 avlPlaneVanilla.csm + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log WARNING:: cannot open "./verify_7.8.1/avlPlaneVanilla.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.235s user 0m0.241s sys 0m0.007s + status=0 + set +x ================================================= data/session06/avlPlaneVanilla passed (as expected) ================================================= ================================================= 1_avl_PlaneVanilla.py test; + python 1_avl_PlaneVanilla.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "avlPlaneVanilla.csm"... ==> Viewing Plane Vanilla bodies... ==> Create avlAIM ==> Viewing AVL Plane Vanilla bodies... ==> Setting analysis values Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing, index = 1 Name = Htail, index = 2 Name = Vtail, index = 3 Getting vortex lattice surface data VLM surface name - Htail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vtail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data 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. Warning: Control AileronRight not found in controls tuple! Only defaults will be used. Warning: Control AileronLeft not found in controls tuple! Only defaults will be used. Warning: Control AileronRight not found in controls tuple! Only defaults will be used. Warning: Control AileronLeft not found in controls tuple! Only defaults will be used. Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 1) Control surface 1 of 1 Section 2 of 3 (ID = 0) Control surface 1 of 1 Section 3 of 3 (ID = 2) Control surface 1 of 1 Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Control surface 1 of 1 Section 2 of 2 (ID = 0) Control surface 1 of 1 Writing surface - Wing (ID = 2) Section 1 of 3 (ID = 1) Control surface 1 of 1 Section 2 of 3 (ID = 0) Control surface 1 of 2 Control surface 2 of 2 Section 3 of 3 (ID = 2) Control surface 1 of 1 --> CLtot = 0.5813612009189711 --> CDtot = 0.006414738598441995 --> CDind = 0.006414738598441995 --> e = 0.9155417145048229 real 0m0.617s user 0m0.650s sys 0m0.261s + status=0 + set +x ================================================= data/session06/1_avl_PlaneVanilla.py passed (as expected) ================================================= ================================================= 2_avl_PlaneVanillaControl.py test; + python 2_avl_PlaneVanillaControl.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "avlPlaneVanilla.csm"... ==> Creating avlAIM ==> Setting analysis values ==> Some stability derivatives (old) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing, index = 1 Name = Htail, index = 2 Name = Vtail, index = 3 Getting vortex lattice control surface data VLM control surface name - AileronLeft VLM control surface name - AileronRight VLM control surface name - Elevator VLM control surface name - Rudder Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Htail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vtail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 1) Control surface 1 of 1 Section 2 of 3 (ID = 0) Control surface 1 of 1 Section 3 of 3 (ID = 2) Control surface 1 of 1 Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Control surface 1 of 1 Section 2 of 2 (ID = 0) Control surface 1 of 1 Writing surface - Wing (ID = 2) Section 1 of 3 (ID = 1) Control surface 1 of 1 Section 2 of 3 (ID = 0) Control surface 1 of 2 Control surface 2 of 2 Section 3 of 3 (ID = 2) Control surface 1 of 1 --> CLa = 6.186807004014293 --> CLb = 0.06076552926076213 --> CLp' = 0.07726884270666666 --> CLq' = 11.77186898086249 --> CLr' = 0.9883703770429457 --> dCL/dAileronRight = 0.02247452142379 --> dCL/dAileronLeft = 0.02252467496153 --> dCL/dElevator = 0.005432144424891 --> dCL/dRudder = -2.654018025316e-06 ==> Some stability derivatives (new) --> dCL/dAlpha = 6.186807004014293 --> dCL/dBeta = 0.06076552926076213 --> dCL/dp' = 0.07726884270666666 --> dCL/dq' = 11.77186898086249 --> dCL/dr' = 0.9883703770429457 --> dCL/dAileronRight = 0.02247452142379324 --> dCL/dAileronLeft = 0.02252467496152878 --> dCL/dElevator = 0.005432144424890901 --> dCL/dRudder = -2.654018025315729e-06 real 0m0.610s user 0m0.641s sys 0m0.265s + status=0 + set +x ================================================= data/session06/2_avl_PlaneVanillaControl.py passed (as expected) ================================================= ================================================= 3_avl_TransportGeom.py test; + python 3_avl_TransportGeom.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... ==> Viewing transport bodies... MESSAGE:: Building wingOml MESSAGE:: Building wingHinges MESSAGE:: Building htailOml MESSAGE:: Building htailHinges MESSAGE:: Building vtailOml MESSAGE:: Building vtailHinges ==> Create AVL aim... ==> Viewing avl bodies... real 0m13.037s user 0m12.695s sys 0m32.734s + status=0 + set +x ================================================= data/session06/3_avl_TransportGeom.py passed (as expected) ================================================= ================================================= 4_avl_TransportControl.py test; + python 4_avl_TransportControl.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... ==> Setting Build Variables and Geometry Values... ==> Creating AVL aim... MESSAGE:: Building wingOml MESSAGE:: Building wingHinges MESSAGE:: Building htailOml MESSAGE:: Building htailHinges MESSAGE:: Building vtailOml MESSAGE:: Building vtailHinges Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing, index = 1 Name = Htail, index = 2 Name = Vtail, index = 3 Getting vortex lattice control surface data VLM control surface name - HtailControl_1 VLM control surface name - VtailControl_1 VLM control surface name - WingControl_1 VLM control surface name - WingControl_2 VLM control surface name - WingControl_3 VLM control surface name - WingControl_4 Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Htail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vtail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Warning: Control htailControl1 not found in controls tuple! Only defaults will be used. Warning: Control htailControl1 not found in controls tuple! Only defaults will be used. Warning: Control htailControl1 not found in controls tuple! Only defaults will be used. Warning: Control htailControl1 not found in controls tuple! Only defaults will be used. Warning: Control VtailControl1 not found in controls tuple! Only defaults will be used. Warning: Control VtailControl1 not found in controls tuple! Only defaults will be used. Warning: Control WingControl1 not found in controls tuple! Only defaults will be used. Warning: Control WingControl1 not found in controls tuple! Only defaults will be used. Warning: Control WingControl2 not found in controls tuple! Only defaults will be used. Warning: Control WingControl2 not found in controls tuple! Only defaults will be used. Warning: Control WingControl3 not found in controls tuple! Only defaults will be used. Warning: Control WingControl3 not found in controls tuple! Only defaults will be used. Warning: Control WingControl3 not found in controls tuple! Only defaults will be used. Warning: Control WingControl3 not found in controls tuple! Only defaults will be used. Warning: Control WingControl2 not found in controls tuple! Only defaults will be used. Warning: Control WingControl2 not found in controls tuple! Only defaults will be used. Warning: Control WingControl4 not found in controls tuple! Only defaults will be used. Warning: Control WingControl4 not found in controls tuple! Only defaults will be used. Writing surface - Htail (ID = 0) Section 1 of 7 (ID = 0) Section 2 of 7 (ID = 3) Control surface 1 of 1 Section 3 of 7 (ID = 4) Control surface 1 of 1 Section 4 of 7 (ID = 1) Section 5 of 7 (ID = 5) Control surface 1 of 1 Section 6 of 7 (ID = 6) Control surface 1 of 1 Section 7 of 7 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 4 (ID = 1) Section 2 of 4 (ID = 3) Control surface 1 of 1 Section 3 of 4 (ID = 2) Control surface 1 of 1 Section 4 of 4 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 17 (ID = 0) Section 2 of 17 (ID = 5) Control surface 1 of 1 Section 3 of 17 (ID = 6) Control surface 1 of 1 Section 4 of 17 (ID = 7) Control surface 1 of 1 Section 5 of 17 (ID = 8) Control surface 1 of 1 Section 6 of 17 (ID = 4) Section 7 of 17 (ID = 9) Control surface 1 of 1 Section 8 of 17 (ID = 10) Control surface 1 of 1 Section 9 of 17 (ID = 1) Section 10 of 17 (ID = 11) Control surface 1 of 1 Section 11 of 17 (ID = 12) Control surface 1 of 1 Section 12 of 17 (ID = 3) Section 13 of 17 (ID = 13) Control surface 1 of 1 Section 14 of 17 (ID = 14) Control surface 1 of 1 Section 15 of 17 (ID = 15) Control surface 1 of 1 Section 16 of 17 (ID = 16) Control surface 1 of 1 Section 17 of 17 (ID = 2) ==> Some stability derivatives --> CLa = 5.329630947526096 --> CLb = 4.550909963080161e-09 --> CLp' = -1.341952384696066e-09 --> CLq' = 28.72846815689969 --> CLr' = -3.260899281924948e-09 --> Xcg = 55.4263 --> Xnp = 91.29113395768172 --> StaticMargin = 1.6523694274698266 --> htailControl1 {'CLtot': 0.008154370130359, 'CYtot': -9.150042215949e-11, "Cl'tot": -4.341969980189e-12, 'Cmtot': -0.03748884158765, "Cn'tot": 5.676266392608e-11, 'CDff': 0.001133243748512, 'e': -0.003225846838851} --> VtailControl1 {'CLtot': -3.394363229977e-11, 'CYtot': 0.001746902759648, "Cl'tot": 0.00015788879711, 'Cmtot': 1.638782106979e-10, "Cn'tot": -0.0009155267227964, 'CDff': 7.439468599435e-12, 'e': -9.055415862979e-11} --> WingControl1 {'CLtot': 0.00245427242356, 'CYtot': 0.0001047561004524, "Cl'tot": 0.0008699288737981, 'Cmtot': -0.006084028421025, "Cn'tot": 0.0001105827384316, 'CDff': 4.762247994044e-05, 'e': 0.002671724673481} --> WingControl2 {'CLtot': 0.00887521630351, 'CYtot': -6.354525089904e-12, "Cl'tot": -1.792994381086e-13, 'Cmtot': -0.01681583906716, "Cn'tot": 3.382459389563e-12, 'CDff': 0.0003695424562226, 'e': 0.007231117327731} --> WingControl3 {'CLtot': 0.005956182076864, 'CYtot': 1.810237567303e-11, "Cl'tot": 7.034779654232e-13, 'Cmtot': -0.005500424410978, "Cn'tot": -1.104493635082e-11, 'CDff': 0.0007054645324542, 'e': -0.0007874262410477} --> WingControl4 {'CLtot': 0.002454272422219, 'CYtot': -0.0001047561036864, "Cl'tot": -0.000869928873921, 'Cmtot': -0.006084028416179, "Cn'tot": -0.0001105827366425, 'CDff': 4.762247984573e-05, 'e': 0.002671724673447} real 0m13.357s user 0m13.014s sys 0m31.813s + status=0 + set +x ================================================= data/session06/4_avl_TransportControl.py passed (as expected) ================================================= ================================================= 5_avl_TransportEigen.py test; + python 5_avl_TransportEigen.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... ==> Setting Build Variables and Geometry Values... ==> Create AVL aim... ==> Running Analysis MESSAGE:: Building wingOml MESSAGE:: Building htailOml MESSAGE:: Building vtailOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing, index = 1 Name = Htail, index = 2 Name = Vtail, index = 3 Getting vortex lattice surface data VLM surface name - Htail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vtail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO ==> Outputs --> Xcg = 89.3122 meter --> Xnp = 92.43912771102477 meter --> StaticMargin = 0.472651679029349 --> EigenValues {'case 1': [[-3.1240286, 0.0], [0.019757061, 0.97330897], [0.019757061, -0.97330897], [-0.01302709, 0.0], [-0.32616585, 0.92439209], [-0.32616585, -0.92439209], [-0.013243777, 0.13183874], [-0.013243777, -0.13183874]]} --> Real Eigen Values = [-3.1240286, 0.019757061, 0.019757061, -0.01302709, -0.32616585, -0.32616585, -0.013243777, -0.013243777] real 0m3.573s user 0m3.217s sys 0m5.926s + status=0 + set +x ================================================= data/session06/5_avl_TransportEigen.py passed (as expected) ================================================= ================================================= 6_avl_masstran_Geom.py test; + python 6_avl_masstran_Geom.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... ==> Vewing AVL geometry MESSAGE:: Building wingOml MESSAGE:: Building htailOml MESSAGE:: Building vtailOml MESSAGE:: Building fuseOml ==> Vewing Masstran geometry real 0m3.608s user 0m3.059s sys 0m6.963s + status=0 + set +x ================================================= data/session06/6_avl_masstran_Geom.py passed (as expected) ================================================= ================================================= 7_avl_masstran_Eigen.py test; + python 7_avl_masstran_Eigen.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... ==> Setting Build Variables and Geometry Values... ==> Creating masstran aim... ==> Creating AVL aim... ==> Running Analysis MESSAGE:: Building wingOml MESSAGE:: Building htailOml MESSAGE:: Building vtailOml MESSAGE:: Building fuseOml Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wingSkin, index = 1 Name = fuseSkin, index = 2 Name = htailSkin, index = 3 Name = vtailSkin, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 5622 Number of elements = 11240 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 11240 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 5460 Number of elements = 10916 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 10916 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 5144 Number of elements = 10284 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 10284 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2722 Number of elements = 5440 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 5440 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 18948 Combined Number of elements = 37880 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 37880 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 4 Property name - fuseSkin Property name - htailSkin Property name - vtailSkin Property name - wingSkin Done getting FEA properties Updating mesh element types based on properties input Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing, index = 1 Name = Htail, index = 2 Name = Vtail, index = 3 Getting vortex lattice surface data VLM surface name - Htail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vtail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO ==> Outputs --> Xcg = 89.6972 meter --> Xnp = 92.42424816606338 meter --> StaticMargin = 0.41220776864756814 --> EigenValues {'case 1': [[-0.70464716, 0.0], [0.13847231, 0.55144718], [0.13847231, -0.55144718], [-0.16139632, 0.51326027], [-0.16139632, -0.51326027], [-0.0068175359, 0.0], [-0.0164897, 0.12092115], [-0.0164897, -0.12092115]]} --> Real Eigen Values = [-0.70464716, 0.13847231, 0.13847231, -0.16139632, -0.16139632, -0.0068175359, -0.0164897, -0.0164897] real 0m5.272s user 0m5.203s sys 0m6.090s + status=0 + set +x ================================================= data/session06/7_avl_masstran_Eigen.py passed (as expected) ================================================= ================================================= 8_avl_friction_Link.py test; + python 8_avl_friction_Link.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... MESSAGE:: Building wingOml MESSAGE:: Building htailOml MESSAGE:: Building vtailOml Lifting Surface: Body = 1, units ft XLE: 118.390617 -97.671924 3.992604 XTE: 123.551941 -97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 2, units ft XLE: 50.000000 0.000000 -8.000000 XTE: 97.200785 -0.000000 -7.176107 Chord: 47.207975 Arc: 97.395848 T/C: 0.145499 Type: Wing Lifting Surface: Body = 3, units ft XLE: 118.390617 97.671924 3.992604 XTE: 123.551941 97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 4, units ft XLE: 75.304787 36.138982 -3.562691 XTE: 97.933561 36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 5, units ft XLE: 75.304787 -36.138982 -3.562691 XTE: 97.933561 -36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 6, units ft XLE: 165.023151 -35.780198 13.605316 XTE: 173.282263 -35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 7, units ft XLE: 135.000000 0.000000 6.000000 XTE: 160.026192 -0.000000 6.000000 Chord: 25.026192 Arc: 50.556450 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 8, units ft XLE: 165.023151 35.780198 13.605316 XTE: 173.282263 35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 9, units ft XLE: 136.456162 0.000000 9.001500 XTE: 159.447890 -0.000000 9.001500 Chord: 22.991728 Arc: 46.446544 T/C: 0.080010 Type: Vertical_Tail Lifting Surface: Body = 10, units ft XLE: 162.940713 0.000000 35.486051 XTE: 169.379597 -0.000000 35.486051 Chord: 6.438884 Arc: 13.007456 T/C: 0.080010 Type: Vertical_Tail Number of sections 7, number of revolution sections 0 Number of Mach-Altitude cases = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing, index = 1 Name = Htail, index = 2 Name = Vtail, index = 3 Getting vortex lattice surface data VLM surface name - Htail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vtail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Lifting Surface: Body = 1, units ft XLE: 118.390617 -97.671924 3.992604 XTE: 123.551941 -97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 2, units ft XLE: 50.000000 0.000000 -8.000000 XTE: 97.200785 -0.000000 -7.176107 Chord: 47.207975 Arc: 97.395848 T/C: 0.145499 Type: Wing Lifting Surface: Body = 3, units ft XLE: 118.390617 97.671924 3.992604 XTE: 123.551941 97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 4, units ft XLE: 75.304787 36.138982 -3.562691 XTE: 97.933561 36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 5, units ft XLE: 75.304787 -36.138982 -3.562691 XTE: 97.933561 -36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 6, units ft XLE: 165.023151 -35.780198 13.605316 XTE: 173.282263 -35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 7, units ft XLE: 135.000000 0.000000 6.000000 XTE: 160.026192 -0.000000 6.000000 Chord: 25.026192 Arc: 50.556450 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 8, units ft XLE: 165.023151 35.780198 13.605316 XTE: 173.282263 35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 9, units ft XLE: 136.456162 0.000000 9.001500 XTE: 159.447890 -0.000000 9.001500 Chord: 22.991728 Arc: 46.446544 T/C: 0.080010 Type: Vertical_Tail Lifting Surface: Body = 10, units ft XLE: 162.940713 0.000000 35.486051 XTE: 169.379597 -0.000000 35.486051 Chord: 6.438884 Arc: 13.007456 T/C: 0.080010 Type: Vertical_Tail Number of sections 7, number of revolution sections 0 Number of Mach-Altitude cases = 1 Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Lifting Surface: Body = 1, units ft XLE: 118.390617 -97.671924 3.992604 XTE: 123.551941 -97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 2, units ft XLE: 50.000000 0.000000 -8.000000 XTE: 97.200785 -0.000000 -7.176107 Chord: 47.207975 Arc: 97.395848 T/C: 0.145499 Type: Wing Lifting Surface: Body = 3, units ft XLE: 118.390617 97.671924 3.992604 XTE: 123.551941 97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 4, units ft XLE: 75.304787 36.138982 -3.562691 XTE: 97.933561 36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 5, units ft XLE: 75.304787 -36.138982 -3.562691 XTE: 97.933561 -36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 6, units ft XLE: 165.023151 -35.780198 13.605316 XTE: 173.282263 -35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 7, units ft XLE: 135.000000 0.000000 6.000000 XTE: 160.026192 -0.000000 6.000000 Chord: 25.026192 Arc: 50.556450 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 8, units ft XLE: 165.023151 35.780198 13.605316 XTE: 173.282263 35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 9, units ft XLE: 136.456162 0.000000 9.001500 XTE: 159.447890 -0.000000 9.001500 Chord: 22.991728 Arc: 46.446544 T/C: 0.080010 Type: Vertical_Tail Lifting Surface: Body = 10, units ft XLE: 162.940713 0.000000 35.486051 XTE: 169.379597 -0.000000 35.486051 Chord: 6.438884 Arc: 13.007456 T/C: 0.080010 Type: Vertical_Tail Number of sections 7, number of revolution sections 0 Number of Mach-Altitude cases = 1 Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Lifting Surface: Body = 1, units ft XLE: 118.390617 -97.671924 3.992604 XTE: 123.551941 -97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 2, units ft XLE: 50.000000 0.000000 -8.000000 XTE: 97.200785 -0.000000 -7.176107 Chord: 47.207975 Arc: 97.395848 T/C: 0.145499 Type: Wing Lifting Surface: Body = 3, units ft XLE: 118.390617 97.671924 3.992604 XTE: 123.551941 97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 4, units ft XLE: 75.304787 36.138982 -3.562691 XTE: 97.933561 36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 5, units ft XLE: 75.304787 -36.138982 -3.562691 XTE: 97.933561 -36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 6, units ft XLE: 165.023151 -35.780198 13.605316 XTE: 173.282263 -35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 7, units ft XLE: 135.000000 0.000000 6.000000 XTE: 160.026192 -0.000000 6.000000 Chord: 25.026192 Arc: 50.556450 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 8, units ft XLE: 165.023151 35.780198 13.605316 XTE: 173.282263 35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 9, units ft XLE: 136.456162 0.000000 9.001500 XTE: 159.447890 -0.000000 9.001500 Chord: 22.991728 Arc: 46.446544 T/C: 0.080010 Type: Vertical_Tail Lifting Surface: Body = 10, units ft XLE: 162.940713 0.000000 35.486051 XTE: 169.379597 -0.000000 35.486051 Chord: 6.438884 Arc: 13.007456 T/C: 0.080010 Type: Vertical_Tail Number of sections 7, number of revolution sections 0 Number of Mach-Altitude cases = 1 Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Lifting Surface: Body = 1, units ft XLE: 118.390617 -97.671924 3.992604 XTE: 123.551941 -97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 2, units ft XLE: 50.000000 0.000000 -8.000000 XTE: 97.200785 -0.000000 -7.176107 Chord: 47.207975 Arc: 97.395848 T/C: 0.145499 Type: Wing Lifting Surface: Body = 3, units ft XLE: 118.390617 97.671924 3.992604 XTE: 123.551941 97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 4, units ft XLE: 75.304787 36.138982 -3.562691 XTE: 97.933561 36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 5, units ft XLE: 75.304787 -36.138982 -3.562691 XTE: 97.933561 -36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 6, units ft XLE: 165.023151 -35.780198 13.605316 XTE: 173.282263 -35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 7, units ft XLE: 135.000000 0.000000 6.000000 XTE: 160.026192 -0.000000 6.000000 Chord: 25.026192 Arc: 50.556450 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 8, units ft XLE: 165.023151 35.780198 13.605316 XTE: 173.282263 35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 9, units ft XLE: 136.456162 0.000000 9.001500 XTE: 159.447890 -0.000000 9.001500 Chord: 22.991728 Arc: 46.446544 T/C: 0.080010 Type: Vertical_Tail Lifting Surface: Body = 10, units ft XLE: 162.940713 0.000000 35.486051 XTE: 169.379597 -0.000000 35.486051 Chord: 6.438884 Arc: 13.007456 T/C: 0.080010 Type: Vertical_Tail Number of sections 7, number of revolution sections 0 Number of Mach-Altitude cases = 1 Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Lifting Surface: Body = 1, units ft XLE: 118.390617 -97.671924 3.992604 XTE: 123.551941 -97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 2, units ft XLE: 50.000000 0.000000 -8.000000 XTE: 97.200785 -0.000000 -7.176107 Chord: 47.207975 Arc: 97.395848 T/C: 0.145499 Type: Wing Lifting Surface: Body = 3, units ft XLE: 118.390617 97.671924 3.992604 XTE: 123.551941 97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 4, units ft XLE: 75.304787 36.138982 -3.562691 XTE: 97.933561 36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 5, units ft XLE: 75.304787 -36.138982 -3.562691 XTE: 97.933561 -36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 6, units ft XLE: 165.023151 -35.780198 13.605316 XTE: 173.282263 -35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 7, units ft XLE: 135.000000 0.000000 6.000000 XTE: 160.026192 -0.000000 6.000000 Chord: 25.026192 Arc: 50.556450 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 8, units ft XLE: 165.023151 35.780198 13.605316 XTE: 173.282263 35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 9, units ft XLE: 136.456162 0.000000 9.001500 XTE: 159.447890 -0.000000 9.001500 Chord: 22.991728 Arc: 46.446544 T/C: 0.080010 Type: Vertical_Tail Lifting Surface: Body = 10, units ft XLE: 162.940713 0.000000 35.486051 XTE: 169.379597 -0.000000 35.486051 Chord: 6.438884 Arc: 13.007456 T/C: 0.080010 Type: Vertical_Tail Number of sections 7, number of revolution sections 0 Number of Mach-Altitude cases = 1 Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Lifting Surface: Body = 1, units ft XLE: 118.390617 -97.671924 3.992604 XTE: 123.551941 -97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 2, units ft XLE: 50.000000 0.000000 -8.000000 XTE: 97.200785 -0.000000 -7.176107 Chord: 47.207975 Arc: 97.395848 T/C: 0.145499 Type: Wing Lifting Surface: Body = 3, units ft XLE: 118.390617 97.671924 3.992604 XTE: 123.551941 97.671924 4.717949 Chord: 5.212043 Arc: 10.531921 T/C: 0.153243 Type: Wing Lifting Surface: Body = 4, units ft XLE: 75.304787 36.138982 -3.562691 XTE: 97.933561 36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 5, units ft XLE: 75.304787 -36.138982 -3.562691 XTE: 97.933561 -36.138982 -2.376767 Chord: 22.659828 Arc: 46.801094 T/C: 0.167991 Type: Wing Lifting Surface: Body = 6, units ft XLE: 165.023151 -35.780198 13.605316 XTE: 173.282263 -35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 7, units ft XLE: 135.000000 0.000000 6.000000 XTE: 160.026192 -0.000000 6.000000 Chord: 25.026192 Arc: 50.556450 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 8, units ft XLE: 165.023151 35.780198 13.605316 XTE: 173.282263 35.780198 13.605316 Chord: 8.259112 Arc: 16.684575 T/C: 0.080010 Type: Horizontal_Tail Lifting Surface: Body = 9, units ft XLE: 136.456162 0.000000 9.001500 XTE: 159.447890 -0.000000 9.001500 Chord: 22.991728 Arc: 46.446544 T/C: 0.080010 Type: Vertical_Tail Lifting Surface: Body = 10, units ft XLE: 162.940713 0.000000 35.486051 XTE: 169.379597 -0.000000 35.486051 Chord: 6.438884 Arc: 13.007456 T/C: 0.080010 Type: Vertical_Tail Number of sections 7, number of revolution sections 0 Number of Mach-Altitude cases = 1 Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) --> Mach = [0.1, 0.2, 0.30000000000000004, 0.4, 0.5, 0.6, 0.7000000000000001] --> CDp = [0.01592, 0.01416, 0.01323, 0.01259, 0.01209, 0.01167, 0.0113] --> CD = [0.02455060220988743, 0.02466896350126657, 0.02487666257532763, 0.02519203549494272, 0.02564765931512183, 0.02630248998864366, 0.02727263653466326] real 0m6.924s user 0m5.311s sys 0m7.036s + status=0 + set +x ================================================= data/session06/8_avl_friction_Link.py passed (as expected) ================================================= ================================================= avl_masstran_MainGear.py test; + python avl_masstran_MainGear.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../../data/ESP/transport.csm"... ==> Setting Build Variables and Geometry Values... ==> Create masstran aim... ==> Computing mass properties... MESSAGE:: Building wingOml MESSAGE:: Building htailOml MESSAGE:: Building vtailOml MESSAGE:: Building fuseOml Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wingSkin, index = 1 Name = fuseSkin, index = 2 Name = htailSkin, index = 3 Name = vtailSkin, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 5622 Number of elements = 11240 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 11240 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 5460 Number of elements = 10916 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 10916 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 5144 Number of elements = 10284 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 10284 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2722 Number of elements = 5440 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 5440 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 18948 Combined Number of elements = 37880 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 37880 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 4 Property name - fuseSkin Property name - htailSkin Property name - vtailSkin Property name - wingSkin Done getting FEA properties Updating mesh element types based on properties input ==> Computed mass properties... --> aircraft_skin = {'mass': , 'CG': , 'massInertia': } ==> Creating AVL aim... ==> Outputs Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing, index = 1 Name = Htail, index = 2 Name = Vtail, index = 3 Getting vortex lattice surface data VLM surface name - Htail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vtail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO --> Xcg = 89.1676 meter --> Xnp = 92.42449260375724 meter --> StaticMargin = 0.4922965606645398 --> EigenValues {'case 1': [[-0.70484997, 0.0], [0.13849195, 0.55140288], [0.13849195, -0.55140288], [-0.1642923, 0.56419037], [-0.1642923, -0.56419037], [-0.006812761, 0.0], [-0.013696194, 0.11026784], [-0.013696194, -0.11026784]]} --> Real Eigen Values = [-0.70484997, 0.13849195, 0.13849195, -0.1642923, -0.1642923, -0.006812761, -0.013696194, -0.013696194] real 0m6.198s user 0m5.792s sys 0m6.472s + status=0 + set +x ================================================= solutions/session06/avl_masstran_MainGear.py passed (as expected) ================================================= ================================================= avl_masstran_MultiMat.py test; + python avl_masstran_MultiMat.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../../data/ESP/transport.csm"... ==> Setting Build Variables and Geometry Values... ==> Create masstran aim... ==> Computing mass properties... MESSAGE:: Building wingOml MESSAGE:: Building htailOml MESSAGE:: Building vtailOml MESSAGE:: Building fuseOml Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wingSkin, index = 1 Name = fuseSkin, index = 2 Name = htailSkin, index = 3 Name = vtailSkin, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 5622 Number of elements = 11240 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 11240 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 5460 Number of elements = 10916 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 10916 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 5144 Number of elements = 10284 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 10284 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2722 Number of elements = 5440 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 5440 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 18948 Combined Number of elements = 37880 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 37880 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 3 Material name - fuseium No "materialType" specified for Material tuple fuseium, defaulting to "Isotropic" Material name - tailium No "materialType" specified for Material tuple tailium, defaulting to "Isotropic" Material name - wingium No "materialType" specified for Material tuple wingium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 4 Property name - fuseSkin Property name - htailSkin Property name - vtailSkin Property name - wingSkin Done getting FEA properties Updating mesh element types based on properties input ==> Computed mass properties... --> aircraft_skin = {'mass': , 'CG': , 'massInertia': } ==> Creating AVL aim... ==> Outputs Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing, index = 1 Name = Htail, index = 2 Name = Vtail, index = 3 Getting vortex lattice surface data VLM surface name - Htail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vtail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Htail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - Vtail (ID = 1) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - Wing (ID = 2) Section 1 of 5 (ID = 0) Section 2 of 5 (ID = 4) Section 3 of 5 (ID = 1) Section 4 of 5 (ID = 3) Section 5 of 5 (ID = 2) Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO --> Xcg = 80.2256 meter --> Xnp = 92.49086428236849 meter --> StaticMargin = 1.853959634679339 --> EigenValues {'case 1': [[-0.67265764, 0.0], [0.12206744, 0.57566409], [0.12206744, -0.57566409], [-0.15647634, 1.0546663], [-0.15647634, -1.0546663], [-0.0068085373, 0.0], [-0.00033021093, 0.049308946], [-0.00033021093, -0.049308946]]} --> Real Eigen Values = [-0.67265764, 0.12206744, 0.12206744, -0.15647634, -0.15647634, -0.0068085373, -0.00033021093, -0.00033021093] real 0m6.118s user 0m5.569s sys 0m5.931s + status=0 + set +x ================================================= solutions/session06/avl_masstran_MultiMat.py passed (as expected) ================================================= ================================================= masstran_MultiAIM.py test; + python masstran_MultiAIM.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../../data/ESP/transport.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading masstran aims... ==> Computing mass properties... MESSAGE:: Building wingOml MESSAGE:: Building htailOml MESSAGE:: Building vtailOml MESSAGE:: Building fuseOml Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = fuseSkin, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 7445 Number of elements = 14886 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 14886 Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - fuseium No "materialType" specified for Material tuple fuseium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - fuseSkin 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 = 1 Name = wingSkin, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 5622 Number of elements = 11240 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 11240 Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - wingium No "materialType" specified for Material tuple wingium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wingSkin 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 = htailSkin, index = 1 Name = vtailSkin, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 3488 Number of elements = 6972 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 6972 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 3480 Number of elements = 6956 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 6956 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6968 Combined Number of elements = 13928 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 13928 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - tailium No "materialType" specified for Material tuple tailium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - htailSkin Property name - vtailSkin Done getting FEA properties Updating mesh element types based on properties input ==> Computed mass properties... --> fuse_skin = {'mass': , 'CG': , 'massInertia': } --> wing_skin = {'mass': , 'CG': , 'massInertia': } --> tail_skin = {'mass': , 'CG': , 'massInertia': } real 0m2.775s user 0m2.509s sys 0m0.880s + status=0 + set +x ================================================= solutions/session06/masstran_MultiAIM.py passed (as expected) ================================================= ================================================= masstran_MultiMat.py test; + python masstran_MultiMat.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../../data/ESP/transport.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading masstran aim... ==> Computing mass properties... MESSAGE:: Building wingOml MESSAGE:: Building htailOml MESSAGE:: Building vtailOml MESSAGE:: Building fuseOml Mapping Csys attributes ................ Number of unique Csys attributes = 0 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 = 4 Name = wingSkin, index = 1 Name = fuseSkin, index = 2 Name = htailSkin, index = 3 Name = vtailSkin, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 5622 Number of elements = 11240 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 11240 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 5460 Number of elements = 10916 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 10916 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 5144 Number of elements = 10284 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 10284 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 2722 Number of elements = 5440 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 5440 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 18948 Combined Number of elements = 37880 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 37880 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 3 Material name - fuseium No "materialType" specified for Material tuple fuseium, defaulting to "Isotropic" Material name - tailium No "materialType" specified for Material tuple tailium, defaulting to "Isotropic" Material name - wingium No "materialType" specified for Material tuple wingium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 4 Property name - fuseSkin Property name - htailSkin Property name - vtailSkin Property name - wingSkin Done getting FEA properties Updating mesh element types based on properties input ==> Computed mass properties... --> aircraft_skin = {'mass': , 'CG': , 'massInertia': } real 0m2.249s user 0m2.664s sys 0m0.437s + status=0 + set +x ================================================= solutions/session06/masstran_MultiMat.py passed (as expected) ================================================= ================================================= 01_aflr4_InviscidWing.py test; + python 01_aflr4_InviscidWing.