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		-lpthread -lz -lm
(cd test; make -f aim.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include aim.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/aim.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/aim /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/aim.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads \
		-lwsserver -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib
cp -p -f testingAIM.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/testingAIM.csm
(cd test; make -f autoExec.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include autoExec.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/autoExec.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/autoExec /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/autoExec.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm \
		-legads -lwsserver -lpthread -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lz -lm -ldl
(cd test; make -f newPhase.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include newPhase.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/newPhase.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/newPhase /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/newPhase.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib \
		-lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(cd test; make -f basic.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include basic.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/basic.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/basic /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/basic.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads\
		-rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(cd test; make -f geomIn.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include geomIn.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/geomIn.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/geomIn /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/geomIn.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads\
		-rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(cd test; make -f utilsTest.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include aimTransferUtilTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/aimTransferUtilTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/aimTransferUtilTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/aimTransferUtilTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -laimUtil -locsm -legads \
		-lpthread -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -ludunits2 -lm -ldl
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include -I../aim/utils miscUtilsTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/miscUtilsTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/miscUtilsTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/miscUtilsTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -laimUtil -locsm -legads \
		-lpthread -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -ludunits2 -lm -ldl
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include -I../aim/utils vlmUtilsTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/vlmUtilsTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/vlmUtilsTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/vlmUtilsTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lutils -laimUtil -locsm -legads \
		-lpthread -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -ludunits2 -lm -ldl
(cd test; make -f vVS.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include vVS.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/vVS.o
clang++ -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/vVS /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/vVS.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib
(cd examples; make)
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/capsPhase/csm
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/capsPhase/pyCAPS
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Astros.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticModal_Fun3D_and_Astros.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aflr2_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aflr2_PyTest.py
cp -p -f pyCAPS/aflr4_Generic_Missile.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aflr4_Generic_Missile.py
cp -p -f pyCAPS/aflr4_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aflr4_PyTest.py
cp -p -f pyCAPS/aflr4_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aflr4_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_TipTreat_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aflr4_TipTreat_PyTest.py
cp -p -f pyCAPS/aflr4_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aflr4_and_Tetgen_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aflr4_and_aflr3_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/aflr4_tetgen_Regions_PyTest.py
cp -p -f pyCAPS/astros_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_AGARD445_PyTest.py
cp -p -f pyCAPS/astros_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_Aeroelastic_PyTest.py
cp -p -f pyCAPS/astros_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/astros_Composite_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_Composite_PyTest.py
cp -p -f pyCAPS/astros_Flutter_15degree.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_Flutter_15degree.py
cp -p -f pyCAPS/astros_MultipleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_MultipleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_PyTest.py
cp -p -f pyCAPS/astros_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/astros_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_ThreeBar_PyTest.py
cp -p -f pyCAPS/astros_Trim_15degree.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/astros_Trim_15degree.py
cp -p -f pyCAPS/autoLink_Pytest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/autoLink_Pytest.py
cp -p -f pyCAPS/avl_AutoSpan_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/avl_AutoSpan_PyTest.py
cp -p -f pyCAPS/avl_ControlSurf_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/avl_ControlSurf_PyTest.py
cp -p -f pyCAPS/avl_DesignSweep_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/avl_DesignSweep_PyTest.py
cp -p -f pyCAPS/avl_EigenValue_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/avl_EigenValue_PyTest.py
cp -p -f pyCAPS/avl_OpenMDAO_1_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/avl_OpenMDAO_1_PyTest.py
cp -p -f pyCAPS/avl_OpenMDAO_2_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/avl_OpenMDAO_2_PyTest.py
cp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/avl_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/avl_PyTest.py
cp -p -f pyCAPS/awave_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/awave_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py
cp -p -f pyCAPS/cart3d_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/cart3d_PyTest.py
cp -p -f pyCAPS/delaundo_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/delaundo_PyTest.py
cp -p -f pyCAPS/egadsTess_Nose_Quad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/egadsTess_Nose_Quad_PyTest.py
cp -p -f pyCAPS/egadsTess_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/egadsTess_PyTest.py
cp -p -f pyCAPS/egadsTess_Spheres_Quad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py
cp -p -f pyCAPS/friction_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/friction_PyTest.py
cp -p -f pyCAPS/fun3d_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/fun3d_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/fun3d_and_AFLR2_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/fun3d_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/fun3d_and_Delaundo_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/fun3d_and_Tetgen_PyTest.py
cp -p -f pyCAPS/hsm_CantileverPlate_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/hsm_CantileverPlate_PyTest.py
cp -p -f pyCAPS/hsm_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/hsm_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/masstran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/masstran_AGARD445_PyTest.py
cp -p -f pyCAPS/masstran_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/masstran_PyTest.py
cp -p -f pyCAPS/mses_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/mses_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/mses_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/mses_PyTest.py
cp -p -f pyCAPS/mystran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/mystran_AGARD445_PyTest.py
cp -p -f pyCAPS/mystran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/mystran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/mystran_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/mystran_PyTest.py
cp -p -f pyCAPS/mystran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/mystran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_AGARD445_PyTest.py
cp -p -f pyCAPS/nastran_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_Aeroelastic_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingDesign_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_CompositeWingDesign_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/nastran_Composite_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_Composite_PyTest.py
cp -p -f pyCAPS/nastran_Flutter_15degree.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_Flutter_15degree.py
cp -p -f pyCAPS/nastran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_OptimizationMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_OptimizationMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_PyTest.py
cp -p -f pyCAPS/nastran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarDesign_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_ThreeBarDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_ThreeBar_PyTest.py
cp -p -f pyCAPS/nastran_Trim_15degree.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/nastran_Trim_15degree.py
cp -p -f pyCAPS/pointwise_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/pointwise_PyTest.py
cp -p -f pyCAPS/pointwise_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/pointwise_Symmetry_PyTest.py
cp -p -f pyCAPS/quading_Pytest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/quading_Pytest.py
cp -p -f pyCAPS/su2_X43a_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/su2_X43a_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/su2_and_AFLR2_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/su2_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/su2_and_Delaundo_PyTest.py
cp -p -f pyCAPS/su2_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/su2_and_Tetgen_PyTest.py
cp -p -f pyCAPS/su2_and_pointwise_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/su2_and_pointwise_PyTest.py
