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Full Logcp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py cp -p -f pyCAPS/avl_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_PyTest.py cp -p -f pyCAPS/awave_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/awave_PyTest.py cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py cp -p -f pyCAPS/cart3d_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_PyTest.py cp -p -f pyCAPS/delaundo_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/delaundo_PyTest.py cp -p -f pyCAPS/egadsTess_Nose_Quad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Nose_Quad_PyTest.py cp -p -f pyCAPS/egadsTess_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_PyTest.py cp -p -f pyCAPS/egadsTess_Spheres_Quad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py cp -p -f pyCAPS/friction_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/friction_PyTest.py cp -p -f 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/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/compositeWing.csm cp -p -f csmData/cyli_box_shell.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cyli_box_shell.csm cp -p -f csmData/cyli_box_solid.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cyli_box_solid.csm cp -p -f csmData/feaAGARD445.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaAGARD445.csm cp -p -f csmData/feaBoxes.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaBoxes.csm cp -p -f csmData/feaCantileverPlate.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaCantileverPlate.csm cp -p -f csmData/feaJoinedPlate.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaJoinedPlate.csm cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaSimplePlate.csm cp -p -f csmData/feaThreeBar.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaThreeBar.csm cp -p -f csmData/feaWingBEM.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaWingBEM.csm cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaWingBEMAero.csm cp -p -f csmData/frictionWingTailFuselage.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/frictionWingTailFuselage.csm cp -p -f csmData/generic_missile.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/generic_missile.csm cp -p -f csmData/interference.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/interference.csm cp -p -f csmData/linearAero.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/linearAero.csm cp -p -f csmData/nosecone1.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/nosecone1.csm cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/regions.csm cp -p -f csmData/simpleWingBox.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/simpleWingBox.csm cp -p -f csmData/spheres.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/spheres.csm cp -p -f csmData/table.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/table.csm cp -p -f csmData/tiptreat.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/tiptreat.csm cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWing.udc mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS cp -p -f corsairlite/boydBox.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/boydBox.py cp -p -f corsairlite/gp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/gp.py cp -p -f corsairlite/hoburg_blackbox.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_blackbox.py cp -p -f corsairlite/hoburg_gp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_gp.py cp -p -f corsairlite/qp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/qp.py cp -p -f corsairlite/sp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/sp.py cp -p -f corsairlite/capsPhase/csm/wing1.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing1.csm cp -p -f corsairlite/capsPhase/csm/wing2.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing2.csm cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py cp -p -f corsairlite/multifidelity/csm/naca.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm/naca.csm cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Camber.py cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/MSES.py cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_CTestRegression.sh cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_PyTestRegression.sh (make -C cCAPS -f aeroelastic_SU2.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl (make -C cCAPS -f avlTest.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include avlTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl (make -C cCAPS -f awaveTest.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include awaveTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl (make -C cCAPS -f frictionTest.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include frictionTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl (make -C cCAPS -f fun3d.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o \ -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o \ -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o \ -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl (make -C cCAPS -f hsm.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o \ -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o \ -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o \ -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o \ -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl (make -C cCAPS -f interferenceTest.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include interferenceTest.c \ -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o \ -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl (make -C cCAPS -f msesTest.