Skipping 341 KB..
Full Logclang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/vlmUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads \
-lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -ludunits2 -lm -ldl
(cd test; make -f vVS.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include vVS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/vVS.o
clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/test/vVS /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/vVS.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
(cd examples; make)
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite
cp -p -f pyCAPS/abaqus_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/abaqus_AGARD445_PyTest.py
cp -p -f pyCAPS/abaqus_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/abaqus_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Astros.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py
cp -p -f pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aflr2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr2_PyTest.py
cp -p -f pyCAPS/aflr4_Generic_Missile.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_Generic_Missile.py
cp -p -f pyCAPS/aflr4_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_PyTest.py
cp -p -f pyCAPS/aflr4_QuadMesh_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_QuadMesh_PyTest.py
cp -p -f pyCAPS/aflr4_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_TipTreat_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_TipTreat_PyTest.py
cp -p -f pyCAPS/aflr4_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_Tetgen_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_aflr3_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_tetgen_Regions_PyTest.py
cp -p -f pyCAPS/astros_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_AGARD445_PyTest.py
cp -p -f pyCAPS/astros_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Aeroelastic_PyTest.py
cp -p -f pyCAPS/astros_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/astros_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Composite_PyTest.py
cp -p -f pyCAPS/astros_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Flutter_15degree.py
cp -p -f pyCAPS/astros_MultipleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_MultipleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_OptControl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_OptControl_PyTest.py
cp -p -f pyCAPS/astros_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_PyTest.py
cp -p -f pyCAPS/astros_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/astros_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBar_PyTest.py
cp -p -f pyCAPS/astros_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Trim_15degree.py
cp -p -f pyCAPS/autoLink_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/autoLink_Pytest.py
cp -p -f pyCAPS/avl_AutoSpan_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_AutoSpan_PyTest.py
cp -p -f pyCAPS/avl_ControlSurf_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_ControlSurf_PyTest.py
cp -p -f pyCAPS/avl_DesignSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_DesignSweep_PyTest.py
cp -p -f pyCAPS/avl_EigenValue_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_EigenValue_PyTest.py
cp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/avl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_PyTest.py
cp -p -f pyCAPS/awave_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/awave_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py
cp -p -f pyCAPS/cart3d_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_PyTest.py
cp -p -f pyCAPS/cbaero_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cbaero_PyTest.py
cp -p -f pyCAPS/delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/delaundo_PyTest.py
cp -p -f pyCAPS/egadsTess_Box_Quad_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_Box_Quad_Pytest.py
cp -p -f pyCAPS/egadsTess_Nose_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_Nose_Quad_PyTest.py
cp -p -f pyCAPS/egadsTess_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_PyTest.py
cp -p -f pyCAPS/egadsTess_Spheres_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py
cp -p -f pyCAPS/friction_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/friction_PyTest.py
cp -p -f pyCAPS/fun3d_Morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_Morph_PyTest.py
cp -p -f pyCAPS/fun3d_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_AFLR2_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/fun3d_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_Delaundo_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_Tetgen_PyTest.py
cp -p -f pyCAPS/fun3d_refine_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_refine_PyTest.py
cp -p -f pyCAPS/hsm_CantileverPlate_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/hsm_CantileverPlate_PyTest.py
cp -p -f pyCAPS/hsm_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/hsm_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/masstran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/masstran_AGARD445_PyTest.py
cp -p -f pyCAPS/masstran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/masstran_PyTest.py
cp -p -f pyCAPS/mses_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mses_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/mses_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mses_PyTest.py
cp -p -f pyCAPS/mystran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_AGARD445_PyTest.py
cp -p -f pyCAPS/mystran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/mystran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_PyTest.py
cp -p -f pyCAPS/mystran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_AGARD445_PyTest.py
cp -p -f pyCAPS/nastran_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Aeroelastic_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_CompositeWingDesign_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/nastran_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Composite_PyTest.py
cp -p -f pyCAPS/nastran_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Flutter_15degree.py
cp -p -f pyCAPS/nastran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_OptimizationMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_OptimizationMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_PlateMisc_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_PlateMisc_PyTest.py
cp -p -f pyCAPS/nastran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_PyTest.py
cp -p -f pyCAPS/nastran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBar_PyTest.py
cp -p -f pyCAPS/nastran_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Trim_15degree.py
cp -p -f pyCAPS/plato_aflr_airfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_airfoil_PyTest.py