cp -p -f pyCAPS/tetgen_Holes_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/tetgen_Holes_PyTest.py
cp -p -f pyCAPS/tetgen_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/tetgen_PyTest.py
cp -p -f pyCAPS/tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/tetgen_Regions_PyTest.py
cp -p -f pyCAPS/tsfoil_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/tsfoil_PyTest.py
cp -p -f pyCAPS/xfoil_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/pyCAPS/xfoil_PyTest.py
cp -p -f csmData/15degreeWing.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/15degreeWing.csm
cp -p -f csmData/aeroelasticDataTransfer.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/aeroelasticDataTransfer.csm
cp -p -f csmData/aeroelasticDataTransferSimple.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/aeroelasticDataTransferSimple.csm
cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/airfoilSection.csm
cp -p -f csmData/avlWing.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/avlWing.csm
cp -p -f csmData/avlWingTail.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/avlWingTail.csm
cp -p -f csmData/avlWings.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/avlWings.csm
cp -p -f csmData/awaveWingTailFuselage.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/awaveWingTailFuselage.csm
cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/cfd2D.csm
cp -p -f csmData/cfd2DArbShape.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/cfd2DArbShape.csm
cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/cfdMultiBody.csm
cp -p -f csmData/cfdSymmetry.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/cfdSymmetry.csm
cp -p -f csmData/cfdX43a.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/cfdX43a.csm
cp -p -f csmData/cfd_airfoilSection.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/cfd_airfoilSection.csm
cp -p -f csmData/compositeWing.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/compositeWing.csm
cp -p -f csmData/feaAGARD445.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/feaAGARD445.csm
cp -p -f csmData/feaBoxes.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/feaBoxes.csm
cp -p -f csmData/feaCantileverPlate.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/feaCantileverPlate.csm
cp -p -f csmData/feaJoinedPlate.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/feaJoinedPlate.csm
cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/feaSimplePlate.csm
cp -p -f csmData/feaThreeBar.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/feaThreeBar.csm
cp -p -f csmData/feaWingBEM.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/feaWingBEM.csm
cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/feaWingBEMAero.csm
cp -p -f csmData/frictionWingTailFuselage.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/frictionWingTailFuselage.csm
cp -p -f csmData/generic_missile.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/generic_missile.csm
cp -p -f csmData/interference.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/interference.csm
cp -p -f csmData/linearAero.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/linearAero.csm
cp -p -f csmData/nosecone1.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/nosecone1.csm
cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/regions.csm
cp -p -f csmData/simpleWingBox.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/simpleWingBox.csm
cp -p -f csmData/spheres.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/spheres.csm
cp -p -f csmData/tiptreat.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/tiptreat.csm
cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/csmData/avlWing.udc
cp -p -f corsairlite/boydBox.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/boydBox.py
cp -p -f corsairlite/gp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/gp.py
cp -p -f corsairlite/hoburg_blackbox.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/hoburg_blackbox.py
cp -p -f corsairlite/hoburg_gp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/hoburg_gp.py
cp -p -f corsairlite/hoburg_lsqp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/hoburg_lsqp.py
cp -p -f corsairlite/qp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/qp.py
cp -p -f corsairlite/sp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/sp.py
cp -p -f corsairlite/capsPhase/csm/wing1.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/capsPhase/csm/wing1.csm
cp -p -f corsairlite/capsPhase/csm/wing2.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/capsPhase/csm/wing2.csm
cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py
cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/execute_CTestRegression.sh
cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/execute_PyTestRegression.sh
(make -C cCAPS -f aeroelastic_SU2.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f avlTest.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include avlTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/avlTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/avlTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -legads -locsm \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f awaveTest.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include awaveTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/awaveTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -legads -locsm \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f frictionTest.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include frictionTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/frictionTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f fun3d.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/fun3dAFLR2Test.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/fun3dAFLR2Test.o \
	-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/fun3dTetgenTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/fun3dTetgenTest.o \
	-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/aeroelasticTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/aeroelasticTest.o \
	-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f hsm.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include hsmTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/hsmTest.o   
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/hsmTest.o \
		-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/hsmSimplePlateTest.o  
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/hsmSimplePlateTest.o \
		-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/hsmCantileverPlateTest.o  
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/hsmCantileverPlateTest.o \
		-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/hsmJoinedPlateTest.o  
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/hsmJoinedPlateTest.o \
		-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f interferenceTest.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include interferenceTest.c \
		-o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/interferenceTest.o   
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/interferenceTest.o \
		-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f msesTest.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include msesTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/msesTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/msesTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -legads -locsm \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f mystran.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include mystranTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/mystranTest.o   
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/mystranTest.o \
		-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f pointwiseTest.make)
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/pointwiseTest.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -legads \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
+++ find /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/CAPS/training/ -name Makefile
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/CAPS/training//data/session01/Makefile
++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/CAPS/training//data/session01
++ make
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include template_avl.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/template_avl.o
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/test/template_avl /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/template_avl.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl
++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/OpenCSM/trunk/src
++ make -f serveESP.make
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/timCapsMode.o
touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib/capsMode.so
clang++ -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -undefined error -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib/capsMode.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/timFlowchart.o
touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib/flowchart.so
clang++ -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -undefined error -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib/flowchart.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/timViewer.o
touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib/viewer.so
rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib/viewer.so
clang++ -m64 -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -undefined error -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib/viewer.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/obj/timViewer.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/lib -lcaps -locsm -lwsserver -legads -ldl -lm
++ ln -f -s /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1
+++ find /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/OpenCSM/trunk/data/training/ -name Makefile
find: /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/OpenCSM/trunk/data/training/: No such file or directory
+ source /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/JenkinsESP/ESP_Sanitize.sh
++ mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/test
++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/test
++ [[ CAPS/STRUCTURE =~ [0-9]+.[0-9]+ ]]
++ export ESPTEST=CAPS/STRUCTURE
++ ESPTEST=CAPS/STRUCTURE
++ [[ CAPS/STRUCTURE == \C\A\P\S* ]]
++ export CAPSTARGET=STRUCTURE
++ CAPSTARGET=STRUCTURE
++ [[ STRUCTURE == \u\n\i\t ]]
++ [[ STRUCTURE == \t\r\a\i\n\i\n\g\2\0\1\8 ]]
++ [[ STRUCTURE == \t\r\a\i\n\i\n\g ]]
++ [[ STRUCTURE == *\_\o\f\f ]]
++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest
++ ./execute_CTestRegression.sh STRUCTURE
Running.... STRUCTURE c-Tests