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include msesTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl (make -C cCAPS -f mystran.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include mystranTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o \ -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl (make -C cCAPS -f pointwiseTest.make) clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -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/DARWIN_ARM64/CAPS/training/ -name Makefile ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//2023/lectures/Makefile == *\l\e\c\t\u\r\e\s* ]] ++ continue ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//2023/data/session01 ++ make clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include template_avl.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/test/template_avl /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -lm -ldl ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//data/session01 ++ make make: Nothing to be done for `default'. ++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/OpenCSM/trunk/src ++ make -f serveESP.make clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so clang++ -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so clang++ -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so clang++ -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -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/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 timPyscript.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so clang++ -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.6/trunk/build_undefined/install/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib ++ ln -f -s /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64 +++ find /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/OpenCSM/trunk/data/training/ -name Makefile find: /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/OpenCSM/trunk/data/training/: No such file or directory + source /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/JenkinsESP/ESP_Sanitize.sh ++ '[' -z '' ']' ++ OUTLEVEL=0 ++ mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/test ++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest ++ ./execute_CTestRegression.sh STRUCTURE Running.... STRUCTURE c-Tests ================================================= + echo './interferenceTest test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt ./interferenceTest test; + ./interferenceTest + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt Note: interferenceTest uses ../csmData/interference.csm classifyClouds: EG_generalBoolean = -7! classifyClouds: EG_generalBoolean = -7! classifyClouds: EG_generalBoolean = -7! classifyClouds: EG_generalBoolean = -7! 1: 1.000000e+00 Box 2: 5.850521e-01 Sphere 3: 7.191810e-01 Cylinder 4: 4.000000e+01 OuterBox 0.000000e+00 -2.715465e-02 0.000000e+00 0.000000e+00 -2.715465e-02 0.000000e+00 0.000000e+00 -2.543571e-02 0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00 -2.543571e-02 0.000000e+00 1.000000e+00 classifyClouds: EG_generalBoolean = -7! classifyClouds: EG_generalBoolean = -7! 1: 1.000000e+00 Box 2: 5.886885e-01 Sphere 3: 7.235323e-01 Cylinder 0.000000e+00 -2.059198e-02 0.000000e+00 -2.059198e-02 0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00 real 0m15.238s user 0m9.935s sys 0m0.118s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt ./hsmCantileverPlateTest test; + ./hsmCantileverPlateTest 0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0.10 0.00) 1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.07 0.00) 1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.07 0.00) 2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.07 0.00) 3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00) 4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00) 5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.07 0.00) 6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.03 0.00) 7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00) 8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.00 0.00) 9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.10 0.00) 10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) iter dr dd dp rlx max 11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.00 0.00) 11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00) 12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00) 13* 0.335E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00) 15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00) 16 0.573E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00) 17 0.253E-15 0.930E-15 0.713E-15 1.000 ddx @ ( 0.56 0.10 0.00) Converging n vectors ... it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 ) it = 2 dn = 0.583E-15 rlx = 1.000 ( 31 ) Converging e1,e2 vectors ... it = 1 de = 0.285E+01 rlx = 0.351 ( 24 ) it = 2 de = 0.269E+01 rlx = 0.372 ( 14 ) it = 3 de = 0.202E+01 rlx = 0.494 ( 14 ) it = 4 de = 0.122E+01 rlx = 0.820 ( 14 ) it = 5 de = 0.378E+00 rlx = 1.000 ( 14 ) it = 6 de = 0.127E-01 rlx = 1.000 ( 40 ) it = 7 de = 0.524E-06 rlx = 1.000 ( 40 ) it = 8 de = 0.128E-15 rlx = 1.000 ( 22 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - hsm_CAPS.dat real 0m0.376s user 0m0.195s sys 0m0.036s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt ./hsmSimplePlateTest test; + ./hsmSimplePlateTest 0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0.240E+01 0.096 ddy @ ( 0.28 0.25 0.00) 1* 0.571E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00) 1* 0.159E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00) 1* 0.254E-02 0.000E+00 0.000E+00 1.000 drz @ ( 0.11 0.14 0.00) 1* 0.837E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.14 