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 6 EGADS : 2 Yes 0 0 1 0 1 1 4 5 EGADS : 3 Yes 0 0 1 0 1 1 4 8 EGADS : 4 Yes 0 0 1 0 1 2 3 5 EGADS : 5 Yes 0 0 1 0 1 2 4 EGADS : 6 Yes 0 0 1 0 1 1 7 8 EGADS : 7 Yes 0 0 1 0 1 6 9 10 EGADS : 8 Yes 0 0 1 0 1 3 6 9 EGADS : 9 Yes 0 0 1 0 1 7 8 10 EGADS : 10 Yes 0 0 1 0 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 428.342 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 8732 16959 0 AFLR4 : Nodes, Trias,Quads= 5233 9961 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 18087 35388 0 AFLR4 : Nodes, Trias,Quads= 5569 10352 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 10182 19859 0 AFLR4 : Nodes, Trias,Quads= 4951 9397 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 16336 31887 0 AFLR4 : Nodes, Trias,Quads= 5435 10085 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 55 71 0 AFLR4 : Nodes, Trias,Quads= 45 51 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 8705 16905 0 AFLR4 : Nodes, Trias,Quads= 5312 10119 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 17908 35030 0 AFLR4 : Nodes, Trias,Quads= 5567 10348 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 8823 17141 0 AFLR4 : Nodes, Trias,Quads= 4980 9455 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 16876 32967 0 AFLR4 : Nodes, Trias,Quads= 5357 9929 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 55 71 0 AFLR4 : Nodes, Trias,Quads= 46 53 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 113 188 0 AFLR4 : Nodes, Trias,Quads= 109 180 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 112 186 0 AFLR4 : Nodes, Trias,Quads= 108 178 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 112 186 0 AFLR4 : Nodes, Trias,Quads= 108 178 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 113 188 0 AFLR4 : Nodes, Trias,Quads= 109 180 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 112 186 0 AFLR4 : Nodes, Trias,Quads= 108 178 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 113 188 0 AFLR4 : Nodes, Trias,Quads= 109 180 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 40416 80824 5436 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 40416 80824 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 8498 16494 0 AFLR4 : Nodes, Trias,Quads= 6521 12540 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 14215 27654 0 AFLR4 : Nodes, Trias,Quads= 10037 19298 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 8900 17298 0 AFLR4 : Nodes, Trias,Quads= 6655 12808 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 13476 26178 0 AFLR4 : Nodes, Trias,Quads= 9810 18846 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 59 77 0 AFLR4 : Nodes, Trias,Quads= 49 57 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 8503 16504 0 AFLR4 : Nodes, Trias,Quads= 6543 12584 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 13624 26478 0 AFLR4 : Nodes, Trias,Quads= 9963 19156 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 8761 17020 0 AFLR4 : Nodes, Trias,Quads= 6664 12826 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 13534 26300 0 AFLR4 : Nodes, Trias,Quads= 9965 19162 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 60 79 0 AFLR4 : Nodes, Trias,Quads= 49 57 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 113 188 0 AFLR4 : Nodes, Trias,Quads= 109 180 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 112 186 0 AFLR4 : Nodes, Trias,Quads= 107 176 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 113 188 0 AFLR4 : Nodes, Trias,Quads= 108 178 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 112 186 0 AFLR4 : Nodes, Trias,Quads= 109 180 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 111 184 0 AFLR4 : Nodes, Trias,Quads= 107 176 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 113 188 0 AFLR4 : Nodes, Trias,Quads= 109 180 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 64206 128404 5374 OVERALL : CPU Time = 1.234 seconds Body 1 (of 2) Number of nodes = 63669 Number of elements = 127334 Number of triangle elements = 127334 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 537 Number of elements = 1070 Number of triangle elements = 1070 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 64206 Total number of elements = 128404 Total number of triangle elements = 128404 Total number of quadrilateral elements = 0 real 0m2.732s user 0m2.558s sys 0m0.465s + status=0 + set +x ================================================= data/session07/01_aflr4_InviscidWing.py passed (as expected) ================================================= ================================================= 02_aflr4_Farfield.py test; + python 02_aflr4_Farfield.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 6 EGADS : 2 Yes 0 0 1 0 1 1 4 5 EGADS : 3 Yes 0 0 1 0 1 1 4 8 EGADS : 4 Yes 0 0 1 0 1 2 3 5 EGADS : 5 Yes 0 0 1 0 1 2 4 EGADS : 6 Yes 0 0 1 0 1 1 7 8 EGADS : 7 Yes 0 0 1 0 1 6 9 10 EGADS : 8 Yes 0 0 1 0 1 3 6 9 EGADS : 9 Yes 0 0 1 0 1 7 8 10 EGADS : 10 Yes 0 0 1 0 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 530.302 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 8732 16959 0 AFLR4 : Nodes, Trias,Quads= 5233 9961 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 18087 35388 0 AFLR4 : Nodes, Trias,Quads= 5569 10352 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 10182 19859 0 AFLR4 : Nodes, Trias,Quads= 4951 9397 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 16336 31887 0 AFLR4 : Nodes, Trias,Quads= 5435 10085 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 55 71 0 AFLR4 : Nodes, Trias,Quads= 45 51 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 8705 16905 0 AFLR4 : Nodes, Trias,Quads= 5312 10119 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 17908 35030 0 AFLR4 : Nodes, Trias,Quads= 5567 10348 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 8823 17141 0 AFLR4 : Nodes, Trias,Quads= 4980 9455 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 16876 32967 0 AFLR4 : Nodes, Trias,Quads= 5357 9929 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 55 71 0 AFLR4 : Nodes, Trias,Quads= 46 53 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 40197 80386 5388 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 40197 80386 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 8498 16494 0 AFLR4 : Nodes, Trias,Quads= 6521 12540 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 14215 27654 0 AFLR4 : Nodes, Trias,Quads= 10037 19298 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 8900 17298 0 AFLR4 : Nodes, Trias,Quads= 6655 12808 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 13476 26178 0 AFLR4 : Nodes, Trias,Quads= 9810 18846 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 59 77 0 AFLR4 : Nodes, Trias,Quads= 49 57 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 8503 16504 0 AFLR4 : Nodes, Trias,Quads= 6543 12584 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 13624 26478 0 AFLR4 : Nodes, Trias,Quads= 9963 19156 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 8761 17020 0 AFLR4 : Nodes, Trias,Quads= 6664 12826 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 13534 26300 0 AFLR4 : Nodes, Trias,Quads= 9965 19162 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 60 79 0 AFLR4 : Nodes, Trias,Quads= 49 57 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 63989 127970 5326 OVERALL : CPU Time = 1.234 seconds Body 1 (of 2) Number of nodes = 63669 Number of elements = 127334 Number of triangle elements = 127334 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 320 Number of elements = 636 Number of triangle elements = 636 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 63989 Total number of elements = 127970 Total number of triangle elements = 127970 Total number of quadrilateral elements = 0 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 6 EGADS : 2 Yes 0 0 1 0 1 1 4 5 EGADS : 3 Yes 0 0 1 0 1 1 4 8 EGADS : 4 Yes 0 0 1 0 1 2 3 5 EGADS : 5 Yes 0 0 1 0 1 2 4 EGADS : 6 Yes 0 0 1 0 1 1 7 8 EGADS : 7 Yes 0 0 1 0 1 6 9 10 EGADS : 8 Yes 0 0 1 0 1 3 6 9 EGADS : 9 Yes 0 0 1 0 1 7 8 10 EGADS : 10 Yes 0 0 1 0 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 168.806 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 8732 16959 0 AFLR4 : Nodes, Trias,Quads= 5233 9961 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 18087 35388 0 AFLR4 : Nodes, Trias,Quads= 5569 10352 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 10182 19859 0 AFLR4 : Nodes, Trias,Quads= 4951 9397 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 16336 31887 0 AFLR4 : Nodes, Trias,Quads= 5435 10085 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 55 71 0 AFLR4 : Nodes, Trias,Quads= 45 51 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 8705 16905 0 AFLR4 : Nodes, Trias,Quads= 5312 10119 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 17908 35030 0 AFLR4 : Nodes, Trias,Quads= 5567 10348 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 8823 17141 0 AFLR4 : Nodes, Trias,Quads= 4980 9455 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 16876 32967 0 AFLR4 : Nodes, Trias,Quads= 5357 9929 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 55 71 0 AFLR4 : Nodes, Trias,Quads= 46 53 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 655 1216 0 AFLR4 : Nodes, Trias,Quads= 645 1196 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 657 1220 0 AFLR4 : Nodes, Trias,Quads= 644 1194 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 653 1212 0 AFLR4 : Nodes, Trias,Quads= 643 1192 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 655 1216 0 AFLR4 : Nodes, Trias,Quads= 644 1194 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 655 1216 0 AFLR4 : Nodes, Trias,Quads= 642 1190 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 653 1212 0 AFLR4 : Nodes, Trias,Quads= 646 1198 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 43461 86914 5772 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 43461 86914 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 8498 16494 0 AFLR4 : Nodes, Trias,Quads= 6521 12540 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 14215 27654 0 AFLR4 : Nodes, Trias,Quads= 10037 19298 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 8900 17298 0 AFLR4 : Nodes, Trias,Quads= 6655 12808 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 13476 26178 0 AFLR4 : Nodes, Trias,Quads= 9810 18846 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 59 77 0 AFLR4 : Nodes, Trias,Quads= 49 57 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 8503 16504 0 AFLR4 : Nodes, Trias,Quads= 6543 12584 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 13624 26478 0 AFLR4 : Nodes, Trias,Quads= 9963 19156 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 8761 17020 0 AFLR4 : Nodes, Trias,Quads= 6664 12826 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 13534 26300 0 AFLR4 : Nodes, Trias,Quads= 9965 19162 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 60 79 0 AFLR4 : Nodes, Trias,Quads= 49 57 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 671 1248 0 AFLR4 : Nodes, Trias,Quads= 647 1200 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 671 1248 0 AFLR4 : Nodes, Trias,Quads= 646 1198 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 672 1250 0 AFLR4 : Nodes, Trias,Quads= 642 1190 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 670 1246 0 AFLR4 : Nodes, Trias,Quads= 645 1196 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 672 1250 0 AFLR4 : Nodes, Trias,Quads= 644 1194 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 670 1246 0 AFLR4 : Nodes, Trias,Quads= 646 1198 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 67259 134510 5710 OVERALL : CPU Time = 1.277 seconds Body 1 (of 2) Number of nodes = 63669 Number of elements = 127334 Number of triangle elements = 127334 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 3590 Number of elements = 7176 Number of triangle elements = 7176 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 67259 Total number of elements = 134510 Total number of triangle elements = 134510 Total number of quadrilateral elements = 0 real 0m4.710s user 0m4.461s sys 0m0.509s + status=0 + set +x ================================================= data/session07/02_aflr4_Farfield.py passed (as expected) ================================================= ================================================= 03_aflr4_MeshLength.py test; + python 03_aflr4_MeshLength.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 6 EGADS : 2 Yes 0 0 1 0 1 1 4 5 EGADS : 3 Yes 0 0 1 0 1 1 4 8 EGADS : 4 Yes 0 0 1 0 1 2 3 5 EGADS : 5 Yes 0 0 1 0 1 2 4 EGADS : 6 Yes 0 0 1 0 1 1 7 8 EGADS : 7 Yes 0 0 1 0 1 6 9 10 EGADS : 8 Yes 0 0 1 0 1 3 6 9 EGADS : 9 Yes 0 0 1 0 1 7 8 10 EGADS : 10 Yes 0 0 1 0 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 530.379 AFLR4 : Abs Min Surf Spacing = 0.0217051 AFLR4 : Min Surf Spacing = 0.217051 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 3815 7343 0 AFLR4 : Nodes, Trias,Quads= 2646 5005 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 7199 13974 0 AFLR4 : Nodes, Trias,Quads= 2681 4938 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3862 7438 0 AFLR4 : Nodes, Trias,Quads= 2506 4726 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 6786 13148 0 AFLR4 : Nodes, Trias,Quads= 2612 4800 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 39 50 0 AFLR4 : Nodes, Trias,Quads= 26 24 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 3812 7337 0 AFLR4 : Nodes, Trias,Quads= 2636 4985 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 7156 13888 0 AFLR4 : Nodes, Trias,Quads= 2677 4930 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 3757 7228 0 AFLR4 : Nodes, Trias,Quads= 2510 4734 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 6920 13416 0 AFLR4 : Nodes, Trias,Quads= 2582 4740 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 39 50 0 AFLR4 : Nodes, Trias,Quads= 26 24 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 19775 39542 3046 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 19775 39542 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 3762 7238 0 AFLR4 : Nodes, Trias,Quads= 3236 6186 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 6248 12075 0 AFLR4 : Nodes, Trias,Quads= 4502 8583 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3744 7203 0 AFLR4 : Nodes, Trias,Quads= 3175 6065 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 6002 11583 0 AFLR4 : Nodes, Trias,Quads= 4327 8233 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 43 56 0 AFLR4 : Nodes, Trias,Quads= 29 28 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 3772 7258 0 AFLR4 : Nodes, Trias,Quads= 3224 6162 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 6181 11942 0 AFLR4 : Nodes, Trias,Quads= 4495 8570 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 3662 7039 0 AFLR4 : Nodes, Trias,Quads= 3196 6107 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 6208 11996 0 AFLR4 : Nodes, Trias,Quads= 4366 8312 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 43 56 0 AFLR4 : Nodes, Trias,Quads= 29 28 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 29459 58910 3032 OVERALL : CPU Time = 0.512 seconds Body 1 (of 2) Number of nodes = 29139 Number of elements = 58274 Number of triangle elements = 58274 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 320 Number of elements = 636 Number of triangle elements = 636 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 29459 Total number of elements = 58910 Total number of triangle elements = 58910 Total number of quadrilateral elements = 0 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 6 EGADS : 2 Yes 0 0 1 0 1 1 4 5 EGADS : 3 Yes 0 0 1 0 1 1 4 8 EGADS : 4 Yes 0 0 1 0 1 2 3 5 EGADS : 5 Yes 0 0 1 0 1 2 4 EGADS : 6 Yes 0 0 1 0 1 1 7 8 EGADS : 7 Yes 0 0 1 0 1 6 9 10 EGADS : 8 Yes 0 0 1 0 1 3 6 9 EGADS : 9 Yes 0 0 1 0 1 7 8 10 EGADS : 10 Yes 0 0 1 0 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 1591.14 AFLR4 : Abs Min Surf Spacing = 0.0217051 AFLR4 : Min Surf Spacing = 0.217051 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 3 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 890 1664 0 AFLR4 : Nodes, Trias,Quads= 575 1034 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1164 2167 0 AFLR4 : Nodes, Trias,Quads= 586 1011 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 884 1654 0 AFLR4 : Nodes, Trias,Quads= 539 964 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1120 2080 0 AFLR4 : Nodes, Trias,Quads= 569 978 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 17 20 0 AFLR4 : Nodes, Trias,Quads= 12 10 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 887 1658 0 AFLR4 : Nodes, Trias,Quads= 575 1034 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 1168 2175 0 AFLR4 : Nodes, Trias,Quads= 589 1017 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 880 1646 0 AFLR4 : Nodes, Trias,Quads= 535 956 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 1113 2066 0 AFLR4 : Nodes, Trias,Quads= 566 972 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 17 20 0 AFLR4 : Nodes, Trias,Quads= 12 10 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 4015 8022 1158 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 4015 8022 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 936 1754 0 AFLR4 : Nodes, Trias,Quads= 785 1452 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1193 2225 0 AFLR4 : Nodes, Trias,Quads= 985 1809 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 937 1757 0 AFLR4 : Nodes, Trias,Quads= 756 1395 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1171 2182 0 AFLR4 : Nodes, Trias,Quads= 949 1738 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 23 30 0 AFLR4 : Nodes, Trias,Quads= 14 12 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 884 1650 0 AFLR4 : Nodes, Trias,Quads= 775 1432 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 1186 2212 0 AFLR4 : Nodes, Trias,Quads= 970 1780 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 884 1651 0 AFLR4 : Nodes, Trias,Quads= 765 1413 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 1164 2169 0 AFLR4 : Nodes, Trias,Quads= 949 1739 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 24 32 0 AFLR4 : Nodes, Trias,Quads= 14 12 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 6413 12818 1170 OVERALL : CPU Time = 0.138 seconds Body 1 (of 2) Number of nodes = 6393 Number of elements = 12782 Number of triangle elements = 12782 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 6413 Total number of elements = 12818 Total number of triangle elements = 12818 Total number of quadrilateral elements = 0 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 6 EGADS : 2 Yes 0 0 1 0 1 1 4 5 EGADS : 3 Yes 0 0 1 0 1 1 4 8 EGADS : 4 Yes 0 0 1 0 1 2 3 5 EGADS : 5 Yes 0 0 1 0 1 2 4 EGADS : 6 Yes 0 0 1 0 1 1 7 8 EGADS : 7 Yes 0 0 1 0 1 6 9 10 EGADS : 8 Yes 0 0 1 0 1 3 6 9 EGADS : 9 Yes 0 0 1 0 1 7 8 10 EGADS : 10 Yes 0 0 1 0 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 4773.42 AFLR4 : Abs Min Surf Spacing = 0.0217051 AFLR4 : Min Surf Spacing = 0.217051 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 9 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 193 334 0 AFLR4 : Nodes, Trias,Quads= 166 280 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 259 452 0 AFLR4 : Nodes, Trias,Quads= 152 238 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 188 325 0 AFLR4 : Nodes, Trias,Quads= 150 249 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 245 424 0 AFLR4 : Nodes, Trias,Quads= 151 236 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 195 338 0 AFLR4 : Nodes, Trias,Quads= 166 280 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 258 450 0 AFLR4 : Nodes, Trias,Quads= 150 234 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 188 325 0 AFLR4 : Nodes, Trias,Quads= 151 251 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 244 422 0 AFLR4 : Nodes, Trias,Quads= 150 234 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1013 2018 486 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1013 2018 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 208 362 0 AFLR4 : Nodes, Trias,Quads= 203 352 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 242 420 0 AFLR4 : Nodes, Trias,Quads= 185 306 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 203 353 0 AFLR4 : Nodes, Trias,Quads= 190 327 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 243 422 0 AFLR4 : Nodes, Trias,Quads= 182 300 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 209 364 0 AFLR4 : Nodes, Trias,Quads= 200 346 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 246 427 0 AFLR4 : Nodes, Trias,Quads= 185 305 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 207 361 0 AFLR4 : Nodes, Trias,Quads= 195 337 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 248 431 0 AFLR4 : Nodes, Trias,Quads= 188 311 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1316 2624 512 OVERALL : CPU Time = 0.072 seconds Body 1 (of 2) Number of nodes = 1296 Number of elements = 2588 Number of triangle elements = 2588 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1316 Total number of elements = 2624 Total number of triangle elements = 2624 Total number of quadrilateral elements = 0 real 0m1.942s user 0m1.745s sys 0m0.495s + status=0 + set +x ================================================= data/session07/03_aflr4_MeshLength.py passed (as expected) ================================================= ================================================= 04_aflr4_EdgeWeight.py test; + python 04_aflr4_EdgeWeight.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - leftWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 6 EGADS : 2 Yes 0 0 1 1 1 1 4 5 EGADS : 3 Yes 0 0 1 1 1 1 4 8 EGADS : 4 Yes 0 0 1 1 1 2 3 5 EGADS : 5 Yes 0 0 1 1 1 2 4 EGADS : 6 Yes 0 0 1 0 1 1 7 8 EGADS : 7 Yes 0 0 1 0 1 6 9 10 EGADS : 8 Yes 0 0 1 0 1 3 6 9 EGADS : 9 Yes 0 0 1 0 1 7 8 10 EGADS : 10 Yes 0 0 1 0 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 2651.51 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 5 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1107 2082 0 AFLR4 : Nodes, Trias,Quads= 685 1238 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1473 2759 0 AFLR4 : Nodes, Trias,Quads= 721 1255 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 1116 2100 0 AFLR4 : Nodes, Trias,Quads= 671 1210 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1458 2729 0 AFLR4 : Nodes, Trias,Quads= 714 1241 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 20 24 0 AFLR4 : Nodes, Trias,Quads= 14 12 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1108 2084 0 AFLR4 : Nodes, Trias,Quads= 683 1234 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 1488 2789 0 AFLR4 : Nodes, Trias,Quads= 714 1241 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 1112 2092 0 AFLR4 : Nodes, Trias,Quads= 653 1174 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 1456 2725 0 AFLR4 : Nodes, Trias,Quads= 708 1229 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 20 24 0 AFLR4 : Nodes, Trias,Quads= 14 12 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 4933 9858 1312 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 4933 9858 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 12796 24695 0 AFLR4 : Nodes, Trias,Quads= 7764 14631 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 29251 57087 0 AFLR4 : Nodes, Trias,Quads= 12448 23481 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 12136 23411 0 AFLR4 : Nodes, Trias,Quads= 7447 14033 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 29424 57435 0 AFLR4 : Nodes, Trias,Quads= 12399 23385 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 196 293 0 AFLR4 : Nodes, Trias,Quads= 188 277 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 2367 4490 0 AFLR4 : Nodes, Trias,Quads= 1726 3208 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 1453 2723 0 AFLR4 : Nodes, Trias,Quads= 1179 2175 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 1738 3267 0 AFLR4 : Nodes, Trias,Quads= 1397 2585 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 1477 2770 0 AFLR4 : Nodes, Trias,Quads= 1147 2110 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 26 35 0 AFLR4 : Nodes, Trias,Quads= 15 13 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 42971 85934 5550 OVERALL : CPU Time = 0.605 seconds Body 1 (of 2) Number of nodes = 42951 Number of elements = 85898 Number of triangle elements = 85898 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 42971 Total number of elements = 85934 Total number of triangle elements = 85934 Total number of quadrilateral elements = 0 real 0m4.324s user 0m4.135s sys 0m0.460s + status=0 + set +x ================================================= data/session07/04_aflr4_EdgeWeight.py passed (as expected) ================================================= ================================================= 05_aflr4_ScaleFactor.py test; + python 05_aflr4_ScaleFactor.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - leftWing Mesh sizing name - riteWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 0.5 2 3 6 EGADS : 2 Yes 0 0 1 0 0.5 1 4 5 EGADS : 3 Yes 0 0 1 0 0.5 1 4 8 EGADS : 4 Yes 0 0 1 0 0.5 2 3 5 EGADS : 5 Yes 0 0 1 0 0.5 2 4 EGADS : 6 Yes 0 0 1 0 2 1 7 8 EGADS : 7 Yes 0 0 1 0 2 6 9 10 EGADS : 8 Yes 0 0 1 0 2 3 6 9 EGADS : 9 Yes 0 0 1 0 2 7 8 10 EGADS : 10 Yes 0 0 1 0 2 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 2651.51 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 5 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 2701 5174 0 AFLR4 : Nodes, Trias,Quads= 1493 2758 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 3758 7177 0 AFLR4 : Nodes, Trias,Quads= 1589 2839 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 2824 5420 0 AFLR4 : Nodes, Trias,Quads= 1415 2602 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 3766 7193 0 AFLR4 : Nodes, Trias,Quads= 1566 2793 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 32 40 0 AFLR4 : Nodes, Trias,Quads= 22 20 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 583 1067 0 AFLR4 : Nodes, Trias,Quads= 453 807 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 616 1125 0 AFLR4 : Nodes, Trias,Quads= 323 539 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 595 1091 0 AFLR4 : Nodes, Trias,Quads= 439 779 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 585 1063 0 AFLR4 : Nodes, Trias,Quads= 314 521 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 11 12 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 6842 13676 1584 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 6842 13676 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 2679 5130 0 AFLR4 : Nodes, Trias,Quads= 2106 3984 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 3434 6540 0 AFLR4 : Nodes, Trias,Quads= 2925 5522 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 2738 5248 0 AFLR4 : Nodes, Trias,Quads= 2089 3950 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 3474 6620 0 AFLR4 : Nodes, Trias,Quads= 2895 5462 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 34 44 0 AFLR4 : Nodes, Trias,Quads= 22 20 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 659 1212 0 AFLR4 : Nodes, Trias,Quads= 565 1024 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 636 1162 0 AFLR4 : Nodes, Trias,Quads= 481 852 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 640 1175 0 AFLR4 : Nodes, Trias,Quads= 542 979 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 608 1107 0 AFLR4 : Nodes, Trias,Quads= 462 815 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 11 12 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 11329 22650 1604 OVERALL : CPU Time = 0.212 seconds Body 1 (of 2) Number of nodes = 11309 Number of elements = 22614 Number of triangle elements = 22614 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 11329 Total number of elements = 22650 Total number of triangle elements = 22650 Total number of quadrilateral elements = 0 real 0m1.236s user 0m1.006s sys 0m0.464s + status=0 + set +x ================================================= data/session07/05_aflr4_ScaleFactor.py passed (as expected) ================================================= ================================================= 06_aflr4_Proximity.py test; + python 06_aflr4_Proximity.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml MESSAGE:: Building nacelleOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Nacelle, index = 1 Name = Wing, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Nacelle, index = 1 Name = leftWing, index = 2 Name = riteWing, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - Nacelle Mesh sizing name - leftWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 4 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 4 Faces EGADS : Body 0 has 8 Edges EGADS : Body 0 has 4 Loops EGADS : Body 0 has 4 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 4 Faces EGADS : Body 1 has 8 Edges EGADS : Body 1 has 4 Loops EGADS : Body 1 has 4 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 10 Faces EGADS : Body 2 has 18 Edges EGADS : Body 2 has 10 Loops EGADS : Body 2 has 10 Nodes EGADS : Body 3 is a SolidBody EGADS : Body 3 has 1 Shells EGADS : Body 3 has 6 Faces EGADS : Body 3 has 12 Edges EGADS : Body 3 has 6 Loops EGADS : Body 3 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 0.5 2 3 EGADS : 2 Yes 0 0 1 0 0.5 1 4 EGADS : 3 Yes 0 0 1 0 0.5 1 4 EGADS : 4 Yes 0 0 1 0 0.5 2 3 EGADS : 5 Yes 1 0 1 0 0.5 6 7 EGADS : 6 Yes 1 0 1 0 0.5 5 8 EGADS : 7 Yes 1 0 1 0 0.5 5 8 EGADS : 8 Yes 1 0 1 0 0.5 6 7 EGADS : 9 Yes 2 0 1 0 50 10 11 14 EGADS : 10 Yes 2 0 1 0 50 9 12 13 EGADS : 11 Yes 2 0 1 0 50 9 12 16 EGADS : 12 Yes 2 0 1 0 50 10 11 13 EGADS : 13 Yes 2 0 1 0 50 10 12 EGADS : 14 Yes 2 0 1 0 1 9 15 16 EGADS : 15 Yes 2 0 1 0 1 14 17 18 EGADS : 16 Yes 2 0 1 0 1 11 14 17 EGADS : 17 Yes 2 0 1 0 1 15 16 18 EGADS : 18 Yes 2 0 1 0 1 15 17 EGADS : 19 Yes 3 0 1 NA NA 21 22 23 24 EGADS : 20 Yes 3 0 1 NA NA 21 22 23 24 EGADS : 21 Yes 3 0 1 NA NA 19 20 23 24 EGADS : 22 Yes 3 0 1 NA NA 19 20 23 24 EGADS : 23 Yes 3 0 1 NA NA 19 20 21 22 EGADS : 24 Yes 3 0 1 NA NA 19 20 21 22 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 3 2 -4 EGADS : 2 -2 5 1 -6 EGADS : 3 7 4 -8 -3 EGADS : 4 8 6 -7 -5 EGADS : 5 9 12 -10 -11 EGADS : 6 10 14 -9 -13 EGADS : 7 -15 11 16 -12 EGADS : 8 -16 13 15 -14 EGADS : 9 -17 18 19 -20 EGADS : 10 -21 20 22 -23 EGADS : 11 -19 24 17 -25 EGADS : 12 -22 25 21 -26 EGADS : 13 23 26 EGADS : 14 27 29 -28 -18 EGADS : 15 30 32 -31 -29 EGADS : 16 28 33 -27 -24 EGADS : 17 31 34 -30 -33 EGADS : 18 -32 -34 EGADS : 19 35 36 -37 -38 EGADS : 20 -39 42 41 -40 EGADS : 21 43 39 -44 -35 EGADS : 22 -45 37 46 -41 EGADS : 23 38 45 -42 -43 EGADS : 24 -36 44 40 -46 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : 19 19 EGADS : 20 20 EGADS : 21 21 EGADS : 22 22 EGADS : 23 23 EGADS : 24 24 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 3 2 -4 EGADS : 2 Yes -2 5 1 -6 EGADS : 3 Yes 7 4 -8 -3 EGADS : 4 Yes 8 6 -7 -5 EGADS : 5 Yes 9 12 -10 -11 EGADS : 6 Yes 10 14 -9 -13 EGADS : 7 Yes -15 11 16 -12 EGADS : 8 Yes -16 13 15 -14 EGADS : 9 Yes -17 18 19 -20 EGADS : 10 Yes -21 20 22 -23 EGADS : 11 Yes -19 24 17 -25 EGADS : 12 Yes -22 25 21 -26 EGADS : 13 Yes 23 26 EGADS : 14 Yes 27 29 -28 -18 EGADS : 15 Yes 30 32 -31 -29 EGADS : 16 Yes 28 33 -27 -24 EGADS : 17 Yes 31 34 -30 -33 EGADS : 18 Yes -32 -34 EGADS : 19 Yes 35 36 -37 -38 EGADS : 20 Yes -39 42 41 -40 EGADS : 21 Yes 43 39 -44 -35 EGADS : 22 Yes -45 37 46 -41 EGADS : 23 Yes 38 45 -42 -43 EGADS : 24 Yes -36 44 40 -46 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 2 EGADS : 2 0 Yes 3 4 1 1 2 EGADS : 3 0 Yes 1 3 1 1 3 EGADS : 4 0 Yes 2 4 1 1 3 EGADS : 5 0 Yes 3 1 1 2 4 EGADS : 6 0 Yes 4 2 1 2 4 EGADS : 7 0 Yes 1 2 1 3 4 EGADS : 8 0 Yes 3 4 1 3 4 EGADS : 9 1 Yes 5 6 1 5 6 EGADS : 10 1 Yes 7 8 1 5 6 EGADS : 11 1 Yes 5 7 1 5 7 EGADS : 12 1 Yes 6 8 1 5 7 EGADS : 13 1 Yes 7 5 1 6 8 EGADS : 14 1 Yes 8 6 1 6 8 EGADS : 15 1 Yes 5 6 1 7 8 EGADS : 16 1 Yes 7 8 1 7 8 EGADS : 17 2 Yes 9 10 1 9 11 EGADS : 18 2 Yes 9 11 1 9 14 EGADS : 19 2 Yes 11 12 1 9 11 EGADS : 20 2 Yes 10 12 1 9 10 EGADS : 21 2 Yes 10 13 1 10 12 EGADS : 22 2 Yes 12 14 1 10 12 EGADS : 23 2 Yes 13 14 1 10 13 EGADS : 24 2 Yes 11 9 1 11 16 EGADS : 25 2 Yes 12 10 1 11 12 EGADS : 26 2 Yes 14 13 1 12 13 EGADS : 27 2 Yes 9 15 1 14 16 EGADS : 28 2 Yes 11 16 1 14 16 EGADS : 29 2 Yes 15 16 1 14 15 EGADS : 30 2 Yes 15 17 1 15 17 EGADS : 31 2 Yes 16 18 1 15 17 EGADS : 32 2 Yes 17 18 1 15 18 EGADS : 33 2 Yes 16 15 1 16 17 EGADS : 34 2 Yes 18 17 1 17 18 EGADS : 35 3 Yes 20 19 NA 19 21 EGADS : 36 3 Yes 19 21 NA 19 24 EGADS : 37 3 Yes 22 21 NA 19 22 EGADS : 38 3 Yes 20 22 NA 19 23 EGADS : 39 3 Yes 24 23 NA 20 21 EGADS : 40 3 Yes 23 25 NA 20 24 EGADS : 41 3 Yes 26 25 NA 20 22 EGADS : 42 3 Yes 24 26 NA 20 23 EGADS : 43 3 Yes 20 24 NA 21 23 EGADS : 44 3 Yes 19 23 NA 21 24 EGADS : 45 3 Yes 22 26 NA 22 23 EGADS : 46 3 Yes 21 25 NA 22 24 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 90.5173952 0 0 EGADS : 2 Yes 90.5173952 0 0 EGADS : 3 Yes 60.5173952 0 0 EGADS : 4 Yes 60.5173952 0 0 EGADS : 5 Yes 90.5173952 29.3018771 0 EGADS : 6 Yes 90.5173952 29.3018771 0 EGADS : 7 Yes 60.5173952 29.3018771 0 EGADS : 8 Yes 60.5173952 29.3018771 0 EGADS : 9 Yes 97.2007855 0 0 EGADS : 10 Yes 97.9335611 0 0 EGADS : 11 Yes 50 0 0 EGADS : 12 Yes 75.3047874 0 0 EGADS : 13 Yes 123.552357 0 4.7180639 EGADS : 14 Yes 118.391317 0 3.99272703 EGADS : 15 Yes 97.9335611 36.1389817 0 EGADS : 16 Yes 75.3047874 36.1389817 0 EGADS : 17 Yes 123.552357 97.6729236 4.7180639 EGADS : 18 Yes 118.391317 97.6729236 3.99272703 EGADS : 19 Yes 0 0 1947.05079 EGADS : 20 Yes 0 0 0 EGADS : 21 Yes 0 1953.45847 1947.05079 EGADS : 22 Yes 0 1953.45847 0 EGADS : 23 Yes 2040.21562 0 1947.05079 EGADS : 24 Yes 2040.21562 0 0 EGADS : 25 Yes 2040.21562 1953.45847 1947.05079 EGADS : 26 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 22.2515 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 530.302 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : 15 CAD geometry 0 STD w/BL AFLR4 : 16 CAD geometry 0 STD w/BL AFLR4 : 17 CAD geometry 0 STD w/BL AFLR4 : 18 CAD geometry 0 STD w/BL AFLR4 : 19 CAD geometry 0 FARFIELD AFLR4 : 20 CAD geometry 0 FARFIELD AFLR4 : 21 CAD geometry 0 FARFIELD AFLR4 : 22 CAD geometry 0 FARFIELD AFLR4 : 23 CAD geometry 0 FARFIELD AFLR4 : 24 CAD geometry 0 FARFIELD AFLR4 : Case has 2 Proximity Checking Components AFLR4 : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18 AFLR4 : Component 2 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR4 : Define CAD surface definition 19 AFLR4 : Define CAD surface definition 20 AFLR4 : Define CAD surface definition 21 AFLR4 : Define CAD surface definition 22 AFLR4 : Define CAD surface definition 23 AFLR4 : Define CAD surface definition 24 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 13740 26927 0 AFLR4 : Nodes, Trias,Quads= 13723 26893 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 18558 36477 0 AFLR4 : Nodes, Trias,Quads= 16589 32539 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 13776 26999 0 AFLR4 : Nodes, Trias,Quads= 13736 26919 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 18524 36409 0 AFLR4 : Nodes, Trias,Quads= 16538 32437 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 13776 26999 0 AFLR4 : Nodes, Trias,Quads= 13736 26919 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 18524 36409 0 AFLR4 : Nodes, Trias,Quads= 16538 32437 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 13740 26927 0 AFLR4 : Nodes, Trias,Quads= 13723 26893 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 18558 36477 0 AFLR4 : Nodes, Trias,Quads= 16589 32539 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 502 907 0 AFLR4 : Nodes, Trias,Quads= 423 749 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 85 133 0 AFLR4 : Nodes, Trias,Quads= 56 75 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 502 907 0 AFLR4 : Nodes, Trias,Quads= 399 701 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 84 131 0 AFLR4 : Nodes, Trias,Quads= 55 73 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 8705 16905 0 AFLR4 : Nodes, Trias,Quads= 5312 10119 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 17908 35030 0 AFLR4 : Nodes, Trias,Quads= 5567 10348 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 8823 17141 0 AFLR4 : Nodes, Trias,Quads= 4980 9455 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 16876 32967 0 AFLR4 : Nodes, Trias,Quads= 5357 9929 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 55 71 0 AFLR4 : Nodes, Trias,Quads= 46 53 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 139862 279716 7794 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 139862 279716 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 13776 26996 0 AFLR4 : Nodes, Trias,Quads= 13887 27218 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 18675 36709 0 AFLR4 : Nodes, Trias,Quads= 16689 32737 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 13883 27210 0 AFLR4 : Nodes, Trias,Quads= 13963 27370 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 18667 36693 0 AFLR4 : Nodes, Trias,Quads= 16618 32595 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 13883 27210 0 AFLR4 : Nodes, Trias,Quads= 13963 27370 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 18667 36693 0 AFLR4 : Nodes, Trias,Quads= 16618 32595 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 13776 26996 0 AFLR4 : Nodes, Trias,Quads= 13887 27218 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 18675 36709 0 AFLR4 : Nodes, Trias,Quads= 16689 32737 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 525 950 0 AFLR4 : Nodes, Trias,Quads= 470 840 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 91 144 0 AFLR4 : Nodes, Trias,Quads= 59 80 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 538 976 0 AFLR4 : Nodes, Trias,Quads= 443 786 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 90 142 0 AFLR4 : Nodes, Trias,Quads= 58 78 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 8695 16888 0 AFLR4 : Nodes, Trias,Quads= 6539 12576 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 13624 26478 0 AFLR4 : Nodes, Trias,Quads= 9963 19156 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 8700 16899 0 AFLR4 : Nodes, Trias,Quads= 6656 12811 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 13534 26300 0 AFLR4 : Nodes, Trias,Quads= 9965 19162 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 60 79 0 AFLR4 : Nodes, Trias,Quads= 49 57 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 153016 306024 7784 AFLR4 : Proximity BG Surface Grid Generation AFLR4 : Nodes, Trias = 153404 306800 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 13935 27308 0 AFLR4 : Nodes, Trias,Quads= 13791 27020 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 18710 36774 0 AFLR4 : Nodes, Trias,Quads= 16564 32482 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 13945 27328 0 AFLR4 : Nodes, Trias,Quads= 13842 27122 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 18677 36708 0 AFLR4 : Nodes, Trias,Quads= 16540 32434 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 13945 27328 0 AFLR4 : Nodes, Trias,Quads= 13842 27122 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 18677 36708 0 AFLR4 : Nodes, Trias,Quads= 16540 32434 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 13935 27308 0 AFLR4 : Nodes, Trias,Quads= 13791 27020 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 18710 36774 0 AFLR4 : Nodes, Trias,Quads= 16564 32482 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 699 1265 0 AFLR4 : Nodes, Trias,Quads= 814 1495 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 103 166 0 AFLR4 : Nodes, Trias,Quads= 63 86 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 1127 2108 0 AFLR4 : Nodes, Trias,Quads= 1745 3344 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 146 239 0 AFLR4 : Nodes, Trias,Quads= 186 319 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 8840 17170 0 AFLR4 : Nodes, Trias,Quads= 7153 13796 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 15659 30521 0 AFLR4 : Nodes, Trias,Quads= 11063 21329 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 9010 17511 0 AFLR4 : Nodes, Trias,Quads= 7795 15081 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 15522 30248 0 AFLR4 : Nodes, Trias,Quads= 11035 21274 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 61 80 0 AFLR4 : Nodes, Trias,Quads= 50 58 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 157772 315536 7996 OVERALL : CPU Time = 4.885 seconds Body 1 (of 4) Number of nodes = 59529 Number of elements = 119058 Number of triangle elements = 119058 Number of quadrilateral elements = 0 Body 2 (of 4) Number of nodes = 59529 Number of elements = 119058 Number of triangle elements = 119058 Number of quadrilateral elements = 0 Body 3 (of 4) Number of nodes = 38394 Number of elements = 76784 Number of triangle elements = 76784 Number of quadrilateral elements = 0 Body 4 (of 4) Number of nodes = 320 Number of elements = 636 Number of triangle elements = 636 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 157772 Total number of elements = 315536 Total number of triangle elements = 315536 Total number of quadrilateral elements = 0 real 0m8.115s user 0m7.869s sys 0m0.521s + status=0 + set +x ================================================= data/session07/06_aflr4_Proximity.py passed (as expected) ================================================= ================================================= 07_aflr4_ProximityComponents.py test; + python 07_aflr4_ProximityComponents.