=================================================
+ echo './interferenceTest test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/cCAPSlog.txt
./interferenceTest test;
+ ./interferenceTest
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/cCAPSlog.txt


Note: interferenceTest uses ../csmData/interference.csm
  1:  1.000000e+00  Box
  2:  5.849802e-01  Sphere
  3:  7.191810e-01  Cylinder
  4:  4.000000e+01  OuterBox

  0.000000e+00  -2.741045e-02   2.000000e-02   5.000000e-01 
 -2.741045e-02   0.000000e+00   8.029220e-01  -2.592150e-02 
  2.000000e-02   8.029220e-01   0.000000e+00   2.000000e-02 
  5.000000e-01  -2.592150e-02   2.000000e-02   1.000000e+00 

  1:  1.000000e+00  Box
  2:  5.886884e-01  Sphere
  3:  7.235323e-01  Cylinder

  0.000000e+00  -2.035193e-02   2.000000e-02 
 -2.035193e-02   0.000000e+00   8.028132e-01 
  2.000000e-02   8.028132e-01   0.000000e+00 


real	0m20.574s
user	0m21.071s
sys	0m0.205s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./interferenceTest passed (as expected)
=============================================


=================================================
+ echo './hsmCantileverPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/cCAPSlog.txt
./hsmCantileverPlateTest test;
+ ./hsmCantileverPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/cCAPSlog.txt


Attention: hsmCantileverPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 40
	Number of elements = 51
	Elemental Tria3 = 0
	Elemental Quad4 = 27

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	No "material" specified for Property tuple plate, defaulting to an index of 1
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedLoad
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
 Matrix Non-zero Entries = 1313

