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Full Loggcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include hsmTest.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmTest.o gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/hsmTest /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmTest.o \ -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include hsmSimplePlateTest.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmSimplePlateTest.o gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/hsmSimplePlateTest /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmSimplePlateTest.o \ -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include hsmCantileverPlateTest.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmCantileverPlateTest.o gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/hsmCantileverPlateTest /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmCantileverPlateTest.o \ -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include hsmJoinedPlateTest.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmJoinedPlateTest.o gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/hsmJoinedPlateTest /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmJoinedPlateTest.o \ -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f interferenceTest.make) make[2]: Entering directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples/cCAPS' gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include interferenceTest.c \ -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/interferenceTest.o gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/interferenceTest /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/interferenceTest.o \ -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f msesTest.make) make[2]: Entering directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples/cCAPS' gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include msesTest.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/msesTest.o gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/msesTest /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/msesTest.o -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -legads -locsm \ -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f mystran.make) make[2]: Entering directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples/cCAPS' gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include mystranTest.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/mystranTest.o gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/mystranTest /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/mystranTest.o \ -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f pointwiseTest.make) make[2]: Entering directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples/cCAPS' gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include pointwiseTest.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/pointwiseTest.o gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/pointwiseTest /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/pointwiseTest.o -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads \ -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples/cCAPS' make[1]: Leaving directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/examples' +++ find /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/ -name Makefile ++ for i in `find $WORKSPACE/CAPS/training/ -name Makefile` ++ [[ /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2023/lectures/Makefile == *\l\e\c\t\u\r\e\s* ]] ++ continue ++ for i in `find $WORKSPACE/CAPS/training/ -name Makefile` ++ [[ /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2023/data/session01/Makefile ++ cd /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2023/data/session01 ++ make gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include template_avl.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/template_avl.o gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/test/template_avl /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/template_avl.o -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -legads -lrt -lm -ldl ++ for i in `find $WORKSPACE/CAPS/training/ -name Makefile` ++ [[ /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/data/session01/Makefile ++ cd /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/data/session01 ++ make make: Nothing to be done for 'default'. ++ cd /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/OpenCSM/trunk/src ++ make -f serveESP.make gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include -I. timCapsMode.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timCapsMode.o touch /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/capsMode.so rm /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/capsMode.so g++-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/capsMode.so /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timCapsMode.o -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lm gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include -I. timFlowchart.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timFlowchart.o touch /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/flowchart.so rm /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/flowchart.so g++-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/flowchart.so /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timFlowchart.o -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lm gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include -I. timViewer.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timViewer.o touch /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/viewer.so rm /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/viewer.so g++-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/viewer.so /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timViewer.o -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lm gcc-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.6 -I/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/include -I. -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.9.13/include/python3.9 -I/home/jenkins/util/ESP/Python/ESP_Python-3.9.13/include/python3.9 timPyscript.c -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timPyscript.o touch /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/pyscript.so rm /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/pyscript.so g++-11 -m64 -g -fsanitize=undefined -fno-omit-frame-pointer -fuse-ld=gold -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib/pyscript.so /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timPyscript.o -L/home/jenkins/util/ESP/Python/ESP_Python-3.9.13/lib -lpython3.9 -lcrypt -lpthread -ldl -lutil -lm -lm -L/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lrt -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.9.13/lib ++ ln -f -s /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/OpenCSM/trunk/udc /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64 +++ find /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/OpenCSM/trunk/data/training/ -name Makefile find: ‘/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/OpenCSM/trunk/data/training/’: No such file or directory + source /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/JenkinsESP/ESP_Sanitize.sh ++ '[' -z '' ']' ++ OUTLEVEL=0 ++ mkdir -p /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test ++ cd /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test ++ [[ CAPS/training2018 =~ [0-9]+.[0-9]+ ]] ++ SUBPARTS=2018 ++ export ESPTEST=CAPS/training2018 ++ ESPTEST=CAPS/training2018 ++ [[ CAPS/training2018 == \C\A\P\S* ]] ++ export CAPSTARGET=training2018 ++ CAPSTARGET=training2018 ++ [[ training2018 == \u\n\i\t ]] ++ [[ training2018 == \t\r\a\i\n\i\n\g\2\0\1\8 ]] ++ mkdir -p /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018 ++ cd /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018 ++ cp /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/runAll.py /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_astrosModal.py /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_astrosStatic.py /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_avl.py /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_dataTransfer.py /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_sansLIP.py /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_su2inviscid.py /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/transport.csm /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/transport.jrnl /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing1.csm /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing1.jrnl /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing2.csm /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing2.jrnl /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing3.csm /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing3.jrnl /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing4.csm /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing4.jrnl . ++ '[' '!' -z ' -L/home/jenkins/util/ESP/Python/ESP_Python-3.9.13/lib -lpython3.9 -lcrypt -lpthread -ldl -lutil -lm -lm ' ']' ++ echo ----------------------------------------------------- ----------------------------------------------------- +++ which python ++ echo 'using python : /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/venv/bin/python' using python : /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/venv/bin/python ++ echo ----------------------------------------------------- ----------------------------------------------------- ++ set -x +++ ls wing1.csm wing2.csm wing3.csm wing4.csm +++ sort -f ++ for i in `ls wing*.csm | sort -f` ++ python runAll.py wing1.csm Help on run_avl() run AVL to compute force coefficients inputs: filename name of .csm or .cpc file outputs: coefs dictionary containing force/moment coefficients: CLtot lift coefficient CDtot drag coefficient CXtot X-force coefficient CYtot Y-force coefficient CZtot Z-force coefficient Cltot rolling moment coefficient Cmtot pitching moment coefficient Cntot yawing moment coefficient e Oswald efficiency factor ==> Loading geometry from file "wing1.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading AVL aim... ==> Running AVL pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000191 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018/wing1.csm:96]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) ERROR:: (name_not_found) in Branch Brch_000295 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAvl.udc:37]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) ERROR:: (name_not_found) in Branch Brch_000309 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAvl.udc:61]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) 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) ==> Running AVL... ==> Running AVL post-analysis... ================ run_avl.py complete ================== AVL results --> Force/moment coefficients: CXtot : 0.1349024876199531 CYtot : -3.902395645668209e-14 CZtot : -1.277076071611152 Cltot : -3.744241516227126e-13 Cmtot : -0.7469983988368554 Cntot : -5.030489710227716e-14 CLtot : 1.281099987646977 CDtot : 0.0889089168685556 e : 0.9627573857401014 Help on run_sansLIP() run sansLIP to compute force coefficients inputs: filename name of .csm or .cpc file outputs: coefs dictionary containing force/moment coefficients: CLtot lift coefficient CDtot drag coefficient CXtot X-force coefficient CYtot Y-force coefficient CZtot Z-force coefficient Cltot rolling moment coefficient Cmtot pitching moment coefficient Cntot yawing moment coefficient e Oswald efficiency factor ==> Loading geometry from file "wing1.