Skipping 469 KB..
Full Logcp -p -f corsairlite/multifidelity/csm/naca.csm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/csm/naca.csm
cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/Camber.py
cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py
cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py
cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py
cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/corsairlite/multifidelity/pyCAPS/MSES.py
cp -p -f regressionTest/execute_CTestRegression.sh /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/regressionTest/execute_CTestRegression.sh
cp -p -f regressionTest/execute_PyTestRegression.sh /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/regressionTest/execute_PyTestRegression.sh
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include avlTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/avlTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/avlTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/avlTest.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include awaveTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/awaveTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/awaveTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/awaveTest.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include frictionTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/frictionTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/frictionTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/frictionTest.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include fun3dAFLR2Test.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/fun3dAFLR2Test.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/fun3dAFLR2Test /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/fun3dAFLR2Test.o \
-L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include fun3dTetgenTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/fun3dTetgenTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/fun3dTetgenTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/fun3dTetgenTest.o \
-L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include aeroelasticTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/aeroelasticTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/aeroelasticTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/aeroelasticTest.o \
-L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include hsmTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/hsmTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmTest.o \
-L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include hsmSimplePlateTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmSimplePlateTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/hsmSimplePlateTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmSimplePlateTest.o \
-L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include hsmCantileverPlateTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmCantileverPlateTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/hsmCantileverPlateTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmCantileverPlateTest.o \
-L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include hsmJoinedPlateTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmJoinedPlateTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/hsmJoinedPlateTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/hsmJoinedPlateTest.o \
-L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include interferenceTest.c \
-o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/interferenceTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/interferenceTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/interferenceTest.o \
-L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include msesTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/msesTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/msesTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/msesTest.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include mystranTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/mystranTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/mystranTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/mystranTest.o \
-L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include pointwiseTest.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/pointwiseTest.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/examples/cCAPS/pointwiseTest /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/pointwiseTest.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples/cCAPS'
make[1]: Leaving directory '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/examples'
+++ find /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/ -name Makefile
++ for i in `find $WORKSPACE/CAPS/training/ -name Makefile`
++ [[ /jenkins/workspace/ESP_MemcheckCaps/7.7/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_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2023/data/session01/Makefile
++ cd /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2023/data/session01
++ make
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include template_avl.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/template_avl.o
gcc-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/test/template_avl /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/template_avl.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -legads -lrt -lm -ldl
++ for i in `find $WORKSPACE/CAPS/training/ -name Makefile`
++ [[ /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/data/session01/Makefile
++ cd /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/data/session01
++ make
make: Nothing to be done for 'default'.
++ cd /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/OpenCSM/trunk/src
++ make -f serveESP.make
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include -I. timCapsMode.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timCapsMode.o
touch /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/capsMode.so
rm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/capsMode.so
g++-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/capsMode.so /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timCapsMode.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include -I. timFlowchart.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timFlowchart.o
touch /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/flowchart.so
rm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/flowchart.so