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   1*   0.326E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   1*   0.438E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2    0.274E+01  0.521E+01  0.106E-07    0.096  ddx @ (   1.00   0.07   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   2*   0.777E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   3    0.202E+01  0.439E+01  0.928E-07    0.114  ddz @ (   1.00   0.03   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.623E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.163E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.167E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4    0.192E+01  0.476E+01  0.126E-07    0.105  ddz @ (   1.00   0.03   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.451E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.394E+01  0.254E-07    0.127  ddz @ (   1.00   0.07   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.638E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6    0.156E+01  0.300E+01  0.112E-06    0.166  ddx @ (   1.00   0.03   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   6*   0.193E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   6*   0.272E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7    0.103E+01  0.323E+01  0.345E-07    0.155  ddx @ (   1.00   0.07   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.435E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8    0.756E+00  0.259E+01  0.139E-07    0.193  ddx @ (   1.00   0.03   0.00)
   8*   0.295E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.350E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.587E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9    0.678E+00  0.179E+01  0.639E-07    0.279  ddx @ (   0.89   0.10   0.00)
   9*   0.330E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.457E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.167E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   9*   0.264E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10    0.452E+00  0.171E+01  0.499E-07    0.292  ddz @ (   1.00   0.10   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.393E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.257E+00  0.120E+01  0.614E-08    0.417  ddz @ (   1.00   0.10   0.00)
  11*   0.206E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.283E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  11*   0.488E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  12    0.131E+00  0.647E+00  0.288E-08    0.772  ddz @ (   0.89   0.10   0.00)
  12*   0.238E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.357E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.849E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13    0.393E-01  0.238E+00  0.325E-07    1.000  ddx @ (   1.00   0.03   0.00)
  13*   0.335E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  13*   0.936E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
  14    0.475E-03  0.514E-02  0.635E-07    1.000  ddx @ (   1.00   0.00   0.00)
  15    0.893E-06  0.651E-06  0.135E-08    1.000  drx @ (   1.00   0.00   0.00)
  16    0.573E-10  0.216E-09  0.140E-11    1.000  ddx @ (   0.44   0.10   0.00)
  17    0.179E-15  0.693E-15  0.745E-15    1.000  dps @ (   0.78   0.00   0.00)

 Converging n vectors ...
 it =  1    dn =  0.193E+01   rlx = 1.000  (   9 )
 it =  2    dn =  0.516E-15   rlx = 1.000  (  13 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.285E+01   rlx = 0.351  (  24 )
 it =  2    de =  0.251E+01   rlx = 0.398  (  21 )
 it =  3    de =  0.182E+01   rlx = 0.550  (   9 )
 it =  4    de =  0.986E+00   rlx = 1.000  (   9 )
 it =  5    de =  0.165E+00   rlx = 1.000  (   9 )
 it =  6    de =  0.113E-02   rlx = 1.000  (   9 )
 it =  7    de =  0.364E-09   rlx = 1.000  (   9 )
 it =  8    de =  0.938E-16   rlx = 1.000  (  26 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat

real	0m0.472s
user	0m0.274s
sys	0m0.056s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmSimplePlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/cCAPSlog.txt
./hsmSimplePlateTest test;
+ ./hsmSimplePlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/cCAPSlog.txt


Attention: hsmTest2 is hard coded to look for ../csmData/feaSimplePlate.csm
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Number of nodal coordinates = 100
	Number of elements = 198
	Elemental Tria3 = 162
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	No "material" specified for Property tuple plate, defaulting to an index of 1
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedLoad
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 7
MaxDim = 36, numBCEdge = 0, numBCNode = 36, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 36
->HSMSOL
 Matrix Non-zero Entries = 8026

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.609E+00  0.519E+01  0.260E+01    0.096  ddy @ (   0.28   0.25   0.00)
   1*   0.571E-01  0.000E+00  0.000E+00    1.000  drz @ (   0.17   0.11   0.00)
   1*   0.159E-01  0.000E+00  0.000E+00    1.000  drz @ (   0.17   0.11   0.00)
   1*   0.254E-02  0.000E+00  0.000E+00    1.000  drz @ (   0.11   0.14   0.00)
   1*   0.838E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.06   0.14   0.00)
   2    0.768E-02  0.754E+00  0.102E+01    0.492  dps @ (   0.00   0.00   0.00)
   2*   0.336E-03  0.000E+00  0.000E+00    1.000  drx @ (   0.06   0.06   0.00)
   2*   0.690E-06  0.000E+00  0.000E+00    1.000  drz @ (   0.06   0.08   0.00)
   3    0.252E-02  0.204E+00  0.299E+00    1.000  dps @ (   0.50   0.03   0.00)
   3*   0.181E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.39   0.11   0.00)
   3*   0.675E-06  0.000E+00  0.000E+00    1.000  drx @ (   0.44   0.03   0.00)
   4    0.108E-03  0.157E-01  0.567E-01    1.000  dps @ (   0.39   0.14   0.00)
   4*   0.249E-05  0.000E+00  0.000E+00    1.000  drx @ (   0.44   0.22   0.00)
   5    0.103E-05  0.374E-03  0.159E-02    1.000  dps @ (   0.06   0.06   0.00)
   6    0.139E-08  0.994E-07  0.421E-06    1.000  dps @ (   0.50   0.00   0.00)
   7    0.106E-15  0.467E-13  0.133E-12    1.000  dps @ (   0.50   0.00   0.00)