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading sansLIP aim... ERROR:: (name_not_found) in Branch Brch_000440 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:57]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) Marking Solid Edge 7 : wingWake Marking Solid Edge 1 : wingWake Wake intersection... 3.98107 s Scribing solid Marking Trailing Vortex/Trefftz edges Wake TrailingVortex edge : 2 wingWake Wake Trefftz edge : 3 wingWake -- solid face : 6 Wake TrailingVortex edge : 6 wingWake Wake Trefftz edge : 7 wingWake -- solid face : 6 ERROR:: (name_not_found) in Branch Brch_000801 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:591]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) ==> Running sansLIP pre-analysis and analysis... Generating AFLR4 surface mesh... AFLR4 success! AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.31.6 AFLR3 : Version Date 08/30/21 @ 12:37AM AFLR3 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR3 : Compile Date 08/30/21 @ 01:15AM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 3196 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 Transparent w/BL UG3 : 14 Transparent w/BL AFLR3 : CPU Time = 0.010 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 3196 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 640 3540 AFLR3 IG : Nodes, Elements = 1280 7032 AFLR3 IG : Nodes, Elements = 1920 10461 AFLR3 IG : Nodes, Elements = 2560 14284 AFLR3 IG : Nodes, Elements = 3200 17976 AFLR3 IG : Nodes, Elements = 3203 17989 AFLR3 IG : Nodes, Elements = 3203 17939 AFLR3 IG : Nodes, Elements = 3196 11457 AFLR3 IG : Nodes, Elements = 3196 11499 AFLR3 IG : Nodes, Elements = 3196 10467 AFLR3 IG : Nodes, Elements = 3196 10340 AFLR3 : CPU Time = 0.095 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 3196 10340 AFLR3 GG : Nodes, Elements = 4456 14122 AFLR3 GG : Nodes, Elements = 4456 18545 AFLR3 GG : Nodes, Elements = 4456 17442 AFLR3 GG : Nodes, Elements = 5588 20845 AFLR3 GG : Nodes, Elements = 5588 25308 AFLR3 GG : Nodes, Elements = 5588 24074 AFLR3 GG : Nodes, Elements = 6702 27422 AFLR3 GG : Nodes, Elements = 6702 31773 AFLR3 GG : Nodes, Elements = 6702 30664 AFLR3 GG : Nodes, Elements = 7758 33839 AFLR3 GG : Nodes, Elements = 7758 38176 AFLR3 GG : Nodes, Elements = 7758 37003 AFLR3 GG : Nodes, Elements = 8776 40060 AFLR3 GG : Nodes, Elements = 8776 44026 AFLR3 GG : Nodes, Elements = 8776 42941 AFLR3 GG : Nodes, Elements = 9765 45910 AFLR3 GG : Nodes, Elements = 9765 49802 AFLR3 GG : Nodes, Elements = 9765 48793 AFLR3 GG : Nodes, Elements = 10712 51637 AFLR3 GG : Nodes, Elements = 10712 55326 AFLR3 GG : Nodes, Elements = 10712 54393 AFLR3 GG : Nodes, Elements = 11620 57118 AFLR3 GG : Nodes, Elements = 11620 60605 AFLR3 GG : Nodes, Elements = 11620 59679 AFLR3 GG : Nodes, Elements = 12481 62264 AFLR3 GG : Nodes, Elements = 12481 65606 AFLR3 GG : Nodes, Elements = 12481 64769 AFLR3 GG : Nodes, Elements = 13267 67127 AFLR3 GG : Nodes, Elements = 13267 70154 AFLR3 GG : Nodes, Elements = 13267 69374 AFLR3 GG : Nodes, Elements = 14046 71712 AFLR3 GG : Nodes, Elements = 14046 74722 AFLR3 GG : Nodes, Elements = 14046 73970 AFLR3 GG : Nodes, Elements = 14761 76115 AFLR3 GG : Nodes, Elements = 14761 78890 AFLR3 GG : Nodes, Elements = 14761 78166 AFLR3 GG : Nodes, Elements = 15420 80144 AFLR3 GG : Nodes, Elements = 15420 82750 AFLR3 GG : Nodes, Elements = 15420 82059 AFLR3 GG : Nodes, Elements = 16077 84031 AFLR3 GG : Nodes, Elements = 16077 86614 AFLR3 GG : Nodes, Elements = 16077 85959 AFLR3 GG : Nodes, Elements = 16667 87730 AFLR3 GG : Nodes, Elements = 16667 90012 AFLR3 GG : Nodes, Elements = 16667 89439 AFLR3 GG : Nodes, Elements = 17179 90976 AFLR3 GG : Nodes, Elements = 17179 92959 AFLR3 GG : Nodes, Elements = 17179 92443 AFLR3 GG : Nodes, Elements = 17638 93820 AFLR3 GG : Nodes, Elements = 17638 95662 AFLR3 GG : Nodes, Elements = 17638 95181 AFLR3 GG : Nodes, Elements = 18022 96334 AFLR3 GG : Nodes, Elements = 18022 97853 AFLR3 GG : Nodes, Elements = 18022 97447 AFLR3 GG : Nodes, Elements = 18358 98456 AFLR3 GG : Nodes, Elements = 18358 99794 AFLR3 GG : Nodes, Elements = 18358 99451 AFLR3 GG : Nodes, Elements = 18633 100278 AFLR3 GG : Nodes, Elements = 18633 101362 AFLR3 GG : Nodes, Elements = 18633 101066 AFLR3 GG : Nodes, Elements = 18837 101678 AFLR3 GG : Nodes, Elements = 18837 102509 AFLR3 GG : Nodes, Elements = 18837 102280 AFLR3 GG : Nodes, Elements = 18973 102688 AFLR3 GG : Nodes, Elements = 18973 103238 AFLR3 GG : Nodes, Elements = 18973 103083 AFLR3 GG : Nodes, Elements = 19066 103363 AFLR3 GG : Nodes, Elements = 19066 103720 AFLR3 GG : Nodes, Elements = 19066 103627 AFLR3 GG : Nodes, Elements = 19107 103750 AFLR3 GG : Nodes, Elements = 19107 103941 AFLR3 GG : Nodes, Elements = 19107 103871 AFLR3 GG : Nodes, Elements = 19124 103922 AFLR3 GG : Nodes, Elements = 19124 103990 AFLR3 GG : Nodes, Elements = 19124 103966 AFLR3 GG : Nodes, Elements = 19129 103981 AFLR3 GG : Nodes, Elements = 19129 104006 AFLR3 GG : Nodes, Elements = 19129 103995 AFLR3 GG : Nodes, Elements = 19144 104040 AFLR3 GG : Nodes, Elements = 19144 104076 AFLR3 GG : Nodes, Elements = 19144 104072 AFLR3 : CPU Time = 1.084 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 19144 104072 AFLR3 QI : Nodes, Elements = 19122 103952 AFLR3 QI : Nodes, Elements = 19121 103948 AFLR3 QI : Nodes, Elements = 19121 104453 AFLR3 QI : Nodes, Elements = 19121 104021 AFLR3 QI : Nodes, Elements = 19121 103889 AFLR3 QI : Nodes, Elements = 19121 104048 AFLR3 QI : Nodes, Elements = 19121 103892 AFLR3 QI : Nodes, Elements = 19121 103869 AFLR3 : CPU Time = 0.212 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 103869 UG3 : Min, Max Ang = 15.58 148.4 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.81e+04 UG3 : No. Tet Elems = 103869 UG3 : Min Vol = 0.000138 UG3 : Average Vol = 0.559 UG3 : Total-Tet-Vol = 5.81e+04 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 103869 UG3 : Min, Max Q = 0.38 1 UG3 : Average Q = 0.878 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 Adding 576 tet centers Trefftz Frames (2) : 2 3 Non-zero time : 0.315797 second(s) Total Degrees of Freedom : 19945 Factorizing matrix... Jacobian time : 0.499572 second(s) Numeric factor time : 0.590281 second(s) Done Solving primal system : MKL_PARDISO solve time : 0.144238 second(s) Solving Fx adjoint : MKL_PARDISO solve time : 0.0334748 second(s) Solving Fy adjoint : MKL_PARDISO solve time : 0.0459613 second(s) Solving Fz adjoint : MKL_PARDISO solve time : 0.0774611 second(s) Solving Mx adjoint : MKL_PARDISO solve time : 0.0279398 second(s) Solving My adjoint : MKL_PARDISO solve time : 0.0267677 second(s) Solving Mz adjoint : MKL_PARDISO solve time : 0.0343747 second(s) output_Tecplot: filename = wing1.dat ==> Running sansLIP post-analysis... ================ run_sansLIP.py complete ================== sansLIP results --> Force/moment coefficients: CXtot : 0.07066315324475123 CYtot : -2.118207976359171e-05 CZtot : -0.9879021287640685 Cltot : -0.00017323483669785992 Cmtot : -0.5526380004325631 Cntot : 0.00010379117974592134 CLtot : 0.9851642034132695 CDtot : 0.10195778320544088 e : 0.5050050708046371 Help on run_astrosStatic() run ASTROS to perform linear static analysis of a built-up-element structure inputs: filename name of .csm or .cpc file outputs: disps dictionary containing maximum displacements: Tmax 3D displacement T1max displacement in X-direction T2max displacement in Y-direction T3max displacement in Z-direction ==> Loading geometry from file "wing1.csm"... File "wing1.csm" not set up to run Astros EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Help on run_astrosModal() run ASTROS to perform modal analysis of a built-up-element structure inputs: filename name of .csm or .cpc file output: freqs list of natural frequencies ==> Loading geometry from file "wing1.csm"... File "wing1.csm" not set up to run Astros EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Help on run_dataTransfer() run sansLIP to compute surface pressures which are transferred to astros static solver inputs: filename name of .csm or .cpc file outputs: disps dictionary containing maximum displacements: Tmax 3D displacement T1max displacement in X-direction T2max displacement in Y-direction T3max displacement in Z-direction ==> Loading geometry from file "wing1.csm"... ==> Setting Build Variables and Geometry Values... File "wing1.csm" not set up to run SansLIP and Astros EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! WARNING: 'capsGeometry.buildGeometry' is deprecated. Please use 'Problem.geometry.build'! WARNING: 'capsGeometry.getGeometryOutVal' is deprecated. Please use 'Problem.geometry.outpmtr["varname"].value'! real 0m27.680s user 0m42.264s sys 0m8.583s ++ for i in `ls wing*.csm | sort -f` ++ python runAll.py wing2.csm Help on run_avl() run AVL to compute force coefficients inputs: filename name of .csm or .cpc file outputs: coefs dictionary containing force/moment coefficients: CLtot lift coefficient CDtot drag coefficient CXtot X-force coefficient CYtot Y-force coefficient CZtot Z-force coefficient Cltot rolling moment coefficient Cmtot pitching moment coefficient Cntot yawing moment coefficient e Oswald efficiency factor ==> Loading geometry from file "wing2.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading AVL aim... ==> Running AVL pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000191 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018/wing2.csm:99]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) ERROR:: (name_not_found) in Branch Brch_000340 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAvl.udc:61]] storage "WingHinge" 3 not found --> catching signal -251 (name_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice control surface data VLM control surface name - WingHinge1 VLM control surface name - WingHinge2 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 Done getting vortex lattice surface data Writing surface - Wing (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) ==> Running AVL... ==> Running AVL post-analysis... ================ run_avl.py complete ================== AVL results --> Force/moment coefficients: CXtot : 0.1320423158252318 CYtot : -0.01023123333958946 CZtot : -1.278726166104227 Cltot : -0.04218058926833301 Cmtot : -0.7466826978744193 Cntot : 0.003425631256815422 CLtot : 1.282228349876992 CDtot : 0.0920121721286445 e : 0.9216037059402639 Help on run_sansLIP() run sansLIP to compute force coefficients inputs: filename name of .csm or .cpc file outputs: coefs dictionary containing force/moment coefficients: CLtot lift coefficient CDtot drag coefficient CXtot X-force coefficient CYtot Y-force coefficient CZtot Z-force coefficient Cltot rolling moment coefficient Cmtot pitching moment coefficient Cntot yawing moment coefficient e Oswald efficiency factor ==> Loading geometry from file "wing2.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading sansLIP aim... ERROR:: (name_not_found) in Branch Brch_000471 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:57]] storage "WingHinge" 3 not found --> catching signal -251 (name_not_found) Marking Solid Edge 19 : wingWake Marking Solid Edge 22 : wingWake Marking Solid Edge 15 : wingWake Marking Solid Edge 5 : wingWake Marking Solid Edge 9 : wingWake Marking Solid Edge 1 : wingWake Wake intersection... 