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml MESSAGE:: Building pylonOml MESSAGE:: Building nacelleOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing, index = 1 Name = Pylon, index = 2 Name = Nacelle, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Pylon, index = 3 Name = Nacelle, index = 4 Name = Farfield, index = 5 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - Nacelle Mesh sizing name - Pylon Mesh sizing name - leftWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 22 Faces EGADS : Body 0 has 48 Edges EGADS : Body 0 has 24 Loops EGADS : Body 0 has 26 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 50 2 3 4 EGADS : 2 Yes 0 0 1 0 50 1 5 6 7 8 EGADS : 3 Yes 0 0 1 0 1 1 5 9 EGADS : 4 Yes 0 0 1 0 50 1 6 10 EGADS : 5 Yes 0 0 1 0 1 2 3 11 12 13 EGADS : 6 Yes 0 0 1 0 50 2 4 10 EGADS : 7 Yes 0 0 1 0 10 2 8 14 EGADS : 8 Yes 0 0 1 0 10 2 7 15 EGADS : 9 Yes 0 0 1 0 1 3 11 16 EGADS : 10 Yes 0 0 1 0 50 4 6 EGADS : 11 Yes 0 0 1 0 1 5 9 16 EGADS : 12 Yes 0 0 1 0 10 5 13 17 EGADS : 13 Yes 0 0 1 0 10 5 12 18 EGADS : 14 Yes 0 0 1 0 0.5 7 15 19 EGADS : 15 Yes 0 0 1 0 0.5 8 14 20 EGADS : 16 Yes 0 0 1 0 1 9 11 EGADS : 17 Yes 0 0 1 0 0.5 12 18 21 EGADS : 18 Yes 0 0 1 0 0.5 13 17 22 EGADS : 19 Yes 0 0 1 0 0.5 14 20 EGADS : 20 Yes 0 0 1 0 0.5 15 19 EGADS : 21 Yes 0 0 1 0 0.5 17 22 EGADS : 22 Yes 0 0 1 0 0.5 18 21 EGADS : 23 Yes 1 0 1 NA NA 25 26 27 28 EGADS : 24 Yes 1 0 1 NA NA 25 26 27 28 EGADS : 25 Yes 1 0 1 NA NA 23 24 27 28 EGADS : 26 Yes 1 0 1 NA NA 23 24 27 28 EGADS : 27 Yes 1 0 1 NA NA 23 24 25 26 EGADS : 28 Yes 1 0 1 NA NA 23 24 25 26 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -3 5 1 -6 7 8 EGADS : 3 9 11 -10 -2 EGADS : 4 -12 4 13 -14 EGADS : 5 10 15 -9 -5 16 17 EGADS : 6 -13 6 12 -18 EGADS : 7 19 20 -7 -21 EGADS : 8 21 -8 -20 -22 EGADS : 9 23 25 -24 -11 EGADS : 10 14 18 EGADS : 11 24 26 -23 -15 EGADS : 12 -27 29 -16 -28 EGADS : 13 -29 30 28 -17 EGADS : 14 31 -19 32 33 -34 -35 EGADS : 15 -31 37 34 -36 -32 22 EGADS : 16 -25 -26 EGADS : 17 38 27 39 40 -41 -42 EGADS : 18 -38 44 41 -43 -39 -30 EGADS : 19 -33 45 35 -46 EGADS : 20 36 46 -37 -45 EGADS : 21 -40 47 42 -48 EGADS : 22 43 48 -44 -47 EGADS : 23 49 50 -51 -52 EGADS : 24 -53 56 55 -54 EGADS : 25 57 53 -58 -49 EGADS : 26 -59 51 60 -55 EGADS : 27 52 59 -56 -57 EGADS : 28 -50 58 54 -60 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 3 EGADS : 3 4 EGADS : 4 5 EGADS : 5 6 7 EGADS : 6 8 EGADS : 7 9 EGADS : 8 10 EGADS : 9 11 EGADS : 10 12 EGADS : 11 13 EGADS : 12 14 EGADS : 13 15 EGADS : 14 16 EGADS : 15 17 EGADS : 16 18 EGADS : 17 19 EGADS : 18 20 EGADS : 19 21 EGADS : 20 22 EGADS : 21 23 EGADS : 22 24 EGADS : 23 25 EGADS : 24 26 EGADS : 25 27 EGADS : 26 28 EGADS : 27 29 EGADS : 28 30 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -3 5 1 -6 EGADS : 3 Yes 7 8 EGADS : 4 Yes 9 11 -10 -2 EGADS : 5 Yes -12 4 13 -14 EGADS : 6 Yes 10 15 -9 -5 EGADS : 7 Yes 16 17 EGADS : 8 Yes -13 6 12 -18 EGADS : 9 Yes 19 20 -7 -21 EGADS : 10 Yes 21 -8 -20 -22 EGADS : 11 Yes 23 25 -24 -11 EGADS : 12 Yes 14 18 EGADS : 13 Yes 24 26 -23 -15 EGADS : 14 Yes -27 29 -16 -28 EGADS : 15 Yes -29 30 28 -17 EGADS : 16 Yes 31 -19 32 33 -34 -35 EGADS : 17 Yes -31 37 34 -36 -32 22 EGADS : 18 Yes -25 -26 EGADS : 19 Yes 38 27 39 40 -41 -42 EGADS : 20 Yes -38 44 41 -43 -39 -30 EGADS : 21 Yes -33 45 35 -46 EGADS : 22 Yes 36 46 -37 -45 EGADS : 23 Yes -40 47 42 -48 EGADS : 24 Yes 43 48 -44 -47 EGADS : 25 Yes 49 50 -51 -52 EGADS : 26 Yes -53 56 55 -54 EGADS : 27 Yes 57 53 -58 -49 EGADS : 28 Yes -59 51 60 -55 EGADS : 29 Yes 52 59 -56 -57 EGADS : 30 Yes -50 58 54 -60 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 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 4 EGADS : 5 0 Yes 3 1 1 2 5 EGADS : 6 0 Yes 4 2 1 2 6 EGADS : 7 0 Yes 5 6 1 2 7 EGADS : 8 0 Yes 6 5 1 2 8 EGADS : 9 0 Yes 1 7 1 3 5 EGADS : 10 0 Yes 3 8 1 3 5 EGADS : 11 0 Yes 7 8 1 3 9 EGADS : 12 0 Yes 2 9 1 4 6 EGADS : 13 0 Yes 4 10 1 4 6 EGADS : 14 0 Yes 9 10 1 4 10 EGADS : 15 0 Yes 8 7 1 5 11 EGADS : 16 0 Yes 11 12 1 5 12 EGADS : 17 0 Yes 12 11 1 5 13 EGADS : 18 0 Yes 10 9 1 6 10 EGADS : 19 0 Yes 13 14 1 7 14 EGADS : 20 0 Yes 14 6 1 7 8 EGADS : 21 0 Yes 13 5 1 7 8 EGADS : 22 0 Yes 13 14 1 8 15 EGADS : 23 0 Yes 7 15 1 9 11 EGADS : 24 0 Yes 8 16 1 9 11 EGADS : 25 0 Yes 15 16 1 9 16 EGADS : 26 0 Yes 16 15 1 11 16 EGADS : 27 0 Yes 17 18 1 12 17 EGADS : 28 0 Yes 18 11 1 12 13 EGADS : 29 0 Yes 17 12 1 12 13 EGADS : 30 0 Yes 17 18 1 13 18 EGADS : 31 0 Yes 19 14 1 14 15 EGADS : 32 0 Yes 13 20 1 14 15 EGADS : 33 0 Yes 20 21 1 14 19 EGADS : 34 0 Yes 22 21 1 14 15 EGADS : 35 0 Yes 19 22 1 14 19 EGADS : 36 0 Yes 20 21 1 15 20 EGADS : 37 0 Yes 19 22 1 15 20 EGADS : 38 0 Yes 23 17 1 17 18 EGADS : 39 0 Yes 18 24 1 17 18 EGADS : 40 0 Yes 24 25 1 17 21 EGADS : 41 0 Yes 26 25 1 17 18 EGADS : 42 0 Yes 23 26 1 17 21 EGADS : 43 0 Yes 24 25 1 18 22 EGADS : 44 0 Yes 23 26 1 18 22 EGADS : 45 0 Yes 20 19 1 19 20 EGADS : 46 0 Yes 21 22 1 19 20 EGADS : 47 0 Yes 24 23 1 21 22 EGADS : 48 0 Yes 25 26 1 21 22 EGADS : 49 1 Yes 28 27 NA 23 25 EGADS : 50 1 Yes 27 29 NA 23 28 EGADS : 51 1 Yes 30 29 NA 23 26 EGADS : 52 1 Yes 28 30 NA 23 27 EGADS : 53 1 Yes 32 31 NA 24 25 EGADS : 54 1 Yes 31 33 NA 24 28 EGADS : 55 1 Yes 34 33 NA 24 26 EGADS : 56 1 Yes 32 34 NA 24 27 EGADS : 57 1 Yes 28 32 NA 25 27 EGADS : 58 1 Yes 27 31 NA 25 28 EGADS : 59 1 Yes 30 34 NA 26 27 EGADS : 60 1 Yes 29 33 NA 26 28 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 72.4759225 0 0 EGADS : 6 Yes 83.5054156 0 0 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 0 4.7180639 EGADS : 10 Yes 118.391317 0 3.99272703 EGADS : 11 Yes 72.4759225 29.3018771 0 EGADS : 12 Yes 83.5054156 29.3018771 0 EGADS : 13 Yes 70.524066 0 0 EGADS : 14 Yes 79.4370049 0 0 EGADS : 15 Yes 123.552357 97.6729236 4.7180639 EGADS : 16 Yes 118.391317 97.6729236 3.99272703 EGADS : 17 Yes 79.4370049 29.3018771 0 EGADS : 18 Yes 70.524066 29.3018771 0 EGADS : 19 Yes 90.5173952 0 0 EGADS : 20 Yes 60.5173952 0 0 EGADS : 21 Yes 60.5173952 0 0 EGADS : 22 Yes 90.5173952 0 0 EGADS : 23 Yes 90.5173952 29.3018771 0 EGADS : 24 Yes 60.5173952 29.3018771 0 EGADS : 25 Yes 60.5173952 29.3018771 0 EGADS : 26 Yes 90.5173952 29.3018771 0 EGADS : 27 Yes 0 0 1947.05079 EGADS : 28 Yes 0 0 0 EGADS : 29 Yes 0 1953.45847 1947.05079 EGADS : 30 Yes 0 1953.45847 0 EGADS : 31 Yes 2040.21562 0 1947.05079 EGADS : 32 Yes 2040.21562 0 0 EGADS : 33 Yes 2040.21562 1953.45847 1947.05079 EGADS : 34 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 22.2515 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 530.302 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : 15 CAD geometry 0 STD w/BL AFLR4 : 16 CAD geometry 0 STD w/BL AFLR4 : 17 CAD geometry 0 STD w/BL AFLR4 : 18 CAD geometry 0 STD w/BL AFLR4 : 19 CAD geometry 0 STD w/BL AFLR4 : 20 CAD geometry 0 STD w/BL AFLR4 : 21 CAD geometry 0 STD w/BL AFLR4 : 22 CAD geometry 0 STD w/BL AFLR4 : 23 CAD geometry 0 FARFIELD AFLR4 : 24 CAD geometry 0 FARFIELD AFLR4 : 25 CAD geometry 0 FARFIELD AFLR4 : 26 CAD geometry 0 FARFIELD AFLR4 : 27 CAD geometry 0 FARFIELD AFLR4 : 28 CAD geometry 0 FARFIELD AFLR4 : Case has 3 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 9 10 11 16 AFLR4 : Component 2 includes Definitions 14 15 17 18 19 20 21 22 AFLR4 : Component 3 includes Definitions 7 8 12 13 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR4 : Define CAD surface definition 19 AFLR4 : Define CAD surface definition 20 AFLR4 : Define CAD surface definition 21 AFLR4 : Define CAD surface definition 22 AFLR4 : Define CAD surface definition 23 AFLR4 : Define CAD surface definition 24 AFLR4 : Define CAD surface definition 25 AFLR4 : Define CAD surface definition 26 AFLR4 : Define CAD surface definition 27 AFLR4 : Define CAD surface definition 28 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 502 907 0 AFLR4 : Nodes, Trias,Quads= 423 749 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 769 1416 0 AFLR4 : Nodes, Trias,Quads= 579 1036 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 8705 16905 0 AFLR4 : Nodes, Trias,Quads= 5312 10119 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 85 133 0 AFLR4 : Nodes, Trias,Quads= 56 75 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 9412 18267 0 AFLR4 : Nodes, Trias,Quads= 5160 9763 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 84 131 0 AFLR4 : Nodes, Trias,Quads= 55 73 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 382 673 0 AFLR4 : Nodes, Trias,Quads= 221 351 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 377 662 0 AFLR4 : Nodes, Trias,Quads= 227 362 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17908 35030 0 AFLR4 : Nodes, Trias,Quads= 5567 10348 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 16876 32967 0 AFLR4 : Nodes, Trias,Quads= 5357 9929 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 536 964 0 AFLR4 : Nodes, Trias,Quads= 324 540 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 530 952 0 AFLR4 : Nodes, Trias,Quads= 325 542 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 14942 29305 0 AFLR4 : Nodes, Trias,Quads= 14513 28447 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 14940 29301 0 AFLR4 : Nodes, Trias,Quads= 14427 28275 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 55 71 0 AFLR4 : Nodes, Trias,Quads= 46 53 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 14942 29305 0 AFLR4 : Nodes, Trias,Quads= 14513 28447 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 14928 29277 0 AFLR4 : Nodes, Trias,Quads= 14400 28221 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 18558 36477 0 AFLR4 : Nodes, Trias,Quads= 16589 32539 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 18524 36409 0 AFLR4 : Nodes, Trias,Quads= 16538 32437 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 18558 36477 0 AFLR4 : Nodes, Trias,Quads= 16589 32539 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 18524 36409 0 AFLR4 : Nodes, Trias,Quads= 16538 32437 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 25 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 26 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 27 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 28 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 143960 287920 8370 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 143960 287920 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 552 1002 0 AFLR4 : Nodes, Trias,Quads= 474 846 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 803 1479 0 AFLR4 : Nodes, Trias,Quads= 727 1327 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 8664 16826 0 AFLR4 : Nodes, Trias,Quads= 6539 12576 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 94 149 0 AFLR4 : Nodes, Trias,Quads= 60 81 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 9289 18022 0 AFLR4 : Nodes, Trias,Quads= 6959 13362 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 92 145 0 AFLR4 : Nodes, Trias,Quads= 59 79 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 375 660 0 AFLR4 : Nodes, Trias,Quads= 275 460 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 386 681 0 AFLR4 : Nodes, Trias,Quads= 270 449 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 13624 26478 0 AFLR4 : Nodes, Trias,Quads= 9963 19156 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 13541 26314 0 AFLR4 : Nodes, Trias,Quads= 9963 19158 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 573 1036 0 AFLR4 : Nodes, Trias,Quads= 363 616 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 580 1049 0 AFLR4 : Nodes, Trias,Quads= 370 629 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 15123 29666 0 AFLR4 : Nodes, Trias,Quads= 14640 28700 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 15402 30224 0 AFLR4 : Nodes, Trias,Quads= 14606 28632 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 60 79 0 AFLR4 : Nodes, Trias,Quads= 49 57 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 15284 29986 0 AFLR4 : Nodes, Trias,Quads= 14698 28814 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 15598 30614 0 AFLR4 : Nodes, Trias,Quads= 14616 28650 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 18664 36687 0 AFLR4 : Nodes, Trias,Quads= 16684 32727 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 18711 36781 0 AFLR4 : Nodes, Trias,Quads= 16625 32609 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 18664 36687 0 AFLR4 : Nodes, Trias,Quads= 16684 32727 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 18712 36783 0 AFLR4 : Nodes, Trias,Quads= 16612 32583 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 25 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 26 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 27 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 28 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 157438 314876 8368 AFLR4 : Proximity BG Surface Grid Generation AFLR4 : Nodes, Trias = 159278 318556 AFLR4 : Nodes, Trias = 159698 319396 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1086 2020 0 AFLR4 : Nodes, Trias,Quads= 962 1772 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 2773 5270 0 AFLR4 : Nodes, Trias,Quads= 2793 5310 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 8880 17250 0 AFLR4 : Nodes, Trias,Quads= 7147 13784 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 184 310 0 AFLR4 : Nodes, Trias,Quads= 138 218 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 16222 31763 0 AFLR4 : Nodes, Trias,Quads= 9485 18289 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 232 397 0 AFLR4 : Nodes, Trias,Quads= 221 375 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 1413 2643 0 AFLR4 : Nodes, Trias,Quads= 911 1639 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 1587 2978 0 AFLR4 : Nodes, Trias,Quads= 1002 1808 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 15659 30521 0 AFLR4 : Nodes, Trias,Quads= 11061 21325 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 15529 30262 0 AFLR4 : Nodes, Trias,Quads= 11050 21304 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 2345 4452 0 AFLR4 : Nodes, Trias,Quads= 1526 2814 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 2241 4252 0 AFLR4 : Nodes, Trias,Quads= 1462 2694 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 17583 34542 0 AFLR4 : Nodes, Trias,Quads= 14782 28940 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 17575 34524 0 AFLR4 : Nodes, Trias,Quads= 14759 28892 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 61 80 0 AFLR4 : Nodes, Trias,Quads= 50 58 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 19924 39212 0 AFLR4 : Nodes, Trias,Quads= 14954 29272 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 18844 37054 0 AFLR4 : Nodes, Trias,Quads= 14853 29072 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 18691 36736 0 AFLR4 : Nodes, Trias,Quads= 16527 32408 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 18718 36790 0 AFLR4 : Nodes, Trias,Quads= 16525 32404 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 18691 36736 0 AFLR4 : Nodes, Trias,Quads= 16527 32408 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 18709 36772 0 AFLR4 : Nodes, Trias,Quads= 16535 32424 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 25 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 26 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 27 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 28 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 168924 337848 9464 OVERALL : CPU Time = 6.607 seconds Body 1 (of 2) Number of nodes = 168604 Number of elements = 337212 Number of triangle elements = 337212 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 320 Number of elements = 636 Number of triangle elements = 636 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 168924 Total number of elements = 337848 Total number of triangle elements = 337848 Total number of quadrilateral elements = 0 real 0m12.697s user 0m14.672s sys 0m2.180s + status=0 + set +x ================================================= data/session07/07_aflr4_ProximityComponents.py passed (as expected) ================================================= ================================================= 08_aflr4_InviscidTransport.py test; + python 08_aflr4_InviscidTransport.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml MESSAGE:: Building wingHinges MESSAGE:: Building nacelleOml MESSAGE:: Building htailOml MESSAGE:: Building htailHinges MESSAGE:: Building vtailOml MESSAGE:: Building vtailHinges MESSAGE:: Building fuseOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Nacelle, index = 1 Name = Vtail, index = 2 Name = Htail, index = 3 Name = Fuselage, index = 4 Name = Wing, index = 5 Name = Farfield, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 7 Name = Nacelle, index = 1 Name = Vtail, index = 2 Name = Htail, index = 3 Name = Fuselage, index = 4 Name = riteWing, index = 5 Name = leftWing, index = 6 Name = Farfield, index = 7 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - Htail Mesh sizing name - Nacelle Mesh sizing name - Vtail Mesh sizing name - leftWing Mesh sizing name - riteWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 4 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 4 Faces EGADS : Body 0 has 8 Edges EGADS : Body 0 has 4 Loops EGADS : Body 0 has 4 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 4 Faces EGADS : Body 1 has 8 Edges EGADS : Body 1 has 4 Loops EGADS : Body 1 has 4 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 100 Faces EGADS : Body 2 has 245 Edges EGADS : Body 2 has 102 Loops EGADS : Body 2 has 145 Nodes EGADS : Body 3 is a SolidBody EGADS : Body 3 has 1 Shells EGADS : Body 3 has 6 Faces EGADS : Body 3 has 12 Edges EGADS : Body 3 has 6 Loops EGADS : Body 3 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 5 2 3 EGADS : 2 Yes 0 0 1 0 5 1 4 EGADS : 3 Yes 0 0 1 0 5 1 4 EGADS : 4 Yes 0 0 1 0 5 2 3 EGADS : 5 Yes 1 0 1 0 5 6 7 EGADS : 6 Yes 1 0 1 0 5 5 8 EGADS : 7 Yes 1 0 1 0 5 5 8 EGADS : 8 Yes 1 0 1 0 5 6 7 EGADS : 9 Yes 2 0 1 0 4 10 14 32 107 EGADS : 10 Yes 2 0 1 0 4 9 11 39 108 EGADS : 11 Yes 2 0 1 0 4 10 12 39 108 EGADS : 12 Yes 2 0 1 0 4 11 13 39 108 EGADS : 13 Yes 2 0 1 0 4 12 14 32 107 EGADS : 14 Yes 2 0 1 0 4 9 13 32 107 EGADS : 15 Yes 2 0 1 0 4 16 17 18 19 EGADS : 16 Yes 2 0 1 0 4 15 17 20 21 22 EGADS : 23 24 EGADS : 17 Yes 2 0 1 0 4 15 16 18 22 EGADS : 18 Yes 2 0 1 0 4 15 17 22 25 EGADS : 19 Yes 2 0 1 0 4 15 20 25 26 EGADS : 20 Yes 2 0 1 0 4 16 19 21 23 24 EGADS : 26 27 EGADS : 21 Yes 2 0 1 0 4 16 20 EGADS : 22 Yes 2 0 1 0 4 16 17 18 27 EGADS : 23 Yes 2 0 1 0 1 16 20 24 28 29 EGADS : 30 EGADS : 24 Yes 2 0 1 0 1 16 20 23 29 31 EGADS : 32 33 EGADS : 25 Yes 2 0 1 0 4 18 19 26 27 EGADS : 26 Yes 2 0 1 0 4 19 20 25 27 EGADS : 27 Yes 2 0 1 0 4 20 22 25 26 EGADS : 28 Yes 2 0 1 0 1 23 29 31 34 35 EGADS : 36 EGADS : 29 Yes 2 0 1 0 1 23 24 28 31 EGADS : 30 Yes 2 0 1 0 1 23 33 36 37 38 EGADS : 31 Yes 2 0 1 0 1 24 28 29 34 35 EGADS : 39 40 EGADS : 32 Yes 2 0 1 0 4 9 13 14 24 39 41 EGADS : 33 Yes 2 0 1 0 1 24 30 40 EGADS : 34 Yes 2 0 1 0 4 28 31 35 42 43 EGADS : 44 45 EGADS : 35 Yes 2 0 1 0 4 28 31 34 42 46 EGADS : 47 48 EGADS : 36 Yes 2 0 1 0 1 28 30 40 49 50 EGADS : 37 Yes 2 0 1 0 4 30 38 51 52 53 EGADS : 54 EGADS : 38 Yes 2 0 1 0 4 30 37 55 56 57 EGADS : 58 EGADS : 39 Yes 2 0 1 0 4 10 11 12 31 32 EGADS : 41 EGADS : 40 Yes 2 0 1 0 1 31 33 36 EGADS : 41 Yes 2 0 1 0 4 32 39 EGADS : 42 Yes 2 0 1 0 4 34 35 EGADS : 43 Yes 2 0 1 0 4 34 44 48 59 EGADS : 44 Yes 2 0 1 0 4 34 43 45 59 EGADS : 45 Yes 2 0 1 0 4 34 44 46 59 EGADS : 46 Yes 2 0 1 0 4 35 45 47 60 EGADS : 47 Yes 2 0 1 0 4 35 46 48 60 EGADS : 48 Yes 2 0 1 0 4 35 43 47 60 EGADS : 49 Yes 2 0 1 0 4 36 50 61 62 63 EGADS : 64 EGADS : 50 Yes 2 0 1 0 4 36 49 65 66 67 EGADS : 68 EGADS : 51 Yes 2 0 1 0 4 37 52 58 69 EGADS : 52 Yes 2 0 1 0 4 37 51 53 69 EGADS : 53 Yes 2 0 1 0 4 37 52 56 69 EGADS : 54 Yes 2 0 1 0 4 37 55 70 71 72 EGADS : 73 74 75 76 EGADS : 55 Yes 2 0 1 0 4 38 54 76 77 78 EGADS : 79 80 81 82 EGADS : 56 Yes 2 0 1 0 4 38 53 57 83 EGADS : 57 Yes 2 0 1 0 4 38 56 58 83 EGADS : 58 Yes 2 0 1 0 4 38 51 57 83 EGADS : 59 Yes 2 0 1 0 4 43 44 45 60 EGADS : 60 Yes 2 0 1 0 4 46 47 48 59 EGADS : 61 Yes 2 0 1 0 4 49 68 84 85 86 EGADS : 87 88 89 90 EGADS : 62 Yes 2 0 1 0 4 49 63 67 91 EGADS : 63 Yes 2 0 1 0 4 49 62 64 91 EGADS : 64 Yes 2 0 1 0 4 49 63 65 91 EGADS : 65 Yes 2 0 1 0 4 50 64 66 92 EGADS : 66 Yes 2 0 1 0 4 50 65 67 92 EGADS : 67 Yes 2 0 1 0 4 50 62 66 92 EGADS : 68 Yes 2 0 1 0 4 50 61 84 93 94 EGADS : 95 96 97 98 EGADS : 69 Yes 2 0 1 0 4 51 52 53 83 EGADS : 70 Yes 2 0 1 0 4 54 71 82 99 EGADS : 71 Yes 2 0 1 0 4 54 70 72 99 EGADS : 72 Yes 2 0 1 0 4 54 71 80 99 EGADS : 73 Yes 2 0 1 0 4 54 74 79 100 EGADS : 74 Yes 2 0 1 0 4 54 73 75 100 EGADS : 75 Yes 2 0 1 0 4 54 74 77 100 EGADS : 76 Yes 2 0 1 0 4 54 55 EGADS : 77 Yes 2 0 1 0 4 55 75 78 101 EGADS : 78 Yes 2 0 1 0 4 55 77 79 101 EGADS : 79 Yes 2 0 1 0 4 55 73 78 101 EGADS : 80 Yes 2 0 1 0 4 55 72 81 102 EGADS : 81 Yes 2 0 1 0 4 55 80 82 102 EGADS : 82 Yes 2 0 1 0 4 55 70 81 102 EGADS : 83 Yes 2 0 1 0 4 56 57 58 69 EGADS : 84 Yes 2 0 1 0 4 61 68 EGADS : 85 Yes 2 0 1 0 4 61 86 98 103 EGADS : 86 Yes 2 0 1 0 4 61 85 87 103 EGADS : 87 Yes 2 0 1 0 4 61 86 96 103 EGADS : 88 Yes 2 0 1 0 4 61 89 95 104 EGADS : 89 Yes 2 0 1 0 4 61 88 90 104 EGADS : 90 Yes 2 0 1 0 4 61 89 93 104 EGADS : 91 Yes 2 0 1 0 4 62 63 64 92 EGADS : 92 Yes 2 0 1 0 4 65 66 67 91 EGADS : 93 Yes 2 0 1 0 4 68 90 94 105 EGADS : 94 Yes 2 0 1 0 4 68 93 95 105 EGADS : 95 Yes 2 0 1 0 4 68 88 94 105 EGADS : 96 Yes 2 0 1 0 4 68 87 97 106 EGADS : 97 Yes 2 0 1 0 4 68 96 98 106 EGADS : 98 Yes 2 0 1 0 4 68 85 97 106 EGADS : 99 Yes 2 0 1 0 4 70 71 72 102 EGADS : 100 Yes 2 0 1 0 4 73 74 75 101 EGADS : 101 Yes 2 0 1 0 4 77 78 79 100 EGADS : 102 Yes 2 0 1 0 4 80 81 82 99 EGADS : 103 Yes 2 0 1 0 4 85 86 87 106 EGADS : 104 Yes 2 0 1 0 4 88 89 90 105 EGADS : 105 Yes 2 0 1 0 4 93 94 95 104 EGADS : 106 Yes 2 0 1 0 4 96 97 98 103 EGADS : 107 Yes 2 0 1 0 4 9 13 14 108 EGADS : 108 Yes 2 0 1 0 4 10 11 12 107 EGADS : 109 Yes 3 0 1 NA NA 111 112 113 114 EGADS : 110 Yes 3 0 1 NA NA 111 112 113 114 EGADS : 111 Yes 3 0 1 NA NA 109 110 113 114 EGADS : 112 Yes 3 0 1 NA NA 109 110 113 114 EGADS : 113 Yes 3 0 1 NA NA 109 110 111 112 EGADS : 114 Yes 3 0 1 NA NA 109 110 111 112 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 3 2 -4 EGADS : 2 -2 5 1 -6 EGADS : 3 7 4 -8 -3 EGADS : 4 8 6 -7 -5 EGADS : 5 9 12 -10 -11 EGADS : 6 10 14 -9 -13 EGADS : 7 -15 11 16 -12 EGADS : 8 -16 13 15 -14 EGADS : 9 -17 20 19 -18 EGADS : 10 -21 18 23 -22 EGADS : 11 -24 22 26 -25 EGADS : 12 27 25 -28 -29 EGADS : 13 30 29 -31 -32 EGADS : 14 33 32 -34 -20 EGADS : 15 35 36 -37 -38 EGADS : 16 39 40 -41 42 -43 -35 -44 45 46 EGADS : 17 43 47 -48 -36 EGADS : 18 -49 37 48 -50 EGADS : 19 51 38 -52 -53 EGADS : 20 44 -51 54 55 41 56 -39 57 58 EGADS : 21 -56 -40 EGADS : 22 -42 59 50 -47 EGADS : 23 -60 64 63 -45 -58 62 -61 EGADS : 24 -63 69 68 67 66 -65 -62 -57 -46 EGADS : 25 49 -70 -71 52 EGADS : 26 -54 53 71 -72 EGADS : 27 -55 72 70 -59 EGADS : 28 -73 78 60 -77 -76 75 74 EGADS : 29 61 65 79 77 EGADS : 30 -80 82 81 -64 -83 -84 EGADS : 31 -68 88 73 87 86 76 -79 -66 85 EGADS : 32 -89 -67 92 -91 -90 -30 -33 17 EGADS : 33 -81 93 94 -69 EGADS : 34 -95 -87 -74 101 100 99 -98 97 -96 EGADS : 35 -101 -75 -86 95 -105 -97 -104 -103 102 EGADS : 36 -106 107 80 -78 108 109 EGADS : 37 110 -111 112 113 114 115 -116 83 EGADS : 38 116 117 -114 118 -119 -120 -110 84 EGADS : 39 -92 -85 89 21 24 -27 90 -121 EGADS : 40 -94 122 106 -88 EGADS : 41 91 121 EGADS : 42 105 96 EGADS : 43 98 123 -124 -125 EGADS : 44 -99 127 126 -123 EGADS : 45 -100 129 128 -127 EGADS : 46 -102 131 130 -129 EGADS : 47 103 132 -133 -131 EGADS : 48 104 125 -134 -132 EGADS : 49 -135 -108 141 140 139 -138 137 -136 EGADS : 50 -141 -109 135 -145 -137 -144 -143 142 EGADS : 51 111 146 -147 -148 EGADS : 52 -112 148 150 -149 EGADS : 53 -113 149 152 -151 EGADS : 54 153 -154 155 156 157 -158 159 160 161 162 -163 -115 EGADS : 55 163 164 -161 165 -166 -167 -157 168 -169 -170 -153 -117 EGADS : 56 -118 151 172 -171 EGADS : 57 119 171 -173 -174 EGADS : 58 120 174 -175 -146 EGADS : 59 176 124 -126 -128 EGADS : 60 -176 -130 133 134 EGADS : 61 -177 136 187 186 185 -184 183 182 181 -180 179 -178 EGADS : 62 138 188 -189 -190 EGADS : 63 -139 192 191 -188 EGADS : 64 -140 194 193 -192 EGADS : 65 -142 196 195 -194 EGADS : 66 143 197 -198 -196 EGADS : 67 144 190 -199 -197 EGADS : 68 -187 145 177 -206 -179 -205 -204 203 -183 -202 -201 200 EGADS : 69 207 -152 -150 147 EGADS : 70 154 208 -209 -210 EGADS : 71 -155 210 212 -211 EGADS : 72 -156 211 214 -213 EGADS : 73 158 215 -216 -217 EGADS : 74 -159 217 219 -218 EGADS : 75 -160 218 221 -220 EGADS : 76 -162 -164 EGADS : 77 -165 220 223 -222 EGADS : 78 166 222 -224 -225 EGADS : 79 167 225 -226 -215 EGADS : 80 -168 213 228 -227 EGADS : 81 169 227 -229 -230 EGADS : 82 170 230 -231 -208 EGADS : 83 175 173 -172 -207 EGADS : 84 206 178 EGADS : 85 180 232 -233 -234 EGADS : 86 -181 236 235 -232 EGADS : 87 -182 238 237 -236 EGADS : 88 184 239 -240 -241 EGADS : 89 -185 243 242 -239 EGADS : 90 -186 245 244 -243 EGADS : 91 -193 246 189 -191 EGADS : 92 -246 -195 198 199 EGADS : 93 -200 248 247 -245 EGADS : 94 201 249 -250 -248 EGADS : 95 202 241 -251 -249 EGADS : 96 -203 253 252 -238 EGADS : 97 204 254 -255 -253 EGADS : 98 205 234 -256 -254 EGADS : 99 257 -214 -212 209 EGADS : 100 -221 -219 216 258 EGADS : 101 -258 226 224 -223 EGADS : 102 231 229 -228 -257 EGADS : 103 -237 259 233 -235 EGADS : 104 -244 260 240 -242 EGADS : 105 -260 -247 250 251 EGADS : 106 -259 -252 255 256 EGADS : 107 -261 -19 34 31 EGADS : 108 -23 261 28 -26 EGADS : 109 262 263 -264 -265 EGADS : 110 -266 269 268 -267 EGADS : 111 270 266 -271 -262 EGADS : 112 -272 264 273 -268 EGADS : 113 265 272 -269 -270 EGADS : 114 -263 271 267 -273 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : 19 19 EGADS : 20 20 EGADS : 21 21 EGADS : 22 22 EGADS : 23 23 EGADS : 24 24 EGADS : 25 25 EGADS : 26 26 EGADS : 27 27 EGADS : 28 28 EGADS : 29 29 EGADS : 30 30 31 EGADS : 31 32 EGADS : 32 33 EGADS : 33 34 EGADS : 34 35 EGADS : 35 36 EGADS : 36 37 38 EGADS : 37 39 EGADS : 38 40 EGADS : 39 41 EGADS : 40 42 EGADS : 41 43 EGADS : 42 44 EGADS : 43 45 EGADS : 44 46 EGADS : 45 47 EGADS : 46 48 EGADS : 47 49 EGADS : 48 50 EGADS : 49 51 EGADS : 50 52 EGADS : 51 53 EGADS : 52 54 EGADS : 53 55 EGADS : 54 56 EGADS : 55 57 EGADS : 56 58 EGADS : 57 59 EGADS : 58 60 EGADS : 59 61 EGADS : 60 62 EGADS : 61 63 EGADS : 62 64 EGADS : 63 65 EGADS : 64 66 EGADS : 65 67 EGADS : 66 68 EGADS : 67 69 EGADS : 68 70 EGADS : 69 71 EGADS : 70 72 EGADS : 71 73 EGADS : 72 74 EGADS : 73 75 EGADS : 74 76 EGADS : 75 77 EGADS : 76 78 EGADS : 77 79 EGADS : 78 80 EGADS : 79 81 EGADS : 80 82 EGADS : 81 83 EGADS : 82 84 EGADS : 83 85 EGADS : 84 86 EGADS : 85 87 EGADS : 86 88 EGADS : 87 89 EGADS : 88 90 EGADS : 89 91 EGADS : 90 92 EGADS : 91 93 EGADS : 92 94 EGADS : 93 95 EGADS : 94 96 EGADS : 95 97 EGADS : 96 98 EGADS : 97 99 EGADS : 98 100 EGADS : 99 101 EGADS : 100 102 EGADS : 101 103 EGADS : 102 104 EGADS : 103 105 EGADS : 104 106 EGADS : 105 107 EGADS : 106 108 EGADS : 107 109 EGADS : 108 110 EGADS : 109 111 EGADS : 110 112 EGADS : 111 113 EGADS : 112 114 EGADS : 113 115 EGADS : 114 116 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 3 2 -4 EGADS : 2 Yes -2 5 1 -6 EGADS : 3 Yes 7 4 -8 -3 EGADS : 4 Yes 8 6 -7 -5 EGADS : 5 Yes 9 12 -10 -11 EGADS : 6 Yes 10 14 -9 -13 EGADS : 7 Yes -15 11 16 -12 EGADS : 8 Yes -16 13 15 -14 EGADS : 9 Yes -17 20 19 -18 EGADS : 10 Yes -21 18 23 -22 EGADS : 11 Yes -24 22 26 -25 EGADS : 12 Yes 27 25 -28 -29 EGADS : 13 Yes 30 29 -31 -32 EGADS : 14 Yes 33 32 -34 -20 EGADS : 15 Yes 35 36 -37 -38 EGADS : 16 Yes 39 40 -41 42 -43 -35 -44 45 46 EGADS : 17 Yes 43 47 -48 -36 EGADS : 18 Yes -49 37 48 -50 EGADS : 19 Yes 51 38 -52 -53 EGADS : 20 Yes 44 -51 54 55 41 56 -39 57 58 EGADS : 21 Yes -56 -40 EGADS : 22 Yes -42 59 50 -47 EGADS : 23 Yes -60 64 63 -45 -58 62 -61 EGADS : 24 Yes -63 69 68 67 66 -65 -62 -57 -46 EGADS : 25 Yes 49 -70 -71 52 EGADS : 26 Yes -54 53 71 -72 EGADS : 27 Yes -55 72 70 -59 EGADS : 28 Yes -73 78 60 -77 -76 75 74 EGADS : 29 Yes 61 65 79 77 EGADS : 30 Yes -80 82 81 -64 EGADS : 31 Yes -83 -84 EGADS : 32 Yes -68 88 73 87 86 76 -79 -66 85 EGADS : 33 Yes -89 -67 92 -91 -90 -30 -33 17 EGADS : 34 Yes -81 93 94 -69 EGADS : 35 Yes -95 -87 -74 101 100 99 -98 97 -96 EGADS : 36 Yes -101 -75 -86 95 -105 -97 -104 -103 102 EGADS : 37 Yes -106 107 80 -78 EGADS : 38 Yes 108 109 EGADS : 39 Yes 110 -111 112 113 114 115 -116 83 EGADS : 40 Yes 116 117 -114 118 -119 -120 -110 84 EGADS : 41 Yes -92 -85 89 21 24 -27 90 -121 EGADS : 42 Yes -94 122 106 -88 EGADS : 43 Yes 91 121 EGADS : 44 Yes 105 96 EGADS : 45 Yes 98 123 -124 -125 EGADS : 46 Yes -99 127 126 -123 EGADS : 47 Yes -100 129 128 -127 EGADS : 48 Yes -102 131 130 -129 EGADS : 49 Yes 103 132 -133 -131 EGADS : 50 Yes 104 125 -134 -132 EGADS : 51 Yes -135 -108 141 140 139 -138 137 -136 EGADS : 52 Yes -141 -109 135 -145 -137 -144 -143 142 EGADS : 53 Yes 111 146 -147 -148 EGADS : 54 Yes -112 148 150 -149 EGADS : 55 Yes -113 149 152 -151 EGADS : 56 Yes 153 -154 155 156 157 -158 159 160 161 162 -163 -115 EGADS : 57 Yes 163 164 -161 165 -166 -167 -157 168 -169 -170 -153 EGADS : -117 EGADS : 58 Yes -118 151 172 -171 EGADS : 59 Yes 119 171 -173 -174 EGADS : 60 Yes 120 174 -175 -146 EGADS : 61 Yes 176 124 -126 -128 EGADS : 62 Yes -176 -130 133 134 EGADS : 63 Yes -177 136 187 186 185 -184 183 182 181 -180 179 -178 EGADS : 64 Yes 138 188 -189 -190 EGADS : 65 Yes -139 192 191 -188 EGADS : 66 Yes -140 194 193 -192 EGADS : 67 Yes -142 196 195 -194 EGADS : 68 Yes 143 197 -198 -196 EGADS : 69 Yes 144 190 -199 -197 EGADS : 70 Yes -187 145 177 -206 -179 -205 -204 203 -183 -202 -201 EGADS : 200 EGADS : 71 Yes 207 -152 -150 147 EGADS : 72 Yes 154 208 -209 -210 EGADS : 73 Yes -155 210 212 -211 EGADS : 74 Yes -156 211 214 -213 EGADS : 75 Yes 158 215 -216 -217 EGADS : 76 Yes -159 217 219 -218 EGADS : 77 Yes -160 218 221 -220 EGADS : 78 Yes -162 -164 EGADS : 79 Yes -165 220 223 -222 EGADS : 80 Yes 166 222 -224 -225 EGADS : 81 Yes 167 225 -226 -215 EGADS : 82 Yes -168 213 228 -227 EGADS : 83 Yes 169 227 -229 -230 EGADS : 84 Yes 170 230 -231 -208 EGADS : 85 Yes 175 173 -172 -207 EGADS : 86 Yes 206 178 EGADS : 87 Yes 180 232 -233 -234 EGADS : 88 Yes -181 236 235 -232 EGADS : 89 Yes -182 238 237 -236 EGADS : 90 Yes 184 239 -240 -241 EGADS : 91 Yes -185 243 242 -239 EGADS : 92 Yes -186 245 244 -243 EGADS : 93 Yes -193 246 189 -191 EGADS : 94 Yes -246 -195 198 199 EGADS : 95 Yes -200 248 247 -245 EGADS : 96 Yes 201 249 -250 -248 EGADS : 97 Yes 202 241 -251 -249 EGADS : 98 Yes -203 253 252 -238 EGADS : 99 Yes 204 254 -255 -253 EGADS : 100 Yes 205 234 -256 -254 EGADS : 101 Yes 257 -214 -212 209 EGADS : 102 Yes -221 -219 216 258 EGADS : 103 Yes -258 226 224 -223 EGADS : 104 Yes 231 229 -228 -257 EGADS : 105 Yes -237 259 233 -235 EGADS : 106 Yes -244 260 240 -242 EGADS : 107 Yes -260 -247 250 251 EGADS : 108 Yes -259 -252 255 256 EGADS : 109 Yes -261 -19 34 31 EGADS : 110 Yes -23 261 28 -26 EGADS : 111 Yes 262 263 -264 -265 EGADS : 112 Yes -266 269 268 -267 EGADS : 113 Yes 270 266 -271 -262 EGADS : 114 Yes -272 264 273 -268 EGADS : 115 Yes 265 272 -269 -270 EGADS : 116 Yes -263 271 267 -273 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 2 EGADS : 2 0 Yes 3 4 1 1 2 EGADS : 3 0 Yes 1 3 1 1 3 EGADS : 4 0 Yes 2 4 1 1 3 EGADS : 5 0 Yes 3 1 1 2 4 EGADS : 6 0 Yes 4 2 1 2 4 EGADS : 7 0 Yes 1 2 1 3 4 EGADS : 8 0 Yes 3 4 1 3 4 EGADS : 9 1 Yes 5 6 1 5 6 EGADS : 10 1 Yes 7 8 1 5 6 EGADS : 11 1 Yes 5 7 1 5 7 EGADS : 12 1 Yes 6 8 1 5 7 EGADS : 13 1 Yes 7 5 1 6 8 EGADS : 14 1 Yes 8 6 1 6 8 EGADS : 15 1 Yes 5 6 1 7 8 EGADS : 16 1 Yes 7 8 1 7 8 EGADS : 17 2 Yes 9 10 1 9 32 EGADS : 18 2 Yes 10 11 1 9 10 EGADS : 19 2 Yes 12 11 1 9 107 EGADS : 20 2 Yes 9 12 1 9 14 EGADS : 21 2 Yes 10 13 1 10 39 EGADS : 22 2 Yes 13 14 1 10 11 EGADS : 23 2 Yes 11 14 1 10 108 EGADS : 24 2 Yes 13 15 1 11 39 EGADS : 25 2 Yes 15 16 1 11 12 EGADS : 26 2 Yes 14 16 1 11 108 EGADS : 27 2 Yes 17 15 1 12 39 EGADS : 28 2 Yes 18 16 1 12 108 EGADS : 29 2 Yes 17 18 1 12 13 EGADS : 30 2 Yes 19 17 1 13 32 EGADS : 31 2 Yes 20 18 1 13 107 EGADS : 32 2 Yes 19 20 1 13 14 EGADS : 33 2 Yes 9 19 1 14 32 EGADS : 34 2 Yes 12 20 1 14 107 EGADS : 35 2 Yes 21 22 1 15 16 EGADS : 36 2 Yes 22 23 1 15 17 EGADS : 37 2 Yes 24 23 1 15 18 EGADS : 38 2 Yes 21 24 1 15 19 EGADS : 39 2 Yes 25 26 1 16 20 EGADS : 40 2 Yes 26 27 1 16 21 EGADS : 41 2 Yes 28 27 1 16 20 EGADS : 42 2 Yes 28 29 1 16 22 EGADS : 43 2 Yes 22 29 1 16 17 EGADS : 44 2 Yes 30 21 1 16 20 EGADS : 45 2 Yes 30 31 1 16 23 EGADS : 46 2 Yes 31 25 1 16 24 EGADS : 47 2 Yes 29 32 1 17 22 EGADS : 48 2 Yes 23 32 1 17 18 EGADS : 49 2 Yes 24 33 1 18 25 EGADS : 50 2 Yes 33 32 1 18 22 EGADS : 51 2 Yes 34 21 1 19 20 EGADS : 52 2 Yes 35 24 1 19 25 EGADS : 53 2 Yes 34 35 1 19 26 EGADS : 54 2 Yes 34 36 1 20 26 EGADS : 55 2 Yes 36 28 1 20 27 EGADS : 56 2 Yes 27 26 1 20 21 EGADS : 57 2 Yes 25 37 1 20 24 EGADS : 58 2 Yes 37 30 1 20 23 EGADS : 59 2 Yes 28 33 1 22 27 EGADS : 60 2 Yes 38 39 1 23 28 EGADS : 61 2 Yes 39 40 1 23 29 EGADS : 62 2 Yes 37 40 1 23 24 EGADS : 63 2 Yes 41 31 1 23 24 EGADS : 64 2 Yes 38 41 1 23 30 EGADS : 65 2 Yes 40 42 1 24 29 EGADS : 66 2 Yes 43 42 1 24 31 EGADS : 67 2 Yes 44 43 1 24 32 EGADS : 68 2 Yes 45 44 1 24 31 EGADS : 69 2 Yes 41 45 1 24 33 EGADS : 70 2 Yes 46 33 1 25 27 EGADS : 71 2 Yes 35 46 1 25 26 EGADS : 72 2 Yes 36 46 1 26 27 EGADS : 73 2 Yes 47 48 1 28 31 EGADS : 74 2 Yes 49 48 1 28 34 EGADS : 75 2 Yes 50 49 1 28 35 EGADS : 76 2 Yes 50 51 1 28 31 EGADS : 77 2 Yes 51 39 1 28 29 EGADS : 78 2 Yes 47 38 1 28 36 EGADS : 79 2 Yes 42 51 1 29 31 EGADS : 80 2 Yes 52 38 1 30 36 EGADS : 81 2 Yes 52 41 1 30 33 EGADS : 82 2 DEGEN 52 52 - 30 EGADS : 83 2 Yes 53 54 1 30 37 EGADS : 84 