 Converging n vectors ...
 it =  1    dn =  0.117E+01   rlx = 1.000  (  66 )
 it =  2    dn =  0.327E-15   rlx = 1.000  (  81 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.357E+00   rlx = 1.000  (  94 )
 it =  2    de =  0.167E+00   rlx = 1.000  (  67 )
 it =  3    de =  0.245E-01   rlx = 1.000  (  76 )
 it =  4    de =  0.567E-02   rlx = 1.000  (  59 )
 it =  5    de =  0.192E-02   rlx = 1.000  (  59 )
 it =  6    de =  0.648E-03   rlx = 1.000  (  59 )
 it =  7    de =  0.219E-03   rlx = 1.000  (  59 )
 it =  8    de =  0.740E-04   rlx = 1.000  (  59 )
 it =  9    de =  0.250E-04   rlx = 1.000  (  59 )
 it = 10    de =  0.845E-05   rlx = 1.000  (  59 )
 it = 11    de =  0.286E-05   rlx = 1.000  (  59 )
 it = 12    de =  0.965E-06   rlx = 1.000  (  59 )
 it = 13    de =  0.326E-06   rlx = 1.000  (  59 )
 it = 14    de =  0.110E-06   rlx = 1.000  (  59 )
 it = 15    de =  0.372E-07   rlx = 1.000  (  59 )
 it = 16    de =  0.126E-07   rlx = 1.000  (  59 )
 it = 17    de =  0.425E-08   rlx = 1.000  (  59 )
 it = 18    de =  0.144E-08   rlx = 1.000  (  59 )
 it = 19    de =  0.485E-09   rlx = 1.000  (  59 )
 it = 20    de =  0.164E-09   rlx = 1.000  (  59 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat

real	0m0.744s
user	0m0.561s
sys	0m0.045s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmJoinedPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/cCAPSlog.txt
./hsmJoinedPlateTest test;
+ ./hsmJoinedPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/cCAPSlog.txt


Attention: hsmJoinedPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 40
	Number of elements = 56
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	No "material" specified for Property tuple plate, defaulting to an index of 1
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedLoad
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 16
MaxDim = 13, numBCEdge = 2, numBCNode = 4, numJoint = 13
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
 Matrix Non-zero Entries = 1242

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   1*   0.325E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.05   0.00)
   1*   0.434E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2    0.274E+01  0.521E+01  0.118E-07    0.096  ddx @ (   1.00   0.05   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   2*   0.772E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3    0.202E+01  0.439E+01  0.107E-06    0.114  ddz @ (   1.00   0.05   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3*   0.622E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3*   0.162E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3*   0.163E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4    0.192E+01  0.476E+01  0.147E-07    0.105  ddz @ (   1.00   0.05   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.448E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.395E+01  0.296E-07    0.127  ddz @ (   1.00   0.05   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5*   0.636E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   6    0.156E+01  0.301E+01  0.131E-06    0.166  ddx @ (   1.00   0.05   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.191E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.265E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7    0.103E+01  0.323E+01  0.408E-07    0.155  ddx @ (   1.00   0.05   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.432E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8    0.757E+00  0.260E+01  0.162E-07    0.192  ddx @ (   1.00   0.05   0.00)
   8*   0.296E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.351E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.586E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9    0.680E+00  0.181E+01  0.753E-07    0.276  ddx @ (   0.88   0.00   0.00)
   9*   0.329E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.452E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9*   0.159E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   9*   0.238E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10    0.457E+00  0.172E+01  0.586E-07    0.290  ddz @ (   1.00   0.10   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.392E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.258E+00  0.122E+01  0.666E-08    0.411  ddz @ (   1.00   0.10   0.00)
  11*   0.207E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.284E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.486E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12    0.135E+00  0.660E+00  0.377E-08    0.758  ddz @ (   0.88   0.00   0.00)
  12*   0.242E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.368E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.869E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13    0.430E-01  0.257E+00  0.505E-07    1.000  ddx @ (   1.00   0.05   0.00)
  13*   0.395E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  13*   0.128E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13*   0.196E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
  14    0.656E-03  0.680E-02  0.885E-07    1.000  ddx @ (   1.00   0.00   0.00)
  15    0.156E-05  0.177E-05  0.268E-10    1.000  ddx @ (   1.00   0.10   0.00)
  16    0.273E-09  0.106E-08  0.893E-11    1.000  ddx @ (   0.50   0.05   0.00)
  17    0.138E-15  0.353E-15  0.907E-15    1.000  dps @ (   0.38   0.10   0.00)

 Converging n vectors ...
 it =  1    dn =  0.197E+01   rlx = 1.000  (  17 )
 it =  2    dn =  0.866E-15   rlx = 1.000  (  18 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.753E+01   rlx = 0.133  (   1 )
 it =  2    de =  0.309E+01   rlx = 0.324  (  20 )
 it =  3    de =  0.324E+01   rlx = 0.309  (   2 )
 it =  4    de =  0.226E+01   rlx = 0.443  (   2 )
 it =  5    de =  0.140E+01   rlx = 0.716  (   2 )
 it =  6    de =  0.660E+00   rlx = 1.000  (   2 )
 it =  7    de =  0.860E-01   rlx = 1.000  (   2 )
 it =  8    de =  0.228E-03   rlx = 1.000  (   2 )
 it =  9    de =  0.428E-11   rlx = 1.000  (   2 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat

real	0m0.392s
user	0m0.221s
sys	0m0.049s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmJoinedPlateTest passed (as expected)
=============================================

=================================================
Did not run examples for:

Mystran
=================================================

All tests pass!