4.99421 s Scribing solid Marking Trailing Vortex/Trefftz edges Wake TrailingVortex edge : 2 wingWake Wake Trefftz edge : 3 wingWake -- solid face : 6 Wake Trefftz edge : 6 wingWake -- solid face : 6 Wake Trefftz edge : 9 wingWake -- solid face : 6 Wake Trefftz edge : 13 wingWake -- solid face : 6 Wake Trefftz edge : 16 wingWake -- solid face : 6 Wake TrailingVortex edge : 18 wingWake Wake Trefftz edge : 19 wingWake -- solid face : 6 ERROR:: (name_not_found) in Branch Brch_000832 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:591]] storage "WingHinge" 3 not found --> catching signal -251 (name_not_found) ==> Running sansLIP pre-analysis and analysis... Generating AFLR4 surface mesh... AFLR4 success! AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.31.6 AFLR3 : Version Date 08/30/21 @ 12:37AM AFLR3 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR3 : Compile Date 08/30/21 @ 01:15AM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 3833 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 Transparent w/BL UG3 : 18 Transparent w/BL UG3 : 19 Transparent w/BL UG3 : 20 Transparent w/BL UG3 : 21 Transparent w/BL UG3 : 22 Transparent w/BL AFLR3 : CPU Time = 0.007 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 3833 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 768 4172 AFLR3 IG : Nodes, Elements = 1536 8404 AFLR3 IG : Nodes, Elements = 2304 12582 AFLR3 IG : Nodes, Elements = 3072 17144 AFLR3 IG : Nodes, Elements = 3840 21444 AFLR3 IG : Nodes, Elements = 3840 21391 AFLR3 IG : Nodes, Elements = 3840 21399 AFLR3 IG : Nodes, Elements = 3840 21380 AFLR3 IG : Nodes, Elements = 3840 21381 AFLR3 IG : Nodes, Elements = 3833 14172 AFLR3 IG : Nodes, Elements = 3833 14220 AFLR3 IG : Nodes, Elements = 3833 13009 AFLR3 IG : Nodes, Elements = 3833 12813 AFLR3 : CPU Time = 0.090 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 3833 12813 AFLR3 GG : Nodes, Elements = 5479 17754 AFLR3 GG : Nodes, Elements = 5479 23989 AFLR3 GG : Nodes, Elements = 5479 22465 AFLR3 GG : Nodes, Elements = 6880 26677 AFLR3 GG : Nodes, Elements = 6880 32211 AFLR3 GG : Nodes, Elements = 6880 30695 AFLR3 GG : Nodes, Elements = 8241 34781 AFLR3 GG : Nodes, Elements = 8241 40353 AFLR3 GG : Nodes, Elements = 8241 38861 AFLR3 GG : Nodes, Elements = 9549 42788 AFLR3 GG : Nodes, Elements = 9549 48036 AFLR3 GG : Nodes, Elements = 9549 46690 AFLR3 GG : Nodes, Elements = 10776 50374 AFLR3 GG : Nodes, Elements = 10776 55126 AFLR3 GG : Nodes, Elements = 10776 53818 AFLR3 GG : Nodes, Elements = 11956 57360 AFLR3 GG : Nodes, Elements = 11956 62019 AFLR3 GG : Nodes, Elements = 11956 60786 AFLR3 GG : Nodes, Elements = 13091 64191 AFLR3 GG : Nodes, Elements = 13091 68613 AFLR3 GG : Nodes, Elements = 13091 67477 AFLR3 GG : Nodes, Elements = 14171 70718 AFLR3 GG : Nodes, Elements = 14171 74907 AFLR3 GG : Nodes, Elements = 14171 73836 AFLR3 GG : Nodes, Elements = 15185 76881 AFLR3 GG : Nodes, Elements = 15185 80812 AFLR3 GG : Nodes, Elements = 15185 79815 AFLR3 GG : Nodes, Elements = 16137 82672 AFLR3 GG : Nodes, Elements = 16137 86405 AFLR3 GG : Nodes, Elements = 16137 85438 AFLR3 GG : Nodes, Elements = 17038 88142 AFLR3 GG : Nodes, Elements = 17038 91654 AFLR3 GG : Nodes, Elements = 17038 90748 AFLR3 GG : Nodes, Elements = 17894 93317 AFLR3 GG : Nodes, Elements = 17894 96695 AFLR3 GG : Nodes, Elements = 17894 95836 AFLR3 GG : Nodes, Elements = 18698 98250 AFLR3 GG : Nodes, Elements = 18698 101401 AFLR3 GG : Nodes, Elements = 18698 100550 AFLR3 GG : Nodes, Elements = 19438 102772 AFLR3 GG : Nodes, Elements = 19438 105708 AFLR3 GG : Nodes, Elements = 19438 104918 AFLR3 GG : Nodes, Elements = 20122 106972 AFLR3 GG : Nodes, Elements = 20122 109676 AFLR3 GG : Nodes, Elements = 20122 108960 AFLR3 GG : Nodes, Elements = 20778 110929 AFLR3 GG : Nodes, Elements = 20778 113414 AFLR3 GG : Nodes, Elements = 20778 112821 AFLR3 GG : Nodes, Elements = 21354 114549 AFLR3 GG : Nodes, Elements = 21354 116794 AFLR3 GG : Nodes, Elements = 21354 116241 AFLR3 GG : Nodes, Elements = 21853 117738 AFLR3 GG : Nodes, Elements = 21853 119697 AFLR3 GG : Nodes, Elements = 21853 119176 AFLR3 GG : Nodes, Elements = 22270 120428 AFLR3 GG : Nodes, Elements = 22270 122085 AFLR3 GG : Nodes, Elements = 22270 121654 AFLR3 GG : Nodes, Elements = 22625 122719 AFLR3 GG : Nodes, Elements = 22625 124151 AFLR3 GG : Nodes, Elements = 22625 123752 AFLR3 GG : Nodes, Elements = 22889 124545 AFLR3 GG : Nodes, Elements = 22889 125622 AFLR3 GG : Nodes, Elements = 22889 125295 AFLR3 GG : Nodes, Elements = 23040 125748 AFLR3 GG : Nodes, Elements = 23040 126371 AFLR3 GG : Nodes, Elements = 23040 126199 AFLR3 GG : Nodes, Elements = 23150 126529 AFLR3 GG : Nodes, Elements = 23150 126974 AFLR3 GG : Nodes, Elements = 23150 126851 AFLR3 GG : Nodes, Elements = 23197 126992 AFLR3 GG : Nodes, Elements = 23197 127180 AFLR3 GG : Nodes, Elements = 23197 127124 AFLR3 GG : Nodes, Elements = 23211 127166 AFLR3 GG : Nodes, Elements = 23211 127235 AFLR3 GG : Nodes, Elements = 23211 127202 AFLR3 GG : Nodes, Elements = 23216 127217 AFLR3 GG : Nodes, Elements = 23216 127240 AFLR3 GG : Nodes, Elements = 23216 127233 AFLR3 GG : Nodes, Elements = 23235 127290 AFLR3 GG : Nodes, Elements = 23235 127344 AFLR3 GG : Nodes, Elements = 23235 127334 AFLR3 : CPU Time = 0.928 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 23235 127334 AFLR3 QI : Nodes, Elements = 23202 127147 AFLR3 QI : Nodes, Elements = 23201 127141 AFLR3 QI : Nodes, Elements = 23201 127786 AFLR3 QI : Nodes, Elements = 23201 127251 AFLR3 QI : Nodes, Elements = 23201 127054 AFLR3 QI : Nodes, Elements = 23201 127224 AFLR3 QI : Nodes, Elements = 23201 127070 AFLR3 QI : Nodes, Elements = 23201 127042 AFLR3 : CPU Time = 0.176 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 127042 UG3 : Min, Max Ang = 10.61 152.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.81e+04 UG3 : No. Tet Elems = 127042 UG3 : Min Vol = 0.00013 UG3 : Average Vol = 0.457 UG3 : Total-Tet-Vol = 5.81e+04 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 127042 UG3 : Min, Max Q = 0.287 0.999 UG3 : Average Q = 0.877 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 Adding 655 tet centers Trefftz Frames (6) : 6 7 8 9 10 11 Non-zero time : 0.408968 second(s) Total Degrees of Freedom : 24455 Factorizing matrix... Jacobian time : 0.641211 second(s) Numeric factor time : 0.645564 second(s) Done Solving primal system : MKL_PARDISO solve time : 0.0293373 second(s) Solving Fx adjoint : MKL_PARDISO solve time : 0.0344817 second(s) Solving Fy adjoint : MKL_PARDISO solve time : 0.0417625 second(s) Solving Fz adjoint : MKL_PARDISO solve time : 0.0292328 second(s) Solving Mx adjoint : MKL_PARDISO solve time : 0.0294306 second(s) Solving My adjoint : MKL_PARDISO solve time : 0.0291123 second(s) Solving Mz adjoint : MKL_PARDISO solve time : 0.0298974 second(s) output_Tecplot: filename = wing2.dat ==> Running sansLIP post-analysis... ================ run_sansLIP.py complete ================== sansLIP results --> Force/moment coefficients: CXtot : 0.0687593542283613 CYtot : -0.0019269859838690069 CZtot : -1.035456522515127 Cltot : -0.034103843541501734 Cmtot : -0.5925394339126006 Cntot : 0.0017149362141873749 CLtot : 1.0316655478392671 CDtot : 0.11209039305188569 e : 0.5037439640076952 Help on run_astrosStatic() run ASTROS to perform linear static analysis of a built-up-element structure inputs: filename name of .csm or .cpc file outputs: disps dictionary containing maximum displacements: Tmax 3D displacement T1max displacement in X-direction T2max displacement in Y-direction T3max displacement in Z-direction ==> Loading geometry from file "wing2.csm"... File "wing2.csm" not set up to run Astros EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Help on run_astrosModal() run ASTROS to perform modal analysis of a built-up-element structure inputs: filename name of .csm or .cpc file output: freqs list of natural frequencies ==> Loading geometry from file "wing2.csm"... File "wing2.csm" not set up to run Astros EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Help on run_dataTransfer() run sansLIP to compute surface pressures which are transferred to astros static solver inputs: filename name of .csm or .cpc file outputs: disps dictionary containing maximum displacements: Tmax 3D displacement T1max displacement in X-direction T2max displacement in Y-direction T3max displacement in Z-direction ==> Loading geometry from file "wing2.csm"... ==> Setting Build Variables and Geometry Values... File "wing2.csm" not set up to run SansLIP and Astros EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! 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.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! WARNING: 'capsGeometry.buildGeometry' is deprecated. Please use 'Problem.geometry.build'! WARNING: 'capsGeometry.getGeometryOutVal' is deprecated. Please use 'Problem.geometry.outpmtr["varname"].value'! real 1m21.128s user 2m18.966s sys 0m12.735s ++ for i in `ls wing*.csm | sort -f` ++ python runAll.py wing3.csm Help on run_avl() run AVL to compute force coefficients inputs: filename name of .csm or .cpc file outputs: coefs dictionary containing force/moment coefficients: CLtot lift coefficient CDtot drag coefficient CXtot X-force coefficient CYtot Y-force coefficient CZtot Z-force coefficient Cltot rolling moment coefficient Cmtot pitching moment coefficient Cntot yawing moment coefficient e Oswald efficiency factor ==> Loading geometry from file "wing3.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading AVL aim... ==> Running AVL pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000191 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018/wing3.csm:102]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) ERROR:: (name_not_found) in Branch Brch_000311 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAvl.udc:37]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) ERROR:: (name_not_found) in Branch Brch_000325 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAvl.udc:61]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) 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 11 (ID = 0) Section 2 of 11 (ID = 1) Section 3 of 11 (ID = 2) Section 4 of 11 (ID = 3) Section 5 of 11 (ID = 4) Section 6 of 11 (ID = 5) Section 7 of 11 (ID = 6) Section 8 of 11 (ID = 7) Section 9 of 11 (ID = 8) Section 10 of 11 (ID = 9) Section 11 of 11 (ID = 10) ==> Running AVL... ==> Running AVL post-analysis... ================ run_avl.py complete ================== AVL results --> Force/moment coefficients: CXtot : 0.1319849250392852 CYtot : 2.384708451758435e-12 CZtot : -1.267949983152357 Cltot : 1.100577441681683e-11 Cmtot : -0.7407359030967515 Cntot : -1.339783779795781e-12 CLtot : 1.271605915552718 CDtot : 0.09019742648779863 e : 0.9518209978295341 Help on run_sansLIP() run sansLIP to compute force coefficients inputs: filename name of .csm or .cpc file outputs: coefs dictionary containing force/moment coefficients: CLtot lift coefficient CDtot drag coefficient CXtot X-force coefficient CYtot Y-force coefficient CZtot Z-force coefficient Cltot rolling moment coefficient Cmtot pitching moment coefficient Cntot yawing moment coefficient e Oswald efficiency factor ==> Loading geometry from file "wing3.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading sansLIP aim... ERROR:: (name_not_found) in Branch Brch_000456 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:57]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) Marking Solid Edge 7 : wingWake Marking Solid Edge 1 : wingWake Wake intersection... 