0.00) 2 0.769E-02 0.753E+00 0.105E+01 0.478 dps @ ( 0.00 0.00 0.00) 2* 0.329E-03 0.000E+00 0.000E+00 1.000 drx @ ( 0.06 0.06 0.00) 2* 0.641E-06 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.08 0.00) 3 0.264E-02 0.213E+00 0.280E+00 1.000 dps @ ( 0.50 0.00 0.00) 3* 0.194E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.39 0.11 0.00) 3* 0.741E-06 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.03 0.00) 4 0.119E-03 0.159E-01 0.631E-01 1.000 dps @ ( 0.39 0.14 0.00) 4* 0.306E-05 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.22 0.00) 5 0.133E-05 0.441E-03 0.208E-02 1.000 dps @ ( 0.06 0.06 0.00) 6 0.233E-08 0.153E-06 0.694E-06 1.000 dps @ ( 0.50 0.00 0.00) 7 0.378E-15 0.119E-12 0.317E-12 1.000 dps @ ( 0.50 0.00 0.00) Converging n vectors ... it = 1 dn = 0.117E+01 rlx = 1.000 ( 66 ) it = 2 dn = 0.236E-15 rlx = 1.000 ( 81 ) Converging e1,e2 vectors ... it = 1 de = 0.357E+00 rlx = 1.000 ( 94 ) it = 2 de = 0.167E+00 rlx = 1.000 ( 67 ) it = 3 de = 0.245E-01 rlx = 1.000 ( 76 ) it = 4 de = 0.567E-02 rlx = 1.000 ( 59 ) it = 5 de = 0.192E-02 rlx = 1.000 ( 59 ) it = 6 de = 0.648E-03 rlx = 1.000 ( 59 ) it = 7 de = 0.219E-03 rlx = 1.000 ( 59 ) it = 8 de = 0.740E-04 rlx = 1.000 ( 59 ) it = 9 de = 0.250E-04 rlx = 1.000 ( 59 ) it = 10 de = 0.845E-05 rlx = 1.000 ( 59 ) it = 11 de = 0.286E-05 rlx = 1.000 ( 59 ) it = 12 de = 0.965E-06 rlx = 1.000 ( 59 ) it = 13 de = 0.326E-06 rlx = 1.000 ( 59 ) it = 14 de = 0.110E-06 rlx = 1.000 ( 59 ) it = 15 de = 0.372E-07 rlx = 1.000 ( 59 ) it = 16 de = 0.126E-07 rlx = 1.000 ( 59 ) it = 17 de = 0.425E-08 rlx = 1.000 ( 59 ) it = 18 de = 0.144E-08 rlx = 1.000 ( 59 ) it = 19 de = 0.485E-09 rlx = 1.000 ( 59 ) it = 20 de = 0.164E-09 rlx = 1.000 ( 59 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - hsm_CAPS.dat real 0m0.899s user 0m0.489s sys 0m0.046s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt ./hsmJoinedPlateTest test; + ./hsmJoinedPlateTest 0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0m0.385s user 0m0.203s sys 0m0.046s + 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-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ']' ++ ./execute_PyTestRegression.sh STRUCTURE ================================================= Using python : /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/venv/bin/python ================================================= Running.... STRUCTURE PyTests ================================================= + echo 'masstran_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Getting results mass properties..... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 1159 Number of elements = 798 Number of 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 3.428666259746 Mass 5383.006027801 Centroid [1.222256036872, 0.1634981473779, -4.406138983522e-11] CG [1.222256036872, 0.1634981473779, -4.406190366478e-11] Ixx 22133.97306028 Iyy 23448.30046701 Izz 1389.213122561 Ixy 164.2055275652 Ixz -7.483319968982e-06 Iyz 1.710429101792e-06 I [22133.97306028, 23448.30046701, 1389.213122561, 164.2055275652, -7.483319968982e-06, 1.710429101792e-06] II [[22133.97306028, -164.2055275652, 7.483319968982e-06], [-164.2055275652, 23448.30046701, -1.710429101792e-06], [7.483319968982e-06, -1.710429101792e-06, 1389.213122561]] real 0m8.735s user 0m12.836s sys 0m3.563s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = yatesPlate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 36 Number of elements = 25 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 25 Getting FEA materials....... Number of materials - 1 Material name - Mahogany Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - yatesPlate Done getting FEA properties Updating mesh element types based on properties input Area 547.7004 Mass 0.01605224431138 Centroid [20.03586282449, 14.01686746988, 0.0] CG [20.03586282449, 14.01686746988, 0.0] Ixx 1.140246300554 Iyy 0.919317482675 Izz 2.059563783229 Ixy 0.7352134614013 Ixz 0.0 Iyz 0.0 I [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0] II [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]] real 0m0.582s user 0m0.420s sys 0m0.109s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0m1.126s user 0m0.721s sys 0m0.086s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0.10 0.00) 1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.03 0.00) 2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00) 3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00) 4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00) 5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.07 0.00) 6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.07 0.00) 7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00) 8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.00 0.00) 9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.10 0.00) 10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) iter dr dd dp rlx max 11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.00 0.00) 11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.00 0.00) 12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.07 0.00) 13* 0.336E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.10 0.00) 15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00) 16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.00 0.00) 17 0.148E-15 0.575E-15 0.104E-14 1.000 dps @ ( 1.00 0.10 0.00) Converging n vectors ... it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 ) it = 2 dn = 0.423E-15 rlx = 1.000 ( 31 ) Converging e1,e2 vectors ... it = 1 de = 0.285E+01 rlx = 0.351 ( 24 ) it = 2 de = 0.269E+01 rlx = 0.372 ( 14 ) it = 3 de = 0.202E+01 rlx = 0.494 ( 40 ) it = 4 de = 0.122E+01 rlx = 0.820 ( 40 ) it = 5 de = 0.378E+00 rlx = 1.000 ( 40 ) it = 6 de = 0.127E-01 rlx = 1.000 ( 14 ) it = 7 de = 0.524E-06 rlx = 1.000 ( 40 ) it = 8 de = 0.938E-16 rlx = 1.000 ( 22 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMCantileverPlate.dat real 0m0.807s user 0m0.615s sys 0m0.085s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 capsReference attributes ................ Number of unique capsReference attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Name = Wing, index = 7 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 367 Number of elements = 525 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 192 Elemental Quad4 = 333 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 368 Combined Number of elements = 526 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 192 Combined Elemental Quad4 = 333 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting vortex lattice control surface data VLM control surface name - CntrlLE VLM control surface name - CntrlTE Done getting vortex lattice control surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 48 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Getting Aero Reference Parameters....... Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Ribs No "material" specified for Property tuple Ribs, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Property name - Spar1 No "material" specified for Property tuple Spar1, defaulting to an index of 1 Property name - Spar2 No "material" specified for Property tuple Spar2, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 43 automatic connections were made for capsConnect Rib_Root (node id 368) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m18.993s user 0m31.285s sys 0m2.926s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = yatesPlate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 36 Number of elements = 25 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 25 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Mahogany Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - yatesPlate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 2 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Natural freq (Mode 1) = 5.78 (Hz) Natural freq (Mode 2) = 30.66 (Hz) real 0m0.562s user 0m0.501s sys 0m0.140s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 15 Number of elements = 8 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 8 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - cantilever No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards real 0m0.764s user 0m0.662s sys 0m0.142s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt astros_CompositeWingFreq_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt + python -u astros_CompositeWingFreq_PyTest.py -outLevel=0 Getting results for natural frequencies..... Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = wing, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - wing Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = wing, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = wing, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 402 Number of elements = 763 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 763 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Aluminum No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic" Material name - Graphite_epoxy Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - root No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Natural freq (Mode 1) = 5.92088 (Hz) Natural freq (Mode 2) = 29.77630 (Hz) Natural freq (Mode 3) = 39.17100 (Hz) Natural freq (Mode 4) = 77.68370 (Hz) Natural freq (Mode 5) = 99.80360 (Hz) Natural freq (Mode 6) = 145.83600 (Hz) Natural freq (Mode 7) = 177.88500 (Hz) Natural freq (Mode 8) = 237.90000 (Hz) Natural freq (Mode 9) = 280.01500 (Hz) Natural freq (Mode 10) = 305.57400 (Hz) Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 402 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 = 402 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 = 402 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 = 402 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 = 402 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 0m36.357s user 0m28.305s sys 0m0.668s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 96 Number of elements = 77 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 77 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 97 Combined Number of elements = 78 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 77 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 96 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - aluminum No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Body Property name - Edge Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - PointConstraint No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Getting FEA connections....... Number of connection tuples - 1 Connection name - Root No "groupName" specified for Connection tuple Root! Looking for automatic connections from the use of capsConnectLink for Root 8 automatic connections were made for capsConnect Root (node id 97) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Flutter Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aero card Writing analysis cards Writing constraint cards--each subcase individually Writing material cards Writing property cards Writing unsteady aeroelastic cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m1.139s user 0m0.777s sys 0m0.243s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 16 Number of elements = 9 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 9 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 5 Load name - load_0 Load name - load_1 