2 Yes 54 53 1 30 38 EGADS : 85 2 Yes 43 44 1 31 39 EGADS : 86 2 Yes 55 50 1 31 35 EGADS : 87 2 Yes 48 55 1 31 34 EGADS : 88 2 Yes 45 47 1 31 40 EGADS : 89 2 Yes 43 10 1 32 39 EGADS : 90 2 Yes 17 56 1 32 39 EGADS : 91 2 Yes 56 57 1 32 41 EGADS : 92 2 Yes 44 57 1 32 39 EGADS : 93 2 DEGEN 52 52 - 33 EGADS : 94 2 Yes 52 45 1 33 40 EGADS : 95 2 Yes 55 58 1 34 35 EGADS : 96 2 Yes 58 59 1 34 42 EGADS : 97 2 Yes 60 59 1 34 35 EGADS : 98 2 Yes 60 61 1 34 43 EGADS : 99 2 Yes 62 61 1 34 44 EGADS : 100 2 Yes 63 62 1 34 45 EGADS : 101 2 Yes 49 63 1 34 35 EGADS : 102 2 Yes 64 63 1 35 46 EGADS : 103 2 Yes 64 65 1 35 47 EGADS : 104 2 Yes 65 60 1 35 48 EGADS : 105 2 Yes 59 58 1 35 42 EGADS : 106 2 Yes 52 47 1 36 40 EGADS : 107 2 DEGEN 52 52 - 36 EGADS : 108 2 Yes 66 67 1 36 49 EGADS : 109 2 Yes 67 66 1 36 50 EGADS : 110 2 Yes 54 68 1 37 38 EGADS : 111 2 Yes 69 68 1 37 51 EGADS : 112 2 Yes 69 70 1 37 52 EGADS : 113 2 Yes 70 71 1 37 53 EGADS : 114 2 Yes 71 72 1 37 38 EGADS : 115 2 Yes 72 73 1 37 54 EGADS : 116 2 Yes 53 73 1 37 38 EGADS : 117 2 Yes 73 72 1 38 55 EGADS : 118 2 Yes 71 74 1 38 56 EGADS : 119 2 Yes 75 74 1 38 57 EGADS : 120 2 Yes 68 75 1 38 58 EGADS : 121 2 Yes 57 56 1 39 41 EGADS : 122 2 DEGEN 52 52 - 40 EGADS : 123 2 Yes 61 76 1 43 44 EGADS : 124 2 Yes 77 76 1 43 59 EGADS : 125 2 Yes 60 77 1 43 48 EGADS : 126 2 Yes 78 76 1 44 59 EGADS : 127 2 Yes 62 78 1 44 45 EGADS : 128 2 Yes 79 78 1 45 59 EGADS : 129 2 Yes 63 79 1 45 46 EGADS : 130 2 Yes 80 79 1 46 60 EGADS : 131 2 Yes 64 80 1 46 47 EGADS : 132 2 Yes 65 81 1 47 48 EGADS : 133 2 Yes 80 81 1 47 60 EGADS : 134 2 Yes 81 77 1 48 60 EGADS : 135 2 Yes 67 82 1 49 50 EGADS : 136 2 Yes 82 83 1 49 61 EGADS : 137 2 Yes 84 83 1 49 50 EGADS : 138 2 Yes 84 85 1 49 62 EGADS : 139 2 Yes 86 85 1 49 63 EGADS : 140 2 Yes 87 86 1 49 64 EGADS : 141 2 Yes 66 87 1 49 50 EGADS : 142 2 Yes 88 87 1 50 65 EGADS : 143 2 Yes 88 89 1 50 66 EGADS : 144 2 Yes 89 84 1 50 67 EGADS : 145 2 Yes 83 82 1 50 68 EGADS : 146 2 Yes 68 90 1 51 58 EGADS : 147 2 Yes 91 90 1 51 69 EGADS : 148 2 Yes 69 91 1 51 52 EGADS : 149 2 Yes 70 92 1 52 53 EGADS : 150 2 Yes 91 92 1 52 69 EGADS : 151 2 Yes 71 93 1 53 56 EGADS : 152 2 Yes 92 93 1 53 69 EGADS : 153 2 Yes 72 94 1 54 55 EGADS : 154 2 Yes 95 94 1 54 70 EGADS : 155 2 Yes 95 96 1 54 71 EGADS : 156 2 Yes 96 97 1 54 72 EGADS : 157 2 Yes 97 98 1 54 55 EGADS : 158 2 Yes 99 98 1 54 73 EGADS : 159 2 Yes 99 100 1 54 74 EGADS : 160 2 Yes 100 101 1 54 75 EGADS : 161 2 Yes 101 102 1 54 55 EGADS : 162 2 Yes 102 103 1 54 76 EGADS : 163 2 Yes 73 103 1 54 55 EGADS : 164 2 Yes 103 102 1 55 76 EGADS : 165 2 Yes 101 104 1 55 77 EGADS : 166 2 Yes 105 104 1 55 78 EGADS : 167 2 Yes 98 105 1 55 79 EGADS : 168 2 Yes 97 106 1 55 80 EGADS : 169 2 Yes 107 106 1 55 81 EGADS : 170 2 Yes 94 107 1 55 82 EGADS : 171 2 Yes 74 108 1 56 57 EGADS : 172 2 Yes 93 108 1 56 83 EGADS : 173 2 Yes 109 108 1 57 83 EGADS : 174 2 Yes 75 109 1 57 58 EGADS : 175 2 Yes 90 109 1 58 83 EGADS : 176 2 Yes 79 77 1 59 60 EGADS : 177 2 Yes 82 110 1 61 68 EGADS : 178 2 Yes 110 111 1 61 84 EGADS : 179 2 Yes 112 111 1 61 68 EGADS : 180 2 Yes 112 113 1 61 85 EGADS : 181 2 Yes 114 113 1 61 86 EGADS : 182 2 Yes 115 114 1 61 87 EGADS : 183 2 Yes 116 115 1 61 68 EGADS : 184 2 Yes 116 117 1 61 88 EGADS : 185 2 Yes 118 117 1 61 89 EGADS : 186 2 Yes 119 118 1 61 90 EGADS : 187 2 Yes 83 119 1 61 68 EGADS : 188 2 Yes 85 120 1 62 63 EGADS : 189 2 Yes 121 120 1 62 91 EGADS : 190 2 Yes 84 121 1 62 67 EGADS : 191 2 Yes 122 120 1 63 91 EGADS : 192 2 Yes 86 122 1 63 64 EGADS : 193 2 Yes 123 122 1 64 91 EGADS : 194 2 Yes 87 123 1 64 65 EGADS : 195 2 Yes 124 123 1 65 92 EGADS : 196 2 Yes 88 124 1 65 66 EGADS : 197 2 Yes 89 125 1 66 67 EGADS : 198 2 Yes 124 125 1 66 92 EGADS : 199 2 Yes 125 121 1 67 92 EGADS : 200 2 Yes 126 119 1 68 93 EGADS : 201 2 Yes 126 127 1 68 94 EGADS : 202 2 Yes 127 116 1 68 95 EGADS : 203 2 Yes 128 115 1 68 96 EGADS : 204 2 Yes 128 129 1 68 97 EGADS : 205 2 Yes 129 112 1 68 98 EGADS : 206 2 Yes 111 110 1 68 84 EGADS : 207 2 Yes 90 93 1 69 83 EGADS : 208 2 Yes 94 130 1 70 82 EGADS : 209 2 Yes 131 130 1 70 99 EGADS : 210 2 Yes 95 131 1 70 71 EGADS : 211 2 Yes 96 132 1 71 72 EGADS : 212 2 Yes 131 132 1 71 99 EGADS : 213 2 Yes 97 133 1 72 80 EGADS : 214 2 Yes 132 133 1 72 99 EGADS : 215 2 Yes 98 134 1 73 79 EGADS : 216 2 Yes 135 134 1 73 100 EGADS : 217 2 Yes 99 135 1 73 74 EGADS : 218 2 Yes 100 136 1 74 75 EGADS : 219 2 Yes 135 136 1 74 100 EGADS : 220 2 Yes 101 137 1 75 77 EGADS : 221 2 Yes 136 137 1 75 100 EGADS : 222 2 Yes 104 138 1 77 78 EGADS : 223 2 Yes 137 138 1 77 101 EGADS : 224 2 Yes 139 138 1 78 101 EGADS : 225 2 Yes 105 139 1 78 79 EGADS : 226 2 Yes 134 139 1 79 101 EGADS : 227 2 Yes 106 140 1 80 81 EGADS : 228 2 Yes 133 140 1 80 102 EGADS : 229 2 Yes 141 140 1 81 102 EGADS : 230 2 Yes 107 141 1 81 82 EGADS : 231 2 Yes 130 141 1 82 102 EGADS : 232 2 Yes 113 142 1 85 86 EGADS : 233 2 Yes 143 142 1 85 103 EGADS : 234 2 Yes 112 143 1 85 98 EGADS : 235 2 Yes 144 142 1 86 103 EGADS : 236 2 Yes 114 144 1 86 87 EGADS : 237 2 Yes 145 144 1 87 103 EGADS : 238 2 Yes 115 145 1 87 96 EGADS : 239 2 Yes 117 146 1 88 89 EGADS : 240 2 Yes 147 146 1 88 104 EGADS : 241 2 Yes 116 147 1 88 95 EGADS : 242 2 Yes 148 146 1 89 104 EGADS : 243 2 Yes 118 148 1 89 90 EGADS : 244 2 Yes 149 148 1 90 104 EGADS : 245 2 Yes 119 149 1 90 93 EGADS : 246 2 Yes 123 121 1 91 92 EGADS : 247 2 Yes 150 149 1 93 105 EGADS : 248 2 Yes 126 150 1 93 94 EGADS : 249 2 Yes 127 151 1 94 95 EGADS : 250 2 Yes 150 151 1 94 105 EGADS : 251 2 Yes 151 147 1 95 105 EGADS : 252 2 Yes 152 145 1 96 106 EGADS : 253 2 Yes 128 152 1 96 97 EGADS : 254 2 Yes 129 153 1 97 98 EGADS : 255 2 Yes 152 153 1 97 106 EGADS : 256 2 Yes 153 143 1 98 106 EGADS : 257 2 Yes 130 133 1 99 102 EGADS : 258 2 Yes 134 137 1 100 101 EGADS : 259 2 Yes 145 143 1 103 106 EGADS : 260 2 Yes 149 147 1 104 105 EGADS : 261 2 Yes 11 18 1 107 108 EGADS : 262 3 Yes 155 154 NA 109 111 EGADS : 263 3 Yes 154 156 NA 109 114 EGADS : 264 3 Yes 157 156 NA 109 112 EGADS : 265 3 Yes 155 157 NA 109 113 EGADS : 266 3 Yes 159 158 NA 110 111 EGADS : 267 3 Yes 158 160 NA 110 114 EGADS : 268 3 Yes 161 160 NA 110 112 EGADS : 269 3 Yes 159 161 NA 110 113 EGADS : 270 3 Yes 155 159 NA 111 113 EGADS : 271 3 Yes 154 158 NA 111 114 EGADS : 272 3 Yes 157 161 NA 112 113 EGADS : 273 3 Yes 156 160 NA 112 114 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 90.5173952 0 0 EGADS : 2 Yes 90.5173952 0 0 EGADS : 3 Yes 60.5173952 0 0 EGADS : 4 Yes 60.5173952 0 0 EGADS : 5 Yes 90.5173952 29.3018771 0 EGADS : 6 Yes 90.5173952 29.3018771 0 EGADS : 7 Yes 60.5173952 29.3018771 0 EGADS : 8 Yes 60.5173952 29.3018771 0 EGADS : 9 Yes 155.279418 0.556318046 17.8486974 EGADS : 10 Yes 162.754076 0 17.8179957 EGADS : 11 Yes 162.923819 0 18.2706428 EGADS : 12 Yes 156.044413 0.521348839 18.2706428 EGADS : 13 Yes 155.279418 0 17.8486974 EGADS : 14 Yes 156.044413 0 18.2706428 EGADS : 15 Yes 166.073363 0 35.1119946 EGADS : 16 Yes 166.308339 0 34.6929244 EGADS : 17 Yes 169.251074 0 35.1433216 EGADS : 18 Yes 169.082175 0 34.6929244 EGADS : 19 Yes 166.073363 0.227596794 35.1119946 EGADS : 20 Yes 166.308339 0.210212312 34.6929244 EGADS : 21 Yes 162.505711 6.6926087 7.42255789 EGADS : 22 Yes 153.264796 6.72114619 6.73834001 EGADS : 23 Yes 153.930225 7.199099 6.86796425 EGADS : 24 Yes 162.623387 7.31455844 6.87508685 EGADS : 25 Yes 139.227902 5.03861756 7.07099122 EGADS : 26 Yes 165.02399 35.781198 13.6055284 EGADS : 27 Yes 173.282633 35.781198 13.6055284 EGADS : 28 Yes 172.798165 34.4735419 13.3275775 EGADS : 29 Yes 168.724656 34.4225125 13.0211892 EGADS : 30 Yes 160.457816 1.16501909 6.24763245 EGADS : 31 Yes 152.092394 3.29252447 6.00142548 EGADS : 32 Yes 168.960236 34.0035224 12.9505074 EGADS : 33 Yes 172.609156 34.051986 12.953497 EGADS : 34 Yes 153.264796 6.72114619 8.11890743 EGADS : 35 Yes 154.029174 7.14485531 8.17706386 EGADS : 36 Yes 168.724656 34.4225125 13.6122726 EGADS : 37 Yes 156.577382 2.32417494 6.86784347 EGADS : 38 Yes 121.026192 0 0 EGADS : 39 Yes 165.026192 0 7 EGADS : 40 Yes 165.026192 0.5 8.5 EGADS : 41 Yes 121.026192 10 0 EGADS : 42 Yes 165.026192 0 10 EGADS : 43 Yes 159.822328 0 10 EGADS : 44 Yes 137.454662 0 10 EGADS : 45 Yes 121.026192 0 10 EGADS : 46 Yes 169.00177 33.9807538 13.4999966 EGADS : 47 Yes 121.026192 0 0 EGADS : 48 Yes 152.092394 0 6.00142548 EGADS : 49 Yes 160.457816 0 6.24763245 EGADS : 50 Yes 156.577382 0 6.86784347 EGADS : 51 Yes 165.026192 0 8.5 EGADS : 52 Yes 0 0 0 EGADS : 53 Yes 54.9020417 7.00084115 0 EGADS : 54 Yes 97.361045 7.90366896 0 EGADS : 55 Yes 139.227902 0 7.07099122 EGADS : 56 Yes 169.38016 0 35.487551 EGADS : 57 Yes 162.942213 0 35.487551 EGADS : 58 Yes 165.02399 0 13.6055284 EGADS : 59 Yes 173.282633 0 13.6055284 EGADS : 60 Yes 172.798165 0 13.3275775 EGADS : 61 Yes 168.724656 0 13.0211892 EGADS : 62 Yes 153.264796 0 6.73834001 EGADS : 63 Yes 162.505711 0 7.42255789 EGADS : 64 Yes 153.264796 0 8.11890743 EGADS : 65 Yes 168.724656 0 13.6122726 EGADS : 66 Yes 97.361045 0 0 EGADS : 67 Yes 54.9020417 0 0 EGADS : 68 Yes 97.4729837 13.4242561 0 EGADS : 69 Yes 93.4471586 13.4242631 0 EGADS : 70 Yes 93.8409288 32.482011 0 EGADS : 71 Yes 97.8594104 32.482018 0 EGADS : 72 Yes 97.9335611 36.1389817 0 EGADS : 73 Yes 75.3047874 36.1389817 0 EGADS : 74 Yes 93.8409288 32.482011 0 EGADS : 75 Yes 93.4471586 13.4242631 0 EGADS : 76 Yes 168.960236 0 12.9505074 EGADS : 77 Yes 172.609156 0 12.953497 EGADS : 78 Yes 153.930225 0 6.86796425 EGADS : 79 Yes 162.623387 0 6.87508685 EGADS : 80 Yes 154.029174 0 8.17706386 EGADS : 81 Yes 169.00177 0 13.4999966 EGADS : 82 Yes 75.3047874 0 0 EGADS : 83 Yes 97.9335611 0 0 EGADS : 84 Yes 97.8594104 0 0 EGADS : 85 Yes 93.8409288 0 0 EGADS : 86 Yes 93.4471586 0 0 EGADS : 87 Yes 97.4729837 0 0 EGADS : 88 Yes 93.4471586 0 0 EGADS : 89 Yes 93.8409288 0 0 EGADS : 90 Yes 97.1624342 13.7926169 0 EGADS : 91 Yes 93.8265357 13.6735644 0 EGADS : 92 Yes 94.2099771 32.2314198 0 EGADS : 93 Yes 97.6079776 32.3498916 0 EGADS : 94 Yes 100.278023 41.7701593 0 EGADS : 95 Yes 94.7972887 41.7748561 0 EGADS : 96 Yes 107.397556 67.6186586 1.83668579 EGADS : 97 Yes 111.041954 67.6241096 1.25345146 EGADS : 98 Yes 111.257254 68.1412393 1.31307624 EGADS : 99 Yes 107.654637 68.146711 1.88687506 EGADS : 100 Yes 121.207308 95.9421381 4.50820234 EGADS : 101 Yes 122.837313 95.9554542 4.52004059 EGADS : 102 Yes 123.552357 97.6729236 4.7180639 EGADS : 103 Yes 118.391317 97.6729236 3.99272703 EGADS : 104 Yes 121.207308 95.9421381 4.21444802 EGADS : 105 Yes 107.654637 68.146711 0.876544084 EGADS : 106 Yes 107.397556 67.6186586 0.813033541 EGADS : 107 Yes 94.7972887 41.7748561 0 EGADS : 108 Yes 93.9108835 32.2329728 0 EGADS : 109 Yes 93.5781103 13.6748542 0 EGADS : 110 Yes 118.391317 0 3.99272703 EGADS : 111 Yes 123.552357 0 4.7180639 EGADS : 112 Yes 122.837313 0 4.52004059 EGADS : 113 Yes 121.207308 0 4.21444802 EGADS : 114 Yes 107.654637 0 0.876544084 EGADS : 115 Yes 111.257254 0 1.31307624 EGADS : 116 Yes 111.041954 0 1.25345146 EGADS : 117 Yes 107.397556 0 0.813033541 EGADS : 118 Yes 94.7972887 0 0 EGADS : 119 Yes 100.278023 0 0 EGADS : 120 Yes 93.9108835 0 0 EGADS : 121 Yes 97.6079776 0 0 EGADS : 122 Yes 93.5781103 0 0 EGADS : 123 Yes 97.1624342 0 0 EGADS : 124 Yes 93.8265357 0 0 EGADS : 125 Yes 94.2099771 0 0 EGADS : 126 Yes 94.7972887 0 0 EGADS : 127 Yes 107.397556 0 1.83668579 EGADS : 128 Yes 107.654637 0 1.88687506 EGADS : 129 Yes 121.207308 0 4.50820234 EGADS : 130 Yes 100.219054 42.1509694 0 EGADS : 131 Yes 95.2324957 41.963173 0 EGADS : 132 Yes 107.613646 67.3581332 1.77910017 EGADS : 133 Yes 110.892704 67.4707526 0.699981401 EGADS : 134 Yes 111.247925 68.471101 0.828432723 EGADS : 135 Yes 108.034544 68.3613138 1.87771912 EGADS : 136 Yes 121.36809 95.7097324 4.49194275 EGADS : 137 Yes 122.742135 95.7387605 4.2753035 EGADS : 138 Yes 121.327393 95.7291979 4.23513353 EGADS : 139 Yes 107.88707 68.4318513 0.947114671 EGADS : 140 Yes 107.462349 67.4305014 0.82436964 EGADS : 141 Yes 94.9817282 42.0831197 0 EGADS : 142 Yes 121.367879 0 4.23512504 EGADS : 143 Yes 122.701966 0 4.70778241 EGADS : 144 Yes 108.034333 0 0.936789144 EGADS : 145 Yes 111.269456 0 1.85592771 EGADS : 146 Yes 107.462349 0 0.82436964 EGADS : 147 Yes 110.892704 0 0.699981401 EGADS : 148 Yes 94.9817282 0 0 EGADS : 149 Yes 100.219054 0 0 EGADS : 150 Yes 95.2324957 0 0 EGADS : 151 Yes 107.613646 0 1.77910017 EGADS : 152 Yes 107.888388 0 1.86745513 EGADS : 153 Yes 121.327604 0 4.49195125 EGADS : 154 Yes 0 0 1962.43554 EGADS : 155 Yes 0 0 0 EGADS : 156 Yes 0 1953.45847 1962.43554 EGADS : 157 Yes 0 1953.45847 0 EGADS : 158 Yes 2040.09979 0 1962.43554 EGADS : 159 Yes 2040.09979 0 0 EGADS : 160 Yes 2040.09979 1953.45847 1962.43554 EGADS : 161 Yes 2040.09979 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 53.021 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 530.302 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : 15 CAD geometry 0 STD w/BL AFLR4 : 16 CAD geometry 0 STD w/BL AFLR4 : 17 CAD geometry 0 STD w/BL AFLR4 : 18 CAD geometry 0 STD w/BL AFLR4 : 19 CAD geometry 0 STD w/BL AFLR4 : 20 CAD geometry 0 STD w/BL AFLR4 : 21 CAD geometry 0 STD w/BL AFLR4 : 22 CAD geometry 0 STD w/BL AFLR4 : 23 CAD geometry 0 STD w/BL AFLR4 : 24 CAD geometry 0 STD w/BL AFLR4 : 25 CAD geometry 0 STD w/BL AFLR4 : 26 CAD geometry 0 STD w/BL AFLR4 : 27 CAD geometry 0 STD w/BL AFLR4 : 28 CAD geometry 0 STD w/BL AFLR4 : 29 CAD geometry 0 STD w/BL AFLR4 : 30 CAD geometry 0 STD w/BL AFLR4 : 31 CAD geometry 0 STD w/BL AFLR4 : 32 CAD geometry 0 STD w/BL AFLR4 : 33 CAD geometry 0 STD w/BL AFLR4 : 34 CAD geometry 0 STD w/BL AFLR4 : 35 CAD geometry 0 STD w/BL AFLR4 : 36 CAD geometry 0 STD w/BL AFLR4 : 37 CAD geometry 0 STD w/BL AFLR4 : 38 CAD geometry 0 STD w/BL AFLR4 : 39 CAD geometry 0 STD w/BL AFLR4 : 40 CAD geometry 0 STD w/BL AFLR4 : 41 CAD geometry 0 STD w/BL AFLR4 : 42 CAD geometry 0 STD w/BL AFLR4 : 43 CAD geometry 0 STD w/BL AFLR4 : 44 CAD geometry 0 STD w/BL AFLR4 : 45 CAD geometry 0 STD w/BL AFLR4 : 46 CAD geometry 0 STD w/BL AFLR4 : 47 CAD geometry 0 STD w/BL AFLR4 : 48 CAD geometry 0 STD w/BL AFLR4 : 49 CAD geometry 0 STD w/BL AFLR4 : 50 CAD geometry 0 STD w/BL AFLR4 : 51 CAD geometry 0 STD w/BL AFLR4 : 52 CAD geometry 0 STD w/BL AFLR4 : 53 CAD geometry 0 STD w/BL AFLR4 : 54 CAD geometry 0 STD w/BL AFLR4 : 55 CAD geometry 0 STD w/BL AFLR4 : 56 CAD geometry 0 STD w/BL AFLR4 : 57 CAD geometry 0 STD w/BL AFLR4 : 58 CAD geometry 0 STD w/BL AFLR4 : 59 CAD geometry 0 STD w/BL AFLR4 : 60 CAD geometry 0 STD w/BL AFLR4 : 61 CAD geometry 0 STD w/BL AFLR4 : 62 CAD geometry 0 STD w/BL AFLR4 : 63 CAD geometry 0 STD w/BL AFLR4 : 64 CAD geometry 0 STD w/BL AFLR4 : 65 CAD geometry 0 STD w/BL AFLR4 : 66 CAD geometry 0 STD w/BL AFLR4 : 67 CAD geometry 0 STD w/BL AFLR4 : 68 CAD geometry 0 STD w/BL AFLR4 : 69 CAD geometry 0 STD w/BL AFLR4 : 70 CAD geometry 0 STD w/BL AFLR4 : 71 CAD geometry 0 STD w/BL AFLR4 : 72 CAD geometry 0 STD w/BL AFLR4 : 73 CAD geometry 0 STD w/BL AFLR4 : 74 CAD geometry 0 STD w/BL AFLR4 : 75 CAD geometry 0 STD w/BL AFLR4 : 76 CAD geometry 0 STD w/BL AFLR4 : 77 CAD geometry 0 STD w/BL AFLR4 : 78 CAD geometry 0 STD w/BL AFLR4 : 79 CAD geometry 0 STD w/BL AFLR4 : 80 CAD geometry 0 STD w/BL AFLR4 : 81 CAD geometry 0 STD w/BL AFLR4 : 82 CAD geometry 0 STD w/BL AFLR4 : 83 CAD geometry 0 STD w/BL AFLR4 : 84 CAD geometry 0 STD w/BL AFLR4 : 85 CAD geometry 0 STD w/BL AFLR4 : 86 CAD geometry 0 STD w/BL AFLR4 : 87 CAD geometry 0 STD w/BL AFLR4 : 88 CAD geometry 0 STD w/BL AFLR4 : 89 CAD geometry 0 STD w/BL AFLR4 : 90 CAD geometry 0 STD w/BL AFLR4 : 91 CAD geometry 0 STD w/BL AFLR4 : 92 CAD geometry 0 STD w/BL AFLR4 : 93 CAD geometry 0 STD w/BL AFLR4 : 94 CAD geometry 0 STD w/BL AFLR4 : 95 CAD geometry 0 STD w/BL AFLR4 : 96 CAD geometry 0 STD w/BL AFLR4 : 97 CAD geometry 0 STD w/BL AFLR4 : 98 CAD geometry 0 STD w/BL AFLR4 : 99 CAD geometry 0 STD w/BL AFLR4 : 100 CAD geometry 0 STD w/BL AFLR4 : 101 CAD geometry 0 STD w/BL AFLR4 : 102 CAD geometry 0 STD w/BL AFLR4 : 103 CAD geometry 0 STD w/BL AFLR4 : 104 CAD geometry 0 STD w/BL AFLR4 : 105 CAD geometry 0 STD w/BL AFLR4 : 106 CAD geometry 0 STD w/BL AFLR4 : 107 CAD geometry 0 STD w/BL AFLR4 : 108 CAD geometry 0 STD w/BL AFLR4 : 109 CAD geometry 0 FARFIELD AFLR4 : 110 CAD geometry 0 FARFIELD AFLR4 : 111 CAD geometry 0 FARFIELD AFLR4 : 112 CAD geometry 0 FARFIELD AFLR4 : 113 CAD geometry 0 FARFIELD AFLR4 : 114 CAD geometry 0 FARFIELD AFLR4 : Case has 5 Proximity Checking Components AFLR4 : Component 1 includes Definitions 23 24 28 29 30 31 33 36 40 AFLR4 : Component 2 includes Definitions 37 38 49 50 51 52 53 54 55 56 57 58 AFLR4 : 61 62 63 64 65 66 67 68 69 70 71 72 AFLR4 : 73 74 75 76 77 78 79 80 81 82 83 84 AFLR4 : 85 86 87 88 89 90 91 92 93 94 95 96 AFLR4 : 97 98 99 100 101 102 103 104 105 106 AFLR4 : Component 3 includes Definitions 15 16 17 18 19 20 21 22 25 26 27 34 AFLR4 : 35 42 43 44 45 46 47 48 59 60 AFLR4 : Component 4 includes Definitions 9 10 11 12 13 14 32 39 41 107 108 AFLR4 : Component 5 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR4 : Define CAD surface definition 19 AFLR4 : Define CAD surface definition 20 AFLR4 : Define CAD surface definition 21 AFLR4 : Define CAD surface definition 22 AFLR4 : Define CAD surface definition 23 AFLR4 : Define CAD surface definition 24 AFLR4 : Define CAD surface definition 25 AFLR4 : Define CAD surface definition 26 AFLR4 : Define CAD surface definition 27 AFLR4 : Define CAD surface definition 28 AFLR4 : Define CAD surface definition 29 AFLR4 : Define CAD surface definition 30 AFLR4 : Define CAD surface definition 31 AFLR4 : Define CAD surface definition 32 AFLR4 : Define CAD surface definition 33 AFLR4 : Define CAD surface definition 34 AFLR4 : Define CAD surface definition 35 AFLR4 : Define CAD surface definition 36 AFLR4 : Define CAD surface definition 37 AFLR4 : Define CAD surface definition 38 AFLR4 : Define CAD surface definition 39 AFLR4 : Define CAD surface definition 40 AFLR4 : Define CAD surface definition 41 AFLR4 : Define CAD surface definition 42 AFLR4 : Define CAD surface definition 43 AFLR4 : Define CAD surface definition 44 AFLR4 : Define CAD surface definition 45 AFLR4 : Define CAD surface definition 46 AFLR4 : Define CAD surface definition 47 AFLR4 : Define CAD surface definition 48 AFLR4 : Define CAD surface definition 49 AFLR4 : Define CAD surface definition 50 AFLR4 : Define CAD surface definition 51 AFLR4 : Define CAD surface definition 52 AFLR4 : Define CAD surface definition 53 AFLR4 : Define CAD surface definition 54 AFLR4 : Define CAD surface definition 55 AFLR4 : Define CAD surface definition 56 AFLR4 : Define CAD surface definition 57 AFLR4 : Define CAD surface definition 58 AFLR4 : Define CAD surface definition 59 AFLR4 : Define CAD surface definition 60 AFLR4 : Define CAD surface definition 61 AFLR4 : Define CAD surface definition 62 AFLR4 : Define CAD surface definition 63 AFLR4 : Define CAD surface definition 64 AFLR4 : Define CAD surface definition 65 AFLR4 : Define CAD surface definition 66 AFLR4 : Define CAD surface definition 67 AFLR4 : Define CAD surface definition 68 AFLR4 : Define CAD surface definition 69 AFLR4 : Define CAD surface definition 70 AFLR4 : Define CAD surface definition 71 AFLR4 : Define CAD surface definition 72 AFLR4 : Define CAD surface definition 73 AFLR4 : Define CAD surface definition 74 AFLR4 : Define CAD surface definition 75 AFLR4 : Define CAD surface definition 76 AFLR4 : Define CAD surface definition 77 AFLR4 : Define CAD surface definition 78 AFLR4 : Define CAD surface definition 79 AFLR4 : Define CAD surface definition 80 AFLR4 : Define CAD surface definition 81 AFLR4 : Define CAD surface definition 82 AFLR4 : Define CAD surface definition 83 AFLR4 : Define CAD surface definition 84 AFLR4 : Define CAD surface definition 85 AFLR4 : Define CAD surface definition 86 AFLR4 : Define CAD surface definition 87 AFLR4 : Define CAD surface definition 88 AFLR4 : Define CAD surface definition 89 AFLR4 : Define CAD surface definition 90 AFLR4 : Define CAD surface definition 91 AFLR4 : Define CAD surface definition 92 AFLR4 : Define CAD surface definition 93 AFLR4 : Define CAD surface definition 94 AFLR4 : Define CAD surface definition 95 AFLR4 : Define CAD surface definition 96 AFLR4 : Define CAD surface definition 97 AFLR4 : Define CAD surface definition 98 AFLR4 : Define CAD surface definition 99 AFLR4 : Define CAD surface definition 100 AFLR4 : Define CAD surface definition 101 AFLR4 : Define CAD surface definition 102 AFLR4 : Define CAD surface definition 103 AFLR4 : Define CAD surface definition 104 AFLR4 : Define CAD surface definition 105 AFLR4 : Define CAD surface definition 106 AFLR4 : Define CAD surface definition 107 AFLR4 : Define CAD surface definition 108 AFLR4 : Define CAD surface definition 109 AFLR4 : Define CAD surface definition 110 AFLR4 : Define CAD surface definition 111 AFLR4 : Define CAD surface definition 112 AFLR4 : Define CAD surface definition 113 AFLR4 : Define CAD surface definition 114 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 339 605 0 AFLR4 : Nodes, Trias,Quads= 362 651 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 319 563 0 AFLR4 : Nodes, Trias,Quads= 284 493 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 340 607 0 AFLR4 : Nodes, Trias,Quads= 362 651 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 321 567 0 AFLR4 : Nodes, Trias,Quads= 284 493 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 340 607 0 AFLR4 : Nodes, Trias,Quads= 362 651 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 321 567 0 AFLR4 : Nodes, Trias,Quads= 284 493 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 339 605 0 AFLR4 : Nodes, Trias,Quads= 362 651 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 319 563 0 AFLR4 : Nodes, Trias,Quads= 284 493 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 15 19 0 AFLR4 : Nodes, Trias,Quads= 9 7 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 15 19 0 AFLR4 : Nodes, Trias,Quads= 9 7 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 47 65 0 AFLR4 : Nodes, Trias,Quads= 27 25 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 24 31 0 AFLR4 : Nodes, Trias,Quads= 23 29 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 24 31 0 AFLR4 : Nodes, Trias,Quads= 22 27 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 47 65 0 AFLR4 : Nodes, Trias,Quads= 27 25 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 51 67 0 AFLR4 : Nodes, Trias,Quads= 58 81 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 1615 3003 0 AFLR4 : Nodes, Trias,Quads= 1188 2149 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 90 127 0 AFLR4 : Nodes, Trias,Quads= 51 49 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 216 367 0 AFLR4 : Nodes, Trias,Quads= 174 283 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 51 67 0 AFLR4 : Nodes, Trias,Quads= 51 67 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 1677 3126 0 AFLR4 : Nodes, Trias,Quads= 1210 2192 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 35 44 0 AFLR4 : Nodes, Trias,Quads= 24 22 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 9 9 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 907 1650 0 AFLR4 : Nodes, Trias,Quads= 569 974 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 3270 6232 0 AFLR4 : Nodes, Trias,Quads= 1907 3506 0 AFLR4 : Generate optimal mesh on surface definition 25 AFLR2 : Nodes, Trias,Quads= 220 375 0 AFLR4 : Nodes, Trias,Quads= 176 287 0 AFLR4 : Generate optimal mesh on surface definition 26 AFLR2 : Nodes, Trias,Quads= 80 108 0 AFLR4 : Nodes, Trias,Quads= 50 48 0 AFLR4 : Generate optimal mesh on surface definition 27 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Generate optimal mesh on surface definition 28 AFLR2 : Nodes, Trias,Quads= 902 1640 0 AFLR4 : Nodes, Trias,Quads= 561 958 0 AFLR4 : Generate optimal mesh on surface definition 29 AFLR2 : Nodes, Trias,Quads= 106 170 0 AFLR4 : Nodes, Trias,Quads= 106 170 0 AFLR4 : Generate optimal mesh on surface definition 30 AFLR2 : Nodes, Trias,Quads= 1586 2835 0 AFLR4 : Nodes, Trias,Quads= 1651 2965 0 AFLR4 : Generate optimal mesh on surface definition 31 AFLR2 : Nodes, Trias,Quads= 3418 6528 0 AFLR4 : Nodes, Trias,Quads= 1888 3468 0 AFLR4 : Generate optimal mesh on surface definition 32 AFLR2 : Nodes, Trias,Quads= 1868 3486 0 AFLR4 : Nodes, Trias,Quads= 1347 2444 0 AFLR4 : Generate optimal mesh on surface definition 33 AFLR2 : Nodes, Trias,Quads= 1026 1838 0 AFLR4 : Nodes, Trias,Quads= 1211 2208 0 AFLR4 : Generate optimal mesh on surface definition 34 AFLR2 : Nodes, Trias,Quads= 1436 2654 0 AFLR4 : Nodes, Trias,Quads= 979 1740 0 AFLR4 : Generate optimal mesh on surface definition 35 AFLR2 : Nodes, Trias,Quads= 1684 3140 0 AFLR4 : Nodes, Trias,Quads= 1216 2204 0 AFLR4 : Generate optimal mesh on surface definition 36 AFLR2 : Nodes, Trias,Quads= 1580 2823 0 AFLR4 : Nodes, Trias,Quads= 1646 2955 0 AFLR4 : Generate optimal mesh on surface definition 37 AFLR2 : Nodes, Trias,Quads= 2154 4060 0 AFLR4 : Nodes, Trias,Quads= 2140 4032 0 AFLR4 : Generate optimal mesh on surface definition 38 AFLR2 : Nodes, Trias,Quads= 2585 4915 0 AFLR4 : Nodes, Trias,Quads= 2189 4123 0 AFLR4 : Generate optimal mesh on surface definition 39 AFLR2 : Nodes, Trias,Quads= 1916 3582 0 AFLR4 : Nodes, Trias,Quads= 1367 2484 0 AFLR4 : Generate optimal mesh on surface definition 40 AFLR2 : Nodes, Trias,Quads= 1026 1838 0 AFLR4 : Nodes, Trias,Quads= 1215 2216 0 AFLR4 : Generate optimal mesh on surface definition 41 AFLR2 : Nodes, Trias,Quads= 47 60 0 AFLR4 : Nodes, Trias,Quads= 32 30 0 AFLR4 : Generate optimal mesh on surface definition 42 AFLR2 : Nodes, Trias,Quads= 35 44 0 AFLR4 : Nodes, Trias,Quads= 24 22 0 AFLR4 : Generate optimal mesh on surface definition 43 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 9 9 0 AFLR4 : Generate optimal mesh on surface definition 44 AFLR2 : Nodes, Trias,Quads= 59 84 0 AFLR4 : Nodes, Trias,Quads= 32 30 0 AFLR4 : Generate optimal mesh on surface definition 45 AFLR2 : Nodes, Trias,Quads= 41 53 0 AFLR4 : Nodes, Trias,Quads= 48 67 0 AFLR4 : Generate optimal mesh on surface definition 46 AFLR2 : Nodes, Trias,Quads= 51 67 0 AFLR4 : Nodes, Trias,Quads= 50 65 0 AFLR4 : Generate optimal mesh on surface definition 47 AFLR2 : Nodes, Trias,Quads= 80 108 0 AFLR4 : Nodes, Trias,Quads= 50 48 0 AFLR4 : Generate optimal mesh on surface definition 48 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Generate optimal mesh on surface definition 49 AFLR2 : Nodes, Trias,Quads= 2582 4909 0 AFLR4 : Nodes, Trias,Quads= 2199 4143 0 AFLR4 : Generate optimal mesh on surface definition 50 AFLR2 : Nodes, Trias,Quads= 2158 4068 0 AFLR4 : Nodes, Trias,Quads= 2139 4030 0 AFLR4 : Generate optimal mesh on surface definition 51 AFLR2 : Nodes, Trias,Quads= 46 65 0 AFLR4 : Nodes, Trias,Quads= 39 51 0 AFLR4 : Generate optimal mesh on surface definition 52 AFLR2 : Nodes, Trias,Quads= 108 144 0 AFLR4 : Nodes, Trias,Quads= 102 132 0 AFLR4 : Generate optimal mesh on surface definition 53 AFLR2 : Nodes, Trias,Quads= 46 65 0 AFLR4 : Nodes, Trias,Quads= 39 51 0 AFLR4 : Generate optimal mesh on surface definition 54 AFLR2 : Nodes, Trias,Quads= 3787 7224 0 AFLR4 : Nodes, Trias,Quads= 2368 4386 0 AFLR4 : Generate optimal mesh on surface definition 55 AFLR2 : Nodes, Trias,Quads= 3490 6642 0 AFLR4 : Nodes, Trias,Quads= 2094 3850 0 AFLR4 : Generate optimal mesh on surface definition 56 AFLR2 : Nodes, Trias,Quads= 74 114 0 AFLR4 : Nodes, Trias,Quads= 49 64 0 AFLR4 : Generate optimal mesh on surface definition 57 AFLR2 : Nodes, Trias,Quads= 148 206 0 AFLR4 : Nodes, Trias,Quads= 111 132 0 AFLR4 : Generate optimal mesh on surface definition 58 AFLR2 : Nodes, Trias,Quads= 70 107 0 AFLR4 : Nodes, Trias,Quads= 49 65 0 AFLR4 : Generate optimal mesh on surface definition 59 AFLR2 : Nodes, Trias,Quads= 130 209 0 AFLR4 : Nodes, Trias,Quads= 94 137 0 AFLR4 : Generate optimal mesh on surface definition 60 AFLR2 : Nodes, Trias,Quads= 215 365 0 AFLR4 : Nodes, Trias,Quads= 176 287 0 AFLR4 : Generate optimal mesh on surface definition 61 AFLR2 : Nodes, Trias,Quads= 3536 6729 0 AFLR4 : Nodes, Trias,Quads= 2180 4017 0 AFLR4 : Generate optimal mesh on surface definition 62 AFLR2 : Nodes, Trias,Quads= 74 114 0 AFLR4 : Nodes, Trias,Quads= 48 62 0 AFLR4 : Generate optimal mesh on surface definition 63 AFLR2 : Nodes, Trias,Quads= 148 206 0 AFLR4 : Nodes, Trias,Quads= 111 132 0 AFLR4 : Generate optimal mesh on surface definition 64 AFLR2 : Nodes, Trias,Quads= 70 107 0 AFLR4 : Nodes, Trias,Quads= 49 65 0 AFLR4 : Generate optimal mesh on surface definition 65 AFLR2 : Nodes, Trias,Quads= 46 65 0 AFLR4 : Nodes, Trias,Quads= 39 51 0 AFLR4 : Generate optimal mesh on surface definition 66 AFLR2 : Nodes, Trias,Quads= 108 144 0 AFLR4 : Nodes, Trias,Quads= 94 116 0 AFLR4 : Generate optimal mesh on surface definition 67 AFLR2 : Nodes, Trias,Quads= 46 65 0 AFLR4 : Nodes, Trias,Quads= 39 51 0 AFLR4 : Generate optimal mesh on surface definition 68 AFLR2 : Nodes, Trias,Quads= 3573 6801 0 AFLR4 : Nodes, Trias,Quads= 2281 4217 0 AFLR4 : Generate optimal mesh on surface definition 69 AFLR2 : Nodes, Trias,Quads= 245 414 0 AFLR4 : Nodes, Trias,Quads= 224 372 0 AFLR4 : Generate optimal mesh on surface definition 70 AFLR2 : Nodes, Trias,Quads= 50 67 0 AFLR4 : Nodes, Trias,Quads= 51 69 0 AFLR4 : Generate optimal mesh on surface definition 71 AFLR2 : Nodes, Trias,Quads= 114 155 0 AFLR4 : Nodes, Trias,Quads= 78 83 0 AFLR4 : Generate optimal mesh on surface definition 72 AFLR2 : Nodes, Trias,Quads= 28 36 0 AFLR4 : Nodes, Trias,Quads= 31 42 0 AFLR4 : Generate optimal mesh on surface definition 73 AFLR2 : Nodes, Trias,Quads= 39 50 0 AFLR4 : Nodes, Trias,Quads= 42 56 0 AFLR4 : Generate optimal mesh on surface definition 74 AFLR2 : Nodes, Trias,Quads= 157 216 0 AFLR4 : Nodes, Trias,Quads= 141 184 0 AFLR4 : Generate optimal mesh on surface definition 75 AFLR2 : Nodes, Trias,Quads= 31 39 0 AFLR4 : Nodes, Trias,Quads= 32 41 0 AFLR4 : Generate optimal mesh on surface definition 76 AFLR2 : Nodes, Trias,Quads= 36 49 0 AFLR4 : Nodes, Trias,Quads= 21 19 0 AFLR4 : Generate optimal mesh on surface definition 77 AFLR2 : Nodes, Trias,Quads= 32 40 0 AFLR4 : Nodes, Trias,Quads= 34 44 0 AFLR4 : Generate optimal mesh on surface definition 78 AFLR2 : Nodes, Trias,Quads= 148 208 0 AFLR4 : Nodes, Trias,Quads= 86 84 0 AFLR4 : Generate optimal mesh on surface definition 79 AFLR2 : Nodes, Trias,Quads= 31 40 0 AFLR4 : Nodes, Trias,Quads= 33 44 0 AFLR4 : Generate optimal mesh on surface definition 80 AFLR2 : Nodes, Trias,Quads= 28 36 0 AFLR4 : Nodes, Trias,Quads= 30 40 0 AFLR4 : Generate optimal mesh on surface definition 81 AFLR2 : Nodes, Trias,Quads= 111 158 0 AFLR4 : Nodes, Trias,Quads= 65 66 0 AFLR4 : Generate optimal mesh on surface definition 82 AFLR2 : Nodes, Trias,Quads= 33 41 0 AFLR4 : Nodes, Trias,Quads= 40 55 0 AFLR4 : Generate optimal mesh on surface definition 83 AFLR2 : Nodes, Trias,Quads= 328 564 0 AFLR4 : Nodes, Trias,Quads= 305 518 0 AFLR4 : Generate optimal mesh on surface definition 84 AFLR2 : Nodes, Trias,Quads= 36 49 0 AFLR4 : Nodes, Trias,Quads= 21 19 0 AFLR4 : Generate optimal mesh on surface definition 85 AFLR2 : Nodes, Trias,Quads= 32 41 0 AFLR4 : Nodes, Trias,Quads= 34 45 0 AFLR4 : Generate optimal mesh on surface definition 86 AFLR2 : Nodes, Trias,Quads= 157 216 0 AFLR4 : Nodes, Trias,Quads= 119 140 0 AFLR4 : Generate optimal mesh on surface definition 87 AFLR2 : Nodes, Trias,Quads= 39 51 0 AFLR4 : Nodes, Trias,Quads= 43 59 0 AFLR4 : Generate optimal mesh on surface definition 88 AFLR2 : Nodes, Trias,Quads= 28 36 0 AFLR4 : Nodes, Trias,Quads= 30 40 0 AFLR4 : Generate optimal mesh on surface definition 89 AFLR2 : Nodes, Trias,Quads= 111 158 0 AFLR4 : Nodes, Trias,Quads= 65 66 0 AFLR4 : Generate optimal mesh on surface definition 90 AFLR2 : Nodes, Trias,Quads= 33 41 0 AFLR4 : Nodes, Trias,Quads= 40 55 0 AFLR4 : Generate optimal mesh on surface definition 91 AFLR2 : Nodes, Trias,Quads= 329 566 0 AFLR4 : Nodes, Trias,Quads= 305 518 0 AFLR4 : Generate optimal mesh on surface definition 92 AFLR2 : Nodes, Trias,Quads= 245 414 0 AFLR4 : Nodes, Trias,Quads= 225 374 0 AFLR4 : Generate optimal mesh on surface definition 93 AFLR2 : Nodes, Trias,Quads= 50 67 0 AFLR4 : Nodes, Trias,Quads= 51 69 0 AFLR4 : Generate optimal mesh on surface definition 94 AFLR2 : Nodes, Trias,Quads= 114 155 0 AFLR4 : Nodes, Trias,Quads= 78 83 0 AFLR4 : Generate optimal mesh on surface definition 95 AFLR2 : Nodes, Trias,Quads= 28 36 0 AFLR4 : Nodes, Trias,Quads= 31 42 0 AFLR4 : Generate optimal mesh on surface definition 96 AFLR2 : Nodes, Trias,Quads= 32 41 0 AFLR4 : Nodes, Trias,Quads= 35 47 0 AFLR4 : Generate optimal mesh on surface definition 97 AFLR2 : Nodes, Trias,Quads= 148 208 0 AFLR4 : Nodes, Trias,Quads= 112 136 0 AFLR4 : Generate optimal mesh on surface definition 98 AFLR2 : Nodes, Trias,Quads= 33 42 0 AFLR4 : Nodes, Trias,Quads= 34 44 0 AFLR4 : Generate optimal mesh on surface definition 99 AFLR2 : Nodes, Trias,Quads= 251 422 0 AFLR4 : Nodes, Trias,Quads= 208 336 0 AFLR4 : Generate optimal mesh on surface definition 100 AFLR2 : Nodes, Trias,Quads= 332 556 0 AFLR4 : Nodes, Trias,Quads= 250 392 0 AFLR4 : Generate optimal mesh on surface definition 101 AFLR2 : Nodes, Trias,Quads= 295 490 0 AFLR4 : Nodes, Trias,Quads= 216 332 0 AFLR4 : Generate optimal mesh on surface definition 102 AFLR2 : Nodes, Trias,Quads= 207 341 0 AFLR4 : Nodes, Trias,Quads= 174 275 0 AFLR4 : Generate optimal mesh on surface definition 103 AFLR2 : Nodes, Trias,Quads= 327 547 0 AFLR4 : Nodes, Trias,Quads= 240 373 0 AFLR4 : Generate optimal mesh on surface definition 104 AFLR2 : Nodes, Trias,Quads= 208 343 0 AFLR4 : Nodes, Trias,Quads= 173 273 0 AFLR4 : Generate optimal mesh on surface definition 105 AFLR2 : Nodes, Trias,Quads= 248 416 0 AFLR4 : Nodes, Trias,Quads= 208 336 0 AFLR4 : Generate optimal mesh on surface definition 106 AFLR2 : Nodes, Trias,Quads= 297 493 0 AFLR4 : Nodes, Trias,Quads= 225 349 0 AFLR4 : Generate optimal mesh on surface definition 107 AFLR2 : Nodes, Trias,Quads= 40 57 0 AFLR4 : Nodes, Trias,Quads= 30 37 0 AFLR4 : Generate optimal mesh on surface definition 108 AFLR2 : Nodes, Trias,Quads= 40 57 0 AFLR4 : Nodes, Trias,Quads= 31 39 0 AFLR4 : Generate optimal mesh on surface definition 109 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 110 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 111 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 112 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 113 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 114 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 39754 79500 9980 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 39754 79500 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 397 713 0 AFLR4 : Nodes, Trias,Quads= 416 751 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 387 691 0 AFLR4 : Nodes, Trias,Quads= 346 609 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 396 711 0 AFLR4 : Nodes, Trias,Quads= 417 753 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 388 693 0 AFLR4 : Nodes, Trias,Quads= 344 605 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 395 709 0 AFLR4 : Nodes, Trias,Quads= 416 751 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 388 693 0 AFLR4 : Nodes, Trias,Quads= 344 605 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 395 709 0 AFLR4 : Nodes, Trias,Quads= 416 751 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 387 691 0 AFLR4 : Nodes, Trias,Quads= 346 609 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 18 23 0 AFLR4 : Nodes, Trias,Quads= 11 9 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 18 23 0 AFLR4 : Nodes, Trias,Quads= 11 9 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 56 77 0 AFLR4 : Nodes, Trias,Quads= 33 31 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 28 37 0 AFLR4 : Nodes, Trias,Quads= 25 31 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 29 38 0 AFLR4 : Nodes, Trias,Quads= 28 36 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 56 77 0 AFLR4 : Nodes, Trias,Quads= 33 31 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 60 80 0 AFLR4 : Nodes, Trias,Quads= 59 78 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 1730 3226 0 AFLR4 : Nodes, Trias,Quads= 1387 2540 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 100 140 0 AFLR4 : Nodes, Trias,Quads= 58 56 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 271 470 0 AFLR4 : Nodes, Trias,Quads= 208 344 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 57 75 0 AFLR4 : Nodes, Trias,Quads= 61 83 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 1821 3408 0 AFLR4 : Nodes, Trias,Quads= 1413 2592 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 38 49 0 AFLR4 : Nodes, Trias,Quads= 25 23 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 15 19 0 AFLR4 : Nodes, Trias,Quads= 15 19 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 1020 1868 0 AFLR4 : Nodes, Trias,Quads= 1567 2962 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 3285 6257 0 AFLR4 : Nodes, Trias,Quads= 2655 4997 0 AFLR4 : Generate optimal mesh on surface definition 25 AFLR2 : Nodes, Trias,Quads= 268 463 0 AFLR4 : Nodes, Trias,Quads= 211 349 0 AFLR4 : Generate optimal mesh on surface definition 26 AFLR2 : Nodes, Trias,Quads= 96 133 0 AFLR4 : Nodes, Trias,Quads= 57 55 0 AFLR4 : Generate optimal mesh on surface definition 27 AFLR2 : Nodes, Trias,Quads= 15 18 0 AFLR4 : Nodes, Trias,Quads= 15 18 0 AFLR4 : Generate optimal mesh on surface definition 28 AFLR2 : Nodes, Trias,Quads= 1004 1837 0 AFLR4 : Nodes, Trias,Quads= 1549 2927 0 AFLR4 : Generate optimal mesh on surface definition 29 AFLR2 : Nodes, Trias,Quads= 106 170 0 AFLR4 : Nodes, Trias,Quads= 116 190 0 