3.5688 s Scribing solid Marking Trailing Vortex/Trefftz edges Wake TrailingVortex edge : 2 wingWake Wake Trefftz edge : 3 wingWake -- solid face : 6 Wake TrailingVortex edge : 6 wingWake Wake Trefftz edge : 7 wingWake -- solid face : 6 ERROR:: (name_not_found) in Branch Brch_000817 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:591]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) ==> Running sansLIP pre-analysis and analysis... Generating AFLR4 surface mesh... AFLR4 success! AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.31.6 AFLR3 : Version Date 08/30/21 @ 12:37AM AFLR3 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR3 : Compile Date 08/30/21 @ 01:15AM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 3196 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 Transparent w/BL UG3 : 14 Transparent w/BL AFLR3 : CPU Time = 0.006 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 3196 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 640 3540 AFLR3 IG : Nodes, Elements = 1280 7032 AFLR3 IG : Nodes, Elements = 1920 10461 AFLR3 IG : Nodes, Elements = 2560 14284 AFLR3 IG : Nodes, Elements = 3200 17976 AFLR3 IG : Nodes, Elements = 3203 17989 AFLR3 IG : Nodes, Elements = 3203 17939 AFLR3 IG : Nodes, Elements = 3196 11457 AFLR3 IG : Nodes, Elements = 3196 11499 AFLR3 IG : Nodes, Elements = 3196 10467 AFLR3 IG : Nodes, Elements = 3196 10340 AFLR3 : CPU Time = 0.064 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 3196 10340 AFLR3 GG : Nodes, Elements = 4456 14122 AFLR3 GG : Nodes, Elements = 4456 18545 AFLR3 GG : Nodes, Elements = 4456 17442 AFLR3 GG : Nodes, Elements = 5588 20845 AFLR3 GG : Nodes, Elements = 5588 25308 AFLR3 GG : Nodes, Elements = 5588 24074 AFLR3 GG : Nodes, Elements = 6702 27422 AFLR3 GG : Nodes, Elements = 6702 31773 AFLR3 GG : Nodes, Elements = 6702 30664 AFLR3 GG : Nodes, Elements = 7758 33839 AFLR3 GG : Nodes, Elements = 7758 38176 AFLR3 GG : Nodes, Elements = 7758 37003 AFLR3 GG : Nodes, Elements = 8776 40060 AFLR3 GG : Nodes, Elements = 8776 44026 AFLR3 GG : Nodes, Elements = 8776 42941 AFLR3 GG : Nodes, Elements = 9765 45910 AFLR3 GG : Nodes, Elements = 9765 49802 AFLR3 GG : Nodes, Elements = 9765 48793 AFLR3 GG : Nodes, Elements = 10712 51637 AFLR3 GG : Nodes, Elements = 10712 55326 AFLR3 GG : Nodes, Elements = 10712 54393 AFLR3 GG : Nodes, Elements = 11620 57118 AFLR3 GG : Nodes, Elements = 11620 60605 AFLR3 GG : Nodes, Elements = 11620 59679 AFLR3 GG : Nodes, Elements = 12481 62264 AFLR3 GG : Nodes, Elements = 12481 65606 AFLR3 GG : Nodes, Elements = 12481 64769 AFLR3 GG : Nodes, Elements = 13267 67127 AFLR3 GG : Nodes, Elements = 13267 70154 AFLR3 GG : Nodes, Elements = 13267 69374 AFLR3 GG : Nodes, Elements = 14046 71712 AFLR3 GG : Nodes, Elements = 14046 74722 AFLR3 GG : Nodes, Elements = 14046 73970 AFLR3 GG : Nodes, Elements = 14761 76115 AFLR3 GG : Nodes, Elements = 14761 78890 AFLR3 GG : Nodes, Elements = 14761 78166 AFLR3 GG : Nodes, Elements = 15420 80144 AFLR3 GG : Nodes, Elements = 15420 82750 AFLR3 GG : Nodes, Elements = 15420 82059 AFLR3 GG : Nodes, Elements = 16077 84031 AFLR3 GG : Nodes, Elements = 16077 86614 AFLR3 GG : Nodes, Elements = 16077 85959 AFLR3 GG : Nodes, Elements = 16667 87730 AFLR3 GG : Nodes, Elements = 16667 90012 AFLR3 GG : Nodes, Elements = 16667 89439 AFLR3 GG : Nodes, Elements = 17179 90976 AFLR3 GG : Nodes, Elements = 17179 92959 AFLR3 GG : Nodes, Elements = 17179 92443 AFLR3 GG : Nodes, Elements = 17638 93820 AFLR3 GG : Nodes, Elements = 17638 95662 AFLR3 GG : Nodes, Elements = 17638 95181 AFLR3 GG : Nodes, Elements = 18022 96334 AFLR3 GG : Nodes, Elements = 18022 97853 AFLR3 GG : Nodes, Elements = 18022 97447 AFLR3 GG : Nodes, Elements = 18358 98456 AFLR3 GG : Nodes, Elements = 18358 99794 AFLR3 GG : Nodes, Elements = 18358 99451 AFLR3 GG : Nodes, Elements = 18633 100278 AFLR3 GG : Nodes, Elements = 18633 101362 AFLR3 GG : Nodes, Elements = 18633 101066 AFLR3 GG : Nodes, Elements = 18837 101678 AFLR3 GG : Nodes, Elements = 18837 102509 AFLR3 GG : Nodes, Elements = 18837 102280 AFLR3 GG : Nodes, Elements = 18973 102688 AFLR3 GG : Nodes, Elements = 18973 103238 AFLR3 GG : Nodes, Elements = 18973 103083 AFLR3 GG : Nodes, Elements = 19066 103363 AFLR3 GG : Nodes, Elements = 19066 103720 AFLR3 GG : Nodes, Elements = 19066 103627 AFLR3 GG : Nodes, Elements = 19107 103750 AFLR3 GG : Nodes, Elements = 19107 103941 AFLR3 GG : Nodes, Elements = 19107 103871 AFLR3 GG : Nodes, Elements = 19124 103922 AFLR3 GG : Nodes, Elements = 19124 103990 AFLR3 GG : Nodes, Elements = 19124 103966 AFLR3 GG : Nodes, Elements = 19129 103981 AFLR3 GG : Nodes, Elements = 19129 104006 AFLR3 GG : Nodes, Elements = 19129 103995 AFLR3 GG : Nodes, Elements = 19144 104040 AFLR3 GG : Nodes, Elements = 19144 104076 AFLR3 GG : Nodes, Elements = 19144 104072 AFLR3 : CPU Time = 0.693 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 19144 104072 AFLR3 QI : Nodes, Elements = 19122 103952 AFLR3 QI : Nodes, Elements = 19121 103948 AFLR3 QI : Nodes, Elements = 19121 104453 AFLR3 QI : Nodes, Elements = 19121 104021 AFLR3 QI : Nodes, Elements = 19121 103889 AFLR3 QI : Nodes, Elements = 19121 104048 AFLR3 QI : Nodes, Elements = 19121 103892 AFLR3 QI : Nodes, Elements = 19121 103869 AFLR3 : CPU Time = 0.178 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 103869 UG3 : Min, Max Ang = 15.58 148.4 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.81e+04 UG3 : No. Tet Elems = 103869 UG3 : Min Vol = 0.000138 UG3 : Average Vol = 0.559 UG3 : Total-Tet-Vol = 5.81e+04 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 103869 UG3 : Min, Max Q = 0.38 1 UG3 : Average Q = 0.878 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 Adding 576 tet centers Trefftz Frames (2) : 2 3 Non-zero time : 0.365456 second(s) Total Degrees of Freedom : 19945 Factorizing matrix... Jacobian time : 0.461637 second(s) Numeric factor time : 0.610965 second(s) Done Solving primal system : MKL_PARDISO solve time : 0.0253497 second(s) Solving Fx adjoint : MKL_PARDISO solve time : 0.0270066 second(s) Solving Fy adjoint : MKL_PARDISO solve time : 0.026662 second(s) Solving Fz adjoint : MKL_PARDISO solve time : 0.0256796 second(s) Solving Mx adjoint : MKL_PARDISO solve time : 0.0260507 second(s) Solving My adjoint : MKL_PARDISO solve time : 0.0267184 second(s) Solving Mz adjoint : MKL_PARDISO solve time : 0.0263688 second(s) output_Tecplot: filename = wing3.dat ==> Running sansLIP post-analysis... ================ run_sansLIP.py complete ================== sansLIP results --> Force/moment coefficients: CXtot : 0.07066315324475118 CYtot : -2.1182079763590323e-05 CZtot : -0.9879021287640682 Cltot : -0.000173234836697837 Cmtot : -0.5526380004325631 Cntot : 0.00010379117974592598 CLtot : 0.9851642034132693 CDtot : 0.10195778320544088 e : 0.5050050708046369 Help on run_astrosStatic() run ASTROS to perform linear static analysis of a built-up-element structure inputs: filename name of .csm or .cpc file outputs: disps dictionary containing maximum displacements: Tmax 3D displacement T1max displacement in X-direction T2max displacement in Y-direction T3max displacement in Z-direction ==> Loading geometry from file "wing3.csm"... ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000191 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018/wing3.csm:102]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) ERROR:: BAD STATUS = -1 from processFile (called from udpExecute:183) processFile: could not open file "editAttr_6.txt" ERROR:: (egads_notfound) in Branch Brch_001668 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAstros.udc:35]] processFile: could not open file "editAttr_6.txt" --> catching signal -1 (egads_notfound) Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = pointConstraint1, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperRiteWing, index = 1 Name = lowerRiteWing, index = 2 Name = upperLeftWing, index = 3 Name = lowerLeftWing, 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 = 3 Name = wingSpar, index = 1 Name = wingSkin, index = 2 Name = wingRib, index = 3 Creating FEA BEM Getting quads for BEM! capsIgnore attribute found for face - 4!! capsIgnore attribute found for face - 9!! capsIgnore attribute found for face - 11!! capsIgnore attribute found for face - 16!! capsIgnore attribute found for face - 18!! capsIgnore attribute found for face - 20!! capsIgnore attribute found for face - 21!! capsIgnore attribute found for face - 22!! capsIgnore attribute found for face - 28!! capsIgnore attribute found for face - 31!! capsIgnore attribute found for face - 32!! capsIgnore attribute found for face - 33!! capsIgnore attribute found for face - 34!! capsIgnore attribute found for face - 40!! capsIgnore attribute found for face - 41!! capsIgnore attribute found for face - 42!! capsIgnore attribute found for face - 44!! capsIgnore attribute found for face - 45!! capsIgnore attribute found for face - 46!! capsIgnore attribute found for face - 47!! capsIgnore attribute found for face - 48!! capsIgnore attribute found for face - 55!! capsIgnore attribute found for face - 56!! capsIgnore attribute found for face - 57!! capsIgnore attribute found for face - 58!! capsIgnore attribute found for face - 59!! capsIgnore attribute found for face - 60!! capsIgnore attribute found for face - 61!! capsIgnore attribute found for face - 67!! capsIgnore attribute found for face - 69!! capsIgnore attribute found for face - 70!! capsIgnore attribute found for face - 71!! capsIgnore attribute found for face - 72!! capsIgnore attribute found for face - 74!! capsIgnore attribute found for face - 76!! capsIgnore attribute found for face - 77!! capsIgnore attribute found for face - 79!! capsIgnore attribute found for face - 80!! capsIgnore attribute found for face - 81!! capsIgnore attribute found for face - 82!! capsIgnore attribute found for face - 83!! capsIgnore attribute found for face - 85!! capsIgnore attribute found for face - 87!! capsIgnore attribute found for face - 88!! capsIgnore attribute found for face - 89!! capsIgnore attribute found for face - 90!! capsIgnore attribute found for face - 91!! capsIgnore attribute found for face - 92!! capsIgnore attribute found for face - 93!! capsIgnore attribute found for face - 94!! capsIgnore attribute found for face - 95!! capsIgnore attribute found for face - 96!! Removing unused nodes... Removed 199 (out of 615) unused nodes! Mesh for body = 0 Number of nodal coordinates = 416 Number of elements = 430 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 6 Elemental Quad4 = 424 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 - 3 Property name - wingRib Property name - wingSkin Property name - wingSpar Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - pointConstraint1 No "constraintType" specified for Constraint tuple pointConstraint1, defaulting to "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 - 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 ==> Running Astros... ==> Running ASTROS post-analysis... ================ run_astrosStatic.py complete ================== astrosStatic results --> Maximum displacements: Tmax : 0.0599508171648642 T1max : 0.00124021 T2max : 0.00470733 T3max : 0.0598442 Help on run_astrosModal() run ASTROS to perform modal analysis of a built-up-element structure inputs: filename name of .csm or .cpc file output: freqs list of natural frequencies ==> Loading geometry from file "wing3.csm"... ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000191 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018/wing3.csm:102]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) ERROR:: BAD STATUS = -1 from processFile (called from udpExecute:183) processFile: could not open file "editAttr_5.txt" ERROR:: (egads_notfound) in Branch Brch_001668 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAstros.udc:35]] processFile: could not open file "editAttr_5.txt" --> catching signal -1 (egads_notfound) Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = pointConstraint1, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperRiteWing, index = 1 Name = lowerRiteWing, index = 2 Name = upperLeftWing, index = 3 Name = lowerLeftWing, 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 = 3 Name = wingSpar, index = 1 Name = wingSkin, index = 2 Name = wingRib, index = 3 Creating FEA BEM Getting quads for BEM! capsIgnore attribute found for face - 4!! capsIgnore attribute found for face - 9!! capsIgnore attribute found for face - 11!! capsIgnore attribute found for face - 16!! capsIgnore attribute found for face - 18!! capsIgnore attribute found for face - 20!! capsIgnore attribute found for face - 21!! capsIgnore attribute found for face - 22!! capsIgnore attribute found for face - 28!! capsIgnore attribute found for face - 31!! capsIgnore attribute found for face - 32!! capsIgnore attribute found for face - 33!! capsIgnore attribute found for face - 34!! capsIgnore attribute found for face - 40!! capsIgnore attribute found for face - 41!! capsIgnore attribute found for face - 42!! capsIgnore attribute found for face - 44!! capsIgnore attribute found for face - 45!! capsIgnore attribute found for face - 46!! capsIgnore attribute found for face - 47!! capsIgnore attribute found for face - 48!! capsIgnore attribute found for face - 55!! capsIgnore attribute found for face - 56!! capsIgnore attribute found for face - 57!! capsIgnore attribute found for face - 58!! capsIgnore attribute found for face - 59!! capsIgnore attribute found for face - 60!! capsIgnore attribute found for face - 61!! capsIgnore attribute found for face - 67!! capsIgnore attribute found for face - 69!! capsIgnore attribute found for face - 70!! capsIgnore attribute found for face - 71!! capsIgnore attribute found for face - 72!! capsIgnore attribute found for face - 74!! capsIgnore attribute found for face - 76!! capsIgnore attribute found for face - 77!! capsIgnore attribute found for face - 79!! capsIgnore attribute found for face - 80!! capsIgnore attribute found for face - 81!! capsIgnore attribute found for face - 82!! capsIgnore attribute found for face - 83!! capsIgnore attribute found for face - 85!! capsIgnore attribute found for face - 87!! capsIgnore attribute found for face - 88!! capsIgnore attribute found for face - 89!! capsIgnore attribute found for face - 90!! capsIgnore attribute found for face - 91!! capsIgnore attribute found for face - 92!! capsIgnore attribute found for face - 93!! capsIgnore attribute found for face - 94!! capsIgnore attribute found for face - 95!! capsIgnore attribute found for face - 96!! Removing unused nodes... Removed 199 (out of 615) unused nodes! Mesh for body = 0 Number of nodal coordinates = 416 Number of elements = 430 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 6 Elemental Quad4 = 424 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 - 3 Property name - wingRib Property name - wingSkin Property name - wingSpar Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - pointConstraint1 No "constraintType" specified for Constraint tuple pointConstraint1, 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 ==> Running Astros... ==> Running ASTROS 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 ================ run_astrosModal.py complete ================== astrosModal results --> Eigen frequencies: 1 : 0.0207653 2 : 0.0415908 3 : 0.139771 4 : 0.16025 5 : 0.193278 6 : 0.279375 7 : 0.363625 8 : 0.436392 9 : 0.444983 10: 0.518093 Help on run_dataTransfer() run sansLIP to compute surface pressures which are transferred to astros static solver inputs: filename name of .csm or .cpc file outputs: disps dictionary containing maximum displacements: Tmax 3D displacement T1max displacement in X-direction T2max displacement in Y-direction T3max displacement in Z-direction ==> Loading geometry from file "wing3.csm"... ==> Setting Build Variables and Geometry Values... ERROR:: (name_not_found) in Branch Brch_000456 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:57]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) Marking Solid Edge 7 : wingWake Marking Solid Edge 1 : wingWake Wake intersection... 3.03613 s Scribing solid Marking Trailing Vortex/Trefftz edges Wake TrailingVortex edge : 2 wingWake Wake Trefftz edge : 3 wingWake -- solid face : 6 Wake TrailingVortex edge : 6 wingWake Wake Trefftz edge : 7 wingWake -- solid face : 6 ERROR:: (name_not_found) in Branch Brch_000817 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:591]] storage "WingHinge" 1 not found --> catching signal -251 (name_not_found) ERROR:: BAD STATUS = -1 from processFile (called from udpExecute:183) processFile: could not open file "editAttr_5.txt" ERROR:: (egads_notfound) in Branch Brch_001668 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAstros.udc:35]] processFile: could not open file "editAttr_5.txt" --> catching signal -1 (egads_notfound) ==> Filling vertex sets... ==> Running sansLIP pre-analysis and analysis... Generating AFLR4 surface mesh... AFLR4 success! AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 5989 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 Transparent w/BL UG3 : 14 Transparent w/BL AFLR3 : CPU Time = 0.011 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 5989 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1200 6996 AFLR3 IG : Nodes, Elements = 2400 13745 AFLR3 IG : Nodes, Elements = 3600 21720 AFLR3 IG : Nodes, Elements = 4800 29564 AFLR3 IG : Nodes, Elements = 5996 36721 AFLR3 IG : Nodes, Elements = 5996 36636 AFLR3 IG : Nodes, Elements = 5989 22392 AFLR3 IG : Nodes, Elements = 5989 22448 AFLR3 IG : Nodes, Elements = 5989 19658 AFLR3 IG : Nodes, Elements = 5989 19235 AFLR3 : CPU Time = 0.136 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 5989 19235 AFLR3 GG : Nodes, Elements = 8707 27395 AFLR3 GG : Nodes, Elements = 8707 37657 AFLR3 GG : Nodes, Elements = 8707 35016 AFLR3 GG : Nodes, Elements = 10923 41706 AFLR3 GG : Nodes, Elements = 10923 50229 AFLR3 GG : Nodes, Elements = 10923 47658 AFLR3 GG : Nodes, Elements = 13133 54331 AFLR3 GG : Nodes, Elements = 13133 63369 AFLR3 GG : Nodes, Elements = 13133 60918 AFLR3 GG : Nodes, Elements = 15316 67495 AFLR3 GG : Nodes, Elements = 15316 76128 AFLR3 GG : Nodes, Elements = 15316 73788 AFLR3 GG : Nodes, Elements = 17418 80114 AFLR3 GG : Nodes, Elements = 17418 88349 AFLR3 GG : Nodes, Elements = 17418 86104 AFLR3 GG : Nodes, Elements = 19462 92245 AFLR3 GG : Nodes, Elements = 19462 100298 AFLR3 GG : Nodes, Elements = 19462 98178 AFLR3 GG : Nodes, Elements = 21395 103988 AFLR3 GG : Nodes, Elements = 21395 111463 AFLR3 GG : Nodes, Elements = 21395 109485 AFLR3 GG : Nodes, Elements = 23262 115098 AFLR3 GG : Nodes, Elements = 23262 122435 AFLR3 GG : Nodes, Elements = 23262 120462 AFLR3 GG : Nodes, Elements = 25032 125780 AFLR3 GG : Nodes, Elements = 25032 132765 AFLR3 GG : Nodes, Elements = 25032 130916 AFLR3 GG : Nodes, Elements = 26727 136009 AFLR3 GG : Nodes, Elements = 26727 142733 AFLR3 GG : Nodes, Elements = 26727 140975 AFLR3 GG : Nodes, Elements = 28322 145768 AFLR3 GG : Nodes, Elements = 28322 152151 AFLR3 GG : Nodes, Elements = 28322 150393 AFLR3 GG : Nodes, Elements = 29846 154974 AFLR3 GG : Nodes, Elements = 29846 161089 AFLR3 GG : Nodes, Elements = 29846 159473 AFLR3 GG : Nodes, Elements = 31296 163827 AFLR3 GG : Nodes, Elements = 31296 169508 AFLR3 GG : Nodes, Elements = 31296 168031 AFLR3 GG : Nodes, Elements = 32604 171957 AFLR3 GG : Nodes, Elements = 32604 177079 AFLR3 GG : Nodes, Elements = 32604 175706 AFLR3 GG : Nodes, Elements = 33864 179489 AFLR3 GG : Nodes, Elements = 33864 184386 AFLR3 GG : Nodes, Elements = 33864 183115 AFLR3 GG : Nodes, Elements = 34976 186453 AFLR3 GG : Nodes, Elements = 34976 190861 AFLR3 GG : Nodes, Elements = 34976 189714 AFLR3 GG : Nodes, Elements = 35982 192733 AFLR3 GG : Nodes, Elements = 35982 196656 AFLR3 GG : Nodes, Elements = 35982 195648 AFLR3 GG : Nodes, Elements = 36919 198460 AFLR3 GG : Nodes, Elements = 36919 202212 AFLR3 GG : Nodes, Elements = 36919 201241 AFLR3 GG : Nodes, Elements = 37740 203705 AFLR3 GG : Nodes, Elements = 37740 206924 AFLR3 GG : Nodes, Elements = 37740 206094 AFLR3 GG : Nodes, Elements = 38484 208327 AFLR3 GG : Nodes, Elements = 38484 211325 AFLR3 GG : Nodes, Elements = 38484 210528 AFLR3 GG : Nodes, Elements = 39151 212531 AFLR3 GG : Nodes, Elements = 39151 215158 AFLR3 GG : Nodes, Elements = 39151 214481 AFLR3 GG : Nodes, Elements = 39723 216199 AFLR3 GG : Nodes, Elements = 39723 218461 AFLR3 GG : Nodes, Elements = 39723 217887 AFLR3 GG : Nodes, Elements = 40206 219336 AFLR3 GG : Nodes, Elements = 40206 221291 AFLR3 GG : Nodes, Elements = 40206 220770 AFLR3 GG : Nodes, Elements = 40612 221988 AFLR3 GG : Nodes, Elements = 40612 223571 AFLR3 GG : Nodes, Elements = 40612 223163 AFLR3 GG : Nodes, Elements = 40967 224228 AFLR3 GG : Nodes, Elements = 40967 225645 AFLR3 GG : Nodes, Elements = 40967 225273 AFLR3 GG : Nodes, Elements = 41264 226165 AFLR3 GG : Nodes, Elements = 41264 227338 AFLR3 GG : Nodes, Elements = 41264 227036 AFLR3 GG : Nodes, Elements = 41491 227717 AFLR3 GG : Nodes, Elements = 41491 228625 AFLR3 GG : Nodes, Elements = 41491 228382 AFLR3 GG : Nodes, Elements = 41660 228889 AFLR3 GG : Nodes, Elements = 41660 229572 AFLR3 GG : Nodes, Elements = 41660 229383 AFLR3 GG : Nodes, Elements = 41768 229707 AFLR3 GG : Nodes, Elements = 41768 230130 AFLR3 GG : Nodes, Elements = 41768 230011 AFLR3 GG : Nodes, Elements = 41836 230215 AFLR3 GG : Nodes, Elements = 41836 230512 AFLR3 GG : Nodes, Elements = 41836 230417 AFLR3 GG : Nodes, Elements = 41884 230561 AFLR3 GG : Nodes, Elements = 41884 230767 AFLR3 GG : Nodes, Elements = 41884 230695 AFLR3 GG : Nodes, Elements = 41897 230734 AFLR3 GG : Nodes, Elements = 41897 230802 AFLR3 GG : Nodes, Elements = 41897 230768 AFLR3 GG : Nodes, Elements = 41904 230789 AFLR3 GG : Nodes, Elements = 41904 230825 AFLR3 GG : Nodes, Elements = 41904 230815 AFLR3 GG : Nodes, Elements = 41905 230818 AFLR3 GG : Nodes, Elements = 41905 230820 AFLR3 GG : Nodes, Elements = 41934 230907 AFLR3 GG : Nodes, Elements = 41934 230973 AFLR3 GG : Nodes, Elements = 41934 230960 AFLR3 GG : Nodes, Elements = 41937 230969 AFLR3 GG : Nodes, Elements = 41937 230979 AFLR3 GG : Nodes, Elements = 41937 230977 AFLR3 GG : Nodes, Elements = 41938 230980 AFLR3 GG : Nodes, Elements = 41938 230984 AFLR3 GG : Nodes, Elements = 41938 230982 AFLR3 : CPU Time = 2.470 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 41938 230982 AFLR3 QI : Nodes, Elements = 41829 230386 AFLR3 QI : Nodes, Elements = 41819 230336 AFLR3 QI : Nodes, Elements = 41819 231404 AFLR3 QI : Nodes, Elements = 41819 230446 AFLR3 QI : Nodes, Elements = 41819 230086 AFLR3 QI : Nodes, Elements = 41819 230359 AFLR3 QI : Nodes, Elements = 41819 230102 AFLR3 QI : Nodes, Elements = 41819 230050 AFLR3 : CPU Time = 0.388 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 230050 UG3 : Min, Max Ang = 13.55 153.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.81e+04 UG3 : No. Tet Elems = 230050 UG3 : Min Vol = 2.64e-06 UG3 : Average Vol = 0.253 UG3 : Total-Tet-Vol = 5.81e+04 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 230050 UG3 : Min, Max Q = 0.35 0.999 UG3 : Average Q = 0.878 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 Adding 584 tet centers Trefftz Frames (2) : 2 3 Non-zero time : 0.636229 second(s) Total Degrees of Freedom : 42798 Factorizing matrix... Jacobian time : 0.878112 second(s) Numeric factor time : 0.866576 second(s) Done Solving primal system : MKL_PARDISO solve time : 0.0490448 second(s) Solving Fx adjoint : MKL_PARDISO solve time : 0.0501997 second(s) Solving Fy adjoint : MKL_PARDISO solve time : 0.0520531 second(s) Solving Fz adjoint : MKL_PARDISO solve time : 0.0503084 second(s) Solving Mx adjoint : MKL_PARDISO solve time : 0.0535875 second(s) Solving My adjoint : MKL_PARDISO solve time : 0.053653 second(s) Solving Mz adjoint : MKL_PARDISO solve time : 0.0550693 second(s) ==> Running sansLIP post-analysis... ==> Executing pressure dataTransfer... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = pointConstraint1, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperRiteWing, index = 1 Name = lowerRiteWing, index = 2 Name = upperLeftWing, index = 3 Name = lowerLeftWing, 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 = 3 Name = wingSpar, index = 1 Name = wingSkin, index = 2 Name = wingRib, index = 3 Creating FEA BEM Getting quads for BEM! capsIgnore attribute found for face - 4!! capsIgnore attribute found for face - 9!! capsIgnore attribute found for face - 11!! capsIgnore attribute found for face - 16!! capsIgnore attribute found for face - 18!! capsIgnore attribute found for face - 20!! capsIgnore attribute found for face - 21!! capsIgnore attribute found for face - 28!! capsIgnore attribute found for face - 31!! capsIgnore attribute found for face - 32!! capsIgnore attribute found for face - 33!! capsIgnore attribute found for face - 40!! capsIgnore attribute found for face - 41!! capsIgnore attribute found for face - 43!! capsIgnore attribute found for face - 44!! capsIgnore attribute found for face - 45!! capsIgnore attribute found for face - 53!! capsIgnore attribute found for face - 54!! capsIgnore attribute found for face - 55!! capsIgnore attribute found for face - 56!! capsIgnore attribute found for face - 63!! capsIgnore attribute found for face - 65!! capsIgnore attribute found for face - 66!! capsIgnore attribute found for face - 67!! capsIgnore attribute found for face - 71!! capsIgnore attribute found for face - 72!! capsIgnore attribute found for face - 74!! capsIgnore attribute found for face - 75!! capsIgnore attribute found for face - 76!! capsIgnore attribute found for face - 77!! capsIgnore attribute found for face - 81!! capsIgnore attribute found for face - 82!! capsIgnore attribute found for face - 83!! capsIgnore attribute found for face - 84!! capsIgnore attribute found for face - 85!! capsIgnore attribute found for face - 86!! capsIgnore attribute found for face - 87!! capsIgnore attribute found for face - 88!! Removing unused nodes... Removed 140 (out of 576) unused nodes! Mesh for body = 0 Number of nodal coordinates = 436 Number of elements = 452 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 28 Elemental Quad4 = 424 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 - 3 Property name - wingRib Property name - wingSkin Property name - wingSpar Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - pointConstraint1 No "constraintType" specified for Constraint tuple pointConstraint1, defaulting to "ZeroDisplacement" Done getting 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 fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing ==> Running Astros pre-analysis... Extracting external pressure loads from data transfer.... TransferName = upperLeftWing Number of Elements = 80 (total = 80) TransferName = upperRiteWing Number of Elements = 80 (total = 160) TransferName = lowerLeftWing Number of Elements = 80 (total = 240) TransferName = lowerRiteWing Number of Elements = 80 (total = 320) Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards ==> Running Astros... ==> Running Astros post-analysis... ================ run_dataTransfer.py complete ================== dataTransfer results --> Maximum displacements: Tmax : 415.38020017514077 T1max : 14.3237 T2max : 25.8234 T3max : 414.798 WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! 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.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! WARNING: 'capsGeometry.buildGeometry' is deprecated. Please use 'Problem.geometry.build'! WARNING: 'capsGeometry.getGeometryOutVal' is deprecated. Please use 'Problem.geometry.outpmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'! WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'! WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'! WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'! WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'! real 4m45.385s user 28m38.097s sys 5m3.390s ++ for i in `ls wing*.csm | sort -f` ++ python runAll.py wing4.csm Help on run_avl() run AVL to compute force coefficients inputs: filename name of .csm or .cpc file outputs: coefs dictionary containing force/moment coefficients: CLtot lift coefficient CDtot drag coefficient CXtot X-force coefficient CYtot Y-force coefficient CZtot Z-force coefficient Cltot rolling moment coefficient Cmtot pitching moment coefficient Cntot yawing moment coefficient e Oswald efficiency factor ==> Loading geometry from file "wing4.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading AVL aim... ==> Running AVL pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000192 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018/wing4.csm:108]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) ERROR:: (name_not_found) in Branch Brch_000357 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAvl.udc:61]] storage "WingHinge" 3 not found --> catching signal -251 (name_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice control surface data VLM control surface name - WingHinge1 VLM control surface name - WingHinge2 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 Done getting vortex lattice surface data Writing surface - Wing (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) ==> Running AVL... ==> Running AVL post-analysis... ================ run_avl.py complete ================== AVL results --> Force/moment coefficients: CXtot : 0.1320423158252318 CYtot : -0.01023123333958946 CZtot : -1.278726166104227 Cltot : -0.04218058926833301 Cmtot : -0.7466826978744193 Cntot : 0.003425631256815422 CLtot : 1.282228349876992 CDtot : 0.0920121721286445 e : 0.9216037059402639 Help on run_sansLIP() run sansLIP to compute force coefficients inputs: filename name of .csm or .cpc file outputs: coefs dictionary containing force/moment coefficients: CLtot lift coefficient CDtot drag coefficient CXtot X-force coefficient CYtot Y-force coefficient CZtot Z-force coefficient Cltot rolling moment coefficient Cmtot pitching moment coefficient Cntot yawing moment coefficient e Oswald efficiency factor ==> Loading geometry from file "wing4.csm"... ==> Setting Build Variables and Geometry Values... ==> Loading sansLIP aim... ERROR:: (name_not_found) in Branch Brch_000488 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:57]] storage "WingHinge" 3 not found --> catching signal -251 (name_not_found) Marking Solid Edge 19 : wingWake Marking Solid Edge 22 : wingWake Marking Solid Edge 15 : wingWake Marking Solid Edge 5 : wingWake Marking Solid Edge 9 : wingWake Marking Solid Edge 1 : wingWake Wake intersection... 4.1425 s Scribing solid Marking Trailing Vortex/Trefftz edges Wake TrailingVortex edge : 2 wingWake Wake Trefftz edge : 3 wingWake -- solid face : 6 Wake Trefftz edge : 6 wingWake -- solid face : 6 Wake Trefftz edge : 9 wingWake -- solid face : 6 Wake Trefftz edge : 13 wingWake -- solid face : 6 Wake Trefftz edge : 16 wingWake -- solid face : 6 Wake TrailingVortex edge : 18 wingWake Wake Trefftz edge : 19 wingWake -- solid face : 6 ERROR:: (name_not_found) in Branch Brch_000849 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:591]] storage "WingHinge" 3 not found --> catching signal -251 (name_not_found) ==> Running sansLIP pre-analysis and analysis... Generating AFLR4 surface mesh... AFLR4 success! AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.31.6 AFLR3 : Version Date 08/30/21 @ 12:37AM AFLR3 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR3 : Compile Date 08/30/21 @ 01:15AM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 3833 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 Transparent w/BL UG3 : 18 Transparent w/BL UG3 : 19 Transparent w/BL UG3 : 20 Transparent w/BL UG3 : 21 Transparent w/BL UG3 : 22 Transparent w/BL AFLR3 : CPU Time = 0.011 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 3833 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 768 4172 AFLR3 IG : Nodes, Elements = 1536 8404 AFLR3 IG : Nodes, Elements = 2304 12582 AFLR3 IG : Nodes, Elements = 3072 17144 AFLR3 IG : Nodes, Elements = 3840 21444 AFLR3 IG : Nodes, Elements = 3840 21391 AFLR3 IG : Nodes, Elements = 3840 21399 AFLR3 IG : Nodes, Elements = 3840 21380 AFLR3 IG : Nodes, Elements = 3840 21381 AFLR3 IG : Nodes, Elements = 3833 14172 AFLR3 IG : Nodes, Elements = 3833 14220 AFLR3 IG : Nodes, Elements = 3833 13009 AFLR3 IG : Nodes, Elements = 3833 12813 AFLR3 : CPU Time = 0.117 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 3833 12813 AFLR3 GG : Nodes, Elements = 5479 17754 AFLR3 GG : Nodes, Elements = 5479 23989 AFLR3 GG : Nodes, Elements = 5479 22465 AFLR3 GG : Nodes, Elements = 6880 26677 AFLR3 GG : Nodes, Elements = 6880 32211 AFLR3 GG : Nodes, Elements = 6880 30695 AFLR3 GG : Nodes, Elements = 8241 34781 AFLR3 GG : Nodes, Elements = 8241 40353 AFLR3 GG : Nodes, Elements = 8241 38861 AFLR3 GG : Nodes, Elements = 9549 42788 AFLR3 GG : Nodes, Elements = 9549 48036 AFLR3 GG : Nodes, Elements = 9549 46690 AFLR3 GG : Nodes, Elements = 10776 50374 AFLR3 GG : Nodes, Elements = 10776 55126 AFLR3 GG : Nodes, Elements = 10776 53818 AFLR3 GG : Nodes, Elements = 11956 57360 AFLR3 GG : Nodes, Elements = 11956 62019 AFLR3 GG : Nodes, Elements = 11956 60786 AFLR3 GG : Nodes, Elements = 13091 64191 AFLR3 GG : Nodes, Elements = 13091 68613 AFLR3 GG : Nodes, Elements = 13091 67477 AFLR3 GG : Nodes, Elements = 14171 70718 AFLR3 GG : Nodes, Elements = 14171 74907 AFLR3 GG : Nodes, Elements = 14171 73836 AFLR3 GG : Nodes, Elements = 15185 76881 AFLR3 GG : Nodes, Elements = 15185 80812 AFLR3 GG : Nodes, Elements = 15185 79815 AFLR3 GG : Nodes, Elements = 16137 82672 AFLR3 GG : Nodes, Elements = 16137 86405 AFLR3 GG : Nodes, Elements = 16137 85438 AFLR3 GG : Nodes, Elements = 17038 88142 AFLR3 GG : Nodes, Elements = 17038 91654 AFLR3 GG : Nodes, Elements = 17038 90748 AFLR3 GG : Nodes, Elements = 17894 93317 AFLR3 GG : Nodes, Elements = 17894 96695 AFLR3 GG : Nodes, Elements = 17894 95836 AFLR3 GG : Nodes, Elements = 18698 98250 AFLR3 GG : Nodes, Elements = 18698 101401 AFLR3 GG : Nodes, Elements = 18698 100550 AFLR3 GG : Nodes, Elements = 19438 102772 AFLR3 GG : Nodes, Elements = 19438 105708 AFLR3 GG : Nodes, Elements = 19438 104918 AFLR3 GG : Nodes, Elements = 20122 106972 AFLR3 GG : Nodes, Elements = 20122 109676 AFLR3 GG : Nodes, Elements = 20122 108960 AFLR3 GG : Nodes, Elements = 20778 110929 AFLR3 GG : Nodes, Elements = 20778 113414 AFLR3 GG : Nodes, Elements = 20778 112821 AFLR3 GG : Nodes, Elements = 21354 114549 AFLR3 GG : Nodes, Elements = 21354 116794 AFLR3 GG : Nodes, Elements = 21354 116241 AFLR3 GG : Nodes, Elements = 21853 117738 AFLR3 GG : Nodes, Elements = 21853 119697 AFLR3 GG : Nodes, Elements = 21853 119176 AFLR3 GG : Nodes, Elements = 22270 120428 AFLR3 GG : Nodes, Elements = 22270 122085 AFLR3 GG : Nodes, Elements = 22270 121654 AFLR3 GG : Nodes, Elements = 22625 122719 AFLR3 GG : Nodes, Elements = 22625 124151 AFLR3 GG : Nodes, Elements = 22625 123752 AFLR3 GG : Nodes, Elements = 22889 124545 AFLR3 GG : Nodes, Elements = 22889 125622 AFLR3 GG : Nodes, Elements = 22889 125295 AFLR3 GG : Nodes, Elements = 23040 125748 AFLR3 GG : Nodes, Elements = 23040 126371 AFLR3 GG : Nodes, Elements = 23040 126199 AFLR3 GG : Nodes, Elements = 23150 126529 AFLR3 GG : Nodes, Elements = 23150 126974 AFLR3 GG : Nodes, Elements = 23150 126851 AFLR3 GG : Nodes, Elements = 23197 126992 AFLR3 GG : Nodes, Elements = 23197 127180 AFLR3 GG : Nodes, Elements = 23197 127124 AFLR3 GG : Nodes, Elements = 23211 127166 AFLR3 GG : Nodes, Elements = 23211 127235 AFLR3 GG : Nodes, Elements = 23211 127202 AFLR3 GG : Nodes, Elements = 23216 127217 AFLR3 GG : Nodes, Elements = 23216 127240 AFLR3 GG : Nodes, Elements = 23216 127233 AFLR3 GG : Nodes, Elements = 23235 127290 AFLR3 GG : Nodes, Elements = 23235 127344 AFLR3 GG : Nodes, Elements = 23235 127334 AFLR3 : CPU Time = 0.893 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 23235 127334 AFLR3 QI : Nodes, Elements = 23202 127147 AFLR3 QI : Nodes, Elements = 23201 127141 AFLR3 QI : Nodes, Elements = 23201 127786 AFLR3 QI : Nodes, Elements = 23201 127251 AFLR3 QI : Nodes, Elements = 23201 127054 AFLR3 QI : Nodes, Elements = 23201 127224 AFLR3 QI : Nodes, Elements = 23201 127070 AFLR3 QI : Nodes, Elements = 23201 127042 AFLR3 : CPU Time = 0.162 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 127042 UG3 : Min, Max Ang = 10.61 152.