Skipping 432 KB..
Full Logcp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/avl_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_PyTest.py
cp -p -f pyCAPS/awave_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/awave_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py
cp -p -f pyCAPS/cart3d_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_PyTest.py
cp -p -f pyCAPS/delaundo_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/delaundo_PyTest.py
cp -p -f pyCAPS/egadsTess_Nose_Quad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Nose_Quad_PyTest.py
cp -p -f pyCAPS/egadsTess_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_PyTest.py
cp -p -f pyCAPS/egadsTess_Spheres_Quad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py
cp -p -f pyCAPS/friction_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/friction_PyTest.py
cp -p -f pyCAPS/fun3d_Morph_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_Morph_PyTest.py
cp -p -f pyCAPS/fun3d_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_AFLR2_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/fun3d_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_Delaundo_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_Tetgen_PyTest.py
cp -p -f pyCAPS/fun3d_refine_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_refine_PyTest.py
cp -p -f pyCAPS/hsm_CantileverPlate_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/hsm_CantileverPlate_PyTest.py
cp -p -f pyCAPS/hsm_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/hsm_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/masstran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/masstran_AGARD445_PyTest.py
cp -p -f pyCAPS/masstran_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/masstran_PyTest.py
cp -p -f pyCAPS/mses_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mses_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/mses_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mses_PyTest.py
cp -p -f pyCAPS/mystran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mystran_AGARD445_PyTest.py
cp -p -f pyCAPS/mystran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mystran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/mystran_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mystran_PyTest.py
cp -p -f pyCAPS/mystran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mystran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_AGARD445_PyTest.py
cp -p -f pyCAPS/nastran_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_Aeroelastic_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingDesign_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_CompositeWingDesign_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/nastran_Composite_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_Composite_PyTest.py
cp -p -f pyCAPS/nastran_Flutter_15degree.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_Flutter_15degree.py
cp -p -f pyCAPS/nastran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_OptimizationMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_OptimizationMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_PlateMisc_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_PlateMisc_PyTest.py
cp -p -f pyCAPS/nastran_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_PyTest.py
cp -p -f pyCAPS/nastran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarDesign_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBarDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBar_PyTest.py
cp -p -f pyCAPS/nastran_Trim_15degree.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_Trim_15degree.py
cp -p -f pyCAPS/plato_aflr_airfoil_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_airfoil_PyTest.py
cp -p -f pyCAPS/plato_aflr_airfoil_morph_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_airfoil_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_table_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_morph_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_table_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_tetgen_table_PyTest.py
cp -p -f pyCAPS/plato_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_tetgen_table_PyTest.py
cp -p -f pyCAPS/pointwise_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/pointwise_PyTest.py
cp -p -f pyCAPS/pointwise_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/pointwise_Symmetry_PyTest.py
cp -p -f pyCAPS/quading_Pytest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/quading_Pytest.py
cp -p -f pyCAPS/su2_Morph_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_Morph_PyTest.py
cp -p -f pyCAPS/su2_X43a_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_X43a_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_AFLR2_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/su2_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_Delaundo_PyTest.py
cp -p -f pyCAPS/su2_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_Tetgen_PyTest.py
cp -p -f pyCAPS/su2_and_pointwise_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_pointwise_PyTest.py
cp -p -f pyCAPS/tetgen_Holes_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/tetgen_Holes_PyTest.py
cp -p -f pyCAPS/tetgen_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/tetgen_PyTest.py
cp -p -f pyCAPS/tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/tetgen_Regions_PyTest.py
cp -p -f pyCAPS/tsfoil_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/tsfoil_PyTest.py
cp -p -f pyCAPS/xfoil_PyTest.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/xfoil_PyTest.py
cp -p -f csmData/15degreeWing.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/15degreeWing.csm
cp -p -f csmData/aeroelasticDataTransfer.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/aeroelasticDataTransfer.csm
cp -p -f csmData/aeroelasticDataTransferSimple.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/aeroelasticDataTransferSimple.csm
cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/airfoilSection.csm
cp -p -f csmData/avlWing.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWing.csm
cp -p -f csmData/avlWingTail.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWingTail.csm
cp -p -f csmData/avlWings.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWings.csm
cp -p -f csmData/awaveWingTailFuselage.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/awaveWingTailFuselage.csm
cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfd2D.csm