g++-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/flowchart.so /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timFlowchart.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include -I. timViewer.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timViewer.o
touch /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/viewer.so
rm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/viewer.so
g++-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/viewer.so /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timViewer.o -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc-11 -g -fsanitize=address -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=7.7 -I/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/include -I. -I. -I/home/jenkins/util/python/Python-3.11.9_address/install/include/python3.11d -I/home/jenkins/util/python/Python-3.11.9_address/install/include/python3.11d timPyscript.c -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timPyscript.o
touch /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/pyscript.so
rm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/pyscript.so
g++-11 -g -fsanitize=address -fno-omit-frame-pointer -fuse-ld=gold -shared -Wl,-no-undefined -o /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib/pyscript.so /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/obj/timPyscript.o -L/home/jenkins/util/python/Python-3.11.9_address/install/lib -lpython3.11d -ldl -lm -L/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64/lib -lcaps -locsm -lwsserver -legads -ldl -lrt -Wl,-rpath /home/jenkins/util/python/Python-3.11.9_address/install/lib
++ ln -f -s /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/OpenCSM/trunk/udc /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/LINUX64
+++ find /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/OpenCSM/trunk/data/training/ -name Makefile
find: ‘/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/OpenCSM/trunk/data/training/’: No such file or directory
+ [[ reynolds == \m\a\c\y\s ]]
+ [[ reynolds == \v\i\g\g\e\n ]]
+ [[ reynolds == *\r\e\y\n\o\l\d\s* ]]
+ export LD_PRELOAD=/usr/lib/x86_64-linux-gnu/libasan.so.6
+ LD_PRELOAD=/usr/lib/x86_64-linux-gnu/libasan.so.6
+ [[ CAPS/training2018 == *\v\s\p\3* ]]
+ source /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/JenkinsESP/ESP_Sanitize.sh
++ '[' -z '' ']'
++ OUTLEVEL=0
++ mkdir -p /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/test
++ cd /jenkins/workspace/ESP_MemcheckCaps/7.7/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_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/test/training2018
++ cd /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/test/training2018
++ cp /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/runAll.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_astrosModal.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_astrosStatic.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_avl.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_dataTransfer.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_sansLIP.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/template_su2inviscid.py /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/transport.csm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/transport.jrnl /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing1.csm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing1.jrnl /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing2.csm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing2.jrnl /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing3.csm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing3.jrnl /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing4.csm /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/CAPS/training/2018/data/wing4.jrnl .
++ '[' '!' -z ' -L/home/jenkins/util/python/Python-3.11.9_address/install/lib -lpython3.11d -ldl -lm ' ']'
++ echo -----------------------------------------------------
-----------------------------------------------------
+++ which python
++ echo 'using python : /jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64/ESP/venv/bin/python'
using python : /jenkins/workspace/ESP_MemcheckCaps/7.7/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...
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...
Marking Solid Edge 7 : wingWake
Marking Solid Edge 1 : wingWake
Wake intersection... 0.858537 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
==> 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 = 0.008 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 = 0.085 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 = 0.930 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 = 0.243 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 : 1.92161 second(s)
Total Degrees of Freedom : 19945
Factorizing matrix...
Jacobian time : 4.2502 second(s)
Numeric factor time : 0.881863 second(s)
Done
Solving primal system : MKL_PARDISO solve time : 0.00644283 second(s)
Solving Fx adjoint : MKL_PARDISO solve time : 0.00673573 second(s)
Solving Fy adjoint : MKL_PARDISO solve time : 0.00667169 second(s)
Solving Fz adjoint : MKL_PARDISO solve time : 0.00679986 second(s)
Solving Mx adjoint : MKL_PARDISO solve time : 0.00677723 second(s)
Solving My adjoint : MKL_PARDISO solve time : 0.00668704 second(s)
Solving Mz adjoint : MKL_PARDISO solve time : 0.00674344 second(s)
output_Tecplot: filename = wing1.dat
==> Running sansLIP post-analysis...
================ run_sansLIP.py complete ==================
sansLIP results --> Force/moment coefficients:
CXtot : 0.07066315324475138
CYtot : -2.118207976359171e-05
CZtot : -0.9879021287640699
Cltot : -0.0001732348366980139
Cmtot : -0.5526380004325637
Cntot : 0.00010379117974591918
CLtot : 0.9851642034132707
CDtot : 0.10195778320544098
e : 0.5050050708046379
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'!
-----------------------------------------------------
Suppressions used:
count bytes template
2 96 *PyFloat_FromDouble*
3 240 *numpy*
-----------------------------------------------------
real 0m29.589s
user 0m32.755s
sys 0m13.815s
++ 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...
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...
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... 1.6653 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
==> 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 = 0.012 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 = 0.140 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 = 1.412 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 = 0.358 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 : 3.37074 second(s)
Total Degrees of Freedom : 24455
Factorizing matrix...