=================================================
=================================================
++ '[' '!' -z '-L/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/lib -lpython3.9 -ldl -framework CoreFoundation' ']'
++ ./execute_PyTestRegression.sh STRUCTURE

=================================================
Using python : /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP_venv/bin/python
=================================================

Running.... STRUCTURE PyTests


=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
+ python -u masstran_PyTest.py -outLevel=0

Getting results mass properties.....

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 1159
Number of elements = 798
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes    = 1159
Total number of elements = 798
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1159
	Number of elements = 798
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 798

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input
Area      3.428666259747
Mass      5383.006027803
Centroid  [1.222256036875, 0.1634981473778, -4.186947998839e-11]
CG        [1.222256036875, 0.1634981473778, -4.187019989324e-11]
Ixx       22133.97306034
Iyy       23448.30046709
Izz       1389.213122581
Ixy       164.2055275656
Ixz       -7.453281823829e-06
Iyz       1.707508261061e-06
I         [22133.97306034, 23448.30046709, 1389.213122581, 164.2055275656, -7.453281823829e-06, 1.707508261061e-06]
II        [[22133.97306034, -164.2055275656, 7.453281823829e-06], [-164.2055275656, 23448.30046709, -1.707508261061e-06], [7.453281823829e-06, -1.707508261061e-06, 1389.213122581]]

real	0m5.749s
user	0m8.473s
sys	0m1.890s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'masstran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
masstran_AGARD445_PyTest.py test;
+ python -u masstran_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 36
	Number of elements = 25
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 25

Getting FEA materials.......
	Number of materials - 1
	Material name - Mahogany
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - yatesPlate
	Done getting FEA properties
Updating mesh element types based on properties input
Area      547.7004
Mass      0.01605224431138
Centroid  [20.03586282449, 14.01686746988, 0.0]
CG        [20.03586282449, 14.01686746988, 0.0]
Ixx       1.140246300554
Iyy       0.919317482675
Izz       2.059563783229
Ixy       0.7352134614013
Ixz       0.0
Iyz       0.0
I         [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0]
II        [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]]

real	0m0.258s
user	0m0.308s
sys	0m0.078s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 81
	Number of elements = 96
	Elemental Tria3 = 0
	Elemental Quad4 = 64

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
 Matrix Non-zero Entries = 5741

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.130E-01  0.165E+00  0.153E-04    1.000  ddy @ (   0.25   0.06   0.00)
   1*   0.260E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   1*   0.240E-05  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.09   0.00)
   2    0.379E-02  0.505E-01  0.750E-04    1.000  ddy @ (   0.25   0.19   0.00)
   2*   0.420E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   3    0.168E-02  0.225E-01  0.208E-04    1.000  ddy @ (   0.25   0.06   0.00)
   4    0.325E-03  0.427E-02  0.250E-05    1.000  ddy @ (   0.25   0.19   0.00)
   5    0.794E-05  0.112E-03  0.170E-06    1.000  ddy @ (   0.25   0.19   0.00)
   6    0.387E-08  0.598E-07  0.197E-09    1.000  ddy @ (   0.25   0.06   0.00)
   7    0.848E-15  0.147E-13  0.924E-15    1.000  ddy @ (   0.25   0.19   0.00)

 Converging n vectors ...
 it =  1    dn =  0.788E-01   rlx = 1.000  (  59 )
 it =  2    dn =  0.566E-16   rlx = 1.000  (  35 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.691E-03   rlx = 1.000  (  45 )
 it =  2    de =  0.404E-04   rlx = 1.000  (   9 )
 it =  3    de =  0.142E-07   rlx = 1.000  (  46 )
 it =  4    de =  0.521E-11   rlx = 1.000  (  62 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat

real	0m0.613s
user	0m0.714s
sys	0m0.079s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_CantileverPlate_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 40
	Number of elements = 51
	Elemental Tria3 = 0
	Elemental Quad4 = 27

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedLoad
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
 Matrix Non-zero Entries = 1313