AFLR4 : Generate optimal mesh on surface definition 30 AFLR2 : Nodes, Trias,Quads= 1642 2942 0 AFLR4 : Nodes, Trias,Quads= 3189 6036 0 AFLR4 : Generate optimal mesh on surface definition 31 AFLR2 : Nodes, Trias,Quads= 3518 6723 0 AFLR4 : Nodes, Trias,Quads= 2629 4945 0 AFLR4 : Generate optimal mesh on surface definition 32 AFLR2 : Nodes, Trias,Quads= 2078 3899 0 AFLR4 : Nodes, Trias,Quads= 1693 3129 0 AFLR4 : Generate optimal mesh on surface definition 33 AFLR2 : Nodes, Trias,Quads= 1089 1958 0 AFLR4 : Nodes, Trias,Quads= 2728 5236 0 AFLR4 : Generate optimal mesh on surface definition 34 AFLR2 : Nodes, Trias,Quads= 1551 2878 0 AFLR4 : Nodes, Trias,Quads= 1231 2238 0 AFLR4 : Generate optimal mesh on surface definition 35 AFLR2 : Nodes, Trias,Quads= 1791 3350 0 AFLR4 : Nodes, Trias,Quads= 1414 2596 0 AFLR4 : Generate optimal mesh on surface definition 36 AFLR2 : Nodes, Trias,Quads= 1643 2944 0 AFLR4 : Nodes, Trias,Quads= 3170 5998 0 AFLR4 : Generate optimal mesh on surface definition 37 AFLR2 : Nodes, Trias,Quads= 2194 4132 0 AFLR4 : Nodes, Trias,Quads= 2357 4458 0 AFLR4 : Generate optimal mesh on surface definition 38 AFLR2 : Nodes, Trias,Quads= 3014 5761 0 AFLR4 : Nodes, Trias,Quads= 2581 4895 0 AFLR4 : Generate optimal mesh on surface definition 39 AFLR2 : Nodes, Trias,Quads= 2124 3993 0 AFLR4 : Nodes, Trias,Quads= 1733 3211 0 AFLR4 : Generate optimal mesh on surface definition 40 AFLR2 : Nodes, Trias,Quads= 1090 1960 0 AFLR4 : Nodes, Trias,Quads= 2713 5206 0 AFLR4 : Generate optimal mesh on surface definition 41 AFLR2 : Nodes, Trias,Quads= 60 81 0 AFLR4 : Nodes, Trias,Quads= 37 35 0 AFLR4 : Generate optimal mesh on surface definition 42 AFLR2 : Nodes, Trias,Quads= 37 47 0 AFLR4 : Nodes, Trias,Quads= 25 23 0 AFLR4 : Generate optimal mesh on surface definition 43 AFLR2 : Nodes, Trias,Quads= 15 18 0 AFLR4 : Nodes, Trias,Quads= 16 20 0 AFLR4 : Generate optimal mesh on surface definition 44 AFLR2 : Nodes, Trias,Quads= 71 100 0 AFLR4 : Nodes, Trias,Quads= 40 38 0 AFLR4 : Generate optimal mesh on surface definition 45 AFLR2 : Nodes, Trias,Quads= 48 63 0 AFLR4 : Nodes, Trias,Quads= 51 69 0 AFLR4 : Generate optimal mesh on surface definition 46 AFLR2 : Nodes, Trias,Quads= 57 75 0 AFLR4 : Nodes, Trias,Quads= 62 85 0 AFLR4 : Generate optimal mesh on surface definition 47 AFLR2 : Nodes, Trias,Quads= 85 111 0 AFLR4 : Nodes, Trias,Quads= 57 55 0 AFLR4 : Generate optimal mesh on surface definition 48 AFLR2 : Nodes, Trias,Quads= 15 18 0 AFLR4 : Nodes, Trias,Quads= 15 18 0 AFLR4 : Generate optimal mesh on surface definition 49 AFLR2 : Nodes, Trias,Quads= 3046 5824 0 AFLR4 : Nodes, Trias,Quads= 2604 4940 0 AFLR4 : Generate optimal mesh on surface definition 50 AFLR2 : Nodes, Trias,Quads= 2207 4159 0 AFLR4 : Nodes, Trias,Quads= 2346 4437 0 AFLR4 : Generate optimal mesh on surface definition 51 AFLR2 : Nodes, Trias,Quads= 53 77 0 AFLR4 : Nodes, Trias,Quads= 41 53 0 AFLR4 : Generate optimal mesh on surface definition 52 AFLR2 : Nodes, Trias,Quads= 121 160 0 AFLR4 : Nodes, Trias,Quads= 99 116 0 AFLR4 : Generate optimal mesh on surface definition 53 AFLR2 : Nodes, Trias,Quads= 55 80 0 AFLR4 : Nodes, Trias,Quads= 44 58 0 AFLR4 : Generate optimal mesh on surface definition 54 AFLR2 : Nodes, Trias,Quads= 4380 8388 0 AFLR4 : Nodes, Trias,Quads= 2756 5140 0 AFLR4 : Generate optimal mesh on surface definition 55 AFLR2 : Nodes, Trias,Quads= 3999 7641 0 AFLR4 : Nodes, Trias,Quads= 2398 4439 0 AFLR4 : Generate optimal mesh on surface definition 56 AFLR2 : Nodes, Trias,Quads= 78 120 0 AFLR4 : Nodes, Trias,Quads= 51 66 0 AFLR4 : Generate optimal mesh on surface definition 57 AFLR2 : Nodes, Trias,Quads= 164 223 0 AFLR4 : Nodes, Trias,Quads= 162 219 0 AFLR4 : Generate optimal mesh on surface definition 58 AFLR2 : Nodes, Trias,Quads= 73 112 0 AFLR4 : Nodes, Trias,Quads= 48 62 0 AFLR4 : Generate optimal mesh on surface definition 59 AFLR2 : Nodes, Trias,Quads= 175 291 0 AFLR4 : Nodes, Trias,Quads= 161 263 0 AFLR4 : Generate optimal mesh on surface definition 60 AFLR2 : Nodes, Trias,Quads= 260 448 0 AFLR4 : Nodes, Trias,Quads= 208 344 0 AFLR4 : Generate optimal mesh on surface definition 61 AFLR2 : Nodes, Trias,Quads= 4125 7885 0 AFLR4 : Nodes, Trias,Quads= 2506 4647 0 AFLR4 : Generate optimal mesh on surface definition 62 AFLR2 : Nodes, Trias,Quads= 78 120 0 AFLR4 : Nodes, Trias,Quads= 51 66 0 AFLR4 : Generate optimal mesh on surface definition 63 AFLR2 : Nodes, Trias,Quads= 175 244 0 AFLR4 : Nodes, Trias,Quads= 163 220 0 AFLR4 : Generate optimal mesh on surface definition 64 AFLR2 : Nodes, Trias,Quads= 73 112 0 AFLR4 : Nodes, Trias,Quads= 48 62 0 AFLR4 : Generate optimal mesh on surface definition 65 AFLR2 : Nodes, Trias,Quads= 53 77 0 AFLR4 : Nodes, Trias,Quads= 41 53 0 AFLR4 : Generate optimal mesh on surface definition 66 AFLR2 : Nodes, Trias,Quads= 124 169 0 AFLR4 : Nodes, Trias,Quads= 111 143 0 AFLR4 : Generate optimal mesh on surface definition 67 AFLR2 : Nodes, Trias,Quads= 56 82 0 AFLR4 : Nodes, Trias,Quads= 43 56 0 AFLR4 : Generate optimal mesh on surface definition 68 AFLR2 : Nodes, Trias,Quads= 4113 7862 0 AFLR4 : Nodes, Trias,Quads= 2649 4934 0 AFLR4 : Generate optimal mesh on surface definition 69 AFLR2 : Nodes, Trias,Quads= 300 515 0 AFLR4 : Nodes, Trias,Quads= 283 481 0 AFLR4 : Generate optimal mesh on surface definition 70 AFLR2 : Nodes, Trias,Quads= 57 78 0 AFLR4 : Nodes, Trias,Quads= 55 74 0 AFLR4 : Generate optimal mesh on surface definition 71 AFLR2 : Nodes, Trias,Quads= 135 188 0 AFLR4 : Nodes, Trias,Quads= 87 92 0 AFLR4 : Generate optimal mesh on surface definition 72 AFLR2 : Nodes, Trias,Quads= 33 42 0 AFLR4 : Nodes, Trias,Quads= 36 48 0 AFLR4 : Generate optimal mesh on surface definition 73 AFLR2 : Nodes, Trias,Quads= 43 55 0 AFLR4 : Nodes, Trias,Quads= 44 57 0 AFLR4 : Generate optimal mesh on surface definition 74 AFLR2 : Nodes, Trias,Quads= 186 257 0 AFLR4 : Nodes, Trias,Quads= 180 245 0 AFLR4 : Generate optimal mesh on surface definition 75 AFLR2 : Nodes, Trias,Quads= 31 39 0 AFLR4 : Nodes, Trias,Quads= 31 39 0 AFLR4 : Generate optimal mesh on surface definition 76 AFLR2 : Nodes, Trias,Quads= 39 53 0 AFLR4 : Nodes, Trias,Quads= 23 21 0 AFLR4 : Generate optimal mesh on surface definition 77 AFLR2 : Nodes, Trias,Quads= 32 40 0 AFLR4 : Nodes, Trias,Quads= 32 40 0 AFLR4 : Generate optimal mesh on surface definition 78 AFLR2 : Nodes, Trias,Quads= 169 238 0 AFLR4 : Nodes, Trias,Quads= 101 102 0 AFLR4 : Generate optimal mesh on surface definition 79 AFLR2 : Nodes, Trias,Quads= 34 44 0 AFLR4 : Nodes, Trias,Quads= 36 48 0 AFLR4 : Generate optimal mesh on surface definition 80 AFLR2 : Nodes, Trias,Quads= 33 43 0 AFLR4 : Nodes, Trias,Quads= 36 49 0 AFLR4 : Generate optimal mesh on surface definition 81 AFLR2 : Nodes, Trias,Quads= 132 188 0 AFLR4 : Nodes, Trias,Quads= 79 82 0 AFLR4 : Generate optimal mesh on surface definition 82 AFLR2 : Nodes, Trias,Quads= 40 51 0 AFLR4 : Nodes, Trias,Quads= 45 61 0 AFLR4 : Generate optimal mesh on surface definition 83 AFLR2 : Nodes, Trias,Quads= 402 701 0 AFLR4 : Nodes, Trias,Quads= 405 707 0 AFLR4 : Generate optimal mesh on surface definition 84 AFLR2 : Nodes, Trias,Quads= 39 53 0 AFLR4 : Nodes, Trias,Quads= 23 21 0 AFLR4 : Generate optimal mesh on surface definition 85 AFLR2 : Nodes, Trias,Quads= 32 41 0 AFLR4 : Nodes, Trias,Quads= 31 39 0 AFLR4 : Generate optimal mesh on surface definition 86 AFLR2 : Nodes, Trias,Quads= 186 260 0 AFLR4 : Nodes, Trias,Quads= 140 168 0 AFLR4 : Generate optimal mesh on surface definition 87 AFLR2 : Nodes, Trias,Quads= 42 54 0 AFLR4 : Nodes, Trias,Quads= 48 66 0 AFLR4 : Generate optimal mesh on surface definition 88 AFLR2 : Nodes, Trias,Quads= 34 44 0 AFLR4 : Nodes, Trias,Quads= 37 50 0 AFLR4 : Generate optimal mesh on surface definition 89 AFLR2 : Nodes, Trias,Quads= 132 188 0 AFLR4 : Nodes, Trias,Quads= 79 82 0 AFLR4 : Generate optimal mesh on surface definition 90 AFLR2 : Nodes, Trias,Quads= 40 51 0 AFLR4 : Nodes, Trias,Quads= 45 61 0 AFLR4 : Generate optimal mesh on surface definition 91 AFLR2 : Nodes, Trias,Quads= 401 699 0 AFLR4 : Nodes, Trias,Quads= 404 705 0 AFLR4 : Generate optimal mesh on surface definition 92 AFLR2 : Nodes, Trias,Quads= 293 502 0 AFLR4 : Nodes, Trias,Quads= 277 470 0 AFLR4 : Generate optimal mesh on surface definition 93 AFLR2 : Nodes, Trias,Quads= 57 78 0 AFLR4 : Nodes, Trias,Quads= 55 74 0 AFLR4 : Generate optimal mesh on surface definition 94 AFLR2 : Nodes, Trias,Quads= 135 188 0 AFLR4 : Nodes, Trias,Quads= 87 92 0 AFLR4 : Generate optimal mesh on surface definition 95 AFLR2 : Nodes, Trias,Quads= 32 41 0 AFLR4 : Nodes, Trias,Quads= 35 47 0 AFLR4 : Generate optimal mesh on surface definition 96 AFLR2 : Nodes, Trias,Quads= 34 43 0 AFLR4 : Nodes, Trias,Quads= 36 47 0 AFLR4 : Generate optimal mesh on surface definition 97 AFLR2 : Nodes, Trias,Quads= 175 245 0 AFLR4 : Nodes, Trias,Quads= 139 173 0 AFLR4 : Generate optimal mesh on surface definition 98 AFLR2 : Nodes, Trias,Quads= 32 40 0 AFLR4 : Nodes, Trias,Quads= 32 40 0 AFLR4 : Generate optimal mesh on surface definition 99 AFLR2 : Nodes, Trias,Quads= 303 516 0 AFLR4 : Nodes, Trias,Quads= 258 426 0 AFLR4 : Generate optimal mesh on surface definition 100 AFLR2 : Nodes, Trias,Quads= 380 642 0 AFLR4 : Nodes, Trias,Quads= 285 452 0 AFLR4 : Generate optimal mesh on surface definition 101 AFLR2 : Nodes, Trias,Quads= 334 560 0 AFLR4 : Nodes, Trias,Quads= 242 376 0 AFLR4 : Generate optimal mesh on surface definition 102 AFLR2 : Nodes, Trias,Quads= 271 457 0 AFLR4 : Nodes, Trias,Quads= 222 359 0 AFLR4 : Generate optimal mesh on surface definition 103 AFLR2 : Nodes, Trias,Quads= 369 622 0 AFLR4 : Nodes, Trias,Quads= 275 434 0 AFLR4 : Generate optimal mesh on surface definition 104 AFLR2 : Nodes, Trias,Quads= 272 459 0 AFLR4 : Nodes, Trias,Quads= 220 355 0 AFLR4 : Generate optimal mesh on surface definition 105 AFLR2 : Nodes, Trias,Quads= 303 516 0 AFLR4 : Nodes, Trias,Quads= 258 426 0 AFLR4 : Generate optimal mesh on surface definition 106 AFLR2 : Nodes, Trias,Quads= 353 594 0 AFLR4 : Nodes, Trias,Quads= 266 420 0 AFLR4 : Generate optimal mesh on surface definition 107 AFLR2 : Nodes, Trias,Quads= 72 113 0 AFLR4 : Nodes, Trias,Quads= 47 63 0 AFLR4 : Generate optimal mesh on surface definition 108 AFLR2 : Nodes, Trias,Quads= 70 109 0 AFLR4 : Nodes, Trias,Quads= 49 67 0 AFLR4 : Generate optimal mesh on surface definition 109 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 110 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 111 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 112 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 113 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 114 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 54863 109718 10706 AFLR4 : Proximity BG Surface Grid Generation AFLR4 : Nodes, Trias = 57095 114182 AFLR4 : Nodes, Trias = 57402 114796 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 779 1451 0 AFLR4 : Nodes, Trias,Quads= 643 1179 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 399 711 0 AFLR4 : Nodes, Trias,Quads= 375 663 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 753 1402 0 AFLR4 : Nodes, Trias,Quads= 682 1260 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 357 630 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 773 1439 0 AFLR4 : Nodes, Trias,Quads= 640 1173 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 400 713 0 AFLR4 : Nodes, Trias,Quads= 372 657 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 751 1398 0 AFLR4 : Nodes, Trias,Quads= 681 1258 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 358 632 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 21 27 0 AFLR4 : Nodes, Trias,Quads= 18 21 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 21 27 0 AFLR4 : Nodes, Trias,Quads= 20 25 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 66 90 0 AFLR4 : Nodes, Trias,Quads= 40 38 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 32 43 0 AFLR4 : Nodes, Trias,Quads= 29 37 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 32 43 0 AFLR4 : Nodes, Trias,Quads= 28 35 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 65 89 0 AFLR4 : Nodes, Trias,Quads= 39 37 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 61 80 0 AFLR4 : Nodes, Trias,Quads= 62 82 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 2575 4845 0 AFLR4 : Nodes, Trias,Quads= 2031 3757 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 109 150 0 AFLR4 : Nodes, Trias,Quads= 66 64 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 298 518 0 AFLR4 : Nodes, Trias,Quads= 228 378 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 62 81 0 AFLR4 : Nodes, Trias,Quads= 62 81 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 2647 4991 0 AFLR4 : Nodes, Trias,Quads= 2128 3953 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 39 50 0 AFLR4 : Nodes, Trias,Quads= 26 24 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 19 25 0 AFLR4 : Nodes, Trias,Quads= 19 25 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 2173 4081 0 AFLR4 : Nodes, Trias,Quads= 1920 3575 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 4843 9261 0 AFLR4 : Nodes, Trias,Quads= 3472 6519 0 AFLR4 : Generate optimal mesh on surface definition 25 AFLR2 : Nodes, Trias,Quads= 310 540 0 AFLR4 : Nodes, Trias,Quads= 242 404 0 AFLR4 : Generate optimal mesh on surface definition 26 AFLR2 : Nodes, Trias,Quads= 106 145 0 AFLR4 : Nodes, Trias,Quads= 65 63 0 AFLR4 : Generate optimal mesh on surface definition 27 AFLR2 : Nodes, Trias,Quads= 18 22 0 AFLR4 : Nodes, Trias,Quads= 19 24 0 AFLR4 : Generate optimal mesh on surface definition 28 AFLR2 : Nodes, Trias,Quads= 2233 4200 0 AFLR4 : Nodes, Trias,Quads= 1939 3612 0 AFLR4 : Generate optimal mesh on surface definition 29 AFLR2 : Nodes, Trias,Quads= 106 170 0 AFLR4 : Nodes, Trias,Quads= 120 198 0 AFLR4 : Generate optimal mesh on surface definition 30 AFLR2 : Nodes, Trias,Quads= 3806 7035 0 AFLR4 : Nodes, Trias,Quads= 4864 9151 0 AFLR4 : Generate optimal mesh on surface definition 31 AFLR2 : Nodes, Trias,Quads= 4917 9413 0 AFLR4 : Nodes, Trias,Quads= 3455 6489 0 AFLR4 : Generate optimal mesh on surface definition 32 AFLR2 : Nodes, Trias,Quads= 2589 4890 0 AFLR4 : Nodes, Trias,Quads= 1963 3638 0 AFLR4 : Generate optimal mesh on surface definition 33 AFLR2 : Nodes, Trias,Quads= 2220 4140 0 AFLR4 : Nodes, Trias,Quads= 2591 4882 0 AFLR4 : Generate optimal mesh on surface definition 34 AFLR2 : Nodes, Trias,Quads= 2344 4396 0 AFLR4 : Nodes, Trias,Quads= 1845 3398 0 AFLR4 : Generate optimal mesh on surface definition 35 AFLR2 : Nodes, Trias,Quads= 2659 5015 0 AFLR4 : Nodes, Trias,Quads= 2130 3957 0 AFLR4 : Generate optimal mesh on surface definition 36 AFLR2 : Nodes, Trias,Quads= 3827 7075 0 AFLR4 : Nodes, Trias,Quads= 4860 9141 0 AFLR4 : Generate optimal mesh on surface definition 37 AFLR2 : Nodes, Trias,Quads= 5597 10778 0 AFLR4 : Nodes, Trias,Quads= 3975 7534 0 AFLR4 : Generate optimal mesh on surface definition 38 AFLR2 : Nodes, Trias,Quads= 3935 7561 0 AFLR4 : Nodes, Trias,Quads= 2905 5501 0 AFLR4 : Generate optimal mesh on surface definition 39 AFLR2 : Nodes, Trias,Quads= 2618 4948 0 AFLR4 : Nodes, Trias,Quads= 2017 3746 0 AFLR4 : Generate optimal mesh on surface definition 40 AFLR2 : Nodes, Trias,Quads= 2224 4148 0 AFLR4 : Nodes, Trias,Quads= 2603 4906 0 AFLR4 : Generate optimal mesh on surface definition 41 AFLR2 : Nodes, Trias,Quads= 62 83 0 AFLR4 : Nodes, Trias,Quads= 39 37 0 AFLR4 : Generate optimal mesh on surface definition 42 AFLR2 : Nodes, Trias,Quads= 39 50 0 AFLR4 : Nodes, Trias,Quads= 26 24 0 AFLR4 : Generate optimal mesh on surface definition 43 AFLR2 : Nodes, Trias,Quads= 18 22 0 AFLR4 : Nodes, Trias,Quads= 19 24 0 AFLR4 : Generate optimal mesh on surface definition 44 AFLR2 : Nodes, Trias,Quads= 86 119 0 AFLR4 : Nodes, Trias,Quads= 51 49 0 AFLR4 : Generate optimal mesh on surface definition 45 AFLR2 : Nodes, Trias,Quads= 54 71 0 AFLR4 : Nodes, Trias,Quads= 58 79 0 AFLR4 : Generate optimal mesh on surface definition 46 AFLR2 : Nodes, Trias,Quads= 61 80 0 AFLR4 : Nodes, Trias,Quads= 62 82 0 AFLR4 : Generate optimal mesh on surface definition 47 AFLR2 : Nodes, Trias,Quads= 106 145 0 AFLR4 : Nodes, Trias,Quads= 65 63 0 AFLR4 : Generate optimal mesh on surface definition 48 AFLR2 : Nodes, Trias,Quads= 18 22 0 AFLR4 : Nodes, Trias,Quads= 19 24 0 AFLR4 : Generate optimal mesh on surface definition 49 AFLR2 : Nodes, Trias,Quads= 3946 7581 0 AFLR4 : Nodes, Trias,Quads= 2941 5571 0 AFLR4 : Generate optimal mesh on surface definition 50 AFLR2 : Nodes, Trias,Quads= 5413 10408 0 AFLR4 : Nodes, Trias,Quads= 3958 7498 0 AFLR4 : Generate optimal mesh on surface definition 51 AFLR2 : Nodes, Trias,Quads= 62 92 0 AFLR4 : Nodes, Trias,Quads= 45 58 0 AFLR4 : Generate optimal mesh on surface definition 52 AFLR2 : Nodes, Trias,Quads= 127 168 0 AFLR4 : Nodes, Trias,Quads= 120 154 0 AFLR4 : Generate optimal mesh on surface definition 53 AFLR2 : Nodes, Trias,Quads= 58 85 0 AFLR4 : Nodes, Trias,Quads= 44 57 0 AFLR4 : Generate optimal mesh on surface definition 54 AFLR2 : Nodes, Trias,Quads= 5057 9716 0 AFLR4 : Nodes, Trias,Quads= 2994 5590 0 AFLR4 : Generate optimal mesh on surface definition 55 AFLR2 : Nodes, Trias,Quads= 4633 8888 0 AFLR4 : Nodes, Trias,Quads= 2620 4862 0 AFLR4 : Generate optimal mesh on surface definition 56 AFLR2 : Nodes, Trias,Quads= 88 138 0 AFLR4 : Nodes, Trias,Quads= 54 70 0 AFLR4 : Generate optimal mesh on surface definition 57 AFLR2 : Nodes, Trias,Quads= 198 270 0 AFLR4 : Nodes, Trias,Quads= 204 282 0 AFLR4 : Generate optimal mesh on surface definition 58 AFLR2 : Nodes, Trias,Quads= 76 117 0 AFLR4 : Nodes, Trias,Quads= 49 63 0 AFLR4 : Generate optimal mesh on surface definition 59 AFLR2 : Nodes, Trias,Quads= 234 399 0 AFLR4 : Nodes, Trias,Quads= 188 307 0 AFLR4 : Generate optimal mesh on surface definition 60 AFLR2 : Nodes, Trias,Quads= 294 509 0 AFLR4 : Nodes, Trias,Quads= 234 389 0 AFLR4 : Generate optimal mesh on surface definition 61 AFLR2 : Nodes, Trias,Quads= 4681 8974 0 AFLR4 : Nodes, Trias,Quads= 2722 5056 0 AFLR4 : Generate optimal mesh on surface definition 62 AFLR2 : Nodes, Trias,Quads= 87 136 0 AFLR4 : Nodes, Trias,Quads= 54 70 0 AFLR4 : Generate optimal mesh on surface definition 63 AFLR2 : Nodes, Trias,Quads= 205 284 0 AFLR4 : Nodes, Trias,Quads= 195 264 0 AFLR4 : Generate optimal mesh on surface definition 64 AFLR2 : Nodes, Trias,Quads= 76 117 0 AFLR4 : Nodes, Trias,Quads= 50 65 0 AFLR4 : Generate optimal mesh on surface definition 65 AFLR2 : Nodes, Trias,Quads= 62 92 0 AFLR4 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Generate optimal mesh on surface definition 66 AFLR2 : Nodes, Trias,Quads= 138 190 0 AFLR4 : Nodes, Trias,Quads= 127 168 0 AFLR4 : Generate optimal mesh on surface definition 67 AFLR2 : Nodes, Trias,Quads= 62 92 0 AFLR4 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Generate optimal mesh on surface definition 68 AFLR2 : Nodes, Trias,Quads= 4678 8970 0 AFLR4 : Nodes, Trias,Quads= 2893 5400 0 AFLR4 : Generate optimal mesh on surface definition 69 AFLR2 : Nodes, Trias,Quads= 350 608 0 AFLR4 : Nodes, Trias,Quads= 324 556 0 AFLR4 : Generate optimal mesh on surface definition 70 AFLR2 : Nodes, Trias,Quads= 70 101 0 AFLR4 : Nodes, Trias,Quads= 62 85 0 AFLR4 : Generate optimal mesh on surface definition 71 AFLR2 : Nodes, Trias,Quads= 149 207 0 AFLR4 : Nodes, Trias,Quads= 95 99 0 AFLR4 : Generate optimal mesh on surface definition 72 AFLR2 : Nodes, Trias,Quads= 36 46 0 AFLR4 : Nodes, Trias,Quads= 38 50 0 AFLR4 : Generate optimal mesh on surface definition 73 AFLR2 : Nodes, Trias,Quads= 50 67 0 AFLR4 : Nodes, Trias,Quads= 48 63 0 AFLR4 : Generate optimal mesh on surface definition 74 AFLR2 : Nodes, Trias,Quads= 220 305 0 AFLR4 : Nodes, Trias,Quads= 209 283 0 AFLR4 : Generate optimal mesh on surface definition 75 AFLR2 : Nodes, Trias,Quads= 31 39 0 AFLR4 : Nodes, Trias,Quads= 31 39 0 AFLR4 : Generate optimal mesh on surface definition 76 AFLR2 : Nodes, Trias,Quads= 39 50 0 AFLR4 : Nodes, Trias,Quads= 26 24 0 AFLR4 : Generate optimal mesh on surface definition 77 AFLR2 : Nodes, Trias,Quads= 32 40 0 AFLR4 : Nodes, Trias,Quads= 33 42 0 AFLR4 : Generate optimal mesh on surface definition 78 AFLR2 : Nodes, Trias,Quads= 196 279 0 AFLR4 : Nodes, Trias,Quads= 113 113 0 AFLR4 : Generate optimal mesh on surface definition 79 AFLR2 : Nodes, Trias,Quads= 35 45 0 AFLR4 : Nodes, Trias,Quads= 38 51 0 AFLR4 : Generate optimal mesh on surface definition 80 AFLR2 : Nodes, Trias,Quads= 36 46 0 AFLR4 : Nodes, Trias,Quads= 36 46 0 AFLR4 : Generate optimal mesh on surface definition 81 AFLR2 : Nodes, Trias,Quads= 157 225 0 AFLR4 : Nodes, Trias,Quads= 95 101 0 AFLR4 : Generate optimal mesh on surface definition 82 AFLR2 : Nodes, Trias,Quads= 47 63 0 AFLR4 : Nodes, Trias,Quads= 46 61 0 AFLR4 : Generate optimal mesh on surface definition 83 AFLR2 : Nodes, Trias,Quads= 520 923 0 AFLR4 : Nodes, Trias,Quads= 508 899 0 AFLR4 : Generate optimal mesh on surface definition 84 AFLR2 : Nodes, Trias,Quads= 39 50 0 AFLR4 : Nodes, Trias,Quads= 26 24 0 AFLR4 : Generate optimal mesh on surface definition 85 AFLR2 : Nodes, Trias,Quads= 32 41 0 AFLR4 : Nodes, Trias,Quads= 31 39 0 AFLR4 : Generate optimal mesh on surface definition 86 AFLR2 : Nodes, Trias,Quads= 199 273 0 AFLR4 : Nodes, Trias,Quads= 152 179 0 AFLR4 : Generate optimal mesh on surface definition 87 AFLR2 : Nodes, Trias,Quads= 51 69 0 AFLR4 : Nodes, Trias,Quads= 48 63 0 AFLR4 : Generate optimal mesh on surface definition 88 AFLR2 : Nodes, Trias,Quads= 37 47 0 AFLR4 : Nodes, Trias,Quads= 41 55 0 AFLR4 : Generate optimal mesh on surface definition 89 AFLR2 : Nodes, Trias,Quads= 159 229 0 AFLR4 : Nodes, Trias,Quads= 95 101 0 AFLR4 : Generate optimal mesh on surface definition 90 AFLR2 : Nodes, Trias,Quads= 46 61 0 AFLR4 : Nodes, Trias,Quads= 46 61 0 AFLR4 : Generate optimal mesh on surface definition 91 AFLR2 : Nodes, Trias,Quads= 516 915 0 AFLR4 : Nodes, Trias,Quads= 504 891 0 AFLR4 : Generate optimal mesh on surface definition 92 AFLR2 : Nodes, Trias,Quads= 354 616 0 AFLR4 : Nodes, Trias,Quads= 320 548 0 AFLR4 : Generate optimal mesh on surface definition 93 AFLR2 : Nodes, Trias,Quads= 70 101 0 AFLR4 : Nodes, Trias,Quads= 62 85 0 AFLR4 : Generate optimal mesh on surface definition 94 AFLR2 : Nodes, Trias,Quads= 140 190 0 AFLR4 : Nodes, Trias,Quads= 96 102 0 AFLR4 : Generate optimal mesh on surface definition 95 AFLR2 : Nodes, Trias,Quads= 34 44 0 AFLR4 : Nodes, Trias,Quads= 35 46 0 AFLR4 : Generate optimal mesh on surface definition 96 AFLR2 : Nodes, Trias,Quads= 36 47 0 AFLR4 : Nodes, Trias,Quads= 37 49 0 AFLR4 : Generate optimal mesh on surface definition 97 AFLR2 : Nodes, Trias,Quads= 204 286 0 AFLR4 : Nodes, Trias,Quads= 165 208 0 AFLR4 : Generate optimal mesh on surface definition 98 AFLR2 : Nodes, Trias,Quads= 32 40 0 AFLR4 : Nodes, Trias,Quads= 34 44 0 AFLR4 : Generate optimal mesh on surface definition 99 AFLR2 : Nodes, Trias,Quads= 344 591 0 AFLR4 : Nodes, Trias,Quads= 292 487 0 AFLR4 : Generate optimal mesh on surface definition 100 AFLR2 : Nodes, Trias,Quads= 442 755 0 AFLR4 : Nodes, Trias,Quads= 340 551 0 AFLR4 : Generate optimal mesh on surface definition 101 AFLR2 : Nodes, Trias,Quads= 377 638 0 AFLR4 : Nodes, Trias,Quads= 268 420 0 AFLR4 : Generate optimal mesh on surface definition 102 AFLR2 : Nodes, Trias,Quads= 327 559 0 AFLR4 : Nodes, Trias,Quads= 273 451 0 AFLR4 : Generate optimal mesh on surface definition 103 AFLR2 : Nodes, Trias,Quads= 419 714 0 AFLR4 : Nodes, Trias,Quads= 304 484 0 AFLR4 : Generate optimal mesh on surface definition 104 AFLR2 : Nodes, Trias,Quads= 326 557 0 AFLR4 : Nodes, Trias,Quads= 271 447 0 AFLR4 : Generate optimal mesh on surface definition 105 AFLR2 : Nodes, Trias,Quads= 345 593 0 AFLR4 : Nodes, Trias,Quads= 292 487 0 AFLR4 : Generate optimal mesh on surface definition 106 AFLR2 : Nodes, Trias,Quads= 409 698 0 AFLR4 : Nodes, Trias,Quads= 301 482 0 AFLR4 : Generate optimal mesh on surface definition 107 AFLR2 : Nodes, Trias,Quads= 89 141 0 AFLR4 : Nodes, Trias,Quads= 66 95 0 AFLR4 : Generate optimal mesh on surface definition 108 AFLR2 : Nodes, Trias,Quads= 94 150 0 AFLR4 : Nodes, Trias,Quads= 67 96 0 AFLR4 : Generate optimal mesh on surface definition 109 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 110 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 111 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 112 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 113 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 114 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 69412 138816 13136 OVERALL : CPU Time = 5.036 seconds Body 1 (of 4) Number of nodes = 1866 Number of elements = 3732 Number of triangle elements = 3732 Number of quadrilateral elements = 0 Body 2 (of 4) Number of nodes = 1860 Number of elements = 3720 Number of triangle elements = 3720 Number of quadrilateral elements = 0 Body 3 (of 4) Number of nodes = 65366 Number of elements = 130728 Number of triangle elements = 130728 Number of quadrilateral elements = 0 Body 4 (of 4) Number of nodes = 320 Number of elements = 636 Number of triangle elements = 636 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 69412 Total number of elements = 138816 Total number of triangle elements = 138816 Total number of quadrilateral elements = 0 real 0m45.716s user 0m49.133s sys 0m15.128s + status=0 + set +x ================================================= data/session07/08_aflr4_InviscidTransport.py passed (as expected) ================================================= ================================================= 09_aflr4_aflr3_InviscidWing.py test; + python 09_aflr4_aflr3_InviscidWing.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml MESSAGE:: Building nacelleOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Nacelle, index = 1 Name = Wing, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Nacelle, index = 1 Name = leftWing, index = 2 Name = riteWing, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - leftWing Mesh sizing name - riteWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 4 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 4 Faces EGADS : Body 0 has 8 Edges EGADS : Body 0 has 4 Loops EGADS : Body 0 has 4 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 4 Faces EGADS : Body 1 has 8 Edges EGADS : Body 1 has 4 Loops EGADS : Body 1 has 4 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 10 Faces EGADS : Body 2 has 18 Edges EGADS : Body 2 has 10 Loops EGADS : Body 2 has 10 Nodes EGADS : Body 3 is a SolidBody EGADS : Body 3 has 1 Shells EGADS : Body 3 has 6 Faces EGADS : Body 3 has 12 Edges EGADS : Body 3 has 6 Loops EGADS : Body 3 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 EGADS : 2 Yes 0 0 1 0 1 1 4 EGADS : 3 Yes 0 0 1 0 1 1 4 EGADS : 4 Yes 0 0 1 0 1 2 3 EGADS : 5 Yes 1 0 1 0 1 6 7 EGADS : 6 Yes 1 0 1 0 1 5 8 EGADS : 7 Yes 1 0 1 0 1 5 8 EGADS : 8 Yes 1 0 1 0 1 6 7 EGADS : 9 Yes 2 0 1 1 1 10 11 14 EGADS : 10 Yes 2 0 1 1 1 9 12 13 EGADS : 11 Yes 2 0 1 1 1 9 12 16 EGADS : 12 Yes 2 0 1 1 1 10 11 13 EGADS : 13 Yes 2 0 1 1 1 10 12 EGADS : 14 Yes 2 0 1 1 1 9 15 16 EGADS : 15 Yes 2 0 1 1 1 14 17 18 EGADS : 16 Yes 2 0 1 1 1 11 14 17 EGADS : 17 Yes 2 0 1 1 1 15 16 18 EGADS : 18 Yes 2 0 1 1 1 15 17 EGADS : 19 Yes 3 0 1 NA NA 21 22 23 24 EGADS : 20 Yes 3 0 1 NA NA 21 22 23 24 EGADS : 21 Yes 3 0 1 NA NA 19 20 23 24 EGADS : 22 Yes 3 0 1 NA NA 19 20 23 24 EGADS : 23 Yes 3 0 1 NA NA 19 20 21 22 EGADS : 24 Yes 3 0 1 NA NA 19 20 21 22 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 3 2 -4 EGADS : 2 -2 5 1 -6 EGADS : 3 7 4 -8 -3 EGADS : 4 8 6 -7 -5 EGADS : 5 9 12 -10 -11 EGADS : 6 10 14 -9 -13 EGADS : 7 -15 11 16 -12 EGADS : 8 -16 13 15 -14 EGADS : 9 -17 18 19 -20 EGADS : 10 -21 20 22 -23 EGADS : 11 -19 24 17 -25 EGADS : 12 -22 25 21 -26 EGADS : 13 23 26 EGADS : 14 27 29 -28 -18 EGADS : 15 30 32 -31 -29 EGADS : 16 28 33 -27 -24 EGADS : 17 31 34 -30 -33 EGADS : 18 -32 -34 EGADS : 19 35 36 -37 -38 EGADS : 20 -39 42 41 -40 EGADS : 21 43 39 -44 -35 EGADS : 22 -45 37 46 -41 EGADS : 23 38 45 -42 -43 EGADS : 24 -36 44 40 -46 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : 19 19 EGADS : 20 20 EGADS : 21 21 EGADS : 22 22 EGADS : 23 23 EGADS : 24 24 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 3 2 -4 EGADS : 2 Yes -2 5 1 -6 EGADS : 3 Yes 7 4 -8 -3 EGADS : 4 Yes 8 6 -7 -5 EGADS : 5 Yes 9 12 -10 -11 EGADS : 6 Yes 10 14 -9 -13 EGADS : 7 Yes -15 11 16 -12 EGADS : 8 Yes -16 13 15 -14 EGADS : 9 Yes -17 18 19 -20 EGADS : 10 Yes -21 20 22 -23 EGADS : 11 Yes -19 24 17 -25 EGADS : 12 Yes -22 25 21 -26 EGADS : 13 Yes 23 26 EGADS : 14 Yes 27 29 -28 -18 EGADS : 15 Yes 30 32 -31 -29 EGADS : 16 Yes 28 33 -27 -24 EGADS : 17 Yes 31 34 -30 -33 EGADS : 18 Yes -32 -34 EGADS : 19 Yes 35 36 -37 -38 EGADS : 20 Yes -39 42 41 -40 EGADS : 21 Yes 43 39 -44 -35 EGADS : 22 Yes -45 37 46 -41 EGADS : 23 Yes 38 45 -42 -43 EGADS : 24 Yes -36 44 40 -46 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 2 EGADS : 2 0 Yes 3 4 1 1 2 EGADS : 3 0 Yes 1 3 1 1 3 EGADS : 4 0 Yes 2 4 1 1 3 EGADS : 5 0 Yes 3 1 1 2 4 EGADS : 6 0 Yes 4 2 1 2 4 EGADS : 7 0 Yes 1 2 1 3 4 EGADS : 8 0 Yes 3 4 1 3 4 EGADS : 9 1 Yes 5 6 1 5 6 EGADS : 10 1 Yes 7 8 1 5 6 EGADS : 11 1 Yes 5 7 1 5 7 EGADS : 12 1 Yes 6 8 1 5 7 EGADS : 13 1 Yes 7 5 1 6 8 EGADS : 14 1 Yes 8 6 1 6 8 EGADS : 15 1 Yes 5 6 1 7 8 EGADS : 16 1 Yes 7 8 1 7 8 EGADS : 17 2 Yes 9 10 1 9 11 EGADS : 18 2 Yes 9 11 1 9 14 EGADS : 19 2 Yes 11 12 1 9 11 EGADS : 20 2 Yes 10 12 1 9 10 EGADS : 21 2 Yes 10 13 1 10 12 EGADS : 22 2 Yes 12 14 1 10 12 EGADS : 23 2 Yes 13 14 1 10 13 EGADS : 24 2 Yes 11 9 1 11 16 EGADS : 25 2 Yes 12 10 1 11 12 EGADS : 26 2 Yes 14 13 1 12 13 EGADS : 27 2 Yes 9 15 1 14 16 EGADS : 28 2 Yes 11 16 1 14 16 EGADS : 29 2 Yes 15 16 1 14 15 EGADS : 30 2 Yes 15 17 1 15 17 EGADS : 31 2 Yes 16 18 1 15 17 EGADS : 32 2 Yes 17 18 1 15 18 EGADS : 33 2 Yes 16 15 1 16 17 EGADS : 34 2 Yes 18 17 1 17 18 EGADS : 35 3 Yes 20 19 NA 19 21 EGADS : 36 3 Yes 19 21 NA 19 24 EGADS : 37 3 Yes 22 21 NA 19 22 EGADS : 38 3 Yes 20 22 NA 19 23 EGADS : 39 3 Yes 24 23 NA 20 21 EGADS : 40 3 Yes 23 25 NA 20 24 EGADS : 41 3 Yes 26 25 NA 20 22 EGADS : 42 3 Yes 24 26 NA 20 23 EGADS : 43 3 Yes 20 24 NA 21 23 EGADS : 44 3 Yes 19 23 NA 21 24 EGADS : 45 3 Yes 22 26 NA 22 23 EGADS : 46 3 Yes 21 25 NA 22 24 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 90.5173952 0 0 EGADS : 2 Yes 90.5173952 0 0 EGADS : 3 Yes 60.5173952 0 0 EGADS : 4 Yes 60.5173952 0 0 EGADS : 5 Yes 90.5173952 29.3018771 0 EGADS : 6 Yes 90.5173952 29.3018771 0 EGADS : 7 Yes 60.5173952 29.3018771 0 EGADS : 8 Yes 60.5173952 29.3018771 0 EGADS : 9 Yes 97.2007855 0 0 EGADS : 10 Yes 97.9335611 0 0 EGADS : 11 Yes 50 0 0 EGADS : 12 Yes 75.3047874 0 0 EGADS : 13 Yes 123.552357 0 4.7180639 EGADS : 14 Yes 118.391317 0 3.99272703 EGADS : 15 Yes 97.9335611 36.1389817 0 EGADS : 16 Yes 75.3047874 36.1389817 0 EGADS : 17 Yes 123.552357 97.6729236 4.7180639 EGADS : 18 Yes 118.391317 97.6729236 3.99272703 EGADS : 19 Yes 0 0 1947.05079 EGADS : 20 Yes 0 0 0 EGADS : 21 Yes 0 1953.45847 1947.05079 EGADS : 22 Yes 0 1953.45847 0 EGADS : 23 Yes 2040.21562 0 1947.05079 EGADS : 24 Yes 2040.21562 0 0 EGADS : 25 Yes 2040.21562 1953.45847 1947.05079 EGADS : 26 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 22.2515 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 2651.51 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 5 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : 15 CAD geometry 0 STD w/BL AFLR4 : 16 CAD geometry 0 STD w/BL AFLR4 : 17 CAD geometry 0 STD w/BL AFLR4 : 18 CAD geometry 0 STD w/BL AFLR4 : 19 CAD geometry 0 FARFIELD AFLR4 : 20 CAD geometry 0 FARFIELD AFLR4 : 21 CAD geometry 0 FARFIELD AFLR4 : 22 CAD geometry 0 FARFIELD AFLR4 : 23 CAD geometry 0 FARFIELD AFLR4 : 24 CAD geometry 0 FARFIELD AFLR4 : Case has 2 Proximity Checking Components AFLR4 : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18 AFLR4 : Component 2 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR4 : Define CAD surface definition 19 AFLR4 : Define CAD surface definition 20 AFLR4 : Define CAD surface definition 21 AFLR4 : Define CAD surface definition 22 AFLR4 : Define CAD surface definition 23 AFLR4 : Define CAD surface definition 24 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 339 605 0 AFLR4 : Nodes, Trias,Quads= 362 651 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 319 563 0 AFLR4 : Nodes, Trias,Quads= 284 493 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 340 607 0 AFLR4 : Nodes, Trias,Quads= 362 651 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 321 567 0 AFLR4 : Nodes, Trias,Quads= 284 493 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 340 607 0 AFLR4 : Nodes, Trias,Quads= 362 651 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 321 567 0 AFLR4 : Nodes, Trias,Quads= 284 493 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 339 605 0 AFLR4 : Nodes, Trias,Quads= 362 651 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 319 563 0 AFLR4 : Nodes, Trias,Quads= 284 493 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 1107 2082 0 AFLR4 : Nodes, Trias,Quads= 685 1238 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 1473 2759 0 AFLR4 : Nodes, Trias,Quads= 721 1255 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 1116 2100 0 AFLR4 : Nodes, Trias,Quads= 671 1210 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 1458 2729 0 AFLR4 : Nodes, Trias,Quads= 714 1241 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 20 24 0 AFLR4 : Nodes, Trias,Quads= 14 12 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 1108 2084 0 AFLR4 : Nodes, Trias,Quads= 683 1234 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 1488 2789 0 AFLR4 : Nodes, Trias,Quads= 714 1241 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 1112 2092 0 AFLR4 : Nodes, Trias,Quads= 653 1174 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 1456 2725 0 AFLR4 : Nodes, Trias,Quads= 708 1229 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 20 24 0 AFLR4 : Nodes, Trias,Quads= 14 12 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 7221 14434 1888 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 7221 14434 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 397 713 0 AFLR4 : Nodes, Trias,Quads= 416 751 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 387 691 0 AFLR4 : Nodes, Trias,Quads= 346 609 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 396 711 0 AFLR4 : Nodes, Trias,Quads= 417 753 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 388 693 0 AFLR4 : Nodes, Trias,Quads= 344 605 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 395 709 0 AFLR4 : Nodes, Trias,Quads= 416 751 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 388 693 0 AFLR4 : Nodes, Trias,Quads= 344 605 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 395 709 0 AFLR4 : Nodes, Trias,Quads= 416 751 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 387 691 0 AFLR4 : Nodes, Trias,Quads= 346 609 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 12796 24695 0 AFLR4 : Nodes, Trias,Quads= 7764 14631 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 29251 57087 0 AFLR4 : Nodes, Trias,Quads= 12448 23481 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 12136 23411 0 AFLR4 : Nodes, Trias,Quads= 7447 14033 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 29424 57435 0 AFLR4 : Nodes, Trias,Quads= 12399 23385 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 196 293 0 AFLR4 : Nodes, Trias,Quads= 188 277 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 12819 24741 0 AFLR4 : Nodes, Trias,Quads= 7725 14553 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 29437 57459 0 AFLR4 : Nodes, Trias,Quads= 12412 23409 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 12144 23427 0 AFLR4 : Nodes, Trias,Quads= 7471 14081 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 29445 57477 0 AFLR4 : Nodes, Trias,Quads= 12478 23543 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 196 293 0 AFLR4 : Nodes, Trias,Quads= 188 277 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 78574 157140 10038 AFLR4 : Proximity BG Surface Grid Generation AFLR4 : Nodes, Trias = 78960 157912 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 850 1593 0 AFLR4 : Nodes, Trias,Quads= 754 1401 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 384 685 0 AFLR4 : Nodes, Trias,Quads= 354 625 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 842 1577 0 AFLR4 : Nodes, Trias,Quads= 803 1499 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 384 685 0 AFLR4 : Nodes, Trias,Quads= 351 619 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 837 1566 0 AFLR4 : Nodes, Trias,Quads= 755 1402 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 384 685 0 AFLR4 : Nodes, Trias,Quads= 351 619 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 834 1560 0 AFLR4 : Nodes, Trias,Quads= 806 1504 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 384 685 0 AFLR4 : Nodes, Trias,Quads= 354 625 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 11687 22537 0 AFLR4 : Nodes, Trias,Quads= 9244 17651 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 22265 43205 0 AFLR4 : Nodes, Trias,Quads= 14799 28273 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 11200 21594 0 AFLR4 : Nodes, Trias,Quads= 8943 17080 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 22072 42820 0 AFLR4 : Nodes, Trias,Quads= 14774 28224 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 184 274 0 AFLR4 : Nodes, Trias,Quads= 178 262 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 11697 22557 0 AFLR4 : Nodes, Trias,Quads= 9237 17637 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 22389 43453 0 AFLR4 : Nodes, Trias,Quads= 14717 28109 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 11243 21680 0 AFLR4 : Nodes, Trias,Quads= 8970 17134 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 22230 43136 0 AFLR4 : Nodes, Trias,Quads= 14757 28190 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 184 274 0 AFLR4 : Nodes, Trias,Quads= 178 262 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 23 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 95580 191152 9546 OVERALL : CPU Time = 2.664 seconds Body 1 (of 4) Number of nodes = 2072 Number of elements = 4144 Number of triangle elements = 4144 Number of quadrilateral elements = 0 Body 2 (of 4) Number of nodes = 2075 Number of elements = 4150 Number of triangle elements = 4150 Number of quadrilateral elements = 0 Body 3 (of 4) Number of nodes = 91413 Number of elements = 182822 Number of triangle elements = 182822 Number of quadrilateral elements = 0 Body 4 (of 4) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 95580 Total number of elements = 191152 Total number of triangle elements = 191152 Total number of quadrilateral elements = 0 Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Nacelle 2: Wing 3: Farfield Finished writing vtk file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Nacelle, index = 1 Name = leftWing, index = 2 Name = riteWing, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Nacelle, index = 1 Name = Wing, index = 2 Name = Farfield, index = 3 Getting volume mesh UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 4 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 4 Faces EGADS : Body 0 has 8 Edges EGADS : Body 0 has 4 Loops EGADS : Body 0 has 4 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 4 Faces EGADS : Body 1 has 8 Edges EGADS : Body 1 has 4 Loops EGADS : Body 1 has 4 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 10 Faces EGADS : Body 2 has 18 Edges EGADS : Body 2 has 10 Loops EGADS : Body 2 has 10 Nodes EGADS : Body 3 is a SolidBody EGADS : Body 3 has 1 Shells EGADS : Body 3 has 6 Faces EGADS : Body 3 has 12 Edges EGADS : Body 3 has 6 Loops EGADS : Body 3 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 EGADS : 2 Yes 0 0 1 0 1 1 4 EGADS : 3 Yes 0 0 1 0 1 1 4 EGADS : 4 Yes 0 0 1 0 1 2 3 EGADS : 5 Yes 1 0 1 0 1 6 7 EGADS : 6 Yes 1 0 1 0 1 5 8 EGADS : 7 Yes 1 0 1 0 1 5 8 EGADS : 8 Yes 1 0 1 0 1 6 7 EGADS : 9 Yes 2 0 1 1 1 10 11 14 EGADS : 10 Yes 2 0 1 1 1 9 12 13 EGADS : 11 Yes 2 0 1 1 1 9 12 16 EGADS : 12 Yes 2 0 1 1 1 10 11 13 EGADS : 13 Yes 2 0 1 1 1 10 12 EGADS : 14 Yes 2 0 1 1 1 9 15 16 EGADS : 15 Yes 2 0 1 1 1 14 17 18 EGADS : 16 Yes 2 0 1 1 1 11 14 17 EGADS : 17 Yes 2 0 1 1 1 15 16 18 EGADS : 18 Yes 2 0 1 1 1 15 17 EGADS : 19 Yes 3 0 1 NA NA 21 22 23 24 EGADS : 20 Yes 3 0 1 NA NA 21 22 23 24 EGADS : 21 Yes 3 0 1 NA NA 19 20 23 24 EGADS : 22 Yes 3 0 1 NA NA 19 20 23 24 EGADS : 23 Yes 3 0 1 NA NA 19 20 21 22 EGADS : 24 Yes 3 0 1 NA NA 19 20 21 22 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 3 2 -4 EGADS : 2 -2 5 1 -6 EGADS : 3 7 4 -8 -3 EGADS : 4 8 6 -7 -5 EGADS : 5 9 12 -10 -11 EGADS : 6 10 14 -9 -13 EGADS : 7 -15 11 16 -12 EGADS : 8 -16 13 15 -14 EGADS : 9 -17 18 19 -20 EGADS : 10 -21 20 22 -23 EGADS : 11 -19 24 17 -25 EGADS : 12 -22 25 21 -26 EGADS : 13 23 26 EGADS : 14 27 29 -28 -18 EGADS : 15 30 32 -31 -29 EGADS : 16 28 33 -27 -24 EGADS : 17 31 34 -30 -33 EGADS : 18 -32 -34 EGADS : 19 35 36 -37 -38 EGADS : 20 -39 42 41 -40 EGADS : 21 43 39 -44 -35 EGADS : 22 -45 37 46 -41 EGADS : 23 38 45 -42 -43 EGADS : 24 -36 44 40 -46 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : 19 19 EGADS : 20 20 EGADS : 21 21 EGADS : 22 22 EGADS : 23 23 EGADS : 24 24 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 3 2 -4 EGADS : 2 Yes -2 5 1 -6 EGADS : 3 Yes 7 4 -8 -3 EGADS : 4 Yes 8 6 -7 -5 EGADS : 5 Yes 9 12 -10 -11 EGADS : 6 Yes 10 14 -9 -13 EGADS : 7 Yes -15 11 16 -12 EGADS : 8 Yes -16 13 15 -14 EGADS : 9 Yes -17 18 19 -20 EGADS : 10 Yes -21 20 22 -23 EGADS : 11 Yes -19 24 17 -25 EGADS : 12 Yes -22 25 21 -26 EGADS : 13 Yes 23 26 EGADS : 14 Yes 27 29 -28 -18 EGADS : 15 Yes 30 32 -31 -29 EGADS : 16 Yes 28 33 -27 -24 EGADS : 17 Yes 31 34 -30 -33 EGADS : 18 Yes -32 -34 EGADS : 19 Yes 35 36 -37 -38 EGADS : 20 Yes -39 42 41 -40 EGADS : 21 Yes 43 39 -44 -35 EGADS : 22 Yes -45 37 46 -41 EGADS : 23 Yes 38 45 -42 -43 EGADS : 24 Yes -36 44 40 -46 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 2 EGADS : 2 0 Yes 3 4 1 1 2 EGADS : 3 0 Yes 1 3 1 1 3 EGADS : 4 0 Yes 2 4 1 1 3 EGADS : 5 0 Yes 3 1 1 2 4 EGADS : 6 0 Yes 4 2 1 2 4 EGADS : 7 0 Yes 1 2 1 3 4 EGADS : 8 0 Yes 3 4 1 3 4 EGADS : 9 1 Yes 5 6 1 5 6 EGADS : 10 1 Yes 7 8 1 5 6 EGADS : 11 1 Yes 5 7 1 5 7 EGADS : 12 1 Yes 6 8 1 5 7 EGADS : 13 1 Yes 7 5 1 6 8 EGADS : 14 1 Yes 8 6 1 6 8 EGADS : 15 1 Yes 5 6 1 7 8 EGADS : 16 1 Yes 7 8 1 7 8 EGADS : 17 2 Yes 9 10 1 9 11 EGADS : 18 2 Yes 9 11 1 9 14 EGADS : 19 2 Yes 11 12 1 9 11 EGADS : 20 2 Yes 10 12 1 9 10 EGADS : 21 2 Yes 10 13 1 10 12 EGADS : 22 2 Yes 12 14 1 10 12 EGADS : 23 2 Yes 13 14 1 10 13 EGADS : 24 2 Yes 11 9 1 11 16 EGADS : 25 2 Yes 12 10 1 11 12 EGADS : 26 2 Yes 14 13 1 12 13 EGADS : 27 2 Yes 9 15 1 14 16 EGADS : 28 2 Yes 11 16 1 14 16 EGADS : 29 2 Yes 15 16 1 14 15 EGADS : 30 2 Yes 15 17 1 15 17 EGADS : 31 2 Yes 16 18 1 15 17 EGADS : 32 2 Yes 17 18 1 15 18 EGADS : 33 2 Yes 16 15 1 16 17 EGADS : 34 2 Yes 18 17 1 17 18 EGADS : 35 3 Yes 20 19 NA 19 21 EGADS : 36 3 Yes 19 21 NA 19 24 EGADS : 37 3 Yes 22 21 NA 19 22 EGADS : 38 3 Yes 20 22 NA 19 23 EGADS : 39 3 Yes 24 23 NA 20 21 EGADS : 40 3 Yes 23 25 NA 20 24 EGADS : 41 3 Yes 26 25 NA 20 22 EGADS : 42 3 Yes 24 26 NA 20 23 EGADS : 43 3 Yes 20 24 NA 21 23 EGADS : 44 3 Yes 19 23 NA 21 24 EGADS : 45 3 Yes 22 26 NA 22 23 EGADS : 46 3 Yes 21 25 NA 22 24 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 90.5173952 0 0 EGADS : 2 Yes 90.5173952 0 0 EGADS : 3 Yes 60.5173952 0 0 EGADS : 4 Yes 60.5173952 0 0 EGADS : 5 Yes 90.5173952 29.3018771 0 EGADS : 6 Yes 90.5173952 29.3018771 0 EGADS : 7 Yes 60.5173952 29.3018771 0 EGADS : 8 Yes 60.5173952 29.3018771 0 EGADS : 9 Yes 97.2007855 0 0 EGADS : 10 Yes 97.9335611 0 0 EGADS : 11 Yes 50 0 0 EGADS : 12 Yes 75.3047874 0 0 EGADS : 13 Yes 123.552357 0 4.7180639 EGADS : 14 Yes 118.391317 0 3.99272703 EGADS : 15 Yes 97.9335611 36.1389817 0 EGADS : 16 Yes 75.3047874 36.1389817 0 EGADS : 17 Yes 123.552357 97.6729236 4.7180639 EGADS : 18 Yes 118.391317 97.6729236 3.99272703 EGADS : 19 Yes 0 0 1947.05079 EGADS : 20 Yes 0 0 0 EGADS : 21 Yes 0 1953.45847 1947.05079 EGADS : 22 Yes 0 1953.45847 0 EGADS : 23 Yes 2040.21562 0 1947.05079 EGADS : 24 Yes 2040.21562 0 0 EGADS : 25 Yes 2040.21562 1953.45847 1947.05079 EGADS : 26 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 22.2515 AFLR4 : Reference Length = 22.2515 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 428.344 AFLR4 : Abs Min Surf Spacing = 0.0556287 AFLR4 : Min Surf Spacing = 0.111257 AFLR4 : Max Surf Spacing = 2.22515 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 STD AFLR4 : 18 CAD geometry 0 STD AFLR4 : 19 CAD geometry 0 FARFIELD AFLR4 : 20 CAD geometry 0 FARFIELD AFLR4 : 21 CAD geometry 0 FARFIELD AFLR4 : 22 CAD geometry 0 FARFIELD AFLR4 : 23 CAD geometry 0 FARFIELD AFLR4 : 24 CAD geometry 0 FARFIELD AFLR4 : Case has 2 Proximity Checking Components AFLR4 : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18 AFLR4 : Component 2 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR4 : Define CAD surface definition 19 AFLR4 : Define CAD surface definition 20 AFLR4 : Define CAD surface definition 21 AFLR4 : Define CAD surface definition 22 AFLR4 : Define CAD surface definition 23 AFLR4 : Define CAD surface definition 24 AFLR43 : INPUT SURFACE MESH FROM TESS AFLR43 : Quad Surface Faces= 0 AFLR43 : Tria Surface Faces= 191152 AFLR43 : Nodes = 95580 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.50 AFLR3 : Version Date 10/31/23 @ 06:31PM AFLR3 : Compile OS Darwin 23.3.0 arm64 AFLR3 : Compile Date 02/08/24 @ 04:22PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 95580 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 Solid UG3 : 18 Solid UG3 : 19 FarField UG3 : 20 FarField UG3 : 21 FarField UG3 : 22 FarField UG3 : 23 FarField UG3 : 24 FarField AFLR3 : CPU Time = 0.159 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 95580 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 19118 113387 AFLR3 IG : Nodes, Elements = 38236 247740 AFLR3 IG : Nodes, Elements = 57354 368381 AFLR3 IG : Nodes, Elements = 76472 521305 AFLR3 IG : Nodes, Elements = 95587 673125 AFLR3 IG : Nodes, Elements = 95587 671793 AFLR3 IG : Nodes, Elements = 95587 671843 AFLR3 IG : Nodes, Elements = 95587 671732 AFLR3 IG : Nodes, Elements = 95587 671730 AFLR3 IG : Nodes, Elements = 95580 378556 AFLR3 IG : Nodes, Elements = 95580 378785 AFLR3 IG : Nodes, Elements = 95580 306254 AFLR3 IG : Nodes, Elements = 95580 287815 AFLR3 : CPU Time = 5.441 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 95580 287815 AFLR3 GGi: Nodes, Elements = 95581 287818 AFLR3 GGi: Nodes, Elements = 95581 287829 AFLR3 GGi: Nodes, Elements = 95581 287828 AFLR3 GGi: Nodes, Elements = 95583 287834 AFLR3 GGi: Nodes, Elements = 95583 287890 AFLR3 GGi: Nodes, Elements = 95583 287912 AFLR3 GG : Nodes, Elements = 136678 411938 AFLR3 GG : Nodes, Elements = 136678 577044 AFLR3 GG : Nodes, Elements = 136678 536154 AFLR3 GG : Nodes, Elements = 171128 640568 AFLR3 GG : Nodes, Elements = 171128 776304 AFLR3 GG : Nodes, Elements = 171128 734094 AFLR3 GG : Nodes, Elements = 206400 840686 AFLR3 GG : Nodes, Elements = 206400 979875 AFLR3 GG : Nodes, Elements = 206400 937908 AFLR3 GG : Nodes, Elements = 241646 1044099 AFLR3 GG : Nodes, Elements = 241646 1188395 AFLR3 GG : Nodes, Elements = 241646 1146956 AFLR3 GG : Nodes, Elements = 241646 1137722 AFLR3 GG : Nodes, Elements = 276767 1243501 AFLR3 GG : Nodes, Elements = 276767 1395480 AFLR3 GG : Nodes, Elements = 276767 1354454 AFLR3 GG : Nodes, Elements = 311737 1459784 AFLR3 GG : Nodes, Elements = 311737 1601038 AFLR3 GG : Nodes, Elements = 311737 1562741 AFLR3 GG : Nodes, Elements = 346382 1667060 AFLR3 GG : Nodes, Elements = 346382 1803912 AFLR3 GG : Nodes, Elements = 346382 1767981 AFLR3 GG : Nodes, Elements = 379866 1868797 AFLR3 GG : Nodes, Elements = 379866 2001420 AFLR3 GG : Nodes, Elements = 379866 1966993 AFLR3 GG : Nodes, Elements = 412236 2064483 AFLR3 GG : Nodes, Elements = 412236 2190563 AFLR3 GG : Nodes, Elements = 412236 2159284 AFLR3 GG : Nodes, Elements = 443624 2253761 AFLR3 GG : Nodes, Elements = 443624 2375880 AFLR3 GG : Nodes, Elements = 443624 2345639 AFLR3 GG : Nodes, Elements = 473758 2436345 AFLR3 GG : Nodes, Elements = 473758 2553524 AFLR3 GG : Nodes, Elements = 473758 2524504 AFLR3 GG : Nodes, Elements = 502809 2611934 AFLR3 GG : Nodes, Elements = 502809 2725931 AFLR3 GG : Nodes, Elements = 502809 2696981 AFLR3 GG : Nodes, Elements = 530466 2780197 AFLR3 GG : Nodes, Elements = 530466 2889393 AFLR3 GG : Nodes, Elements = 530466 2861633 AFLR3 GG : Nodes, Elements = 557117 2941852 AFLR3 GG : Nodes, Elements = 557117 3045248 AFLR3 GG : Nodes, Elements = 557117 3019721 AFLR3 GG : Nodes, Elements = 582598 3096375 AFLR3 GG : Nodes, Elements = 582598 3195656 AFLR3 GG : Nodes, Elements = 582598 3171187 AFLR3 GG : Nodes, Elements = 607120 3245004 AFLR3 GG : Nodes, Elements = 607120 3341157 AFLR3 GG : Nodes, Elements = 607120 3316708 AFLR3 GG : Nodes, Elements = 630670 3387605 AFLR3 GG : Nodes, Elements = 630670 3480180 AFLR3 GG : Nodes, Elements = 630670 3456797 AFLR3 GG : Nodes, Elements = 653200 3524630 AFLR3 GG : Nodes, Elements = 653200 3613020 AFLR3 GG : Nodes, Elements = 653200 3590696 AFLR3 GG : Nodes, Elements = 675084 3656585 AFLR3 GG : Nodes, Elements = 675084 3741278 AFLR3 GG : Nodes, Elements = 675084 3720774 AFLR3 GG : Nodes, Elements = 696108 3784042 AFLR3 GG : Nodes, Elements = 696108 3866035 AFLR3 GG : Nodes, Elements = 696108 3845633 AFLR3 GG : Nodes, Elements = 716356 3906549 AFLR3 GG : Nodes, Elements = 716356 3984761 AFLR3 GG : Nodes, Elements = 716356 3965561 AFLR3 GG : Nodes, Elements = 735889 4024306 AFLR3 GG : Nodes, Elements = 735889 4100723 AFLR3 GG : Nodes, Elements = 735889 4081584 AFLR3 GG : Nodes, Elements = 754458 4137443 AFLR3 GG : Nodes, Elements = 754458 4209831 AFLR3 GG : Nodes, Elements = 754458 4191783 AFLR3 GG : Nodes, Elements = 772291 4245412 AFLR3 GG : Nodes, Elements = 772291 4315501 AFLR3 GG : Nodes, Elements = 772291 4297710 AFLR3 GG : Nodes, Elements = 789443 4349276 AFLR3 GG : Nodes, Elements = 789443 4416475 AFLR3 GG : Nodes, Elements = 789443 4399563 AFLR3 GG : Nodes, Elements = 806051 4449471 AFLR3 GG : Nodes, Elements = 806051 4514571 AFLR3 GG : Nodes, Elements = 806051 4498171 AFLR3 GG : Nodes, Elements = 821873 4545711 AFLR3 GG : Nodes, Elements = 821873 4607158 AFLR3 GG : Nodes, Elements = 821873 4592064 AFLR3 GG : Nodes, Elements = 837118 4637853 AFLR3 GG : Nodes, Elements = 837118 4697402 AFLR3 GG : Nodes, Elements = 837118 4682546 AFLR3 GG : Nodes, Elements = 851739 4726464 AFLR3 GG : Nodes, Elements = 851739 4782603 AFLR3 GG : Nodes, Elements = 851739 4769065 AFLR3 GG : Nodes, Elements = 865824 4811353 AFLR3 GG : Nodes, Elements = 865824 4866088 AFLR3 GG : Nodes, Elements = 865824 4852550 AFLR3 GG : Nodes, Elements = 879359 4893188 AFLR3 GG : Nodes, Elements = 879359 4945198 AFLR3 GG : Nodes, Elements = 879359 4932618 AFLR3 GG : Nodes, Elements = 892295 4971462 AFLR3 GG : Nodes, Elements = 892295 5021252 AFLR3 GG : Nodes, Elements = 892295 5009183 AFLR3 GG : Nodes, Elements = 904796 5046719 AFLR3 GG : Nodes, Elements = 904796 5094609 AFLR3 GG : Nodes, Elements = 904796 5082935 AFLR3 GG : Nodes, Elements = 917006 5119589 AFLR3 GG : Nodes, Elements = 917006 5167108 AFLR3 GG : Nodes, Elements = 917006 5155238 AFLR3 GG : Nodes, Elements = 928945 5191076 AFLR3 GG : Nodes, Elements = 928945 5236714 AFLR3 GG : Nodes, Elements = 928945 5225614 AFLR3 GG : Nodes, Elements = 940659 5260766 AFLR3 GG : Nodes, Elements = 940659 5306192 AFLR3 GG : Nodes, Elements = 940659 5294917 AFLR3 GG : Nodes, Elements = 952358 5330036 AFLR3 GG : Nodes, Elements = 952358 5374827 AFLR3 GG : Nodes, Elements = 952358 5364090 AFLR3 GG : Nodes, Elements = 963772 5398344 AFLR3 GG : Nodes, Elements = 963772 5442371 AFLR3 GG : Nodes, Elements = 963772 5431527 AFLR3 GG : Nodes, Elements = 975235 5465936 AFLR3 GG : Nodes, Elements = 975235 5510168 AFLR3 GG : Nodes, Elements = 975235 5499163 AFLR3 GG : Nodes, Elements = 986552 5533128 AFLR3 GG : Nodes, Elements = 986552 5576100 AFLR3 GG : Nodes, Elements = 986552 5565791 AFLR3 GG : Nodes, Elements = 997689 5599215 AFLR3 GG : Nodes, Elements = 997689 5641662 AFLR3 GG : Nodes, Elements = 997689 5631301 AFLR3 GG : Nodes, Elements = 1008693 5664321 AFLR3 GG : Nodes, Elements = 1008693 5706246 AFLR3 GG : Nodes, Elements = 1008693 5696151 AFLR3 GG : Nodes, Elements = 1019592 5728860 AFLR3 GG : Nodes, Elements = 1019592 5771162 AFLR3 GG : Nodes, Elements = 1019592 5760605 AFLR3 GG : Nodes, Elements = 1030418 5793103 AFLR3 GG : Nodes, Elements = 1030418 5834841 AFLR3 GG : Nodes, Elements = 1030418 5824463 AFLR3 GG : Nodes, Elements = 1040850 5855769 AFLR3 GG : Nodes, Elements = 1040850 5895951 AFLR3 GG : Nodes, Elements = 1040850 5885943 AFLR3 GG : Nodes, Elements = 1051188 5916972 AFLR3 GG : Nodes, Elements = 1051188 5957000 AFLR3 GG : Nodes, Elements = 1051188 5946966 AFLR3 GG : Nodes, Elements = 1061495 5977893 AFLR3 GG : Nodes, Elements = 1061495 6017359 AFLR3 GG : Nodes, Elements = 1061495 6007786 AFLR3 GG : Nodes, Elements = 1071564 6038008 AFLR3 GG : Nodes, Elements = 1071564 6076351 AFLR3 GG : Nodes, Elements = 1071564 6067022 AFLR3 GG : Nodes, Elements = 1081243 6096066 AFLR3 GG : Nodes, Elements = 1081243 6133873 AFLR3 GG : Nodes, Elements = 1081243 6124235 AFLR3 GG : Nodes, Elements = 1090504 6152024 AFLR3 GG : Nodes, Elements = 1090504 6188229 AFLR3 GG : Nodes, Elements = 1090504 6178954 AFLR3 GG : Nodes, Elements = 1099257 6205218 AFLR3 GG : Nodes, Elements = 1099257 6239457 AFLR3 GG : Nodes, Elements = 1099257 6230836 AFLR3 GG : Nodes, Elements = 1107059 6254252 AFLR3 GG : Nodes, Elements = 1107059 6284884 AFLR3 GG : Nodes, Elements = 1107059 6276999 AFLR3 GG : Nodes, Elements = 1113848 6297377 AFLR3 GG : Nodes, Elements = 1113848 6323612 AFLR3 GG : Nodes, Elements = 1113848 6316993 AFLR3 GG : Nodes, Elements = 1119760 6334736 AFLR3 GG : Nodes, Elements = 1119760 6358254 AFLR3 GG : Nodes, Elements = 1119760 6351947 AFLR3 GG : Nodes, Elements = 1124553 6366331 AFLR3 GG : Nodes, Elements = 1124553 6385564 AFLR3 GG : Nodes, Elements = 1124553 6380400 AFLR3 GG : Nodes, Elements = 1128268 6391547 AFLR3 GG : Nodes, Elements = 1128268 6406066 AFLR3 GG : Nodes, Elements = 1128268 6402254 AFLR3 GG : Nodes, Elements = 1130923 6410221 AFLR3 GG : Nodes, Elements = 1130923 6421060 AFLR3 GG : Nodes, Elements = 1130923 6417908 AFLR3 GG : Nodes, Elements = 1132691 6423216 AFLR3 GG : Nodes, Elements = 1132691 6430239 AFLR3 GG : Nodes, Elements = 1132691 6428275 AFLR3 GG : Nodes, Elements = 1133857 6431773 AFLR3 GG : Nodes, Elements = 1133857 6436705 AFLR3 GG : Nodes, Elements = 1133857 6435176 AFLR3 GG : Nodes, Elements = 1134481 6437048 AFLR3 GG : Nodes, Elements = 1134481 6439565 AFLR3 GG : Nodes, Elements = 1134481 6438803 AFLR3 GG : Nodes, Elements = 1134784 6439712 AFLR3 GG : Nodes, Elements = 1134784 6440912 AFLR3 GG : Nodes, Elements = 1134784 6440547 AFLR3 GG : Nodes, Elements = 1134914 6440937 AFLR3 GG : Nodes, Elements = 1134914 6441430 AFLR3 GG : Nodes, Elements = 1134914 6441281 AFLR3 GG : Nodes, Elements = 1134969 6441446 AFLR3 GG : Nodes, Elements = 1134969 6441682 AFLR3 GG : Nodes, Elements = 1134969 6441599 AFLR3 GG : Nodes, Elements = 1134985 6441647 AFLR3 GG : Nodes, Elements = 1134985 6441720 AFLR3 GG : Nodes, Elements = 1134985 6441692 AFLR3 GG : Nodes, Elements = 1134992 6441713 AFLR3 GG : Nodes, Elements = 1134992 6441745 AFLR3 GG : Nodes, Elements = 1134992 6441730 AFLR3 GG : Nodes, Elements = 1134993 6441733 AFLR3 GG : Nodes, Elements = 1134993 6441738 AFLR3 GG : Nodes, Elements = 1134993 6441736 AFLR3 GG : Nodes, Elements = 1135116 6442105 AFLR3 GG : Nodes, Elements = 1135116 6442576 AFLR3 GG : Nodes, Elements = 1135116 6442430 AFLR3 GG : Nodes, Elements = 1135150 6442532 AFLR3 GG : Nodes, Elements = 1135150 6442653 AFLR3 GG : Nodes, Elements = 1135150 6442602 AFLR3 GG : Nodes, Elements = 1135162 6442638 AFLR3 GG : Nodes, Elements = 1135162 6442684 AFLR3 GG : Nodes, Elements = 1135162 6442668 AFLR3 GG : Nodes, Elements = 1135164 6442674 AFLR3 GG : Nodes, Elements = 1135164 6442683 AFLR3 GG : Nodes, Elements = 1135164 6442680 AFLR3 GG : Nodes, Elements = 1135166 6442686 AFLR3 GG : Nodes, Elements = 1135166 6442692 AFLR3 GG : Nodes, Elements = 1135166 6442691 AFLR3 GG : Nodes, Elements = 1135167 6442694 AFLR3 GG : Nodes, Elements = 1135167 6442697 AFLR3 GG : Nodes, Elements = 1135167 6442696 AFLR3 : CPU Time = 1.368 minutes AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 1135167 6442696 AFLR3 QI : Nodes, Elements = 1129670 6411684 AFLR3 QI : Nodes, Elements = 1128689 6406154 AFLR3 QI : Nodes, Elements = 1128464 6404899 AFLR3 QI : Nodes, Elements = 1128424 6404669 AFLR3 QI : Nodes, Elements = 1128409 6404587 AFLR3 QI : Nodes, Elements = 1128407 6404575 AFLR3 QI : Nodes, Elements = 1128406 6404568 AFLR3 QI : Nodes, Elements = 1128405 6404563 AFLR3 QI : Nodes, Elements = 1128405 6427353 AFLR3 QI : Nodes, Elements = 1128405 6402765 AFLR3 QI : Nodes, Elements = 1128405 6391678 AFLR3 QI : Nodes, Elements = 1128405 6408644 AFLR3 QI : Nodes, Elements = 1128405 6391271 AFLR3 QI : Nodes, Elements = 1128405 6390811 AFLR3 QI : Nodes, Elements = 1128405 6406750 AFLR3 QI : Nodes, Elements = 1128405 6390982 AFLR3 QI : Nodes, Elements = 1128405 6390667 AFLR3 QI : Nodes, Elements = 1128405 6395803 AFLR3 QI : Nodes, Elements = 1128405 6389758 AFLR3 QI : Nodes, Elements = 1128405 6389206 AFLR3 QI : Nodes, Elements = 1128405 6391898 AFLR3 QI : Nodes, Elements = 1128405 6388765 AFLR3 QI : Nodes, Elements = 1128405 6388419 AFLR3 : CPU Time = 24.072 seconds AFLR3 QRG: QUALITY GRID RE-GENERATION AFLR3 QRG: Nodes, Elements = 1128405 6388419 AFLR3 QRG: Nodes, Elements = 1128425 6388539 AFLR3 : CPU Time = 0.629 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 6388539 UG3 : Min, Max Ang = 3.386 162.2 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 5 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.96e+10 UG3 : No. Tet Elems = 6388539 UG3 : Min Vol = 1.42e-05 UG3 : Average Vol = 9.33e+03 UG3 : Total-Tet-Vol = 5.96e+10 UG3 : No. Vol160.0 = 5 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.96e+10 UG3 : No. Tet Elems = 6388539 UG3 : Min Vol = 1.42e-05 UG3 : Average Vol = 9.33e+03 UG3 : Total-Tet-Vol = 5.96e+10 UG3 : No. Vol160.0 = 13 UG3 : No. Angle>179.9 = 0 UG3 : No. Pyramid Elems = 147 UG3 : Min, Max Ang = 8.861 172.3 UG3 : Average Angle = 80.9 UG3 : No. Angle>160.0 = 12 UG3 : No. Angle>179.9 = 0 UG3 : No. Prism Elems = 156367 UG3 : Min, Max Ang = 9.482 174.2 UG3 : Average Angle = 80 UG3 : No. Angle>160.0 = 421 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.96e+10 UG3 : No. Tet Elems = 396475 UG3 : Min Vol = 0.00131 UG3 : Average Vol = 1.5e+05 UG3 : Total-Tet-Vol = 5.96e+10 UG3 : No. Vol160.0 = 293 UG3 : No. Angle>179.9 = 0 UG3 : No. Pyramid Elems = 2793 UG3 : Min, Max Ang = 7.032 171.7 UG3 : Average Angle = 82.6 UG3 : No. Angle>160.0 = 56 UG3 : No. Angle>179.9 = 0 UG3 : No. Prism Elems = 104033 UG3 : Min, Max Ang = 6.792 174.6 UG3 : Average Angle = 80.1 UG3 : No. Angle>160.0 = 561 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.96e+10 UG3 : No. Tet Elems = 318835 UG3 : Min Vol = 0.000481 UG3 : Average Vol = 1.87e+05 UG3 : Total-Tet-Vol = 5.96e+10 UG3 : No. Vol160.0 = 338 UG3 : No. Angle>179.9 = 0 UG3 : No. Pyramid Elems = 20687 UG3 : Min, Max Ang = 7.23 174.4 UG3 : Average Angle = 82.6 UG3 : No. Angle>160.0 = 129 UG3 : No. Angle>179.9 = 0 UG3 : No. Prism Elems = 390947 UG3 : Min, Max Ang = 6.851 174.6 UG3 : Average Angle = 80.1 UG3 : No. Angle>160.0 = 732 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.96e+10 UG3 : No. Tet Elems = 1473376 UG3 : Min Vol = 5.2e-06 UG3 : Average Vol = 4.05e+04 UG3 : Total-Tet-Vol = 5.96e+10 UG3 : No. Vol Toal Elements 71406 real 0m9.704s user 0m13.156s sys 0m2.714s + status=0 + set +x ================================================= solutions/session07/aflr4_InviscidTransport_150k.py passed (as expected) ================================================= execute_Training.sh: line 293: ulimit: stack size: cannot modify limit: Operation not permitted flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC//flowCart ================================================= 1_cart3d_InviscidWing.py test; + python 1_cart3d_InviscidWing.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 209.164356 Tessellating body 1 with MaxEdge = 5.229109 Sag = 0.209164 Angle = 15.000000 Executing: autoInputs -r 8.000000 -nDiv 6 -maxR 9 > autoInputs.out Executing: ./aero.csh > aero.out C_A 0.086485028 C_Y -2.1874522e-05 C_N 0.55362646 C_D 0.10094764 C_S -2.1874522e-05 C_L 0.55117283 C_l -6.33338e-05 C_m 0.893921 C_n -0.000182003 C_M_x -6.80764e-05 C_M_y 0.893921 C_M_z -0.000180283 real 0m23.812s user 0m43.241s sys 0m0.814s + status=0 + set +x ================================================= data/session08/1_cart3d_InviscidWing.py passed (as expected) ================================================= ================================================= 4_cart3d_OpenMDAO_alpha.py test; + python 4_cart3d_OpenMDAO_alpha.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:41023] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/2228289536/sm_segment.VIGGEN.502.84d10000.0 could be created. MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - alpha Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - CL2 Done getting CFD functional Body size = 196.565248 Tessellating body 1 with MaxEdge = 4.914131 Sag = 0.196565 Angle = 15.000000 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:58:38) Running aero.csh on 2 core(s) in M0.4A1.5B0_DP1 (00:59:28) aero.csh done o case M0.4A1.5B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:59:29) Running aero.csh on 2 core(s) in M0.4A1.5B0_DP1 (01:00:38) aero.csh done Max memory allowed: 32 GB Flow hexes: 264563 Estimated cutter memory: 0.026456 GB / DV Estimated xsensit memory: 0.502670 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:00:38) Linearizing cut-cells (01:00:38) ... done o Number of simultaneous xsensit jobs: 1 (01:00:38) Computing gradients (01:00:42) ... done o case M0.4A1.5B0_DP1, averaging data over 1 cycle(s) RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 1.88225D-02 |proj g|= 2.44220D-02 o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:00:43) Running aero.csh on 2 core(s) in M0.4A1.47558B0_DP1 (01:01:31) aero.csh done o case M0.4A1.47558B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:01:31) Running aero.csh on 2 core(s) in M0.4A1.47558B0_DP1 (01:02:40) aero.csh done Max memory allowed: 32 GB Flow hexes: 264563 Estimated cutter memory: 0.026456 GB / DV Estimated xsensit memory: 0.502670 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:02:41) Linearizing cut-cells (01:02:41) ... done o Number of simultaneous xsensit jobs: 1 (01:02:41) Computing gradients (01:02:45) ... done o case M0.4A1.47558B0_DP1, averaging data over 1 cycle(s) At iterate 1 f= 1.82188D-02 |proj g|= 2.40420D-02 o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:02:45) Running aero.csh on 2 core(s) in M0.4A-0.0696926B0_DP1 (01:03:33) aero.csh done o case M0.4A-0.0696926B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:03:34) Running aero.csh on 2 core(s) in M0.4A-0.0696926B0_DP1 (01:04:43) aero.csh done Max memory allowed: 32 GB Flow hexes: 264563 Estimated cutter memory: 0.026456 GB / DV Estimated xsensit memory: 0.502670 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:04:44) Linearizing cut-cells (01:04:44) ... done o Number of simultaneous xsensit jobs: 1 (01:04:44) Computing gradients (01:04:48) ... done o case M0.4A-0.0696926B0_DP1, averaging data over 1 cycle(s) At iterate 2 f= 4.17947D-05 |proj g|= 1.18177D-03 o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:04:48) Running aero.csh on 2 core(s) in M0.4A0.00270572B0_DP1 (01:05:36) aero.csh done o case M0.4A0.00270572B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:05:37) Running aero.csh on 2 core(s) in M0.4A0.00270572B0_DP1 (01:06:46) aero.csh done Max memory allowed: 32 GB Flow hexes: 264563 Estimated cutter memory: 0.026456 GB / DV Estimated xsensit memory: 0.502670 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:06:46) Linearizing cut-cells (01:06:46) ... done o Number of simultaneous xsensit jobs: 1 (01:06:46) Computing gradients (01:06:50) ... done o case M0.4A0.00270572B0_DP1, averaging data over 1 cycle(s) At iterate 3 f= 8.59678D-08 |proj g|= 5.37728D-05 o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:06:51) Running aero.csh on 2 core(s) in M0.4A-0.000445155B0_DP1 (01:07:39) aero.csh done o case M0.4A-0.000445155B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:07:40) Running aero.csh on 2 core(s) in M0.4A-0.000445155B0_DP1 (01:08:49) aero.csh done Max memory allowed: 32 GB Flow hexes: 264563 Estimated cutter memory: 0.026456 GB / DV Estimated xsensit memory: 0.502670 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:08:49) Linearizing cut-cells (01:08:49) ... done o Number of simultaneous xsensit jobs: 1 (01:08:49) Computing gradients (01:08:53) ... done o case M0.4A-0.000445155B0_DP1, averaging data over 1 cycle(s) At iterate 4 f= 1.39004D-11 |proj g|= 6.83912D-07 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 4 5 4 0 0 6.839D-07 1.390D-11 F = 1.3900449050999998E-011 CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL Optimization Complete ----------------------------------- Optimized alpha: [-0.00044516] real 10m18.229s user 19m22.246s sys 0m7.051s + status=0 + set +x ================================================= data/session08/4_cart3d_OpenMDAO_alpha.py passed (as expected) ================================================= ================================================= 5_cart3d_OpenMDAO_twist.py test; + python 5_cart3d_OpenMDAO_twist.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:44534] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/397934592/sm_segment.VIGGEN.502.17b80000.0 could be created. MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - wing:alphab Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - CL2 Done getting CFD functional Body size = 196.567836 Tessellating body 1 with MaxEdge = 4.914196 Sag = 0.196568 Angle = 15.000000 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:08:56) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:09:44) aero.csh done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) MESSAGE:: Building wingOml o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:09:45) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:10:53) aero.csh done Max memory allowed: 32 GB Flow hexes: 260350 Estimated cutter memory: 0.026035 GB / DV Estimated xsensit memory: 0.494665 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:10:54) Linearizing cut-cells (01:10:56) ... done o Number of simultaneous xsensit jobs: 1 (01:10:56) Computing gradients (01:11:00) ... done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 5.30094D-03 |proj g|= 7.31928D-03 MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 196.567822 Tessellating body 1 with MaxEdge = 4.914196 Sag = 0.196568 Angle = 15.000000 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:11:01) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:11:49) aero.csh done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) MESSAGE:: Building wingOml o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:11:49) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:12:58) aero.csh done Max memory allowed: 32 GB Flow hexes: 260454 Estimated cutter memory: 0.026045 GB / DV Estimated xsensit memory: 0.494863 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:12:58) Linearizing cut-cells (01:13:00) ... done o Number of simultaneous xsensit jobs: 1 (01:13:00) Computing gradients (01:13:04) ... done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) At iterate 1 f= 5.25523D-03 |proj g|= 7.29015D-03 MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 196.565774 Tessellating body 1 with MaxEdge = 4.914144 Sag = 0.196566 Angle = 15.000000 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:13:06) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:13:53) aero.csh done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) MESSAGE:: Building wingOml o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:13:54) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:15:05) aero.csh done Max memory allowed: 32 GB Flow hexes: 261758 Estimated cutter memory: 0.026176 GB / DV Estimated xsensit memory: 0.497340 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:15:05) Linearizing cut-cells (01:15:07) ... done o Number of simultaneous xsensit jobs: 1 (01:15:07) Computing gradients (01:15:11) ... done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) At iterate 2 f= 2.98455D-04 |proj g|= 1.85742D-03 MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 196.565298 Tessellating body 1 with MaxEdge = 4.914132 Sag = 0.196565 Angle = 15.000000 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:15:13) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:16:01) aero.csh done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) MESSAGE:: Building wingOml o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:16:02) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:17:11) aero.csh done Max memory allowed: 32 GB Flow hexes: 264228 Estimated cutter memory: 0.026423 GB / DV Estimated xsensit memory: 0.502033 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:17:11) Linearizing cut-cells (01:17:13) ... done o Number of simultaneous xsensit jobs: 1 (01:17:13) Computing gradients (01:17:17) ... done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) At iterate 3 f= 3.84355D-06 |proj g|= 2.40011D-04 MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 196.565263 Tessellating body 1 with MaxEdge = 4.914132 Sag = 0.196565 Angle = 15.000000 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:17:18) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:18:06) aero.csh done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) MESSAGE:: Building wingOml o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:18:07) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:19:16) aero.csh done Max memory allowed: 32 GB Flow hexes: 264265 Estimated cutter memory: 0.026426 GB / DV Estimated xsensit memory: 0.502104 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:19:16) Linearizing cut-cells (01:19:18) ... done o Number of simultaneous xsensit jobs: 1 (01:19:19) Computing gradients (01:19:23) ... done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) At iterate 4 f= 3.66987D-07 |proj g|= 7.23152D-05 MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 196.565248 Tessellating body 1 with MaxEdge = 4.914131 Sag = 0.196565 Angle = 15.000000 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:19:24) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:20:12) aero.csh done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) MESSAGE:: Building wingOml o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (01:20:13) Running aero.csh on 2 core(s) in M0.4A0B0_DP1 (01:21:22) aero.csh done Max memory allowed: 32 GB Flow hexes: 264535 Estimated cutter memory: 0.026454 GB / DV Estimated xsensit memory: 0.502617 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (01:21:22) Linearizing cut-cells (01:21:24) ... done o Number of simultaneous xsensit jobs: 1 (01:21:24) Computing gradients (01:21:28) ... done o case M0.4A0B0_DP1, averaging data over 1 cycle(s) At iterate 5 f= 2.00842D-09 |proj g|= 5.37815D-06 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 5 6 5 0 0 5.378D-06 2.008D-09 F = 2.0084224803000001E-009 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized wing:alphab: [0.00011371] real 12m34.954s user 23m18.625s sys 0m8.681s + status=0 + set +x ================================================= data/session08/5_cart3d_OpenMDAO_twist.py passed (as expected) ================================================= ================================================= 2_su2_InviscidWing.py test; + python 2_su2_InviscidWing.