cp -p -f csmData/cfd2DArbShape.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfd2DArbShape.csm
cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfdMultiBody.csm
cp -p -f csmData/cfdSymmetry.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfdSymmetry.csm
cp -p -f csmData/cfdX43a.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfdX43a.csm
cp -p -f csmData/cfd_airfoilSection.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfd_airfoilSection.csm
cp -p -f csmData/compositeWing.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/compositeWing.csm
cp -p -f csmData/cyli_box_shell.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cyli_box_shell.csm
cp -p -f csmData/cyli_box_solid.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cyli_box_solid.csm
cp -p -f csmData/feaAGARD445.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaAGARD445.csm
cp -p -f csmData/feaBoxes.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaBoxes.csm
cp -p -f csmData/feaCantileverPlate.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaCantileverPlate.csm
cp -p -f csmData/feaJoinedPlate.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaJoinedPlate.csm
cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaSimplePlate.csm
cp -p -f csmData/feaThreeBar.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaThreeBar.csm
cp -p -f csmData/feaWingBEM.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaWingBEM.csm
cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaWingBEMAero.csm
cp -p -f csmData/frictionWingTailFuselage.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/frictionWingTailFuselage.csm
cp -p -f csmData/generic_missile.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/generic_missile.csm
cp -p -f csmData/interference.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/interference.csm
cp -p -f csmData/linearAero.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/linearAero.csm
cp -p -f csmData/nosecone1.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/nosecone1.csm
cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/regions.csm
cp -p -f csmData/simpleWingBox.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/simpleWingBox.csm
cp -p -f csmData/spheres.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/spheres.csm
cp -p -f csmData/table.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/table.csm
cp -p -f csmData/tiptreat.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/tiptreat.csm
cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWing.udc
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm
mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS
cp -p -f corsairlite/boydBox.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/boydBox.py
cp -p -f corsairlite/gp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/gp.py
cp -p -f corsairlite/hoburg_blackbox.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_blackbox.py
cp -p -f corsairlite/hoburg_gp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_gp.py
cp -p -f corsairlite/qp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/qp.py
cp -p -f corsairlite/sp.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/sp.py
cp -p -f corsairlite/capsPhase/csm/wing1.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing1.csm
cp -p -f corsairlite/capsPhase/csm/wing2.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing2.csm
cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py
cp -p -f corsairlite/multifidelity/csm/naca.csm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm/naca.csm
cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py
cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Camber.py
cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py
cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py
cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/MSES.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py
cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_CTestRegression.sh
cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_PyTestRegression.sh
(make -C cCAPS -f aeroelastic_SU2.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f avlTest.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include avlTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f awaveTest.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include awaveTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f frictionTest.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include frictionTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f fun3d.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o \
-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o \
-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o \
-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f hsm.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o \
-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o \
-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o \
-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o \
-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f interferenceTest.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include interferenceTest.c \
-o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o \
-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f msesTest.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include msesTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f mystran.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include mystranTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o \
-L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
(make -C cCAPS -f pointwiseTest.make)
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
+++ find /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training/ -name Makefile
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//2023/lectures/Makefile == *\l\e\c\t\u\r\e\s* ]]
++ continue
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile
++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//2023/data/session01
++ make
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include template_avl.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/test/template_avl /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -lm -ldl
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//data/session01/Makefile
++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/training//data/session01
++ make
make: Nothing to be done for `default'.