Jacobian time : 7.68152 second(s)
Numeric factor time : 1.29766 second(s)
Done
Solving primal system : MKL_PARDISO solve time : 0.00729692 second(s)
Solving Fx adjoint : MKL_PARDISO solve time : 0.00792472 second(s)
Solving Fy adjoint : MKL_PARDISO solve time : 0.00808188 second(s)
Solving Fz adjoint : MKL_PARDISO solve time : 0.0134381 second(s)
Solving Mx adjoint : MKL_PARDISO solve time : 0.0120006 second(s)
Solving My adjoint : MKL_PARDISO solve time : 0.00822709 second(s)
Solving Mz adjoint : MKL_PARDISO solve time : 0.00825349 second(s)
output_Tecplot: filename = wing2.dat
==> Running sansLIP post-analysis...
================ run_sansLIP.py complete ==================
sansLIP results --> Force/moment coefficients:
CXtot : 0.06875935422836148
CYtot : -0.0019269859838689947
CZtot : -1.0354565225151278
Cltot : -0.03410384354150172
Cmtot : -0.5925394339126008
Cntot : 0.0017149362141873688
CLtot : 1.0316655478392678
CDtot : 0.11209039305188565
e : 0.5037439640076959
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: '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'!
-----------------------------------------------------
Suppressions used:
count bytes template
2 96 *PyFloat_FromDouble*
3 240 *numpy*
-----------------------------------------------------
real 0m55.569s
user 1m6.368s
sys 0m23.347s
++ 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...
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...
Marking Solid Edge 7 : wingWake
Marking Solid Edge 1 : wingWake
Wake intersection... 0.856597 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
==> 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 = 0.007 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 = 0.066 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 = 0.706 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 = 0.180 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 : 2.61096 second(s)
Total Degrees of Freedom : 19945
Factorizing matrix...
Jacobian time : 5.20621 second(s)
Numeric factor time : 0.911627 second(s)
Done
Solving primal system : MKL_PARDISO solve time : 0.00849503 second(s)
Solving Fx adjoint : MKL_PARDISO solve time : 0.00822509 second(s)
Solving Fy adjoint : MKL_PARDISO solve time : 0.00661644 second(s)
Solving Fz adjoint : MKL_PARDISO solve time : 0.0129262 second(s)
Solving Mx adjoint : MKL_PARDISO solve time : 0.00725622 second(s)
Solving My adjoint : MKL_PARDISO solve time : 0.00721163 second(s)
Solving Mz adjoint : MKL_PARDISO solve time : 0.00699456 second(s)
output_Tecplot: filename = wing3.dat
==> Running sansLIP post-analysis...
================ run_sansLIP.py complete ==================
sansLIP results --> Force/moment coefficients:
CXtot : 0.07066315324475138
CYtot : -2.118207976359171e-05
CZtot : -0.9879021287640699
Cltot : -0.0001732348366980139
Cmtot : -0.5526380004325637
Cntot : 0.00010379117974591918
CLtot : 0.9851642034132707
CDtot : 0.10195778320544098
e : 0.5050050708046379
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:: BAD STATUS = -1 from processFile (called from udpExecute:184)
processFile: could not open file "editAttr_6.txt"
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = 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
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!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 725 (out of 1271) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 546
Number of elements = 564
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 54
Elemental Quad4 = 510
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 : 0.061370476695590356
T1max : 0.00133137
T2max : 0.00481702
T3max : 0.0612608
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:: BAD STATUS = -1 from processFile (called from udpExecute:184)
processFile: could not open file "editAttr_5.txt"
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = 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
capsIgnore attribute found for face - 41!!
capsIgnore attribute found for face - 46!!
capsIgnore attribute found for face - 56!!
capsIgnore attribute found for face - 59!!
capsIgnore attribute found for face - 71!!
capsIgnore attribute found for face - 76!!
capsIgnore attribute found for face - 77!!
capsIgnore attribute found for face - 82!!
capsIgnore attribute found for face - 87!!
capsIgnore attribute found for face - 88!!
capsIgnore attribute found for face - 90!!
capsIgnore attribute found for face - 92!!
capsIgnore attribute found for face - 94!!
capsIgnore attribute found for face - 96!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 725 (out of 1271) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 546
Number of elements = 564
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 54
Elemental Quad4 = 510
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 : 0.0201498
2 : 0.0415608
3 : 0.139456
4 : 0.15929
5 : 0.192769
6 : 0.278402
7 : 0.363917
8 : 0.436326
9 : 0.442441
10: 0.515325
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...