cp -p -f pyCAPS/plato_aflr_airfoil_morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_airfoil_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_table_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_table_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_tetgen_table_PyTest.py
cp -p -f pyCAPS/plato_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_tetgen_table_PyTest.py
cp -p -f pyCAPS/pointwise_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/pointwise_PyTest.py
cp -p -f pyCAPS/pointwise_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/pointwise_Symmetry_PyTest.py
cp -p -f pyCAPS/su2_Morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_Morph_PyTest.py
cp -p -f pyCAPS/su2_X43a_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_X43a_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_AFLR2_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/su2_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_Delaundo_PyTest.py
cp -p -f pyCAPS/su2_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_Tetgen_PyTest.py
cp -p -f pyCAPS/su2_and_pointwise_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_pointwise_PyTest.py
cp -p -f pyCAPS/tetgen_Holes_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tetgen_Holes_PyTest.py
cp -p -f pyCAPS/tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tetgen_PyTest.py
cp -p -f pyCAPS/tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tetgen_Regions_PyTest.py
cp -p -f pyCAPS/tsfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tsfoil_PyTest.py
cp -p -f pyCAPS/xfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/xfoil_PyTest.py
cp -p -f csmData/15degreeWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/15degreeWing.csm
cp -p -f csmData/aeroelasticDataTransfer.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/aeroelasticDataTransfer.csm
cp -p -f csmData/aeroelasticDataTransferSimple.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/aeroelasticDataTransferSimple.csm
cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/airfoilSection.csm
cp -p -f csmData/avlWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/avlWing.csm
cp -p -f csmData/avlWingTail.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/avlWingTail.csm
cp -p -f csmData/avlWings.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/avlWings.csm
cp -p -f csmData/awaveWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/awaveWingTailFuselage.csm
cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/cfd2D.csm
cp -p -f csmData/cfd2DArbShape.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/cfd2DArbShape.csm
cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/cfdMultiBody.csm
cp -p -f csmData/cfdSymmetry.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/cfdSymmetry.csm
cp -p -f csmData/cfdX43a.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/cfdX43a.csm
cp -p -f csmData/cfd_airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/cfd_airfoilSection.csm
cp -p -f csmData/compositeWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/compositeWing.csm
cp -p -f csmData/cyli_box_shell.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/cyli_box_shell.csm
cp -p -f csmData/cyli_box_solid.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/cyli_box_solid.csm
cp -p -f csmData/feaAGARD445.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/feaAGARD445.csm
cp -p -f csmData/feaBoxes.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/feaBoxes.csm
cp -p -f csmData/feaCantileverPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/feaCantileverPlate.csm
cp -p -f csmData/feaJoinedPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/feaJoinedPlate.csm
cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/feaSimplePlate.csm
cp -p -f csmData/feaThreeBar.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/feaThreeBar.csm
cp -p -f csmData/feaWingBEM.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/feaWingBEM.csm
cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/feaWingBEMAero.csm
cp -p -f csmData/frictionWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/frictionWingTailFuselage.csm
cp -p -f csmData/generic_missile.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/generic_missile.csm
cp -p -f csmData/interference.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/interference.csm
cp -p -f csmData/linearAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/linearAero.csm
cp -p -f csmData/nosecone1.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/nosecone1.csm
cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/regions.csm
cp -p -f csmData/simpleWingBox.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/simpleWingBox.csm
cp -p -f csmData/spheres.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/spheres.csm
cp -p -f csmData/table.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/table.csm
cp -p -f csmData/tiptreat.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/tiptreat.csm
cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/csmData/avlWing.udc
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/csm
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS
cp -p -f corsairlite/boydBox.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/boydBox.py
cp -p -f corsairlite/gp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/gp.py
cp -p -f corsairlite/hoburg_blackbox.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/hoburg_blackbox.py
cp -p -f corsairlite/hoburg_gp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/hoburg_gp.py
cp -p -f corsairlite/qp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/qp.py
cp -p -f corsairlite/sp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/sp.py
cp -p -f corsairlite/capsPhase/csm/wing1.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm/wing1.csm
cp -p -f corsairlite/capsPhase/csm/wing2.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm/wing2.csm
cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py
cp -p -f corsairlite/multifidelity/csm/naca.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/csm/naca.csm
cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py
cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/Camber.py
cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py
cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py
cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/MSES.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py
cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/execute_CTestRegression.sh
cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/execute_PyTestRegression.sh