++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/OpenCSM/trunk/src
++ make -f serveESP.make
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o
touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so
clang++ -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o
touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so
clang++ -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o
touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so
rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so
clang++ -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 timPyscript.c -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o
touch /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so
rm /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so
clang++ -g -target arm64-apple-darwin -fsanitize=undefined -fno-sanitize=vptr -fno-omit-frame-pointer -bundle -o /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -L/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib
++ ln -f -s /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64
+++ find /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/OpenCSM/trunk/data/training/ -name Makefile
find: /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/OpenCSM/trunk/data/training/: No such file or directory
+ source /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/JenkinsESP/ESP_Sanitize.sh
++ '[' -z '' ']'
++ OUTLEVEL=0
++ mkdir -p /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/test
++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/test
++ [[ CAPS/STRUCTURE =~ [0-9]+.[0-9]+ ]]
++ export ESPTEST=CAPS/STRUCTURE
++ ESPTEST=CAPS/STRUCTURE
++ [[ CAPS/STRUCTURE == \C\A\P\S* ]]
++ export CAPSTARGET=STRUCTURE
++ CAPSTARGET=STRUCTURE
++ [[ STRUCTURE == \u\n\i\t ]]
++ [[ STRUCTURE == \t\r\a\i\n\i\n\g\2\0\1\8 ]]
++ [[ STRUCTURE == \t\r\a\i\n\i\n\g ]]
++ [[ STRUCTURE == *\_\o\f\f ]]
++ cd /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest
++ ./execute_CTestRegression.sh STRUCTURE
Running.... STRUCTURE c-Tests
=================================================
+ echo './interferenceTest test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt
./interferenceTest test;
+ ./interferenceTest
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt
Note: interferenceTest uses ../csmData/interference.csm
classifyClouds: EG_generalBoolean = -7!
classifyClouds: EG_generalBoolean = -7!
classifyClouds: EG_generalBoolean = -7!
classifyClouds: EG_generalBoolean = -7!
1: 1.000000e+00 Box
2: 5.850521e-01 Sphere
3: 7.191810e-01 Cylinder
4: 4.000000e+01 OuterBox
0.000000e+00 -2.715465e-02 0.000000e+00 0.000000e+00
-2.715465e-02 0.000000e+00 0.000000e+00 -2.543571e-02
0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00
0.000000e+00 -2.543571e-02 0.000000e+00 1.000000e+00
classifyClouds: EG_generalBoolean = -7!
classifyClouds: EG_generalBoolean = -7!
1: 1.000000e+00 Box
2: 5.886885e-01 Sphere
3: 7.235323e-01 Cylinder
0.000000e+00 -2.059198e-02 0.000000e+00
-2.059198e-02 0.000000e+00 0.000000e+00
0.000000e+00 0.000000e+00 0.000000e+00
real 0m11.974s
user 0m10.495s
sys 0m0.171s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./interferenceTest passed (as expected)
=============================================
=================================================
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt
+ echo './hsmCantileverPlateTest test;'
./hsmCantileverPlateTest test;
+ ./hsmCantileverPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt
Attention: hsmCantileverPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 51
Elemental Tria3 = 0
Elemental Quad4 = 27
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
No "material" specified for Property tuple plate, defaulting to an index of 1
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1313
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.07 0.00)
1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.07 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.07 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.07 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.03 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00)
8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.00 0.00)
9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.10 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
iter dr dd dp rlx max
11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.00 0.00)
11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00)
12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00)
13* 0.335E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00)
15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00)
16 0.573E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00)
17 0.253E-15 0.930E-15 0.713E-15 1.000 ddx @ ( 0.56 0.10 0.00)
Converging n vectors ...
it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 )
it = 2 dn = 0.583E-15 rlx = 1.000 ( 31 )
Converging e1,e2 vectors ...