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - leftWing Mesh sizing name - riteWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 6 EGADS : 2 Yes 0 0 1 1 1 1 4 5 EGADS : 3 Yes 0 0 1 1 1 1 4 8 EGADS : 4 Yes 0 0 1 1 1 2 3 5 EGADS : 5 Yes 0 0 1 1 1 2 4 EGADS : 6 Yes 0 0 1 1 1 1 7 8 EGADS : 7 Yes 0 0 1 1 1 6 9 10 EGADS : 8 Yes 0 0 1 1 1 3 6 9 EGADS : 9 Yes 0 0 1 1 1 7 8 10 EGADS : 10 Yes 0 0 1 1 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 2651.51 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 5 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1107 2082 0 AFLR4 : Nodes, Trias,Quads= 685 1238 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1473 2759 0 AFLR4 : Nodes, Trias,Quads= 721 1255 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 1116 2100 0 AFLR4 : Nodes, Trias,Quads= 671 1210 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1458 2729 0 AFLR4 : Nodes, Trias,Quads= 714 1241 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 20 24 0 AFLR4 : Nodes, Trias,Quads= 14 12 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1108 2084 0 AFLR4 : Nodes, Trias,Quads= 683 1234 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 1488 2789 0 AFLR4 : Nodes, Trias,Quads= 714 1241 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 1112 2092 0 AFLR4 : Nodes, Trias,Quads= 653 1174 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 1456 2725 0 AFLR4 : Nodes, Trias,Quads= 708 1229 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 20 24 0 AFLR4 : Nodes, Trias,Quads= 14 12 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 4933 9858 1312 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 4933 9858 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 12796 24695 0 AFLR4 : Nodes, Trias,Quads= 7764 14631 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 29251 57087 0 AFLR4 : Nodes, Trias,Quads= 12448 23481 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 12136 23411 0 AFLR4 : Nodes, Trias,Quads= 7447 14033 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 29424 57435 0 AFLR4 : Nodes, Trias,Quads= 12399 23385 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 196 293 0 AFLR4 : Nodes, Trias,Quads= 188 277 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 12819 24741 0 AFLR4 : Nodes, Trias,Quads= 7725 14553 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 29437 57459 0 AFLR4 : Nodes, Trias,Quads= 12412 23409 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 12144 23427 0 AFLR4 : Nodes, Trias,Quads= 7471 14081 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 29445 57477 0 AFLR4 : Nodes, Trias,Quads= 12478 23543 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 196 293 0 AFLR4 : Nodes, Trias,Quads= 188 277 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 75857 151706 9398 OVERALL : CPU Time = 0.983 seconds Body 1 (of 2) Number of nodes = 75837 Number of elements = 151670 Number of triangle elements = 151670 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75857 Total number of elements = 151706 Total number of triangle elements = 151706 Total number of quadrilateral elements = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Getting volume mesh UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 6 EGADS : 2 Yes 0 0 1 1 1 1 4 5 EGADS : 3 Yes 0 0 1 1 1 1 4 8 EGADS : 4 Yes 0 0 1 1 1 2 3 5 EGADS : 5 Yes 0 0 1 1 1 2 4 EGADS : 6 Yes 0 0 1 1 1 1 7 8 EGADS : 7 Yes 0 0 1 1 1 6 9 10 EGADS : 8 Yes 0 0 1 1 1 3 6 9 EGADS : 9 Yes 0 0 1 1 1 7 8 10 EGADS : 10 Yes 0 0 1 1 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 13.1976 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 428.309 AFLR4 : Abs Min Surf Spacing = 0.032994 AFLR4 : Min Surf Spacing = 0.065988 AFLR4 : Max Surf Spacing = 1.31976 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 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR43 : INPUT SURFACE MESH FROM TESS AFLR43 : Quad Surface Faces= 0 AFLR43 : Tria Surface Faces= 151706 AFLR43 : Nodes = 75857 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.50 AFLR3 : Version Date 10/31/23 @ 06:31PM AFLR3 : Compile OS Darwin 23.3.0 arm64 AFLR3 : Compile Date 02/08/24 @ 04:22PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 75857 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 FarField UG3 : 12 FarField UG3 : 13 FarField UG3 : 14 FarField UG3 : 15 FarField UG3 : 16 FarField AFLR3 : CPU Time = 0.086 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 75857 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 15172 111199 AFLR3 IG : Nodes, Elements = 30344 239871 AFLR3 IG : Nodes, Elements = 45516 364757 AFLR3 IG : Nodes, Elements = 60688 488029 AFLR3 IG : Nodes, Elements = 75860 649416 AFLR3 IG : Nodes, Elements = 75864 649502 AFLR3 IG : Nodes, Elements = 75864 648282 AFLR3 IG : Nodes, Elements = 75864 648415 AFLR3 IG : Nodes, Elements = 75864 647563 AFLR3 IG : Nodes, Elements = 75857 416423 AFLR3 IG : Nodes, Elements = 75857 417606 AFLR3 IG : Nodes, Elements = 75857 261925 AFLR3 IG : Nodes, Elements = 75857 238679 AFLR3 : CPU Time = 2.413 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 75857 238679 AFLR3 GG : Nodes, Elements = 97036 302794 AFLR3 GG : Nodes, Elements = 97036 381323 AFLR3 GG : Nodes, Elements = 97036 348553 AFLR3 GG : Nodes, Elements = 114433 404125 AFLR3 GG : Nodes, Elements = 114433 479502 AFLR3 GG : Nodes, Elements = 114433 449390 AFLR3 GG : Nodes, Elements = 137578 521259 AFLR3 GG : Nodes, Elements = 137578 620175 AFLR3 GG : Nodes, Elements = 137578 582534 AFLR3 GG : Nodes, Elements = 137578 570299 AFLR3 GG : Nodes, Elements = 162763 647836 AFLR3 GG : Nodes, Elements = 162763 770341 AFLR3 GG : Nodes, Elements = 162763 731548 AFLR3 GG : Nodes, Elements = 190585 816203 AFLR3 GG : Nodes, Elements = 190585 935984 AFLR3 GG : Nodes, Elements = 190585 899107 AFLR3 GG : Nodes, Elements = 219816 987499 AFLR3 GG : Nodes, Elements = 219816 1108410 AFLR3 GG : Nodes, Elements = 219816 1073232 AFLR3 GG : Nodes, Elements = 250105 1164614 AFLR3 GG : Nodes, Elements = 250105 1287642 AFLR3 GG : Nodes, Elements = 250105 1252761 AFLR3 GG : Nodes, Elements = 279892 1342494 AFLR3 GG : Nodes, Elements = 279892 1462443 AFLR3 GG : Nodes, Elements = 279892 1429923 AFLR3 GG : Nodes, Elements = 309074 1517784 AFLR3 GG : Nodes, Elements = 309074 1634324 AFLR3 GG : Nodes, Elements = 309074 1603191 AFLR3 GG : Nodes, Elements = 337155 1687725 AFLR3 GG : Nodes, Elements = 337155 1799086 AFLR3 GG : Nodes, Elements = 337155 1770201 AFLR3 GG : Nodes, Elements = 364031 1851037 AFLR3 GG : Nodes, Elements = 364031 1958040 AFLR3 GG : Nodes, Elements = 364031 1929929 AFLR3 GG : Nodes, Elements = 389893 2007694 AFLR3 GG : Nodes, Elements = 389893 2110445 AFLR3 GG : Nodes, Elements = 389893 2083831 AFLR3 GG : Nodes, Elements = 414588 2158046 AFLR3 GG : Nodes, Elements = 414588 2256223 AFLR3 GG : Nodes, Elements = 414588 2230399 AFLR3 GG : Nodes, Elements = 437949 2300612 AFLR3 GG : Nodes, Elements = 437949 2392665 AFLR3 GG : Nodes, Elements = 437949 2369220 AFLR3 GG : Nodes, Elements = 460028 2435556 AFLR3 GG : Nodes, Elements = 460028 2523443 AFLR3 GG : Nodes, Elements = 460028 2500481 AFLR3 GG : Nodes, Elements = 481028 2563562 AFLR3 GG : Nodes, Elements = 481028 2645943 AFLR3 GG : Nodes, Elements = 481028 2625418 AFLR3 GG : Nodes, Elements = 500564 2684111 AFLR3 GG : Nodes, Elements = 500564 2760869 AFLR3 GG : Nodes, Elements = 500564 2741486 AFLR3 GG : Nodes, Elements = 519023 2796921 AFLR3 GG : Nodes, Elements = 519023 2869294 AFLR3 GG : Nodes, Elements = 519023 2851235 AFLR3 GG : Nodes, Elements = 536227 2902907 AFLR3 GG : Nodes, Elements = 536227 2970978 AFLR3 GG : Nodes, Elements = 536227 2953488 AFLR3 GG : Nodes, Elements = 552417 3002099 AFLR3 GG : Nodes, Elements = 552417 3066275 AFLR3 GG : Nodes, Elements = 552417 3049807 AFLR3 GG : Nodes, Elements = 567559 3095278 AFLR3 GG : Nodes, Elements = 567559 3155304 AFLR3 GG : Nodes, Elements = 567559 3139713 AFLR3 GG : Nodes, Elements = 581855 3182642 AFLR3 GG : Nodes, Elements = 581855 3239064 AFLR3 GG : Nodes, Elements = 581855 3224765 AFLR3 GG : Nodes, Elements = 595142 3264660 AFLR3 GG : Nodes, Elements = 595142 3317200 AFLR3 GG : Nodes, Elements = 595142 3303799 AFLR3 GG : Nodes, Elements = 607536 3341007 AFLR3 GG : Nodes, Elements = 607536 3389453 AFLR3 GG : Nodes, Elements = 607536 3377251 AFLR3 GG : Nodes, Elements = 619010 3411685 AFLR3 GG : Nodes, Elements = 619010 3457021 AFLR3 GG : Nodes, Elements = 619010 3445397 AFLR3 GG : Nodes, Elements = 629458 3476760 AFLR3 GG : Nodes, Elements = 629458 3517836 AFLR3 GG : Nodes, Elements = 629458 3507282 AFLR3 GG : Nodes, Elements = 638979 3535863 AFLR3 GG : Nodes, Elements = 638979 3573549 AFLR3 GG : Nodes, Elements = 638979 3563786 AFLR3 GG : Nodes, Elements = 647722 3590028 AFLR3 GG : Nodes, Elements = 647722 3624053 AFLR3 GG : Nodes, Elements = 647722 3615570 AFLR3 GG : Nodes, Elements = 655612 3639251 AFLR3 GG : Nodes, Elements = 655612 3670585 AFLR3 GG : Nodes, Elements = 655612 3662351 AFLR3 GG : Nodes, Elements = 662779 3683858 AFLR3 GG : Nodes, Elements = 662779 3712160 AFLR3 GG : Nodes, Elements = 662779 3704757 AFLR3 GG : Nodes, Elements = 669454 3724790 AFLR3 GG : Nodes, Elements = 669454 3750712 AFLR3 GG : Nodes, Elements = 669454 3744123 AFLR3 GG : Nodes, Elements = 675397 3761956 AFLR3 GG : Nodes, Elements = 675397 3785252 AFLR3 GG : Nodes, Elements = 675397 3779313 AFLR3 GG : Nodes, Elements = 680809 3795555 AFLR3 GG : Nodes, Elements = 680809 3817005 AFLR3 GG : Nodes, Elements = 680809 3811333 AFLR3 GG : Nodes, Elements = 685665 3825906 AFLR3 GG : Nodes, Elements = 685665 3844891 AFLR3 GG : Nodes, Elements = 685665 3840070 AFLR3 GG : Nodes, Elements = 690086 3853337 AFLR3 GG : Nodes, Elements = 690086 3871017 AFLR3 GG : Nodes, Elements = 690086 3866262 AFLR3 GG : Nodes, Elements = 694035 3878112 AFLR3 GG : Nodes, Elements = 694035 3893779 AFLR3 GG : Nodes, Elements = 694035 3889637 AFLR3 GG : Nodes, Elements = 697620 3900399 AFLR3 GG : Nodes, Elements = 697620 3914441 AFLR3 GG : Nodes, Elements = 697620 3910923 AFLR3 GG : Nodes, Elements = 700718 3920220 AFLR3 GG : Nodes, Elements = 700718 3932327 AFLR3 GG : Nodes, Elements = 700718 3929172 AFLR3 GG : Nodes, Elements = 703391 3937194 AFLR3 GG : Nodes, Elements = 703391 3947746 AFLR3 GG : Nodes, Elements = 703391 3944953 AFLR3 GG : Nodes, Elements = 705696 3951869 AFLR3 GG : Nodes, Elements = 705696 3960843 AFLR3 GG : Nodes, Elements = 705696 3958600 AFLR3 GG : Nodes, Elements = 707556 3964183 AFLR3 GG : Nodes, Elements = 707556 3971425 AFLR3 GG : Nodes, Elements = 707556 3969536 AFLR3 GG : Nodes, Elements = 709105 3974184 AFLR3 GG : Nodes, Elements = 709105 3980363 AFLR3 GG : Nodes, Elements = 709105 3978685 AFLR3 GG : Nodes, Elements = 710382 3982517 AFLR3 GG : Nodes, Elements = 710382 3987670 AFLR3 GG : Nodes, Elements = 710382 3986193 AFLR3 GG : Nodes, Elements = 711500 3989547 AFLR3 GG : Nodes, Elements = 711500 3993879 AFLR3 GG : Nodes, Elements = 711500 3992791 AFLR3 GG : Nodes, Elements = 712386 3995449 AFLR3 GG : Nodes, Elements = 712386 3998928 AFLR3 GG : Nodes, Elements = 712386 3997984 AFLR3 GG : Nodes, Elements = 713092 4000102 AFLR3 GG : Nodes, Elements = 713092 4002840 AFLR3 GG : Nodes, Elements = 713092 4002110 AFLR3 GG : Nodes, Elements = 713683 4003883 AFLR3 GG : Nodes, Elements = 713683 4006165 AFLR3 GG : Nodes, Elements = 713683 4005545 AFLR3 GG : Nodes, Elements = 714102 4006803 AFLR3 GG : Nodes, Elements = 714102 4008493 AFLR3 GG : Nodes, Elements = 714102 4007992 AFLR3 GG : Nodes, Elements = 714383 4008836 AFLR3 GG : Nodes, Elements = 714383 4009992 AFLR3 GG : Nodes, Elements = 714383 4009630 AFLR3 GG : Nodes, Elements = 714565 4010176 AFLR3 GG : Nodes, Elements = 714565 4010905 AFLR3 GG : Nodes, Elements = 714565 4010667 AFLR3 GG : Nodes, Elements = 714710 4011102 AFLR3 GG : Nodes, Elements = 714710 4011707 AFLR3 GG : Nodes, Elements = 714710 4011510 AFLR3 GG : Nodes, Elements = 714817 4011832 AFLR3 GG : Nodes, Elements = 714817 4012263 AFLR3 GG : Nodes, Elements = 714817 4012113 AFLR3 GG : Nodes, Elements = 714886 4012320 AFLR3 GG : Nodes, Elements = 714886 4012623 AFLR3 GG : Nodes, Elements = 714886 4012501 AFLR3 GG : Nodes, Elements = 714931 4012636 AFLR3 GG : Nodes, Elements = 714931 4012830 AFLR3 GG : Nodes, Elements = 714931 4012764 AFLR3 GG : Nodes, Elements = 714965 4012866 AFLR3 GG : Nodes, Elements = 714965 4013013 AFLR3 GG : Nodes, Elements = 714965 4012950 AFLR3 GG : Nodes, Elements = 714994 4013037 AFLR3 GG : Nodes, Elements = 714994 4013157 AFLR3 GG : Nodes, Elements = 714994 4013121 AFLR3 GG : Nodes, Elements = 715020 4013199 AFLR3 GG : Nodes, Elements = 715020 4013311 AFLR3 GG : Nodes, Elements = 715020 4013266 AFLR3 GG : Nodes, Elements = 715040 4013326 AFLR3 GG : Nodes, Elements = 715040 4013398 AFLR3 GG : Nodes, Elements = 715040 4013378 AFLR3 GG : Nodes, Elements = 715056 4013426 AFLR3 GG : Nodes, Elements = 715056 4013497 AFLR3 GG : Nodes, Elements = 715056 4013477 AFLR3 GG : Nodes, Elements = 715069 4013516 AFLR3 GG : Nodes, Elements = 715069 4013568 AFLR3 GG : Nodes, Elements = 715069 4013551 AFLR3 GG : Nodes, Elements = 715076 4013572 AFLR3 GG : Nodes, Elements = 715076 4013609 AFLR3 GG : Nodes, Elements = 715076 4013590 AFLR3 GG : Nodes, Elements = 715080 4013602 AFLR3 GG : Nodes, Elements = 715080 4013619 AFLR3 GG : Nodes, Elements = 715080 4013611 AFLR3 GG : Nodes, Elements = 715221 4014034 AFLR3 GG : Nodes, Elements = 715221 4014794 AFLR3 GG : Nodes, Elements = 715221 4014418 AFLR3 GG : Nodes, Elements = 715295 4014640 AFLR3 GG : Nodes, Elements = 715295 4014974 AFLR3 GG : Nodes, Elements = 715295 4014832 AFLR3 GG : Nodes, Elements = 715340 4014967 AFLR3 GG : Nodes, Elements = 715340 4015216 AFLR3 GG : Nodes, Elements = 715340 4015085 AFLR3 GG : Nodes, Elements = 715398 4015259 AFLR3 GG : Nodes, Elements = 715398 4015521 AFLR3 GG : Nodes, Elements = 715398 4015431 AFLR3 GG : Nodes, Elements = 715428 4015521 AFLR3 GG : Nodes, Elements = 715428 4015681 AFLR3 GG : Nodes, Elements = 715428 4015602 AFLR3 GG : Nodes, Elements = 715441 4015641 AFLR3 GG : Nodes, Elements = 715441 4015712 AFLR3 GG : Nodes, Elements = 715441 4015681 AFLR3 GG : Nodes, Elements = 715446 4015696 AFLR3 GG : Nodes, Elements = 715446 4015717 AFLR3 GG : Nodes, Elements = 715446 4015706 AFLR3 GG : Nodes, Elements = 715447 4015709 AFLR3 GG : Nodes, Elements = 715447 4015712 AFLR3 GG : Nodes, Elements = 715447 4015710 AFLR3 : CPU Time = 48.708 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 715447 4015710 AFLR3 QI : Nodes, Elements = 708655 3977757 AFLR3 QI : Nodes, Elements = 706642 3966512 AFLR3 QI : Nodes, Elements = 706080 3963343 AFLR3 QI : Nodes, Elements = 705965 3962681 AFLR3 QI : Nodes, Elements = 705940 3962544 AFLR3 QI : Nodes, Elements = 705936 3962520 AFLR3 QI : Nodes, Elements = 705936 3980235 AFLR3 QI : Nodes, Elements = 705936 3958971 AFLR3 QI : Nodes, Elements = 705936 3950968 AFLR3 QI : Nodes, Elements = 705936 3964620 AFLR3 QI : Nodes, Elements = 705936 3950929 AFLR3 QI : Nodes, Elements = 705936 3950401 AFLR3 QI : Nodes, Elements = 705936 3963184 AFLR3 QI : Nodes, Elements = 705936 3950747 AFLR3 QI : Nodes, Elements = 705936 3950348 AFLR3 QI : Nodes, Elements = 705936 3962853 AFLR3 QI : Nodes, Elements = 705936 3950630 AFLR3 QI : Nodes, Elements = 705936 3950330 AFLR3 QI : Nodes, Elements = 705936 3962713 AFLR3 QI : Nodes, Elements = 705936 3950584 AFLR3 QI : Nodes, Elements = 705936 3950299 AFLR3 QI : Nodes, Elements = 705936 3950298 AFLR3 QI : Nodes, Elements = 705962 3950412 AFLR3 QI : Nodes, Elements = 705962 3962907 AFLR3 QI : Nodes, Elements = 705962 3950755 AFLR3 QI : Nodes, Elements = 705962 3950478 AFLR3 QI : Nodes, Elements = 705962 3962751 AFLR3 QI : Nodes, Elements = 705962 3950718 AFLR3 QI : Nodes, Elements = 705962 3950478 AFLR3 : CPU Time = 14.899 seconds AFLR3 QRG: QUALITY GRID RE-GENERATION AFLR3 QRG: Nodes, Elements = 705962 3950478 AFLR3 QRG: Nodes, Elements = 705956 3950446 AFLR3 QRG: Nodes, Elements = 705950 3950421 AFLR3 QRG: Nodes, Elements = 705949 3950418 AFLR3 QRG: Nodes, Elements = 705947 3950409 AFLR3 QRG: Nodes, Elements = 705945 3950399 AFLR3 QRG: Nodes, Elements = 705963 3950505 AFLR3 QRG: Nodes, Elements = 705960 3950492 AFLR3 QRG: Nodes, Elements = 705958 3950483 AFLR3 QRG: Nodes, Elements = 705955 3950470 AFLR3 QRG: Nodes, Elements = 705954 3950465 AFLR3 QRG: Nodes, Elements = 705954 3950467 AFLR3 QRG: Nodes, Elements = 705953 3950463 AFLR3 QRG: Nodes, Elements = 705952 3950459 AFLR3 QRG: Nodes, Elements = 705951 3950455 AFLR3 QRG: Nodes, Elements = 705950 3950452 AFLR3 QRG: Nodes, Elements = 705949 3950449 AFLR3 QRG: Nodes, Elements = 705948 3950445 AFLR3 QRG: Nodes, Elements = 705947 3950439 AFLR3 QRG: Nodes, Elements = 705948 3950443 AFLR3 QRG: Nodes, Elements = 705947 3950439 AFLR3 QRG: Nodes, Elements = 705946 3950435 AFLR3 QRG: Nodes, Elements = 705971 3950587 AFLR3 QRG: Nodes, Elements = 705970 3950583 AFLR3 QRG: Nodes, Elements = 705969 3950579 AFLR3 QRG: Nodes, Elements = 705976 3950614 AFLR3 QRG: Nodes, Elements = 705977 3950623 AFLR3 QRG: Nodes, Elements = 706039 3950970 AFLR3 : CPU Time = 0.352 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 3950970 UG3 : Min, Max Ang = 0.00123 180 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 182 UG3 : No. Angle>179.9 = 8 UG3 : VOL CHECK UG3 : Total-Volume = 5.96e+10 UG3 : No. Tet Elems = 3950970 UG3 : Min Vol = 6.4e-09 UG3 : Average Vol = 1.51e+04 UG3 : Total-Tet-Vol = 5.96e+10 UG3 : No. Vol160.0 = 182 UG3 : No. Angle>179.9 = 8 UG3 : VOL CHECK UG3 : Total-Volume = 5.96e+10 UG3 : No. Tet Elems = 3950970 UG3 : Min Vol = 6.4e-09 UG3 : Average Vol = 1.51e+04 UG3 : Total-Tet-Vol = 5.96e+10 UG3 : No. Vol. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.5. Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 4240 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 195.346 m. Reference origin for moment evaluation is (55.4263, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Input mesh file name: ../aflr3/aflr3_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-8. 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| | PARAVIEW| 250| | SURFACE_PARAVIEW| 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_inviscidWing.dat. Surface file name: surface_flow_inviscidWing. Volume file name: flow_inviscidWing. Restart file name: restart_flow_inviscidWing.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 706039 grid points. 3950970 volume elements. 2 surface markers. 151670 boundary elements in index 0 (Marker = BC_1). 36 boundary elements in index 1 (Marker = BC_2). 3950970 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 5.96352e+10. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 122.726. Mean K: 4.02932. Standard deviation K: 11.9593. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 12.0095| 87.3048| | CV Face Area Aspect Ratio| 1.03091| 15816.5| | CV Sub-Volume Ratio| 1.00173| 567326| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 706039| 1/1.00| 10| | 1| 116093| 1/6.08| 8.2177| | 2| 17733| 1/6.55| 6.58922| +-------------------------------------------+ Finding max control volume width. Semi-span length = 97.6729 m. Wetted area = 8795.17 m^2. Area projection in the x-plane = 681.45 m^2, y-plane = 449.381 m^2, z-plane = 4224.13 m^2. Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m. Min. coordinate in the x-direction = 49.9621 m, y-direction = -97.6729 m, z-direction = -8.47903 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. 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| 221265| 1| m^2/s^2| 221265| | Velocity-X| 170.123| 1| m/s| 170.123| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 2.9695| 1| m/s| 2.9695| | Velocity Magnitude| 170.149| 1| m/s| 170.149| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.5| +------------------------------------------------------------------------------+ 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| 1.2660e+01| 0.413477| 2.693384| 2.166473| 5.896322| -0.410143| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.2355e+01| 3.050554| 5.559574| 5.273010| 8.536816| -0.135737| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.1482e+01| 4.801359| 7.342376| 6.970135| 10.293693| 14.702205| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.1075e+01| 6.706527| 9.081364| 9.135145| 12.120102| -66.410775| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.0784e+01| 6.306706| 8.650493| 8.379244| 11.723915| -15.500630| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.0621e+01| 5.992382| 8.154250| 8.212880| 11.438780| 95.651198| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.0511e+01| 6.230651| 8.555249| 8.572561| 11.716780| 18.259965| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.0356e+01| 6.372540| 8.839403| 8.672407| 11.840955| 27.521211| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.0277e+01| 6.462239| 8.690028| 8.766410| 11.848066| 7.259007| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.0224e+01| 6.377436| 8.657118| 8.783328| 11.816921| 11.546451| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 6.37744| < -8| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_inviscidWing.dat | Writing the forces breakdown file (forces_breakdown_inviscidWing.dat). |CSV file |surface_flow_inviscidWing.csv | Writing the forces breakdown file (forces_breakdown_inviscidWing.dat). |Paraview |flow_inviscidWing.vtu | Writing the forces breakdown file (forces_breakdown_inviscidWing.dat). |Paraview surface |surface_flow_inviscidWing.vtu | Writing the forces breakdown file (forces_breakdown_inviscidWing.dat). +-----------------------------------------------------------------------+ Warning: there are 774 non-physical points in the solution. Warning: 21 reconstructed states for upwinding are non-physical. --------------------------- 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 Forces and Moments --> Cl = -3.418779 Cd = -0.296089 --> Cmx = 0.005741 Cmy = 0.587705 Cmz = 0.008331 --> Cx = -0.236378 Cy = 0.038895 Cz = -3.423426 real 4m27.696s user 4m20.454s sys 0m5.544s + status=0 + set +x ================================================= data/session08/2_su2_InviscidWing.py passed (as expected) ================================================= ================================================= 1_astros_ModalCantilever.py test; + python 1_astros_ModalCantilever.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... ==> Running mASTROS pre-analysis... MESSAGE:: Building wingOml MESSAGE:: Building wingWaffle Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = wingSpar1, index = 1 Name = wingSpar2, index = 2 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 425 Number of elements = 482 Number of triangle elements = 0 Number of quadrilateral elements = 482 ---------------------------- Total number of nodes = 425 Total number of elements = 482 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 = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 4 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Name = leftPointLoad, index = 3 Name = ritePointLoad, index = 4 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 425 Number of elements = 482 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 482 Aero_Reference value is NULL - No aero reference parameters set 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 - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... ==> Running mASTROS post-analysis... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 --> Eigen-frequencies: 1 : 0.00145606 2 : 0.0014575 3 : 0.00332859 4 : 0.00333096 5 : 0.00445176 6 : 0.00445507 7 : 0.00894917 8 : 0.0089521 9 : 0.0110353 10: 0.0110413 real 0m49.061s user 0m37.316s sys 0m31.659s + status=0 + set +x ================================================= data/session09/1_astros_ModalCantilever.py passed (as expected) ================================================= ================================================= 2_astros_ModalSupport.py test; + python 2_astros_ModalSupport.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... ==> Running mASTROS pre-analysis... MESSAGE:: Building wingOml MESSAGE:: Building wingWaffle Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Name = ribSupport, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = wingSpar1, index = 1 Name = wingSpar2, 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 = 831 Number of elements = 962 Number of triangle elements = 0 Number of quadrilateral elements = 962 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 = 832 Total number of elements = 962 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 = 1 Name = ribRootPoint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = leftPointLoad, index = 1 Name = ritePointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = ribRoot, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Name = ribSupport, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 831 Number of elements = 962 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 962 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 = 832 Combined Number of elements = 963 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 962 Aero_Reference value is NULL - No aero reference parameters set 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 - 6 Property name - leftWingSkin Property name - ribSupport Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribRootPoint No "constraintType" specified for Constraint tuple ribRootPoint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple ribRootPoint, going to use constraint name Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribRootPoint No "groupName" specified for Support tuple ribRootPoint, going to use support name Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - ribRoot No "groupName" specified for Connection tuple ribRoot! Looking for automatic connections from the use of capsConnectLink for ribRoot 9 automatic connections were made for capsConnect ribRoot (node id 832) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing support cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... ==> Running mASTROS post-analysis... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 --> Eigen-frequencies: 1 : 1.54136e-08 2 : 0.00142051 3 : 0.0017451 4 : 0.00323704 5 : 0.00324885 6 : 0.00432995 7 : 0.00512483 8 : 0.0087361 9 : 0.010063 10: 0.0107025 real 2m45.167s user 2m24.278s sys 0m56.037s + status=0 + set +x ================================================= data/session09/2_astros_ModalSupport.py passed (as expected) ================================================= ================================================= 3_astros_StaticCantilever.py test; + python 3_astros_StaticCantilever.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... ==> Running mASTROS pre-analysis... MESSAGE:: Building wingOml MESSAGE:: Building wingWaffle Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = wingSpar1, index = 1 Name = wingSpar2, index = 2 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 425 Number of elements = 482 Number of triangle elements = 0 Number of quadrilateral elements = 482 ---------------------------- Total number of nodes = 425 Total number of elements = 482 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 = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 4 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Name = leftPointLoad, index = 3 Name = ritePointLoad, index = 4 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 425 Number of elements = 482 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 482 Aero_Reference value is NULL - No aero reference parameters set 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 - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - leftPointLoad No "groupName" specified for Load tuple leftPointLoad, going to use load name Load name - ritePointLoad No "groupName" specified for Load tuple ritePointLoad, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG ==> Running mASTROS post-analysis... --> Maximum displacements: --> Tmax 238433.3403112283 --> T1max 16861.9 --> T2max 16414.9 --> T3max 237286.0 real 0m13.412s user 0m17.403s sys 0m16.064s + status=0 + set +x ================================================= data/session09/3_astros_StaticCantilever.py passed (as expected) ================================================= ================================================= 4_astros_Composite.py test; + python 4_astros_Composite.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log ==> Loading geometry from file "../ESP/transport.csm"... MESSAGE:: Building wingOml MESSAGE:: Building wingWaffle ==> Running mASTROS pre-analysis... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = wingSpar1, index = 1 Name = wingSpar2, index = 2 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 425 Number of elements = 482 Number of triangle elements = 0 Number of quadrilateral elements = 482 ---------------------------- Total number of nodes = 425 Total number of elements = 482 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 = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 4 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Name = leftPointLoad, index = 3 Name = ritePointLoad, index = 4 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 425 Number of elements = 482 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 482 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Aluminum No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic" Material name - Graphite_epoxy Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - leftPointLoad No "groupName" specified for Load tuple leftPointLoad, going to use load name Load name - ritePointLoad No "groupName" specified for Load tuple ritePointLoad, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG ==> Running mASTROS post-analysis... --> Maximum displacements: --> Tmax 52594.60117638786 --> T1max 4359.68 --> T2max 3216.5 --> T3max 52322.2 real 0m13.591s user 0m17.513s sys 0m16.904s + status=0 + set +x ================================================= data/session09/4_astros_Composite.py passed (as expected) ================================================= [VIGGEN.MIT.EDU:48819] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/220266496/sm_segment.VIGGEN.502.d210000.0 could be created. ================================================= 6_tacs_StaticCantilever.py test; + python 6_tacs_StaticCantilever.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:48829] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/4251910144/sm_segment.VIGGEN.502.fd6f0000.0 could be created. ==> Loading geometry from file "../ESP/transport.csm"... ==> Running TACS pre-analysis... MESSAGE:: Building wingOml MESSAGE:: Building wingWaffle Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = wingSpar1, index = 1 Name = wingSpar2, index = 2 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 425 Number of elements = 482 Number of triangle elements = 0 Number of quadrilateral elements = 482 ---------------------------- Total number of nodes = 425 Total number of elements = 482 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 = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 4 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Name = leftPointLoad, index = 3 Name = ritePointLoad, index = 4 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 425 Number of elements = 482 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 482 Getting FEA materials....... Number of materials - 1 Material name - aluminum Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - leftWingSkin No "groupName" specified for Load tuple leftWingSkin, going to use load name Load name - riteWingSkin No "groupName" specified for Load tuple riteWingSkin, going to use load name Done getting FEA loads Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing coordinate system cards [0] Creating TACSAssembler with numOwnedNodes = 425 numElements = 482 [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 2.84, nnz(ILU) = 11729 ==> Running TACS... ==> Running TACS post-analysis... Tacs Analysis Outputs... functional mass = 511406.7093694836 functional ks_vmfailure = 0.01913505172742016 real 0m14.522s user 0m17.266s sys 0m15.625s + status=0 + set +x ================================================= data/session09/6_tacs_StaticCantilever.py passed (as expected) ================================================= ================================================= 7_tacs_sizing.py test; + python 7_tacs_sizing.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log [VIGGEN.MIT.EDU:48857] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/1939013632/sm_segment.VIGGEN.502.73930000.0 could be created. ==> Loading geometry from file "../ESP/transport.csm"... ==> Starting optimization... MESSAGE:: Building wingOml MESSAGE:: Building wingWaffle Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = wingSpar1, index = 1 Name = wingSpar2, index = 2 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 3852 Number of elements = 4061 Number of triangle elements = 0 Number of quadrilateral elements = 4061 ---------------------------- Total number of nodes = 3852 Total number of elements = 4061 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 = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 4 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Name = leftPointLoad, index = 3 Name = ritePointLoad, index = 4 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 3852 Number of elements = 4061 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 4061 Getting FEA materials....... Number of materials - 1 Material name - aluminum Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - leftWingSkin No "groupName" specified for Load tuple leftWingSkin, going to use load name Load name - riteWingSkin No "groupName" specified for Load tuple riteWingSkin, going to use load name Done getting FEA loads Getting FEA design variables....... Number of design variables - 3 Design_Variable name - ribThk Design_Variable name - skinThk Design_Variable name - sparThk Design_Variable_Relation name - relLeftSkin Design_Variable_Relation name - relRib Design_Variable_Relation name - relRiteSkin Design_Variable_Relation name - relSpar Number of design variable relations - 4 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing coordinate system cards Writing design variable cards Writing design variable relation cards [0] Creating TACSAssembler with numOwnedNodes = 3852 numElements = 4061 [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session09/7_tacs_sizing.py:144: DeprecationWarning: Conversion of an array with ndim > 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.) xarray[ithick] = float(inputs[thick_dv]) --> ribThk [0.05] --> skinThk [0.003] --> sparThk [0.1] --> mass [351348.85842654] --> ks_vmfailure [0.1846542] --> mass [351348.85842654] --> ks_vmfailure [0.1846542] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00701648]] --> ks_vmfailure skinThk [[-0.77735853]] --> ks_vmfailure sparThk [[-0.0041996]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.001] --> skinThk [0.0073915] --> sparThk [0.001] --> mass [164785.66958227] --> ks_vmfailure [0.18458243] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.27196737]] --> ks_vmfailure skinThk [[-0.30937548]] --> ks_vmfailure sparThk [[-0.20964257]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.001] --> skinThk [0.001] --> sparThk [0.02275036] --> mass [129250.70931662] --> ks_vmfailure [0.202395] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.001] --> skinThk [0.00647724] --> sparThk [0.00411124] --> mass [159702.63601836] --> ks_vmfailure [0.1846874] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.28436096]] --> ks_vmfailure skinThk [[-0.36624822]] --> ks_vmfailure sparThk [[-0.04559206]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.01796767] --> skinThk [0.001] --> sparThk [0.0012266] --> mass [135757.93266609] --> ks_vmfailure [0.20100422] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00335945] --> skinThk [0.0057156] --> sparThk [0.00371011] --> mass [156372.98610093] --> ks_vmfailure [0.184766] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.04729604]] --> ks_vmfailure skinThk [[-0.42959551]] --> ks_vmfailure sparThk [[-0.0555554]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00375231] --> skinThk [0.01186673] --> sparThk [0.00559871] --> mass [221373.85547163] --> ks_vmfailure [0.18335011] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00339874] --> skinThk [0.00633071] --> sparThk [0.00389897] --> mass [162873.073038] --> ks_vmfailure [0.18451376] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00336363] --> skinThk [0.00578104] --> sparThk [0.00373021] --> mass [157064.50395361] --> ks_vmfailure [0.18473687] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.04666555]] --> ks_vmfailure skinThk [[-0.42080693]] --> ks_vmfailure sparThk [[-0.05455913]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.001] --> skinThk [0.01144045] --> sparThk [0.01226502] --> mass [220214.90621319] --> ks_vmfailure [0.18348938] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.22365806]] --> ks_vmfailure skinThk [[-0.11520218]] --> ks_vmfailure sparThk [[-0.00935336]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.0072684] --> skinThk [0.01192856] --> sparThk [0.01559744] --> mass [242347.90075183] --> ks_vmfailure [0.18318684] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00374641] --> skinThk [0.01165431] --> sparThk [0.01372508] --> mass [229912.18133305] --> ks_vmfailure [0.18327621] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00242408] --> skinThk [0.01155134] --> sparThk [0.01302209] --> mass [225243.1650107] --> ks_vmfailure [0.1833334] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.0434139]] --> ks_vmfailure skinThk [[-0.10912079]] --> ks_vmfailure sparThk [[-0.00870169]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00273287] --> skinThk [0.02302448] --> sparThk [0.0208413] --> mass [351261.40661445] --> ks_vmfailure [0.18265034] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.0024606] --> skinThk [0.01290839] --> sparThk [0.01394695] --> mass [240148.65608909] --> ks_vmfailure [0.18319167] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.04034006]] --> ks_vmfailure skinThk [[-0.08778047]] --> ks_vmfailure sparThk [[-0.00731659]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.006155] --> skinThk [0.0257837] --> sparThk [0.00197909] --> mass [361169.22513746] --> ks_vmfailure [0.18264483] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00640593]] --> ks_vmfailure skinThk [[-0.02501034]] --> ks_vmfailure sparThk [[-0.04889085]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00712924] --> skinThk [0.0266472] --> sparThk [0.01459881] --> mass [388418.28899787] --> ks_vmfailure [0.18252538] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00664408] --> skinThk [0.02621719] --> sparThk [0.00831441] --> mass [374848.72598794] --> ks_vmfailure [0.18255641] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00573855]] --> ks_vmfailure skinThk [[-0.02377713]] --> ks_vmfailure sparThk [[-0.00357553]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.01009093] --> skinThk [0.04871646] --> sparThk [0.00877853] --> mass [608257.37495975] --> ks_vmfailure [0.18224988] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.00758534] --> skinThk [0.03236121] --> sparThk [0.00844115] --> mass [438587.11278419] --> ks_vmfailure [0.18243234] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00425207]] --> ks_vmfailure skinThk [[-0.01579314]] --> ks_vmfailure sparThk [[-0.00300188]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.0124328] --> skinThk [0.05769986] --> sparThk [0.01228772] --> mass [707801.04480008] --> ks_vmfailure [0.1821848] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00154459]] --> ks_vmfailure skinThk [[-0.00512032]] --> ks_vmfailure sparThk [[-0.00130412]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.01950989] --> skinThk [0.08934871] --> sparThk [0.0213468] --> mass [1051747.85053898] --> ks_vmfailure [0.1820658] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00063906]] --> ks_vmfailure skinThk [[-0.00214823]] --> ks_vmfailure sparThk [[-0.00044876]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.02583689] --> skinThk [0.11659568] --> sparThk [0.02854152] --> mass [1347542.82109991] --> ks_vmfailure [0.18201544] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00036949]] --> ks_vmfailure skinThk [[-0.001262]] --> ks_vmfailure sparThk [[-0.00025396]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.02866513] --> skinThk [0.12727245] --> sparThk [0.03216313] --> mass [1465220.87471137] --> ks_vmfailure [0.18200133] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00030315]] --> ks_vmfailure skinThk [[-0.0010584]] --> ks_vmfailure sparThk [[-0.00020293]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.02925022] --> skinThk [0.12815145] --> sparThk [0.03326292] --> mass [1476685.21150207] --> ks_vmfailure [0.18200002] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00029294]] --> ks_vmfailure skinThk [[-0.00104297]] --> ks_vmfailure sparThk [[-0.00019215]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.03009621] --> skinThk [0.1275515] --> sparThk [0.03531214] --> mass [1475094.60332159] --> ks_vmfailure [0.18200002] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00028081]] --> ks_vmfailure skinThk [[-0.00105015]] --> ks_vmfailure sparThk [[-0.00017649]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.0328392] --> skinThk [0.12577741] --> sparThk [0.04163974] --> mass [1471238.3581688] --> ks_vmfailure [0.18200018] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00024714]] --> ks_vmfailure skinThk [[-0.00107055]] --> ks_vmfailure sparThk [[-0.00014459]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.03383625] --> skinThk [0.12543563] --> sparThk [0.04369691] --> mass [1472558.27241667] --> ks_vmfailure [0.18200001] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00023649]] --> ks_vmfailure skinThk [[-0.00107307]] --> ks_vmfailure sparThk [[-0.00013766]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.03427623] --> skinThk [0.12525038] --> sparThk [0.04448082] --> mass [1472632.44194227] --> ks_vmfailure [0.182] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00023207]] --> ks_vmfailure skinThk [[-0.00107486]] --> ks_vmfailure sparThk [[-0.00013542]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.03444291] --> skinThk [0.12519626] --> sparThk [0.04463972] --> mass [1472640.20078909] --> ks_vmfailure [0.182] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.0002304]] --> ks_vmfailure skinThk [[-0.00107543]] --> ks_vmfailure sparThk [[-0.00013502]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.0348802] --> skinThk [0.12509099] --> sparThk [0.04473341] --> mass [1472603.98217904] --> ks_vmfailure [0.182] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00022607]] --> ks_vmfailure skinThk [[-0.0010767]] --> ks_vmfailure sparThk [[-0.00013492]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.03534323] --> skinThk [0.12504137] --> sparThk [0.04436116] --> mass [1472566.46844939] --> ks_vmfailure [0.182] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00022152]] --> ks_vmfailure skinThk [[-0.00107758]] --> ks_vmfailure sparThk [[-0.00013618]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.0356444] --> skinThk [0.125092] --> sparThk [0.04348019] --> mass [1472534.17646355] --> ks_vmfailure [0.182] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00021851]] --> ks_vmfailure skinThk [[-0.00107752]] --> ks_vmfailure sparThk [[-0.00013901]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.03558665] --> skinThk [0.12517522] --> sparThk [0.04293808] --> mass [1472538.0779954] --> ks_vmfailure [0.182] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00021892]] --> ks_vmfailure skinThk [[-0.0010768]] --> ks_vmfailure sparThk [[-0.00014078]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.03548923] --> skinThk [0.12520791] --> sparThk [0.0428432] --> mass [1472541.53467339] --> ks_vmfailure [0.182] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.0002198]] --> ks_vmfailure skinThk [[-0.00107644]] --> ks_vmfailure sparThk [[-0.00014107]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.03546489] --> skinThk [0.12521187] --> sparThk [0.04285139] --> mass [1472542.05815828] --> ks_vmfailure [0.182] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00022003]] --> ks_vmfailure skinThk [[-0.00107639]] --> ks_vmfailure sparThk [[-0.00014103]] [0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414 --> ribThk [0.03546431] --> skinThk [0.12521175] --> sparThk [0.04285324] --> mass [1472542.08686109] --> ks_vmfailure [0.182] --> mass ribThk [[2050883.76790736]] --> mass skinThk [[10032748.65482082]] --> mass sparThk [[1314431.32692686]] --> ks_vmfailure ribThk [[-0.00022003]] --> ks_vmfailure skinThk [[-0.00107639]] --> ks_vmfailure sparThk [[-0.00014102]] Optimization terminated successfully (Exit mode 0) Current function value: 4.207263105317389 Iterations: 28 Function evaluations: 37 Gradient evaluations: 28 Optimization Complete ----------------------------------- ==> Optimized value: --> ribThk [0.03546431] --> skinThk [0.12521175] --> sparThk [0.04285324] real 0m40.197s user 0m44.922s sys 0m15.676s + status=0 + set +x ================================================= data/session09/7_tacs_sizing.py passed (as expected) ================================================= ================================================= 2_aeroelastic_Iterative_SU2_Astros.py test; + python 2_aeroelastic_Iterative_SU2_Astros.py + tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log MESSAGE:: Building wingOml MESSAGE:: Building wingWaffle ==> Running SU2 pre-analysis... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - leftWing Mesh sizing name - riteWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0.5 1 2 3 6 EGADS : 2 Yes 0 0 1 0.5 1 1 4 5 EGADS : 3 Yes 0 0 1 0.5 1 1 4 8 EGADS : 4 Yes 0 0 1 0.5 1 2 3 5 EGADS : 5 Yes 0 0 1 0.5 1 2 4 EGADS : 6 Yes 0 0 1 0.5 1 1 7 8 EGADS : 7 Yes 0 0 1 0.5 1 6 9 10 EGADS : 8 Yes 0 0 1 0.5 1 3 6 9 EGADS : 9 Yes 0 0 1 0.5 1 7 8 10 EGADS : 10 Yes 0 0 1 0.5 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 11135.8 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 16 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 242 426 0 AFLR4 : Nodes, Trias,Quads= 203 348 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 301 529 0 AFLR4 : Nodes, Trias,Quads= 178 283 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 233 409 0 AFLR4 : Nodes, Trias,Quads= 189 321 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 292 511 0 AFLR4 : Nodes, Trias,Quads= 174 275 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 9 10 0 AFLR4 : Nodes, Trias,Quads= 6 4 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 241 424 0 AFLR4 : Nodes, Trias,Quads= 202 346 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 302 531 0 AFLR4 : Nodes, Trias,Quads= 177 281 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 235 413 0 AFLR4 : Nodes, Trias,Quads= 189 321 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 293 513 0 AFLR4 : Nodes, Trias,Quads= 173 273 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 9 10 0 AFLR4 : Nodes, Trias,Quads= 6 4 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 5 4 0 AFLR4 : Nodes, Trias,Quads= 4 2 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1238 2468 542 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1238 2468 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1695 3170 0 AFLR4 : Nodes, Trias,Quads= 1371 2522 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 3139 5972 0 AFLR4 : Nodes, Trias,Quads= 1805 3304 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 1597 2983 0 AFLR4 : Nodes, Trias,Quads= 1311 2411 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 3114 5923 0 AFLR4 : Nodes, Trias,Quads= 1786 3267 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 36 46 0 AFLR4 : Nodes, Trias,Quads= 24 22 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1691 3162 0 AFLR4 : Nodes, Trias,Quads= 1376 2532 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 3162 6018 0 AFLR4 : Nodes, Trias,Quads= 1802 3298 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 1600 2989 0 AFLR4 : Nodes, Trias,Quads= 1326 2441 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 3109 5913 0 AFLR4 : Nodes, Trias,Quads= 1784 3263 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 36 46 0 AFLR4 : Nodes, Trias,Quads= 24 22 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 11563 23118 2164 OVERALL : CPU Time = 0.149 seconds Body 1 (of 2) Number of nodes = 11543 Number of elements = 23082 Number of triangle elements = 23082 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 11563 Total number of elements = 23118 Total number of triangle elements = 23118 Total number of quadrilateral elements = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Getting volume mesh UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.18.1 AFLR2 : Version Date 06/11/24 @ 05:52PM AFLR2 : Compile OS Darwin 23.5.0 arm64 AFLR2 : Compile Date 06/11/24 @ 05:52PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.15 AFLR4 : Version Date 07/19/24 @ 07:04PM AFLR4 : Compile OS Darwin 23.5.0 arm64 AFLR4 : Compile Date 07/19/24 @ 07:06PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.26 EGADS : OpenCASCADE Version 7.8.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 10 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 10 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0.5 1 2 3 6 EGADS : 2 Yes 0 0 1 0.5 1 1 4 5 EGADS : 3 Yes 0 0 1 0.5 1 1 4 8 EGADS : 4 Yes 0 0 1 0.5 1 2 3 5 EGADS : 5 Yes 0 0 1 0.5 1 2 4 EGADS : 6 Yes 0 0 1 0.5 1 1 7 8 EGADS : 7 Yes 0 0 1 0.5 1 6 9 10 EGADS : 8 Yes 0 0 1 0.5 1 3 6 9 EGADS : 9 Yes 0 0 1 0.5 1 7 8 10 EGADS : 10 Yes 0 0 1 0.5 1 7 9 EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16 EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16 EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14 EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -5 4 6 -7 EGADS : 3 -3 8 1 -9 EGADS : 4 -6 9 5 -10 EGADS : 5 7 10 EGADS : 6 11 13 -12 -2 EGADS : 7 14 16 -15 -13 EGADS : 8 12 17 -11 -8 EGADS : 9 15 18 -14 -17 EGADS : 10 -16 -18 EGADS : 11 19 20 -21 -22 EGADS : 12 -23 26 25 -24 EGADS : 13 27 23 -28 -19 EGADS : 14 -29 21 30 -25 EGADS : 15 22 29 -26 -27 EGADS : 16 -20 28 24 -30 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 3 -4 EGADS : 2 Yes -5 4 6 -7 EGADS : 3 Yes -3 8 1 -9 EGADS : 4 Yes -6 9 5 -10 EGADS : 5 Yes 7 10 EGADS : 6 Yes 11 13 -12 -2 EGADS : 7 Yes 14 16 -15 -13 EGADS : 8 Yes 12 17 -11 -8 EGADS : 9 Yes 15 18 -14 -17 EGADS : 10 Yes -16 -18 EGADS : 11 Yes 19 20 -21 -22 EGADS : 12 Yes -23 26 25 -24 EGADS : 13 Yes 27 23 -28 -19 EGADS : 14 Yes -29 21 30 -25 EGADS : 15 Yes 22 29 -26 -27 EGADS : 16 Yes -20 28 24 -30 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 6 EGADS : 3 0 Yes 3 4 1 1 3 EGADS : 4 0 Yes 2 4 1 1 2 EGADS : 5 0 Yes 2 5 1 2 4 EGADS : 6 0 Yes 4 6 1 2 4 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 3 1 1 3 8 EGADS : 9 0 Yes 4 2 1 3 4 EGADS : 10 0 Yes 6 5 1 4 5 EGADS : 11 0 Yes 1 7 1 6 8 EGADS : 12 0 Yes 3 8 1 6 8 EGADS : 13 0 Yes 7 8 1 6 7 EGADS : 14 0 Yes 7 9 1 7 9 EGADS : 15 0 Yes 8 10 1 7 9 EGADS : 16 0 Yes 9 10 1 7 10 EGADS : 17 0 Yes 8 7 1 8 9 EGADS : 18 0 Yes 10 9 1 9 10 EGADS : 19 1 Yes 12 11 NA 11 13 EGADS : 20 1 Yes 11 13 NA 11 16 EGADS : 21 1 Yes 14 13 NA 11 14 EGADS : 22 1 Yes 12 14 NA 11 15 EGADS : 23 1 Yes 16 15 NA 12 13 EGADS : 24 1 Yes 15 17 NA 12 16 EGADS : 25 1 Yes 18 17 NA 12 14 EGADS : 26 1 Yes 16 18 NA 12 15 EGADS : 27 1 Yes 12 16 NA 13 15 EGADS : 28 1 Yes 11 15 NA 13 16 EGADS : 29 1 Yes 14 18 NA 14 15 EGADS : 30 1 Yes 13 17 NA 14 16 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 97.2007855 0 0 EGADS : 2 Yes 97.9335611 0 0 EGADS : 3 Yes 50 0 0 EGADS : 4 Yes 75.3047874 0 0 EGADS : 5 Yes 123.552357 0 4.7180639 EGADS : 6 Yes 118.391317 0 3.99272703 EGADS : 7 Yes 97.9335611 36.1389817 0 EGADS : 8 Yes 75.3047874 36.1389817 0 EGADS : 9 Yes 123.552357 97.6729236 4.7180639 EGADS : 10 Yes 118.391317 97.6729236 3.99272703 EGADS : 11 Yes 0 0 1951.57774 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 1953.45847 1951.57774 EGADS : 14 Yes 0 1953.45847 0 EGADS : 15 Yes 2040.21562 0 1951.57774 EGADS : 16 Yes 2040.21562 0 0 EGADS : 17 Yes 2040.21562 1953.45847 1951.57774 EGADS : 18 Yes 2040.21562 1953.45847 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 3906.92 AFLR4 : Min Bounding Box Length = 3906.92 AFLR4 : Max Ref Bounding Box Length = 195.346 AFLR4 : Min Ref Bounding Box Length = 13.1976 AFLR4 : Reference Length = 13.1976 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 428.309 AFLR4 : Abs Min Surf Spacing = 0.032994 AFLR4 : Min Surf Spacing = 0.065988 AFLR4 : Max Surf Spacing = 1.31976 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 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : 13 CAD geometry 0 FARFIELD AFLR4 : 14 CAD geometry 0 FARFIELD AFLR4 : 15 CAD geometry 0 FARFIELD AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR43 : INPUT SURFACE MESH FROM TESS AFLR43 : Quad Surface Faces= 0 AFLR43 : Tria Surface Faces= 23118 AFLR43 : Nodes = 11563 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.50 AFLR3 : Version Date 10/31/23 @ 06:31PM AFLR3 : Compile OS Darwin 23.3.0 arm64 AFLR3 : Compile Date 02/08/24 @ 04:22PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 11563 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 FarField UG3 : 12 FarField UG3 : 13 FarField UG3 : 14 FarField UG3 : 15 FarField UG3 : 16 FarField AFLR3 : CPU Time = 0.013 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 11563 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 2314 16714 AFLR3 IG : Nodes, Elements = 4628 33743 AFLR3 IG : Nodes, Elements = 6942 53624 AFLR3 IG : Nodes, Elements = 9256 74436 AFLR3 IG : Nodes, Elements = 11570 95707 AFLR3 IG : Nodes, Elements = 11570 95489 AFLR3 IG : Nodes, Elements = 11563 61785 AFLR3 IG : Nodes, Elements = 11563 61867 AFLR3 IG : Nodes, Elements = 11563 39359 AFLR3 IG : Nodes, Elements = 11563 34535 AFLR3 : CPU Time = 0.227 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 11563 34535 AFLR3 GG : Nodes, Elements = 16525 49704 AFLR3 GG : Nodes, Elements = 16525 69885 AFLR3 GG : Nodes, Elements = 16525 65013 AFLR3 GG : Nodes, Elements = 20386 77202 AFLR3 GG : Nodes, Elements = 20386 92123 AFLR3 GG : Nodes, Elements = 20386 87006 AFLR3 GG : Nodes, Elements = 24822 100916 AFLR3 GG : Nodes, Elements = 24822 118200 AFLR3 GG : Nodes, Elements = 24822 112948 AFLR3 GG : Nodes, Elements = 29519 127291 AFLR3 GG : Nodes, Elements = 29519 145892 AFLR3 GG : Nodes, Elements = 29519 140775 AFLR3 GG : Nodes, Elements = 34324 155453 AFLR3 GG : Nodes, Elements = 34324 174282 AFLR3 GG : Nodes, Elements = 34324 169182 AFLR3 GG : Nodes, Elements = 39084 183684 AFLR3 GG : Nodes, Elements = 39084 202336 AFLR3 GG : Nodes, Elements = 39084 197247 AFLR3 GG : Nodes, Elements = 43818 211662 AFLR3 GG : Nodes, Elements = 43818 230292 AFLR3 GG : Nodes, Elements = 43818 225444 AFLR3 GG : Nodes, Elements = 48511 239700 AFLR3 GG : Nodes, Elements = 48511 258017 AFLR3 GG : Nodes, Elements = 48511 253224 AFLR3 GG : Nodes, Elements = 53101 267164 AFLR3 GG : Nodes, Elements = 53101 285093 AFLR3 GG : Nodes, Elements = 53101 280451 AFLR3 GG : Nodes, Elements = 57604 294108 AFLR3 GG : Nodes, Elements = 57604 311685 AFLR3 GG : Nodes, Elements = 57604 307135 AFLR3 GG : Nodes, Elements = 62067 320645 AFLR3 GG : Nodes, Elements = 62067 338004 AFLR3 GG : Nodes, Elements = 62067 333601 AFLR3 GG : Nodes, Elements = 66391 346694 AFLR3 GG : Nodes, Elements = 66391 363633 AFLR3 GG : Nodes, Elements = 66391 359230 AFLR3 GG : Nodes, Elements = 70516 371704 AFLR3 GG : Nodes, Elements = 70516 387833 AFLR3 GG : Nodes, Elements = 70516 383696 AFLR3 GG : Nodes, Elements = 74523 395825 AFLR3 GG : Nodes, Elements = 74523 411729 AFLR3 GG : Nodes, Elements = 74523 407650 AFLR3 GG : Nodes, Elements = 78413 419413 AFLR3 GG : Nodes, Elements = 78413 434611 AFLR3 GG : Nodes, Elements = 78413 430668 AFLR3 GG : Nodes, Elements = 82208 442123 AFLR3 GG : Nodes, Elements = 82208 457159 AFLR3 GG : Nodes, Elements = 82208 453185 AFLR3 GG : Nodes, Elements = 85872 464258 AFLR3 GG : Nodes, Elements = 85872 478768 AFLR3 GG : Nodes, Elements = 85872 474956 AFLR3 GG : Nodes, Elements = 89401 485605 AFLR3 GG : Nodes, Elements = 89401 499363 AFLR3 GG : Nodes, Elements = 89401 495883 AFLR3 GG : Nodes, Elements = 92759 506025 AFLR3 GG : Nodes, Elements = 92759 519137 AFLR3 GG : Nodes, Elements = 92759 515850 AFLR3 GG : Nodes, Elements = 95939 525449 AFLR3 GG : Nodes, Elements = 95939 538022 AFLR3 GG : Nodes, Elements = 95939 534737 AFLR3 GG : Nodes, Elements = 99028 544057 AFLR3 GG : Nodes, Elements = 99028 556170 AFLR3 GG : Nodes, Elements = 99028 553136 AFLR3 GG : Nodes, Elements = 102008 562117 AFLR3 GG : Nodes, Elements = 102008 573799 AFLR3 GG : Nodes, Elements = 102008 570827 AFLR3 GG : Nodes, Elements = 104803 579263 AFLR3 GG : Nodes, Elements = 104803 590234 AFLR3 GG : Nodes, Elements = 104803 587447 AFLR3 GG : Nodes, Elements = 107453 595433 AFLR3 GG : Nodes, Elements = 107453 605916 AFLR3 GG : Nodes, Elements = 107453 603236 AFLR3 GG : Nodes, Elements = 109923 610689 AFLR3 GG : Nodes, Elements = 109923 620440 AFLR3 GG : Nodes, Elements = 109923 617990 AFLR3 GG : Nodes, Elements = 112260 625039 AFLR3 GG : Nodes, Elements = 112260 634220 AFLR3 GG : Nodes, Elements = 112260 631837 AFLR3 GG : Nodes, Elements = 114474 638520 AFLR3 GG : Nodes, Elements = 114474 647152 AFLR3 GG : Nodes, Elements = 114474 644938 AFLR3 GG : Nodes, Elements = 116549 651205 AFLR3 GG : Nodes, Elements = 116549 659395 AFLR3 GG : Nodes, Elements = 116549 657359 AFLR3 GG : Nodes, Elements = 118447 663072 AFLR3 GG : Nodes, Elements = 118447 670422 AFLR3 GG : Nodes, Elements = 118447 668566 AFLR3 GG : Nodes, Elements = 120236 673959 AFLR3 GG : Nodes, Elements = 120236 681057 AFLR3 GG : Nodes, Elements = 120236 679214 AFLR3 GG : Nodes, Elements = 121880 684170 AFLR3 GG : Nodes, Elements = 121880 690665 AFLR3 GG : Nodes, Elements = 121880 689024 AFLR3 GG : Nodes, Elements = 123448 693740 AFLR3 GG : Nodes, Elements = 123448 699826 AFLR3 GG : Nodes, Elements = 123448 698293 AFLR3 GG : Nodes, Elements = 124867 702554 AFLR3 GG : Nodes, Elements = 124867 708149 AFLR3 GG : Nodes, Elements = 124867 706720 AFLR3 GG : Nodes, Elements = 126121 710487 AFLR3 GG : Nodes, Elements = 126121 715334 AFLR3 GG : Nodes, Elements = 126121 714109 AFLR3 GG : Nodes, Elements = 127350 717801 AFLR3 GG : Nodes, Elements = 127350 722600 AFLR3 GG : Nodes, Elements = 127350 721452 AFLR3 GG : Nodes, Elements = 128544 725036 AFLR3 GG : Nodes, Elements = 128544 729737 AFLR3 GG : Nodes, Elements = 128544 728560 AFLR3 GG : Nodes, Elements = 129628 731815 AFLR3 GG : Nodes, Elements = 129628 736103 AFLR3 GG : Nodes, Elements = 129628 735026 AFLR3 GG : Nodes, Elements = 130592 737919 AFLR3 GG : Nodes, Elements = 130592 741755 AFLR3 GG : Nodes, Elements = 130592 740765 AFLR3 GG : Nodes, Elements = 131410 743221 AFLR3 GG : Nodes, Elements = 131410 746515 AFLR3 GG : Nodes, Elements = 131410 745664 AFLR3 GG : Nodes, Elements = 132080 747674 AFLR3 GG : Nodes, Elements = 132080 750316 AFLR3 GG : Nodes, Elements = 132080 749618 AFLR3 GG : Nodes, Elements = 132588 751142 AFLR3 GG : Nodes, Elements = 132588 753195 AFLR3 GG : Nodes, Elements = 132588 752603 AFLR3 GG : Nodes, Elements = 132972 753755 AFLR3 GG : Nodes, Elements = 132972 755360 AFLR3 GG : Nodes, Elements = 132972 754907 AFLR3 GG : Nodes, Elements = 133214 755633 AFLR3 GG : Nodes, Elements = 133214 756626 AFLR3 GG : Nodes, Elements = 133214 756330 AFLR3 GG : Nodes, Elements = 133352 756745 AFLR3 GG : Nodes, Elements = 133352 757366 AFLR3 GG : Nodes, Elements = 133352 757138 AFLR3 GG : Nodes, Elements = 133430 757373 AFLR3 GG : Nodes, Elements = 133430 757692 AFLR3 GG : Nodes, Elements = 133430 757594 AFLR3 GG : Nodes, Elements = 133459 757681 AFLR3 GG : Nodes, Elements = 133459 757812 AFLR3 GG : Nodes, Elements = 133459 757759 AFLR3 GG : Nodes, Elements = 133468 757786 AFLR3 GG : Nodes, Elements = 133468 757829 AFLR3 GG : Nodes, Elements = 133468 757810 AFLR3 GG : Nodes, Elements = 133469 757813 AFLR3 GG : Nodes, Elements = 133469 757820 AFLR3 GG : Nodes, Elements = 133469 757814 AFLR3 GG : Nodes, Elements = 133477 757838 AFLR3 GG : Nodes, Elements = 133477 757872 AFLR3 GG : Nodes, Elements = 133477 757864 AFLR3 GG : Nodes, Elements = 133484 757885 AFLR3 GG : Nodes, Elements = 133484 757906 AFLR3 GG : Nodes, Elements = 133484 757903 AFLR3 GG : Nodes, Elements = 133485 757906 AFLR3 GG : Nodes, Elements = 133485 757912 AFLR3 GG : Nodes, Elements = 133485 757907 AFLR3 : CPU Time = 3.652 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 133485 757907 AFLR3 QI : Nodes, Elements = 132790 753987 AFLR3 QI : Nodes, Elements = 132727 753627 AFLR3 QI : Nodes, Elements = 132723 753604 AFLR3 QI : Nodes, Elements = 132723 756877 AFLR3 QI : Nodes, Elements = 132723 753222 AFLR3 QI : Nodes, Elements = 132723 751692 AFLR3 QI : Nodes, Elements = 132723 752117 AFLR3 QI : Nodes, Elements = 132723 751465 AFLR3 QI : Nodes, Elements = 132723 751290 AFLR3 QI : Nodes, Elements = 132723 751620 AFLR3 QI : Nodes, Elements = 132723 751268 AFLR3 QI : Nodes, Elements = 132723 751203 AFLR3 : CPU Time = 0.775 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 751203 UG3 : Min, Max Ang = 4.734 157.3 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.96e+10 UG3 : No. Tet Elems = 751203 UG3 : Min Vol = 0.000926 UG3 : Average Vol = 7.94e+04 UG3 : Total-Tet-Vol = 5.96e+10 UG3 : No. Vol160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.96e+10 UG3 : No. Tet Elems = 751203 UG3 : Min Vol = 0.000926 UG3 : Average Vol = 7.94e+04 UG3 : Total-Tet-Vol = 5.96e+10 UG3 : No. Vol Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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 4240 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 195.346 m. Reference origin for moment evaluation is (55.4263, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Surface(s) affected by the design variables: BC_1. Input mesh file name: ../aflr3/aflr3_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: 5. 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_aeroelasticIterative.dat. Surface file name: surface_flow_aeroelasticIterative. Volume file name: flow_aeroelasticIterative. Restart file name: restart_flow_aeroelasticIterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 132723 grid points. 751203 volume elements. 2 surface markers. 23082 boundary elements in index 0 (Marker = BC_1). 36 boundary elements in index 1 (Marker = BC_2). 751203 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 5.96352e+10. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 29.8369. Mean K: 1.54048. Standard deviation K: 3.02418. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 47.3726| 86.9759| | CV Face Area Aspect Ratio| 1.14239| 3795.09| | CV Sub-Volume Ratio| 1.04381| 115687| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 132723| 1/1.00| 10| | 1| 21758| 1/6.1| 8.20948| | 2| 3346| 1/6.5| 6.59744| +-------------------------------------------+ Finding max control volume width. Semi-span length = 97.6729 m. Wetted area = 8661.74 m^2. Area projection in the x-plane = 677.811 m^2, y-plane = 441.377 m^2, z-plane = 4150.71 m^2. Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m. Min. coordinate in the x-direction = 50 m, y-direction = -97.6729 m, z-direction = -8.47948 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.2489e+00| 0.757177| 2.916188| 2.653440| 6.226283| -0.775751| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.0824e+00| 2.574443| 5.017027| 4.781322| 8.040241| -0.479679| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.0212e+00| 3.858160| 6.333961| 6.098920| 9.332939| 1.635601| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.9860e+00| 5.223634| 7.673267| 7.503470| 10.698941| -2.127392| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.9479e+00| 6.615086| 9.149149| 9.019247| 12.079542| -4.018876| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 6.61509| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticIterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |CSV file |surface_flow_aeroelasticIterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary |flow_aeroelasticIterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary surface |surface_flow_aeroelasticIterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). +-----------------------------------------------------------------------+ Warning: there are 3 non-physical points in the solution. --------------------------- 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) ------------------------ ==> Running SU2 post-analysis... ==> Running ASTROS pre-analysis... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = wingSpar1, index = 1 Name = wingSpar2, index = 2 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 425 Number of elements = 482 Number of triangle elements = 0 Number of quadrilateral elements = 482 ---------------------------- Total number of nodes = 425 Total number of elements = 482 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 = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 4 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Name = leftPointLoad, index = 3 Name = ritePointLoad, index = 4 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = leftWingSkin, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = wingSpar2, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 425 Number of elements = 482 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 482 Aero_Reference value is NULL - No aero reference parameters set 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 - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 16 Number of data points = 11543 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 2.503940e+12, tgt = 2.503940e+12, diff = 1.023664e+03 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 16 Number of data points = 11543 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 2.583276e+12, tgt = 2.583276e+12, diff = 3.634692e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 16 Number of data points = 11543 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 7.267917e+08, tgt = 7.267914e+08, diff = 2.835776e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 16 Number of data points = 11543 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 1.043301e+09, tgt = 1.043301e+09, diff = 1.942098e+01 Extracting external pressure loads from data transfer.... TransferName = upperWing Number of Elements = 98 (total = 98) Extracting external pressure loads from data transfer.... TransferName = lowerWing Number of Elements = 98 (total = 196) Extracting external pressure loads from data transfer.... TransferName = leftTip Number of Elements = 17 (total = 213) Extracting external pressure loads from data transfer.... TransferName = riteTip Number of Elements = 17 (total = 230) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG ==> Running ASTROS post-analysis... ==> Running SU2 pre-analysis... Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticIterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ==> Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, 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 . | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 132723 grid points. 751203 volume elements. 2 surface markers. 23082 boundary elements in index 0 (Marker = BC_1). 36 boundary elements in index 1 (Marker = BC_2). 751203 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. All volume elements are correctly orientend. All surface elements are correctly orientend. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 5.96352e+10. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 26.456199 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "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 2012-2024, 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. 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 4240 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 195.346 m. Reference origin for moment evaluation is (55.4263, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Surface(s) affected by the design variables: BC_1. Input mesh file name: ../aflr3/aflr3_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: 5. 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_aeroelasticIterative.dat. Surface file name: surface_flow_aeroelasticIterative. Volume file name: flow_aeroelasticIterative. Restart file name: restart_flow_aeroelasticIterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- 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 ) ------------------- Three dimensional problem. 132723 grid points. 751203 volume elements. 2 surface markers. 23082 boundary elements in index 0 (Marker = BC_1). 36 boundary elements in index 1 (Marker = BC_2). 751203 tetrahedra. 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 250696 TETRAHEDRON volume elements. There has been a re-orientation of 6783 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 5.96826e+10. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 41.8009. Mean K: 2.14585. Standard deviation K: 2.71635. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.818248| 85.2465| | CV Face Area Aspect Ratio| 1.04159| 6407.79| | CV Sub-Volume Ratio| 1.06384| 4.77146e+07| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 132723| 1/1.00| 10| | 1| 21846| 1/6.08| 8.22053| | 2| 3296| 1/6.63| 6.56442| +-------------------------------------------+ Finding max control volume width. Semi-span length = 106.94 m. Wetted area = 791941 m^2. Area projection in the x-plane = 231145 m^2, y-plane = 194382 m^2, z-plane = 48405 m^2. Max. coordinate in the x-direction = 196.517 m, y-direction = 106.94 m, z-direction = 195.22 m. Min. coordinate in the x-direction = 43.0455 m, y-direction = -101.327 m, z-direction = -715.562 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.2634e+00| 4.673200| 7.638651| 7.576090| 10.142306| 0.141770| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.3455e+00| 5.008593| 7.643312| 7.553614| 10.445096| 0.141722| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.3700e+00| 6.374832| 8.817725| 8.645414| 11.867759| 0.129229| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.3805e+00| 6.336595| 8.835720| 8.660112| 11.798289| 0.119932| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.3860e+00| 6.111086| 8.432272| 8.320868| 11.591449| 0.123147| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 6.11109| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticIterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |CSV file |surface_flow_aeroelasticIterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary |flow_aeroelasticIterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary surface |surface_flow_aeroelasticIterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). +-----------------------------------------------------------------------+ Warning: there are 8888 non-physical points in the solution. Warning: 3286 reconstructed states for upwinding are non-physical. --------------------------- 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) ------------------------ ==> Running SU2 post-analysis... ==> Running ASTROS pre-analysis... Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 16 Number of data points = 11543 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 1.623565e+12, tgt = 1.623565e+12, diff = 8.361079e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 16 Number of data points = 11543 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 1.501616e+12, tgt = 1.501616e+12, diff = 9.721191e+00 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 16 Number of data points = 11543 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 3.543784e+08, tgt = 3.543784e+08, diff = 5.294120e+00 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 16 Number of data points = 11543 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 3.165568e+08, tgt = 3.165562e+08, diff = 6.172774e+02 Extracting external pressure loads from data transfer.... TransferName = upperWing Number of Elements = 98 (total = 98) Extracting external pressure loads from data transfer.... TransferName = lowerWing Number of Elements = 98 (total = 196) Extracting external pressure loads from data transfer.... TransferName = leftTip Number of Elements = 17 (total = 213) Extracting external pressure loads from data transfer.... TransferName = riteTip Number of Elements = 17 (total = 230) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG ==> Running ASTROS post-analysis... real 1m48.140s user 1m53.958s sys 0m20.060s + status=0 + set +x ================================================= data/session10/2_aeroelastic_Iterative_SU2_Astros.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: session08 fun3d session09 nastran session11 fun3d+astros ================================================= All tests pass! ================================================= ================================================= + cd /Users/jenkins/workspace/ESP_bPreBuilt + mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs + cd /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs + find /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs -name 'plugs0*.csm' + sort -f + awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsFailure.txt + cp /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsIgnore.txt . + set +x Testing CSM files: data/Plugs/plugs0a.csm data/Plugs/plugs0b.csm data/Plugs/plugs0c.csm data/Plugs/plugs0d.csm total 46744 -rw-r--r-- 1 jenkins staff 1.2M Jul 26 10:47 ASTRO.D01 -rw-r--r-- 1 jenkins staff 277K Jul 26 10:47 ASTRO.IDX -rwxr-xr-x 1 jenkins staff 130K Jul 26 10:47 ESPxddm -rwxr-xr-x 1 jenkins staff 212K Jul 26 10:47 Slugs -rwxr-xr-x 1 jenkins staff 86K Jul 26 10:47 TestFit -rwxr-xr-x 1 jenkins staff 1.6M Jul 26 10:47 avl -rwxr-xr-x 1 jenkins staff 51K Jul 26 10:54 cart3dTest -rwxr-xr-x 1 jenkins staff 51K Jul 26 10:54 egads2cart -rwxr-xr-x 1 jenkins staff 70K Jul 26 10:47 egads2cgt -rwxr-xr-x 1 jenkins staff 402K Jul 26 10:47 friction -rwxr-xr-x 1 jenkins staff 10M Jul 26 10:47 mastros.exe -rwxr-xr-x 1 jenkins staff 749K Jul 26 10:47 mses -rwxr-xr-x 1 jenkins staff 1.4M Jul 26 10:47 mset -rwxr-xr-x 1 jenkins staff 51K Jul 26 10:54 phaseUtil -rw-r--r-- 1 jenkins staff 1.6K Jul 28 00:01 pod.egads -rw-r--r-- 1 jenkins staff 0B Jul 28 00:01 port7681.jrnl -rwxr-xr-x 1 jenkins staff 1.2M Jul 26 10:47 pplot -rwxr-xr-x 1 jenkins staff 1.1M Jul 26 10:47 pxplot -rwxr-xr-x 1 jenkins staff 68K Jul 26 10:54 sensCSM -rwxr-xr-x 1 jenkins staff 192K Jul 26 10:54 serveCSM -rwxr-xr-x 1 jenkins staff 176K Jul 26 10:54 serveESP -rwxr-xr-x 1 jenkins staff 52K Jul 26 10:47 vCurvature -rwxr-xr-x 1 jenkins staff 51K Jul 26 10:47 vGeom -rwxr-xr-x 1 jenkins staff 53K Jul 26 10:47 vTess -rwxr-xr-x 1 jenkins staff 1.8M Jul 26 10:47 vTesstatic -rw-r--r-- 1 jenkins staff 196K Jul 28 00:01 wingMultiModel.bdf -rwxr-xr-x 1 jenkins staff 1.7M Jul 26 10:47 xfoil ( 1 / 4 ) data/Plugs/plugs0a.csm; ++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/verify_7.8.1/plugs0a.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 converged, dmax= 5.416e-07, rmsbest= 6.132e-04, reclass= 4562, unclass= 0 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 2, unclass= 0 Starting pass 3 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m4.365s user 0m4.321s sys 0m0.213s ++ set +x data/Plugs/plugs0a passed (as expected) -------------------------------------------------------------------------------------------------- ( 2 / 4 ) data/Plugs/plugs0b.csm; ++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/verify_7.8.1/plugs0b.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 converged, dmax= 3.039e-07, rmsbest= 4.036e-02, reclass= 4562, unclass= 0 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 2.814e-07, rmsbest= 1.924e-03, reclass= 1033, unclass= 0 Starting pass 3 (of 25) of phase2 Pass 3 converged, dmax= 4.494e-07, rmsbest= 5.920e-04, reclass= 473, unclass= 0 Starting pass 4 (of 25) of phase2 Pass 4 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 17, unclass= 0 Starting pass 5 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m3.826s user 0m4.791s sys 0m0.020s ++ set +x data/Plugs/plugs0b passed (as expected) -------------------------------------------------------------------------------------------------- ( 3 / 4 ) data/Plugs/plugs0c.csm; ++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/verify_7.8.1/plugs0c.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0 Starting pass 3 (of 25) of phase2 Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0 Starting pass 4 (of 25) of phase2 Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0 Starting pass 5 (of 25) of phase2 Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0 Starting pass 6 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m12.035s user 0m19.112s sys 0m0.036s ++ set +x data/Plugs/plugs0c passed (as expected) -------------------------------------------------------------------------------------------------- ( 4 / 4 ) data/Plugs/plugs0d.csm; ++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/verify_7.8.1/plugs0d.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0 Starting pass 3 (of 25) of phase2 Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0 Starting pass 4 (of 25) of phase2 Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0 Starting pass 5 (of 25) of phase2 Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0 Starting pass 6 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m11.988s user 0m19.017s sys 0m0.036s ++ set +x data/Plugs/plugs0d passed (as expected) -------------------------------------------------------------------------------------------------- [Execution node] check if [viggen] is in [[windows10x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt') [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_bPreBuilt/ESPVersion=126,buildnode=viggen #77'. [Checks API] No suitable checks publisher found. [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] done Finished: SUCCESS