(make -C cCAPS -f aeroelastic_SU2.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f avlTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include avlTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/avlTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/avlTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f awaveTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include awaveTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/awaveTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f frictionTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include frictionTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/frictionTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f fun3d.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/fun3dAFLR2Test.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/fun3dAFLR2Test.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/fun3dTetgenTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/fun3dTetgenTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/aeroelasticTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/aeroelasticTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f hsm.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include hsmTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/hsmTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/hsmTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/hsmSimplePlateTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/hsmSimplePlateTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/hsmCantileverPlateTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/hsmCantileverPlateTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/hsmJoinedPlateTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/hsmJoinedPlateTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f interferenceTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include interferenceTest.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/interferenceTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/interferenceTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f msesTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include msesTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/msesTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/msesTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f mystran.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include mystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/mystranTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/mystranTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f pointwiseTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/pointwiseTest.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
+++ find /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/training/ -name Makefile
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/training//2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/training//2023/data/session01/Makefile
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/training//2023/data/session01
++ make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include template_avl.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/template_avl.o
clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/test/template_avl /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/template_avl.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/training//data/session01/Makefile
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/training//data/session01
++ make
make: Nothing to be done for `default'.
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/OpenCSM/trunk/src
++ make -f serveESP.make
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/timCapsMode.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/capsMode.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/capsMode.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/timFlowchart.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/flowchart.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/flowchart.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/timViewer.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/viewer.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/viewer.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/viewer.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/timViewer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/include -I. -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 timPyscript.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/timPyscript.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/pyscript.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/pyscript.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib/pyscript.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/obj/timPyscript.o -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin
++ ln -f -s /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64
+++ find /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/OpenCSM/trunk/data/training/ -name Makefile
+ mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/test
+ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/test
+ source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/JenkinsESP/RunRegression.sh
++ [[ 0 == 1 ]]
++ [[ 0 == 2 ]]
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64 == '' ]]
++ [[ CAPS/STRUCTURE == '' ]]
++ [[ 7.8 == '' ]]
++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/JenkinsESP ]]
++ rm -f csmFiles.txt
++ [[ CAPS/STRUCTURE =~ [0-9]+.[0-9]+ ]]
++ export ESPTEST=CAPS/STRUCTURE
++ ESPTEST=CAPS/STRUCTURE
++ [[ CAPS/STRUCTURE == \C\A\P\S* ]]
++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS ]]
++ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/examples/
++ make test TYPE=STRUCTURE
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
(make -C cCAPS -f avlTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/frictionTest' is up to date.
(make -C cCAPS -f fun3d.make)
make[1]: Nothing to be done for `fun3d'.
(make -C cCAPS -f hsm.make)
make[1]: `hsm' is up to date.
(make -C cCAPS -f interferenceTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/cCAPS/pointwiseTest' is up to date.
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest; ./execute_CTestRegression.sh STRUCTURE)
Running.... STRUCTURE c-Tests
=================================================
+ echo './interferenceTest test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt
./interferenceTest test;
+ ./interferenceTest
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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: 5.849417e-01 Sphere
3: 7.191810e-01 Cylinder
4: 4.000000e+01 OuterBox
0.000000e+00 -2.685383e-02 0.000000e+00 0.000000e+00
-2.685383e-02 0.000000e+00 0.000000e+00 -2.592150e-02
0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00
0.000000e+00 -2.592150e-02 0.000000e+00 1.000000e+00
classifyClouds: EG_generalBoolean = -7!
classifyClouds: EG_generalBoolean = -7!