it = 1 de = 0.285E+01 rlx = 0.351 ( 24 )
it = 2 de = 0.269E+01 rlx = 0.372 ( 14 )
it = 3 de = 0.202E+01 rlx = 0.494 ( 14 )
it = 4 de = 0.122E+01 rlx = 0.820 ( 14 )
it = 5 de = 0.378E+00 rlx = 1.000 ( 14 )
it = 6 de = 0.127E-01 rlx = 1.000 ( 40 )
it = 7 de = 0.524E-06 rlx = 1.000 ( 40 )
it = 8 de = 0.128E-15 rlx = 1.000 ( 22 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat
real 0m0.479s
user 0m0.215s
sys 0m0.054s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected)
=============================================
=================================================
+ echo './hsmSimplePlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt
./hsmSimplePlateTest test;
+ ./hsmSimplePlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt
Attention: hsmTest2 is hard coded to look for ../csmData/feaSimplePlate.csm
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Number of nodal coordinates = 100
Number of elements = 198
Elemental Tria3 = 162
Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
No "material" specified for Property tuple plate, defaulting to an index of 1
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 7
MaxDim = 36, numBCEdge = 0, numBCNode = 36, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 36
->HSMSOL
Matrix Non-zero Entries = 8026
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.609E+00 0.519E+01 0.240E+01 0.096 ddy @ ( 0.28 0.25 0.00)
1* 0.571E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00)
1* 0.159E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00)
1* 0.254E-02 0.000E+00 0.000E+00 1.000 drz @ ( 0.11 0.14 0.00)
1* 0.837E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.14 0.00)
2 0.769E-02 0.753E+00 0.105E+01 0.478 dps @ ( 0.00 0.00 0.00)
2* 0.329E-03 0.000E+00 0.000E+00 1.000 drx @ ( 0.06 0.06 0.00)
2* 0.641E-06 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.08 0.00)
3 0.264E-02 0.213E+00 0.280E+00 1.000 dps @ ( 0.50 0.00 0.00)
3* 0.194E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.39 0.11 0.00)
3* 0.741E-06 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.03 0.00)
4 0.119E-03 0.159E-01 0.631E-01 1.000 dps @ ( 0.39 0.14 0.00)
4* 0.306E-05 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.22 0.00)
5 0.133E-05 0.441E-03 0.208E-02 1.000 dps @ ( 0.06 0.06 0.00)
6 0.233E-08 0.153E-06 0.694E-06 1.000 dps @ ( 0.50 0.00 0.00)
7 0.378E-15 0.119E-12 0.317E-12 1.000 dps @ ( 0.50 0.00 0.00)
Converging n vectors ...
it = 1 dn = 0.117E+01 rlx = 1.000 ( 66 )
it = 2 dn = 0.236E-15 rlx = 1.000 ( 81 )
Converging e1,e2 vectors ...
it = 1 de = 0.357E+00 rlx = 1.000 ( 94 )
it = 2 de = 0.167E+00 rlx = 1.000 ( 67 )
it = 3 de = 0.245E-01 rlx = 1.000 ( 76 )
it = 4 de = 0.567E-02 rlx = 1.000 ( 59 )
it = 5 de = 0.192E-02 rlx = 1.000 ( 59 )
it = 6 de = 0.648E-03 rlx = 1.000 ( 59 )
it = 7 de = 0.219E-03 rlx = 1.000 ( 59 )
it = 8 de = 0.740E-04 rlx = 1.000 ( 59 )
it = 9 de = 0.250E-04 rlx = 1.000 ( 59 )
it = 10 de = 0.845E-05 rlx = 1.000 ( 59 )
it = 11 de = 0.286E-05 rlx = 1.000 ( 59 )
it = 12 de = 0.965E-06 rlx = 1.000 ( 59 )
it = 13 de = 0.326E-06 rlx = 1.000 ( 59 )
it = 14 de = 0.110E-06 rlx = 1.000 ( 59 )
it = 15 de = 0.372E-07 rlx = 1.000 ( 59 )
it = 16 de = 0.126E-07 rlx = 1.000 ( 59 )
it = 17 de = 0.425E-08 rlx = 1.000 ( 59 )
it = 18 de = 0.144E-08 rlx = 1.000 ( 59 )
it = 19 de = 0.485E-09 rlx = 1.000 ( 59 )
it = 20 de = 0.164E-09 rlx = 1.000 ( 59 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat
real 0m0.753s
user 0m0.464s
sys 0m0.042s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected)
=============================================
=================================================
+ echo './hsmJoinedPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt
./hsmJoinedPlateTest test;
+ ./hsmJoinedPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt
Attention: hsmJoinedPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 56
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
No "material" specified for Property tuple plate, defaulting to an index of 1
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 16