Marking Solid Edge 7 : wingWake
Marking Solid Edge 1 : wingWake
Wake intersection... 0.964608 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:: BAD STATUS = -1 from processFile (called from udpExecute:184)
processFile: could not open file "editAttr_5.txt"
==> 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 = 0.020 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 = 0.213 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 = 2.944 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 = 0.446 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 : 5.71177 second(s)
Total Degrees of Freedom : 42798
Factorizing matrix...
Jacobian time : 10.5295 second(s)
Numeric factor time : 1.37591 second(s)
Done
Solving primal system : MKL_PARDISO solve time : 0.014291 second(s)
Solving Fx adjoint : MKL_PARDISO solve time : 0.0145292 second(s)
Solving Fy adjoint : MKL_PARDISO solve time : 0.0141158 second(s)
Solving Fz adjoint : MKL_PARDISO solve time : 0.0141961 second(s)
Solving Mx adjoint : MKL_PARDISO solve time : 0.0136196 second(s)
Solving My adjoint : MKL_PARDISO solve time : 0.0138028 second(s)
Solving Mz adjoint : MKL_PARDISO solve time : 0.0136026 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
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!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 630 (out of 1230) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 600
Number of elements = 618
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 108
Elemental Quad4 = 510
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 = 100 (total = 100)
Extracting external pressure loads from data transfer....
TransferName = upperRiteWing
Number of Elements = 100 (total = 200)
Extracting external pressure loads from data transfer....
TransferName = lowerLeftWing
Number of Elements = 100 (total = 300)
Extracting external pressure loads from data transfer....
TransferName = lowerRiteWing
Number of Elements = 100 (total = 400)
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 : 413.1012888865428
T1max : 14.3215
T2max : 25.741
T3max : 412.521
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'!
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'!
-----------------------------------------------------
Suppressions used:
count bytes template
2 96 *PyFloat_FromDouble*
3 240 *numpy*
-----------------------------------------------------
real 3m29.849s
user 8m13.672s
sys 4m17.911s
++ 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...
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...
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... 1.06331 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
==> 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 = 0.122 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 = 1.118 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 = 0.269 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 : 2.75702 second(s)
Total Degrees of Freedom : 24455
Factorizing matrix...
Jacobian time : 5.70634 second(s)
Numeric factor time : 1.11641 second(s)
Done
Solving primal system : MKL_PARDISO solve time : 0.00753595 second(s)
Solving Fx adjoint : MKL_PARDISO solve time : 0.0091534 second(s)
Solving Fy adjoint : MKL_PARDISO solve time : 0.00888113 second(s)
Solving Fz adjoint : MKL_PARDISO solve time : 0.0107947 second(s)
Solving Mx adjoint : MKL_PARDISO solve time : 0.00965539 second(s)
Solving My adjoint : MKL_PARDISO solve time : 0.00942886 second(s)
Solving Mz adjoint : MKL_PARDISO solve time : 0.011209 second(s)
output_Tecplot: filename = wing4.dat
==> Running sansLIP post-analysis...