1: 1.000000e+00 Box
2: 5.886880e-01 Sphere
3: 7.235323e-01 Cylinder
0.000000e+00 -2.035193e-02 0.000000e+00
-2.035193e-02 0.000000e+00 0.000000e+00
0.000000e+00 0.000000e+00 0.000000e+00
real 0m6.489s
user 0m6.630s
sys 0m0.257s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./interferenceTest passed (as expected)
=============================================
=================================================
+ echo './hsmCantileverPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt
./hsmCantileverPlateTest test;
+ ./hsmCantileverPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt
Attention: hsmCantileverPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 51
Elemental Tria3 = 0
Elemental Quad4 = 27
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
No "material" specified for Property tuple plate, defaulting to an index of 1
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1313
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.07 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.03 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.07 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00)
8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.10 0.00)
9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.10 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
iter dr dd dp rlx max
11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.10 0.00)
11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00)
12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00)
13* 0.335E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00)
15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00)
16 0.573E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00)
17 0.179E-15 0.693E-15 0.745E-15 1.000 dps @ ( 0.78 0.00 0.00)
Converging n vectors ...
it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 )
it = 2 dn = 0.516E-15 rlx = 1.000 ( 13 )
Converging e1,e2 vectors ...
it = 1 de = 0.285E+01 rlx = 0.351 ( 24 )
it = 2 de = 0.269E+01 rlx = 0.372 ( 37 )
it = 3 de = 0.249E+01 rlx = 0.402 ( 21 )
it = 4 de = 0.179E+01 rlx = 0.559 ( 21 )
it = 5 de = 0.954E+00 rlx = 1.000 ( 21 )
it = 6 de = 0.152E+00 rlx = 1.000 ( 21 )
it = 7 de = 0.887E-03 rlx = 1.000 ( 21 )
it = 8 de = 0.177E-09 rlx = 1.000 ( 21 )
it = 9 de = 0.876E-16 rlx = 1.000 ( 28 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat
real 0m1.376s
user 0m0.352s
sys 0m0.099s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected)
=============================================
=================================================
+ echo './hsmSimplePlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt
./hsmSimplePlateTest test;
+ ./hsmSimplePlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt
Attention: hsmTest2 is hard coded to look for ../csmData/feaSimplePlate.csm
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Number of nodal coordinates = 100
Number of elements = 198
Elemental Tria3 = 162
Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
No "material" specified for Property tuple plate, defaulting to an index of 1
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 7
MaxDim = 36, numBCEdge = 0, numBCNode = 36, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 36
->HSMSOL
Matrix Non-zero Entries = 8026
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.609E+00 0.519E+01 0.260E+01 0.096 ddy @ ( 0.28 0.25 0.00)
1* 0.571E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00)
1* 0.159E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00)
1* 0.254E-02 0.000E+00 0.000E+00 1.000 drz @ ( 0.11 0.14 0.00)
1* 0.838E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.14 0.00)
2 0.768E-02 0.754E+00 0.102E+01 0.492 dps @ ( 0.00 0.00 0.00)
2* 0.336E-03 0.000E+00 0.000E+00 1.000 drx @ ( 0.06 0.06 0.00)
2* 0.690E-06 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.08 0.00)
3 0.252E-02 0.204E+00 0.299E+00 1.000 dps @ ( 0.50 0.03 0.00)
3* 0.181E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.39 0.11 0.00)
3* 0.675E-06 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.03 0.00)
4 0.108E-03 0.157E-01 0.567E-01 1.000 dps @ ( 0.39 0.14 0.00)
4* 0.249E-05 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.22 0.00)
5 0.103E-05 0.374E-03 0.159E-02 1.000 dps @ ( 0.06 0.06 0.00)
6 0.139E-08 0.994E-07 0.421E-06 1.000 dps @ ( 0.50 0.00 0.00)
7 0.106E-15 0.467E-13 0.133E-12 1.000 dps @ ( 0.50 0.00 0.00)
Converging n vectors ...
it = 1 dn = 0.117E+01 rlx = 1.000 ( 66 )
it = 2 dn = 0.327E-15 rlx = 1.000 ( 81 )
Converging e1,e2 vectors ...