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.81e+04 UG3 : No. Tet Elems = 127042 UG3 : Min Vol = 0.00013 UG3 : Average Vol = 0.457 UG3 : Total-Tet-Vol = 5.81e+04 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 127042 UG3 : Min, Max Q = 0.287 0.999 UG3 : Average Q = 0.877 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 Adding 655 tet centers Trefftz Frames (6) : 6 7 8 9 10 11 Non-zero time : 0.478271 second(s) Total Degrees of Freedom : 24455 Factorizing matrix... Jacobian time : 0.723112 second(s) Numeric factor time : 0.725004 second(s) Done Solving primal system : MKL_PARDISO solve time : 0.0698199 second(s) Solving Fx adjoint : MKL_PARDISO solve time : 0.0683648 second(s) Solving Fy adjoint : MKL_PARDISO solve time : 0.0733026 second(s) Solving Fz adjoint : MKL_PARDISO solve time : 0.0535902 second(s) Solving Mx adjoint : MKL_PARDISO solve time : 0.0478002 second(s) Solving My adjoint : MKL_PARDISO solve time : 0.0419107 second(s) Solving Mz adjoint : MKL_PARDISO solve time : 0.02951 second(s) output_Tecplot: filename = wing4.dat ==> Running sansLIP post-analysis... ================ run_sansLIP.py complete ================== sansLIP results --> Force/moment coefficients: CXtot : 0.0687593542283613 CYtot : -0.0019269859838690069 CZtot : -1.035456522515127 Cltot : -0.034103843541501734 Cmtot : -0.5925394339126006 Cntot : 0.0017149362141873749 CLtot : 1.0316655478392671 CDtot : 0.11209039305188569 e : 0.5037439640076952 Help on run_astrosStatic() run ASTROS to perform linear static analysis of a built-up-element structure inputs: filename name of .csm or .cpc file outputs: disps dictionary containing maximum displacements: Tmax 3D displacement T1max displacement in X-direction T2max displacement in Y-direction T3max displacement in Z-direction ==> Loading geometry from file "wing4.csm"... ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000192 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018/wing4.csm:108]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) ERROR:: BAD STATUS = -1 from processFile (called from udpExecute:183) processFile: could not open file "editAttr_6.txt" ERROR:: (egads_notfound) in Branch Brch_001700 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAstros.udc:35]] processFile: could not open file "editAttr_6.txt" --> catching signal -1 (egads_notfound) Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = pointConstraint1, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperRiteWing, index = 1 Name = lowerRiteWing, index = 2 Name = upperLeftWing, index = 3 Name = lowerLeftWing, 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 = 3 Name = wingSpar, index = 1 Name = wingSkin, index = 2 Name = wingRib, index = 3 Creating FEA BEM Getting quads for BEM! capsIgnore attribute found for face - 4!! capsIgnore attribute found for face - 9!! capsIgnore attribute found for face - 11!! capsIgnore attribute found for face - 16!! capsIgnore attribute found for face - 18!! capsIgnore attribute found for face - 20!! capsIgnore attribute found for face - 21!! capsIgnore attribute found for face - 22!! capsIgnore attribute found for face - 28!! capsIgnore attribute found for face - 31!! capsIgnore attribute found for face - 32!! capsIgnore attribute found for face - 33!! capsIgnore attribute found for face - 34!! capsIgnore attribute found for face - 40!! capsIgnore attribute found for face - 41!! capsIgnore attribute found for face - 42!! capsIgnore attribute found for face - 44!! capsIgnore attribute found for face - 45!! capsIgnore attribute found for face - 46!! capsIgnore attribute found for face - 47!! capsIgnore attribute found for face - 48!! capsIgnore attribute found for face - 55!! capsIgnore attribute found for face - 56!! capsIgnore attribute found for face - 57!! capsIgnore attribute found for face - 58!! capsIgnore attribute found for face - 59!! capsIgnore attribute found for face - 60!! capsIgnore attribute found for face - 61!! capsIgnore attribute found for face - 67!! capsIgnore attribute found for face - 69!! capsIgnore attribute found for face - 70!! capsIgnore attribute found for face - 71!! capsIgnore attribute found for face - 72!! capsIgnore attribute found for face - 74!! capsIgnore attribute found for face - 76!! capsIgnore attribute found for face - 77!! capsIgnore attribute found for face - 79!! capsIgnore attribute found for face - 80!! capsIgnore attribute found for face - 81!! capsIgnore attribute found for face - 82!! capsIgnore attribute found for face - 83!! capsIgnore attribute found for face - 85!! capsIgnore attribute found for face - 87!! capsIgnore attribute found for face - 88!! capsIgnore attribute found for face - 89!! capsIgnore attribute found for face - 90!! capsIgnore attribute found for face - 91!! capsIgnore attribute found for face - 92!! capsIgnore attribute found for face - 93!! capsIgnore attribute found for face - 94!! capsIgnore attribute found for face - 95!! capsIgnore attribute found for face - 96!! Removing unused nodes... Removed 199 (out of 615) unused nodes! Mesh for body = 0 Number of nodal coordinates = 416 Number of elements = 430 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 6 Elemental Quad4 = 424 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 - 3 Property name - wingRib Property name - wingSkin Property name - wingSpar Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - pointConstraint1 No "constraintType" specified for Constraint tuple pointConstraint1, defaulting to "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 - 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 ==> Running Astros... ==> Running ASTROS post-analysis... ================ run_astrosStatic.py complete ================== astrosStatic results --> Maximum displacements: Tmax : 0.0599508171648642 T1max : 0.00124021 T2max : 0.00470733 T3max : 0.0598442 Help on run_astrosModal() run ASTROS to perform modal analysis of a built-up-element structure inputs: filename name of .csm or .cpc file output: freqs list of natural frequencies ==> Loading geometry from file "wing4.csm"... ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000192 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/test/training2018/wing4.csm:108]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) ERROR:: BAD STATUS = -1 from processFile (called from udpExecute:183) processFile: could not open file "editAttr_5.txt" ERROR:: (egads_notfound) in Branch Brch_001700 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAstros.udc:35]] processFile: could not open file "editAttr_5.txt" --> catching signal -1 (egads_notfound) Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = pointConstraint1, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperRiteWing, index = 1 Name = lowerRiteWing, index = 2 Name = upperLeftWing, index = 3 Name = lowerLeftWing, 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 = 3 Name = wingSpar, index = 1 Name = wingSkin, index = 2 Name = wingRib, index = 3 Creating FEA BEM Getting quads for BEM! capsIgnore attribute found for face - 4!! capsIgnore attribute found for face - 9!! capsIgnore attribute found for face - 11!! capsIgnore attribute found for face - 16!! capsIgnore attribute found for face - 18!! capsIgnore attribute found for face - 20!! capsIgnore attribute found for face - 21!! capsIgnore attribute found for face - 22!! capsIgnore attribute found for face - 28!! capsIgnore attribute found for face - 31!! capsIgnore attribute found for face - 32!! capsIgnore attribute found for face - 33!! capsIgnore attribute found for face - 34!! capsIgnore attribute found for face - 40!! capsIgnore attribute found for face - 41!! capsIgnore attribute found for face - 42!! capsIgnore attribute found for face - 44!! capsIgnore attribute found for face - 45!! capsIgnore attribute found for face - 46!! capsIgnore attribute found for face - 47!! capsIgnore attribute found for face - 48!! capsIgnore attribute found for face - 55!! capsIgnore attribute found for face - 56!! capsIgnore attribute found for face - 57!! capsIgnore attribute found for face - 58!! capsIgnore attribute found for face - 59!! capsIgnore attribute found for face - 60!! capsIgnore attribute found for face - 61!! capsIgnore attribute found for face - 67!! capsIgnore attribute found for face - 69!! capsIgnore attribute found for face - 70!! capsIgnore attribute found for face - 71!! capsIgnore attribute found for face - 72!! capsIgnore attribute found for face - 74!! capsIgnore attribute found for face - 76!! capsIgnore attribute found for face - 77!! capsIgnore attribute found for face - 79!! capsIgnore attribute found for face - 80!! capsIgnore attribute found for face - 81!! capsIgnore attribute found for face - 82!! capsIgnore attribute found for face - 83!! capsIgnore attribute found for face - 85!! capsIgnore attribute found for face - 87!! capsIgnore attribute found for face - 88!! capsIgnore attribute found for face - 89!! capsIgnore attribute found for face - 90!! capsIgnore attribute found for face - 91!! capsIgnore attribute found for face - 92!! capsIgnore attribute found for face - 93!! capsIgnore attribute found for face - 94!! capsIgnore attribute found for face - 95!! capsIgnore attribute found for face - 96!! Removing unused nodes... Removed 199 (out of 615) unused nodes! Mesh for body = 0 Number of nodal coordinates = 416 Number of elements = 430 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 6 Elemental Quad4 = 424 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 - 3 Property name - wingRib Property name - wingSkin Property name - wingSpar Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - pointConstraint1 No "constraintType" specified for Constraint tuple pointConstraint1, 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 ==> Running Astros... ==> Running ASTROS 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 ================ run_astrosModal.py complete ================== astrosModal results --> Eigen frequencies: 1 : 0.0207653 2 : 0.0415908 3 : 0.139771 4 : 0.16025 5 : 0.193278 6 : 0.279375 7 : 0.363625 8 : 0.436392 9 : 0.444983 10: 0.518093 Help on run_dataTransfer() run sansLIP to compute surface pressures which are transferred to astros static solver inputs: filename name of .csm or .cpc file outputs: disps dictionary containing maximum displacements: Tmax 3D displacement T1max displacement in X-direction T2max displacement in Y-direction T3max displacement in Z-direction ==> Loading geometry from file "wing4.csm"... ==> Setting Build Variables and Geometry Values... ERROR:: (name_not_found) in Branch Brch_000488 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:57]] storage "WingHinge" 3 not found --> catching signal -251 (name_not_found) Marking Solid Edge 19 : wingWake Marking Solid Edge 22 : wingWake Marking Solid Edge 15 : wingWake Marking Solid Edge 5 : wingWake Marking Solid Edge 9 : wingWake Marking Solid Edge 1 : wingWake Wake intersection... 