MaxDim = 13, numBCEdge = 2, numBCNode = 4, numJoint = 13
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1242
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
1* 0.325E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.05 0.00)
1* 0.434E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2 0.274E+01 0.521E+01 0.118E-07 0.096 ddx @ ( 1.00 0.05 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
2* 0.772E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
3 0.202E+01 0.439E+01 0.107E-06 0.114 ddz @ ( 1.00 0.05 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
3* 0.622E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
3* 0.162E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
3* 0.163E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4 0.192E+01 0.476E+01 0.147E-07 0.105 ddz @ ( 1.00 0.05 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.448E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.395E+01 0.296E-07 0.127 ddz @ ( 1.00 0.05 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5* 0.636E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
6 0.156E+01 0.301E+01 0.131E-06 0.166 ddx @ ( 1.00 0.05 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.191E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.265E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7 0.103E+01 0.323E+01 0.408E-07 0.155 ddx @ ( 1.00 0.05 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.432E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8 0.757E+00 0.260E+01 0.162E-07 0.192 ddx @ ( 1.00 0.05 0.00)
8* 0.296E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.351E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.586E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
9 0.680E+00 0.181E+01 0.753E-07 0.276 ddx @ ( 0.88 0.00 0.00)
9* 0.329E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.452E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
9* 0.159E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
9* 0.238E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10 0.457E+00 0.172E+01 0.586E-07 0.290 ddz @ ( 1.00 0.10 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.392E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
iter dr dd dp rlx max
11 0.258E+00 0.122E+01 0.666E-08 0.411 ddz @ ( 1.00 0.10 0.00)
11* 0.207E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.284E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.486E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12 0.135E+00 0.660E+00 0.377E-08 0.758 ddz @ ( 0.88 0.00 0.00)
12* 0.242E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.368E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.869E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13 0.430E-01 0.257E+00 0.505E-07 1.000 ddx @ ( 1.00 0.05 0.00)
13* 0.395E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
13* 0.128E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13* 0.196E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
14 0.656E-03 0.680E-02 0.885E-07 1.000 ddx @ ( 1.00 0.00 0.00)
15 0.156E-05 0.177E-05 0.268E-10 1.000 ddx @ ( 1.00 0.10 0.00)
16 0.273E-09 0.106E-08 0.893E-11 1.000 ddx @ ( 0.50 0.05 0.00)
17 0.138E-15 0.353E-15 0.907E-15 1.000 dps @ ( 0.38 0.10 0.00)
Converging n vectors ...
it = 1 dn = 0.197E+01 rlx = 1.000 ( 17 )
it = 2 dn = 0.866E-15 rlx = 1.000 ( 18 )
Converging e1,e2 vectors ...
it = 1 de = 0.753E+01 rlx = 0.133 ( 1 )
it = 2 de = 0.309E+01 rlx = 0.324 ( 20 )
it = 3 de = 0.324E+01 rlx = 0.309 ( 2 )
it = 4 de = 0.226E+01 rlx = 0.443 ( 2 )
it = 5 de = 0.140E+01 rlx = 0.716 ( 2 )
it = 6 de = 0.660E+00 rlx = 1.000 ( 2 )
it = 7 de = 0.860E-01 rlx = 1.000 ( 2 )
it = 8 de = 0.228E-03 rlx = 1.000 ( 2 )
it = 9 de = 0.428E-11 rlx = 1.000 ( 2 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat
real 0m0.451s
user 0m0.218s
sys 0m0.048s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmJoinedPlateTest passed (as expected)
=============================================
=================================================
Did not run examples for:
Mystran
=================================================
All tests pass!