it = 1 de = 0.357E+00 rlx = 1.000 ( 94 )
it = 2 de = 0.167E+00 rlx = 1.000 ( 67 )
it = 3 de = 0.245E-01 rlx = 1.000 ( 76 )
it = 4 de = 0.567E-02 rlx = 1.000 ( 59 )
it = 5 de = 0.192E-02 rlx = 1.000 ( 59 )
it = 6 de = 0.648E-03 rlx = 1.000 ( 59 )
it = 7 de = 0.219E-03 rlx = 1.000 ( 59 )
it = 8 de = 0.740E-04 rlx = 1.000 ( 59 )
it = 9 de = 0.250E-04 rlx = 1.000 ( 59 )
it = 10 de = 0.845E-05 rlx = 1.000 ( 59 )
it = 11 de = 0.286E-05 rlx = 1.000 ( 59 )
it = 12 de = 0.965E-06 rlx = 1.000 ( 59 )
it = 13 de = 0.326E-06 rlx = 1.000 ( 59 )
it = 14 de = 0.110E-06 rlx = 1.000 ( 59 )
it = 15 de = 0.372E-07 rlx = 1.000 ( 59 )
it = 16 de = 0.126E-07 rlx = 1.000 ( 59 )
it = 17 de = 0.425E-08 rlx = 1.000 ( 59 )
it = 18 de = 0.144E-08 rlx = 1.000 ( 59 )
it = 19 de = 0.485E-09 rlx = 1.000 ( 59 )
it = 20 de = 0.164E-09 rlx = 1.000 ( 59 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat
real 0m3.460s
user 0m1.095s
sys 0m0.150s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected)
=============================================
=================================================
+ echo './hsmJoinedPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt
./hsmJoinedPlateTest test;
+ ./hsmJoinedPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 ( 4 )
it = 6 de = 0.660E+00 rlx = 1.000 ( 2 )
it = 7 de = 0.860E-01 rlx = 1.000 ( 4 )
it = 8 de = 0.228E-03 rlx = 1.000 ( 2 )
it = 9 de = 0.428E-11 rlx = 1.000 ( 4 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat
real 0m2.017s
user 0m0.336s
sys 0m0.118s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmJoinedPlateTest passed (as expected)
=============================================
=================================================
Did not run examples for:
Mystran
=================================================
All tests pass!
=================================================
=================================================
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest; ./execute_PyTestRegression.sh STRUCTURE)
=================================================
Using python : /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/venv/bin/python
=================================================
Running.... STRUCTURE PyTests
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 3.428666259747
Mass 5383.006027803
Centroid [1.222256036874, 0.1634981473778, -4.234492548615e-11]
CG [1.222256036874, 0.1634981473778, -4.234574416087e-11]
Ixx 22133.97306033
Iyy 23448.30046709
Izz 1389.213122582
Ixy 164.2055275657
Ixz -7.454849830627e-06
Iyz 1.707682983295e-06
I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454849830627e-06, 1.707682983295e-06]
II [[22133.97306033, -164.2055275657, 7.454849830627e-06], [-164.2055275657, 23448.30046709, -1.707682983295e-06], [7.454849830627e-06, -1.707682983295e-06, 1389.213122582]]
real 0m57.679s
user 0m9.757s
sys 0m6.244s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
masstran_AGARD445_PyTest.py test;
+ python -u masstran_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 0m11.506s
user 0m0.702s
sys 0m0.302s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 0m8.973s
user 0m0.947s
sys 0m0.189s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 51
Elemental Tria3 = 0
Elemental Quad4 = 27
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1313
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.03 0.00)
1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.03 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.03 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.03 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.07 0.00)
8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.10 0.00)
9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.00 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
iter dr dd dp rlx max
11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.10 0.00)
11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00)
12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00)
13* 0.336E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00)
15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.10 0.00)
16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00)
17 0.558E-15 0.304E-14 0.603E-15 1.000 ddx @ ( 1.00 0.00 0.00)
Converging n vectors ...
it = 1 dn = 0.193E+01 rlx = 1.000 ( 12 )
it = 2 dn = 0.435E-15 rlx = 1.000 ( 28 )
Converging e1,e2 vectors ...