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   1*   0.326E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.03   0.00)
   1*   0.438E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2    0.274E+01  0.521E+01  0.106E-07    0.096  ddx @ (   1.00   0.03   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   2*   0.777E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3    0.202E+01  0.439E+01  0.928E-07    0.114  ddz @ (   1.00   0.03   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.623E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.163E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.167E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4    0.192E+01  0.476E+01  0.126E-07    0.105  ddz @ (   1.00   0.03   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.451E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.394E+01  0.254E-07    0.127  ddz @ (   1.00   0.07   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.638E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6    0.156E+01  0.300E+01  0.112E-06    0.166  ddx @ (   1.00   0.03   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   6*   0.193E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.272E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7    0.103E+01  0.323E+01  0.345E-07    0.155  ddx @ (   1.00   0.03   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.435E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8    0.756E+00  0.259E+01  0.139E-07    0.193  ddx @ (   1.00   0.07   0.00)
   8*   0.295E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   8*   0.350E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   8*   0.587E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9    0.678E+00  0.179E+01  0.639E-07    0.279  ddx @ (   0.89   0.10   0.00)
   9*   0.330E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.457E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.167E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   9*   0.264E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10    0.452E+00  0.171E+01  0.499E-07    0.292  ddz @ (   1.00   0.00   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.393E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.257E+00  0.120E+01  0.614E-08    0.417  ddz @ (   1.00   0.10   0.00)
  11*   0.206E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.283E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.488E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12    0.131E+00  0.647E+00  0.288E-08    0.772  ddz @ (   0.89   0.10   0.00)
  12*   0.238E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.357E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.849E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13    0.393E-01  0.238E+00  0.325E-07    1.000  ddx @ (   1.00   0.03   0.00)
  13*   0.336E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  13*   0.936E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  14    0.475E-03  0.514E-02  0.635E-07    1.000  ddx @ (   1.00   0.00   0.00)
  15    0.893E-06  0.651E-06  0.135E-08    1.000  drx @ (   1.00   0.10   0.00)
  16    0.574E-10  0.216E-09  0.140E-11    1.000  ddx @ (   0.44   0.10   0.00)
  17    0.558E-15  0.304E-14  0.603E-15    1.000  ddx @ (   1.00   0.00   0.00)

 Converging n vectors ...
 it =  1    dn =  0.193E+01   rlx = 1.000  (  12 )
 it =  2    dn =  0.435E-15   rlx = 1.000  (  28 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.285E+01   rlx = 0.351  (  24 )
 it =  2    de =  0.292E+01   rlx = 0.342  (  34 )
 it =  3    de =  0.226E+01   rlx = 0.442  (  34 )
 it =  4    de =  0.151E+01   rlx = 0.660  (  34 )
 it =  5    de =  0.665E+00   rlx = 1.000  (  34 )
 it =  6    de =  0.609E-01   rlx = 1.000  (  34 )
 it =  7    de =  0.573E-04   rlx = 1.000  (  34 )
 it =  8    de =  0.479E-13   rlx = 1.000  (  34 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMCantileverPlate.dat

real	0m0.576s
user	0m0.611s
sys	0m0.089s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected)
=================================================

ASTROS_ROOT: /Users/jenkins/util/astros/Astros/Darwin-64bit

=================================================
+ echo 'astros_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Wing, index = 6
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 246
	Number of elements = 329
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 74
	Elemental Quad4 = 255
Creating FEA BEM
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 247
	Combined Number of elements = 330
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 74
	Combined Elemental Quad4 = 255
Getting vortex lattice surface data
	VLM surface name - Skin_Top
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 48
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - Rib_Root
	No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
	Property name - Ribs
	No "material" specified for Property tuple Ribs, defaulting to an index of 1
	Property name - Skin
	No "material" specified for Property tuple Skin, defaulting to an index of 1
	Property name - Spar1
	No "material" specified for Property tuple Spar1, defaulting to an index of 1
	Property name - Spar2
	No "material" specified for Property tuple Spar2, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - ribSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Rib_Root
	No "groupName" specified for Connection tuple Rib_Root!
	Looking for automatic connections from the use of capsConnectLink for Rib_Root
	22 automatic connections were made for capsConnect Rib_Root (node id 247)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim1
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aeros card
	Writing analysis cards
	Writing constraint cards--each subcase individually
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m14.121s
user	0m28.702s
sys	0m2.109s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_AGARD445_PyTest.py test;
+ python -u astros_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt

Getting results natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 36
	Number of elements = 25
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 25

Getting FEA materials.......
	Number of materials - 1
	Material name - Mahogany
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - yatesPlate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 2
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
Natural freq (Mode 1) = 5.78 (Hz)
Natural freq (Mode 2) = 30.66 (Hz)

real	0m0.502s
user	0m0.605s
sys	0m0.153s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_Composite_PyTest.py test;
+ python -u astros_Composite_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 100
	Number of elements = 81
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 81