================ run_sansLIP.py complete ==================
sansLIP results --> Force/moment coefficients:
CXtot : 0.06875935422836148
CYtot : -0.0019269859838689947
CZtot : -1.0354565225151278
Cltot : -0.03410384354150172
Cmtot : -0.5925394339126008
Cntot : 0.0017149362141873688
CLtot : 1.0316655478392678
CDtot : 0.11209039305188565
e : 0.5037439640076959
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:: BAD STATUS = -1 from processFile (called from udpExecute:184)
processFile: could not open file "editAttr_6.txt"
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = 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
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!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 725 (out of 1271) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 546
Number of elements = 564
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 54
Elemental Quad4 = 510
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 : 0.061370476695590356
T1max : 0.00133137
T2max : 0.00481702
T3max : 0.0612608
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:: BAD STATUS = -1 from processFile (called from udpExecute:184)
processFile: could not open file "editAttr_5.txt"
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = 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
capsIgnore attribute found for face - 41!!
capsIgnore attribute found for face - 46!!
capsIgnore attribute found for face - 56!!
capsIgnore attribute found for face - 59!!
capsIgnore attribute found for face - 71!!
capsIgnore attribute found for face - 76!!
capsIgnore attribute found for face - 77!!
capsIgnore attribute found for face - 82!!
capsIgnore attribute found for face - 87!!
capsIgnore attribute found for face - 88!!
capsIgnore attribute found for face - 90!!
capsIgnore attribute found for face - 92!!
capsIgnore attribute found for face - 94!!
capsIgnore attribute found for face - 96!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 725 (out of 1271) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 546
Number of elements = 564
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 54
Elemental Quad4 = 510
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 : 0.0201498
2 : 0.0415608
3 : 0.139456
4 : 0.15929
5 : 0.192769
6 : 0.278402
7 : 0.363917
8 : 0.436326
9 : 0.442441
10: 0.515325
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...
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... 1.14928 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:: BAD STATUS = -1 from processFile (called from udpExecute:184)
processFile: could not open file "editAttr_5.txt"
==> 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 = 0.013 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 = 0.172 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 = 2.533 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 = 0.587 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 : 5.30723 second(s)
Total Degrees of Freedom : 46210
Factorizing matrix...
Jacobian time : 8.64298 second(s)
Numeric factor time : 1.41995 second(s)
Done
Solving primal system : MKL_PARDISO solve time : 0.0155733 second(s)
Solving Fx adjoint : MKL_PARDISO solve time : 0.0131418 second(s)
Solving Fy adjoint : MKL_PARDISO solve time : 0.0129199 second(s)
Solving Fz adjoint : MKL_PARDISO solve time : 0.0129859 second(s)
Solving Mx adjoint : MKL_PARDISO solve time : 0.0130983 second(s)
Solving My adjoint : MKL_PARDISO solve time : 0.0129307 second(s)
Solving Mz adjoint : MKL_PARDISO solve time : 0.0128412 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
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!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 630 (out of 1230) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 600
Number of elements = 618
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 108
Elemental Quad4 = 510
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 = 100 (total = 100)
Extracting external pressure loads from data transfer....
TransferName = upperRiteWing
Number of Elements = 100 (total = 200)
Extracting external pressure loads from data transfer....
TransferName = lowerLeftWing
Number of Elements = 100 (total = 300)
Extracting external pressure loads from data transfer....
TransferName = lowerRiteWing
Number of Elements = 100 (total = 400)
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 : 676.2114209132377
T1max : 18.8866
T2max : 47.6188
T3max : 675.077
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'!
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'!
-----------------------------------------------------
Suppressions used:
count bytes template
2 96 *PyFloat_FromDouble*
3 240 *numpy*
-----------------------------------------------------
real 3m39.238s
user 8m45.232s
sys 7m13.072s
++ set +x
[GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_MemcheckCaps/7.7/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_MemcheckCaps/7.7/CAPS/training2018/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_MemcheckCaps/7.7/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] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Parsing console log (workspace: '/jenkins/workspace/ESP_MemcheckCaps/7.7/CAPS/training2018/LINUX64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_MemcheckCaps/CASREV=7.7,ESPTEST=CAPS/training2018,ESP_ARCH=LINUX64,buildnode=reynolds #1424'.
[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