it = 1 de = 0.285E+01 rlx = 0.351 ( 24 )
it = 2 de = 0.292E+01 rlx = 0.342 ( 34 )
it = 3 de = 0.226E+01 rlx = 0.442 ( 34 )
it = 4 de = 0.151E+01 rlx = 0.660 ( 34 )
it = 5 de = 0.665E+00 rlx = 1.000 ( 34 )
it = 6 de = 0.609E-01 rlx = 1.000 ( 34 )
it = 7 de = 0.573E-04 rlx = 1.000 ( 34 )
it = 8 de = 0.478E-13 rlx = 1.000 ( 34 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMCantileverPlate.dat
real 0m10.232s
user 0m0.882s
sys 0m0.215s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 = 365
Number of elements = 521
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 188
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 = 366
Combined Number of elements = 522
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 188
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
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Aeroelastic_PyTest.py", line 137, in <module>
myProblem.analysis["astros"].runAnalysis()
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_BADVALUE:
================================================================================
feaUtils.c:4592 in fea_getProperty():
Error: Number of Property (5) does not match number of capsGroups (7)!
capsGroups:
Ribs
Skin
Spar1
Rib_Root
Spar2
Rib_Root_Point
Wing
Property names:
Rib_Root
Ribs
Skin
Spar1
Spar2
astrosAIM.c:1773 in aimUpdateState(): Error status = -311
================================================================================
real 0m40.817s
user 0m13.749s
sys 0m3.477s
+ status=1
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py failed (as NOT expected)
=================================================
=================================================
+ echo 'astros_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_AGARD445_PyTest.py test;
+ python -u astros_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 0m21.262s
user 0m0.754s
sys 0m0.397s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_Composite_PyTest.py test;
+ python -u astros_Composite_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 0m1.693s
user 0m0.901s
sys 0m0.412s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Getting results for natural frequencies.....
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = wing, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - wing
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = root, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = wing, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = wing, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping 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 = 429
Number of elements = 817
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 817
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) = 5.91949 (Hz)
Natural freq (Mode 2) = 29.79990 (Hz)
Natural freq (Mode 3) = 39.10550 (Hz)
Natural freq (Mode 4) = 77.71580 (Hz)
Natural freq (Mode 5) = 99.79550 (Hz)
Natural freq (Mode 6) = 146.97500 (Hz)
Natural freq (Mode 7) = 176.90300 (Hz)
Natural freq (Mode 8) = 235.53300 (Hz)
Natural freq (Mode 9) = 274.42600 (Hz)
Natural freq (Mode 10) = 311.35900 (Hz)
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 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 = 429 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 = 429 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 = 429 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 = 429 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 1m35.019s
user 0m50.788s
sys 0m1.791s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 - 4
Property name - Body
Property name - Edge
Property name - Root
Property name - Wing
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 IEEE_DENORMAL
real 0m20.873s
user 0m1.365s
sys 0m0.737s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 IEEE_DENORMAL
real 0m9.785s
user 0m1.385s
sys 0m0.630s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 0m28.446s
user 0m23.159s
sys 0m4.554s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 IEEE_DENORMAL
real 0m4.383s
user 0m0.825s
sys 0m0.369s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ python -u astros_ThreeBarFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 0m2.358s
user 0m0.855s
sys 0m0.363s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarLinkDesign_PyTest.py test;
+ python -u astros_ThreeBarLinkDesign_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 0m7.057s
user 0m0.997s
sys 0m0.430s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ python -u astros_ThreeBarMultiLoad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 0m9.835s
user 0m0.885s
sys 0m0.459s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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 0m5.267s
user 0m0.920s
sys 0m0.399s
+ 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_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ python -u astros_Trim_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/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
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Trim_15degree.py", line 143, in <module>
myAnalysis.runAnalysis()
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_BADVALUE:
================================================================================
feaUtils.c:4592 in fea_getProperty():
Error: Number of Property (3) does not match number of capsGroups (4)!
capsGroups:
Edge
Body
Root
Wing
Property names:
Body
Edge
Root
astrosAIM.c:1773 in aimUpdateState(): Error status = -311
================================================================================
real 0m3.760s
user 0m0.667s
sys 0m0.227s
+ status=1
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py failed (as NOT expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
Nastran
Mystran
Plato
=================================================
=================================================
Summary of examples NOT finished as expected
astros_Aeroelastic_PyTest.py
astros_Trim_15degree.py
See pyCAPSlog.txt for more details.
=================================================
=================================================
=================================================
make: *** [pyCAPStest] Error 1
Build step 'Conditional step (single)' marked build as failure
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE
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