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - cantilever
	No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards

real	0m0.903s
user	0m0.978s
sys	0m0.175s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Composite_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = wing, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - wing
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = wing, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = wing, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Creating FEA BEM
	Mesh for body = 0
	Number of nodal coordinates = 320
	Number of elements = 606
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 606
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - Aluminum
	No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
	Material name - Graphite_epoxy
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - root
	No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
Natural freq (Mode 1) = 5.41785 (Hz)
Natural freq (Mode 2) = 27.74730 (Hz)
Natural freq (Mode 3) = 34.69110 (Hz)
Natural freq (Mode 4) = 72.93980 (Hz)
Natural freq (Mode 5) = 88.09620 (Hz)
Natural freq (Mode 6) = 137.40100 (Hz)
Natural freq (Mode 7) = 159.33600 (Hz)
Natural freq (Mode 8) = 216.04800 (Hz)
Natural freq (Mode 9) = 249.48200 (Hz)
Natural freq (Mode 10) = 267.01400 (Hz)
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 320 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 320 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 320 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 320 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 320 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10

real	0m22.014s
user	0m12.582s
sys	0m0.431s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_CompositeWingFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 80
	Number of elements = 63
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 63
Creating FEA BEM
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 81
	Combined Number of elements = 64
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 63
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 80

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Body
	Property name - Edge
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	8 automatic connections were made for capsConnect Root (node id 81)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Flutter
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aero card
	Writing analysis cards
	Writing constraint cards--each subcase individually
	Writing material cards
	Writing property cards
	Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.881s
user	0m0.884s
sys	0m0.246s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'astros_MultipleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 16
	Number of elements = 9
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 9

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 5
	Load name - load_0
	Load name - load_1
	Load name - load_2
	Load name - load_3
	Load name - load_4
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 5
	Analysis name - load_0
	Analysis name - load_1
	Analysis name - load_2
	Analysis name - load_3
	Analysis name - load_4
	Done getting FEA analyses

Writing Astros grid and connectivity file (in 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 load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.735s
user	0m0.824s
sys	0m0.145s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_MultipleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 293
Number of elements = 217
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes    = 293
Total number of elements = 217
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 293
	Number of elements = 217
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 217

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02335 (Hz)
Natural freq (Mode 2) = 0.02335 (Hz)
Natural freq (Mode 3) = 0.11619 (Hz)
Natural freq (Mode 4) = 0.11619 (Hz)
Natural freq (Mode 5) = 0.14468 (Hz)
Natural freq (Mode 6) = 0.14468 (Hz)
Natural freq (Mode 7) = 0.23352 (Hz)
Natural freq (Mode 8) = 0.23352 (Hz)
Natural freq (Mode 9) = 0.30497 (Hz)
Natural freq (Mode 10) = 0.30497 (Hz)

real	0m14.940s
user	0m15.843s
sys	0m2.059s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 6
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 6

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.656s
user	0m0.717s
sys	0m0.143s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ python -u astros_ThreeBarFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Creating FEA BEM
	capsIgnore attribute found for edge - 3!!
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 2
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
Natural freq (Mode 1) = 86.13400 (Hz)
Natural freq (Mode 2) = 168.53300 (Hz)

real	0m0.669s
user	0m0.686s
sys	0m0.141s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarLinkDesign_PyTest.py test;
+ python -u astros_ThreeBarLinkDesign_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Creating FEA BEM
	capsIgnore attribute found for edge - 3!!
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - Bar1A
	Design_Variable name - Bar2A
	Design_Variable name - Bar3A
	Design_Variable_Relation name - Bar1A
	Design_Variable_Relation name - Bar2A
	Design_Variable_Relation name - Bar3A
	Number of design variable relations - 3
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 3
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing Nastran instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
	Writing design constraints and responses cards


Running Astros......
Done running Astros!

real	0m0.517s
user	0m0.445s
sys	0m0.111s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarLinkDesign_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ python -u astros_ThreeBarMultiLoad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Creating FEA BEM
	capsIgnore attribute found for edge - 3!!
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 2
	Constraint name - conOne
	No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
	Constraint name - conTwo
	No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - loadOne
	Load name - loadTwo
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 2
	Analysis name - analysisOne
	Analysis name - analysisTwo
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m0.895s
user	0m0.688s
sys	0m0.148s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Creating FEA BEM
	capsIgnore attribute found for edge - 3!!
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m0.573s
user	0m0.696s
sys	0m0.135s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ python -u astros_Trim_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1/ESP/DARWINM1/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 80
	Number of elements = 63
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 63
Creating FEA BEM
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 81
	Combined Number of elements = 64
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 63
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 80
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - Body
	Property name - Edge
	Property name - Root
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - PointSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	8 automatic connections were made for capsConnect Root (node id 81)
	Done getting FEA connections

Getting FEA loads.......
	Number of loads - 2
	Load name - GravityLoad
	No "groupName" specified for Load tuple GravityLoad, going to use load name
	Load name - PointLoad
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aeros card
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m1.016s
user	0m0.784s
sys	0m0.195s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================


*************************************************
*************************************************

=================================================
Did not run examples for:

Nastran
Mystran
=================================================

All tests pass!


=================================================
=================================================
[GNU C Compiler (gcc)] Sleeping for 5 seconds due to JENKINS-32191...
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1')
[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] Sleeping for 5 seconds due to JENKINS-32191...
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWINM1')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.6,CAPS/STRUCTURE,DARWINM1,viggen)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWINM1,buildnode=viggen #161' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWINM1,buildnode=viggen #162'.
[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