3.78335 s Scribing solid Marking Trailing Vortex/Trefftz edges Wake TrailingVortex edge : 2 wingWake Wake Trefftz edge : 3 wingWake -- solid face : 6 Wake Trefftz edge : 6 wingWake -- solid face : 6 Wake Trefftz edge : 9 wingWake -- solid face : 6 Wake Trefftz edge : 13 wingWake -- solid face : 6 Wake Trefftz edge : 16 wingWake -- solid face : 6 Wake TrailingVortex edge : 18 wingWake Wake Trefftz edge : 19 wingWake -- solid face : 6 ERROR:: (name_not_found) in Branch Brch_000849 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewSansLIP.udc:591]] storage "WingHinge" 3 not found --> catching signal -251 (name_not_found) ERROR:: BAD STATUS = -1 from processFile (called from udpExecute:183) processFile: could not open file "editAttr_5.txt" ERROR:: (egads_notfound) in Branch Brch_001700 at [[/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64/ESP/LINUX64/udc/viewAstros.udc:35]] processFile: could not open file "editAttr_5.txt" --> catching signal -1 (egads_notfound) ==> Filling vertex sets... ==> Running sansLIP pre-analysis and analysis... Generating AFLR4 surface mesh... AFLR4 success! AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 6456 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 Transparent w/BL UG3 : 18 Transparent w/BL UG3 : 19 Transparent w/BL UG3 : 20 Transparent w/BL UG3 : 21 Transparent w/BL UG3 : 22 Transparent w/BL AFLR3 : CPU Time = 0.015 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 6456 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1292 7494 AFLR3 IG : Nodes, Elements = 2584 14666 AFLR3 IG : Nodes, Elements = 3876 23357 AFLR3 IG : Nodes, Elements = 5168 31503 AFLR3 IG : Nodes, Elements = 6460 39278 AFLR3 IG : Nodes, Elements = 6463 39291 AFLR3 IG : Nodes, Elements = 6463 39220 AFLR3 IG : Nodes, Elements = 6463 39228 AFLR3 IG : Nodes, Elements = 6463 39218 AFLR3 IG : Nodes, Elements = 6456 24366 AFLR3 IG : Nodes, Elements = 6456 24420 AFLR3 IG : Nodes, Elements = 6456 21482 AFLR3 IG : Nodes, Elements = 6456 21017 AFLR3 : CPU Time = 0.177 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 6456 21017 AFLR3 GG : Nodes, Elements = 9411 29885 AFLR3 GG : Nodes, Elements = 9411 41262 AFLR3 GG : Nodes, Elements = 9411 38411 AFLR3 GG : Nodes, Elements = 11929 46022 AFLR3 GG : Nodes, Elements = 11929 55733 AFLR3 GG : Nodes, Elements = 11929 52946 AFLR3 GG : Nodes, Elements = 14365 60305 AFLR3 GG : Nodes, Elements = 14365 70085 AFLR3 GG : Nodes, Elements = 14365 67371 AFLR3 GG : Nodes, Elements = 16686 74364 AFLR3 GG : Nodes, Elements = 16686 83803 AFLR3 GG : Nodes, Elements = 16686 81223 AFLR3 GG : Nodes, Elements = 18943 88023 AFLR3 GG : Nodes, Elements = 18943 96875 AFLR3 GG : Nodes, Elements = 18943 94473 AFLR3 GG : Nodes, Elements = 21093 100938 AFLR3 GG : Nodes, Elements = 21093 109548 AFLR3 GG : Nodes, Elements = 21093 107126 AFLR3 GG : Nodes, Elements = 23102 113167 AFLR3 GG : Nodes, Elements = 23102 121237 AFLR3 GG : Nodes, Elements = 23102 118971 AFLR3 GG : Nodes, Elements = 25042 124803 AFLR3 GG : Nodes, Elements = 25042 132608 AFLR3 GG : Nodes, Elements = 25042 130458 AFLR3 GG : Nodes, Elements = 26892 136023 AFLR3 GG : Nodes, Elements = 26892 143323 AFLR3 GG : Nodes, Elements = 26892 141381 AFLR3 GG : Nodes, Elements = 28654 146678 AFLR3 GG : Nodes, Elements = 28654 153694 AFLR3 GG : Nodes, Elements = 28654 151787 AFLR3 GG : Nodes, Elements = 30296 156721 AFLR3 GG : Nodes, Elements = 30296 163361 AFLR3 GG : Nodes, Elements = 30296 161514 AFLR3 GG : Nodes, Elements = 31866 166228 AFLR3 GG : Nodes, Elements = 31866 172387 AFLR3 GG : Nodes, Elements = 31866 170781 AFLR3 GG : Nodes, Elements = 33375 175320 AFLR3 GG : Nodes, Elements = 33375 181314 AFLR3 GG : Nodes, Elements = 33375 179744 AFLR3 GG : Nodes, Elements = 34769 183931 AFLR3 GG : Nodes, Elements = 34769 189347 AFLR3 GG : Nodes, Elements = 34769 187909 AFLR3 GG : Nodes, Elements = 36030 191695 AFLR3 GG : Nodes, Elements = 36030 196650 AFLR3 GG : Nodes, Elements = 36030 195318 AFLR3 GG : Nodes, Elements = 37219 198889 AFLR3 GG : Nodes, Elements = 37219 203695 AFLR3 GG : Nodes, Elements = 37219 202384 AFLR3 GG : Nodes, Elements = 38304 205641 AFLR3 GG : Nodes, Elements = 38304 209914 AFLR3 GG : Nodes, Elements = 38304 208804 AFLR3 GG : Nodes, Elements = 39314 211837 AFLR3 GG : Nodes, Elements = 39314 215857 AFLR3 GG : Nodes, Elements = 39314 214782 AFLR3 GG : Nodes, Elements = 40241 217566 AFLR3 GG : Nodes, Elements = 40241 221283 AFLR3 GG : Nodes, Elements = 40241 220318 AFLR3 GG : Nodes, Elements = 41069 222807 AFLR3 GG : Nodes, Elements = 41069 226033 AFLR3 GG : Nodes, Elements = 41069 225168 AFLR3 GG : Nodes, Elements = 41793 227340 AFLR3 GG : Nodes, Elements = 41793 230218 AFLR3 GG : Nodes, Elements = 41793 229458 AFLR3 GG : Nodes, Elements = 42448 231424 AFLR3 GG : Nodes, Elements = 42448 234005 AFLR3 GG : Nodes, Elements = 42448 233336 AFLR3 GG : Nodes, Elements = 42994 234974 AFLR3 GG : Nodes, Elements = 42994 237153 AFLR3 GG : Nodes, Elements = 42994 236586 AFLR3 GG : Nodes, Elements = 43475 238031 AFLR3 GG : Nodes, Elements = 43475 239966 AFLR3 GG : Nodes, Elements = 43475 239457 AFLR3 GG : Nodes, Elements = 43877 240663 AFLR3 GG : Nodes, Elements = 43877 242216 AFLR3 GG : Nodes, Elements = 43877 241820 AFLR3 GG : Nodes, Elements = 44206 242807 AFLR3 GG : Nodes, Elements = 44206 244151 AFLR3 GG : Nodes, Elements = 44206 243766 AFLR3 GG : Nodes, Elements = 44456 244517 AFLR3 GG : Nodes, Elements = 44456 245540 AFLR3 GG : Nodes, Elements = 44456 245252 AFLR3 GG : Nodes, Elements = 44659 245862 AFLR3 GG : Nodes, Elements = 44659 246678 AFLR3 GG : Nodes, Elements = 44659 246467 AFLR3 GG : Nodes, Elements = 44797 246882 AFLR3 GG : Nodes, Elements = 44797 247476 AFLR3 GG : Nodes, Elements = 44797 247289 AFLR3 GG : Nodes, Elements = 44898 247592 AFLR3 GG : Nodes, Elements = 44898 248017 AFLR3 GG : Nodes, Elements = 44898 247888 AFLR3 GG : Nodes, Elements = 44958 248068 AFLR3 GG : Nodes, Elements = 44958 248308 AFLR3 GG : Nodes, Elements = 44958 248241 AFLR3 GG : Nodes, Elements = 44987 248328 AFLR3 GG : Nodes, Elements = 44987 248461 AFLR3 GG : Nodes, Elements = 44987 248413 AFLR3 GG : Nodes, Elements = 44995 248437 AFLR3 GG : Nodes, Elements = 44995 248470 AFLR3 GG : Nodes, Elements = 44995 248460 AFLR3 GG : Nodes, Elements = 44998 248469 AFLR3 GG : Nodes, Elements = 44998 248480 AFLR3 GG : Nodes, Elements = 44998 248477 AFLR3 GG : Nodes, Elements = 45028 248567 AFLR3 GG : Nodes, Elements = 45028 248643 AFLR3 GG : Nodes, Elements = 45028 248629 AFLR3 GG : Nodes, Elements = 45030 248635 AFLR3 GG : Nodes, Elements = 45030 248644 AFLR3 GG : Nodes, Elements = 45030 248641 AFLR3 : CPU Time = 2.057 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 45030 248641 AFLR3 QI : Nodes, Elements = 44918 248024 AFLR3 QI : Nodes, Elements = 44911 247987 AFLR3 QI : Nodes, Elements = 44911 249107 AFLR3 QI : Nodes, Elements = 44911 248127 AFLR3 QI : Nodes, Elements = 44911 247755 AFLR3 QI : Nodes, Elements = 44911 247963 AFLR3 QI : Nodes, Elements = 44911 247696 AFLR3 QI : Nodes, Elements = 44911 247659 AFLR3 : CPU Time = 0.405 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 247659 UG3 : Min, Max Ang = 15.43 155.6 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 5.81e+04 UG3 : No. Tet Elems = 247659 UG3 : Min Vol = 2.71e-06 UG3 : Average Vol = 0.235 UG3 : Total-Tet-Vol = 5.81e+04 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 247659 UG3 : Min, Max Q = 0.357 1 UG3 : Average Q = 0.896 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 Adding 659 tet centers Trefftz Frames (6) : 6 7 8 9 10 11 Non-zero time : 0.673391 second(s) Total Degrees of Freedom : 46210 Factorizing matrix... Jacobian time : 1.06363 second(s) Numeric factor time : 0.955391 second(s) Done Solving primal system : MKL_PARDISO solve time : 0.0437321 second(s) Solving Fx adjoint : MKL_PARDISO solve time : 0.0491475 second(s) Solving Fy adjoint : MKL_PARDISO solve time : 0.05192 second(s) Solving Fz adjoint : MKL_PARDISO solve time : 0.0554614 second(s) Solving Mx adjoint : MKL_PARDISO solve time : 0.0562885 second(s) Solving My adjoint : MKL_PARDISO solve time : 0.0485235 second(s) Solving Mz adjoint : MKL_PARDISO solve time : 0.0483184 second(s) ==> Running sansLIP post-analysis... ==> Executing pressure dataTransfer... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = pointConstraint1, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperRiteWing, index = 1 Name = lowerRiteWing, index = 2 Name = upperLeftWing, index = 3 Name = lowerLeftWing, 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 = 3 Name = wingSpar, index = 1 Name = wingSkin, index = 2 Name = wingRib, index = 3 Creating FEA BEM Getting quads for BEM! capsIgnore attribute found for face - 4!! capsIgnore attribute found for face - 9!! capsIgnore attribute found for face - 11!! capsIgnore attribute found for face - 16!! capsIgnore attribute found for face - 18!! capsIgnore attribute found for face - 20!! capsIgnore attribute found for face - 21!! capsIgnore attribute found for face - 28!! capsIgnore attribute found for face - 31!! capsIgnore attribute found for face - 32!! capsIgnore attribute found for face - 33!! capsIgnore attribute found for face - 40!! capsIgnore attribute found for face - 41!! capsIgnore attribute found for face - 43!! capsIgnore attribute found for face - 44!! capsIgnore attribute found for face - 45!! capsIgnore attribute found for face - 53!! capsIgnore attribute found for face - 54!! capsIgnore attribute found for face - 55!! capsIgnore attribute found for face - 56!! capsIgnore attribute found for face - 63!! capsIgnore attribute found for face - 65!! capsIgnore attribute found for face - 66!! capsIgnore attribute found for face - 67!! capsIgnore attribute found for face - 71!! capsIgnore attribute found for face - 72!! capsIgnore attribute found for face - 74!! capsIgnore attribute found for face - 75!! capsIgnore attribute found for face - 76!! capsIgnore attribute found for face - 77!! capsIgnore attribute found for face - 81!! capsIgnore attribute found for face - 82!! capsIgnore attribute found for face - 83!! capsIgnore attribute found for face - 84!! capsIgnore attribute found for face - 85!! capsIgnore attribute found for face - 86!! capsIgnore attribute found for face - 87!! capsIgnore attribute found for face - 88!! Removing unused nodes... Removed 140 (out of 576) unused nodes! Mesh for body = 0 Number of nodal coordinates = 436 Number of elements = 452 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 28 Elemental Quad4 = 424 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 - 3 Property name - wingRib Property name - wingSkin Property name - wingSpar Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - pointConstraint1 No "constraintType" specified for Constraint tuple pointConstraint1, defaulting to "ZeroDisplacement" Done getting 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 fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound upperRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerLeftWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing fea_fillDiscr: WARNING: capsIgnore found on bound lowerRiteWing ==> Running Astros pre-analysis... Extracting external pressure loads from data transfer.... TransferName = upperLeftWing Number of Elements = 80 (total = 80) TransferName = upperRiteWing Number of Elements = 80 (total = 160) TransferName = lowerLeftWing Number of Elements = 80 (total = 240) TransferName = lowerRiteWing Number of Elements = 80 (total = 320) Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards ==> Running Astros... ==> Running Astros post-analysis... ================ run_dataTransfer.py complete ================== dataTransfer results --> Maximum displacements: Tmax : 672.0116412742714 T1max : 18.1473 T2max : 47.161 T3max : 670.891 WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! 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.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! WARNING: 'capsGeometry.buildGeometry' is deprecated. Please use 'Problem.geometry.build'! WARNING: 'capsGeometry.getGeometryOutVal' is deprecated. Please use 'Problem.geometry.outpmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'! WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'! WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'! WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'! WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'! real 4m55.389s user 30m4.698s sys 7m16.934s ++ set +x [GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/training2018/LINUX64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] Obtaining reference build from same job (7.6,CAPS/training2018,LINUX64,reynolds) [Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/training2018,ESP_ARCH=LINUX64,buildnode=reynolds #175' to compute new, fixed, and outstanding issues [Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0 [Static Analysis] Evaluating quality gates [Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1 [Static Analysis] -> All quality gates have been passed [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_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/training2018,ESP_ARCH=LINUX64,buildnode=reynolds #176'. [Checks API] No suitable checks publisher found. [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] done Finished: SUCCESS