Load name - load_2 Load name - load_3 Load name - load_4 Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 5 Analysis name - load_0 Analysis name - load_1 Analysis name - load_2 Analysis name - load_3 Analysis name - load_4 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case load_0, assuming all constraints are applied!!!! Warning: No constraints specified for case load_1, assuming all constraints are applied!!!! Warning: No constraints specified for case load_2, assuming all constraints are applied!!!! Warning: No constraints specified for case load_3, assuming all constraints are applied!!!! Warning: No constraints specified for case load_4, assuming all constraints are applied!!!! Writing analysis cards Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m0.983s user 0m0.729s sys 0m0.172s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 293 Number of elements = 217 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 217 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - Ribs_and_Spars Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Natural freq (Mode 1) = 0.02335 (Hz) Natural freq (Mode 2) = 0.02335 (Hz) Natural freq (Mode 3) = 0.11619 (Hz) Natural freq (Mode 4) = 0.11619 (Hz) Natural freq (Mode 5) = 0.14468 (Hz) Natural freq (Mode 6) = 0.14468 (Hz) Natural freq (Mode 7) = 0.23352 (Hz) Natural freq (Mode 8) = 0.23352 (Hz) Natural freq (Mode 9) = 0.30497 (Hz) Natural freq (Mode 10) = 0.30497 (Hz) real 0m17.117s user 0m19.494s sys 0m4.266s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 6 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 6 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m0.696s user 0m0.732s sys 0m0.166s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt + echo 'astros_ThreeBarFreq_PyTest.py test;' astros_ThreeBarFreq_PyTest.py test; + python -u astros_ThreeBarFreq_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Getting results for natural frequencies..... WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 2 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Natural freq (Mode 1) = 86.13400 (Hz) Natural freq (Mode 2) = 168.53300 (Hz) real 0m0.623s user 0m0.676s sys 0m0.155s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedForce Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Getting FEA design variables....... Number of design variables - 3 Design_Variable name - Bar1A Design_Variable name - Bar2A Design_Variable name - Bar3A Design_Variable_Relation name - Bar1A Design_Variable_Relation name - Bar2A Design_Variable_Relation name - Bar3A Number of design variable relations - 3 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 3 Design_Constraint name - stress1 Design_Constraint name - stress2 Design_Constraint name - stress3 Done getting FEA design constraints Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing design constraint cards Writing load cards Writing material cards Writing property cards Writing design variable cards Running Astros...... Done running Astros! real 0m0.944s user 0m0.756s sys 0m0.150s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 2 Constraint name - conOne No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement" Constraint name - conTwo No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - loadOne Load name - loadTwo Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 2 Analysis name - analysisOne Analysis name - analysisTwo Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards real 0m0.764s user 0m0.648s sys 0m0.145s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedForce Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards real 0m0.676s user 0m0.677s sys 0m0.144s + 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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 96 Number of elements = 77 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 77 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 97 Combined Number of elements = 78 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 77 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 96 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - aluminum No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - Body Property name - Edge Property name - Root Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - PointConstraint No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - PointSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Root No "groupName" specified for Connection tuple Root! Looking for automatic connections from the use of capsConnectLink for Root 8 automatic connections were made for capsConnect Root (node id 97) Done getting FEA connections Getting FEA loads....... Number of loads - 2 Load name - GravityLoad No "groupName" specified for Load tuple GravityLoad, going to use load name Load name - PointLoad Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m1.722s user 0m0.862s sys 0m0.246s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: abaqus Nastran Mystran Plato ================================================= All tests pass! ================================================= ================================================= [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64') [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/DARWIN_ARM64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/DARWIN_ARM64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] Obtaining reference build from same job (7.6,CAPS/STRUCTURE,DARWIN_ARM64,viggen) [Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #189' 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=DARWIN_ARM64,buildnode=viggen #190'. [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