=================================================
=================================================
++ '[' '!' -z '-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ']'
++ ./execute_PyTestRegression.sh STRUCTURE
=================================================
Using python : /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/venv/bin/python
=================================================
Running.... STRUCTURE PyTests
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Getting results mass properties.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Area 3.428666259746
Mass 5383.006027801
Centroid [1.222256036872, 0.1634981473779, -4.406119555156e-11]
CG [1.222256036872, 0.1634981473779, -4.406215709976e-11]
Ixx 22133.97306028
Iyy 23448.30046701
Izz 1389.213122561
Ixy 164.2055275652
Ixz -7.483321030013e-06
Iyz 1.710429211156e-06
I [22133.97306028, 23448.30046701, 1389.213122561, 164.2055275652, -7.483321030013e-06, 1.710429211156e-06]
II [[22133.97306028, -164.2055275652, 7.483321030013e-06], [-164.2055275652, 23448.30046701, -1.710429211156e-06], [7.483321030013e-06, -1.710429211156e-06, 1389.213122561]]
real 0m11.958s
user 0m15.755s
sys 0m2.830s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'masstran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
masstran_AGARD445_PyTest.py test;
+ python -u masstran_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Getting results mass properties.....
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 36
Number of elements = 25
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 25
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Area 547.7004
Mass 0.01605224431138
Centroid [20.03586282449, 14.01686746988, 0.0]
CG [20.03586282449, 14.01686746988, 0.0]
Ixx 1.140246300554
Iyy 0.919317482675
Izz 2.059563783229
Ixy 0.7352134614013
Ixz 0.0
Iyz 0.0
I [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0]
II [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]]
real 0m0.444s
user 0m0.419s
sys 0m0.113s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
real 0m0.786s
user 0m0.765s
sys 0m0.096s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_CantileverPlate_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 51
Elemental Tria3 = 0
Elemental Quad4 = 27
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1313
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.03 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.07 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.07 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00)
8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.00 0.00)
9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.10 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
iter dr dd dp rlx max
11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.00 0.00)
11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.00 0.00)
12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.07 0.00)
13* 0.336E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.10 0.00)
15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00)
16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.00 0.00)
17 0.148E-15 0.575E-15 0.104E-14 1.000 dps @ ( 1.00 0.10 0.00)
Converging n vectors ...
it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 )
it = 2 dn = 0.423E-15 rlx = 1.000 ( 31 )
Converging e1,e2 vectors ...
it = 1 de = 0.285E+01 rlx = 0.351 ( 24 )
it = 2 de = 0.269E+01 rlx = 0.372 ( 14 )
it = 3 de = 0.202E+01 rlx = 0.494 ( 40 )
it = 4 de = 0.122E+01 rlx = 0.820 ( 40 )
it = 5 de = 0.378E+00 rlx = 1.000 ( 40 )
it = 6 de = 0.127E-01 rlx = 1.000 ( 14 )
it = 7 de = 0.524E-06 rlx = 1.000 ( 40 )
it = 8 de = 0.938E-16 rlx = 1.000 ( 22 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMCantileverPlate.dat
real 0m0.743s
user 0m0.697s
sys 0m0.098s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected)
=================================================
ASTROS_ROOT: /Users/jenkins/util/astros/Astros/Darwin-64bit
=================================================
+ echo 'astros_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 367
Number of elements = 525
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 192
Elemental Quad4 = 333
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 368
Combined Number of elements = 526
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 192
Combined Elemental Quad4 = 333
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting vortex lattice control surface data
VLM control surface name - CntrlLE
VLM control surface name - CntrlTE
Done getting vortex lattice control surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 48
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Getting Aero Reference Parameters.......
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Ribs
No "material" specified for Property tuple Ribs, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Property name - Spar1
No "material" specified for Property tuple Spar1, defaulting to an index of 1
Property name - Spar2
No "material" specified for Property tuple Spar2, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
43 automatic connections were made for capsConnect Rib_Root (node id 368)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
real 0m20.007s
user 0m36.499s
sys 0m3.623s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_AGARD445_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
+ python -u astros_AGARD445_PyTest.py -outLevel=0
Getting results natural frequencies.....
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 36
Number of elements = 25
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 25
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 2
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Natural freq (Mode 1) = 5.78 (Hz)
Natural freq (Mode 2) = 30.66 (Hz)
real 0m0.566s
user 0m0.635s
sys 0m0.169s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_Composite_PyTest.py test;
+ python -u astros_Composite_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 15
Number of elements = 8
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 8
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - cantilever
No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
real 0m0.764s
user 0m0.686s
sys 0m0.177s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Composite_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/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 = 402
Number of elements = 763
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 763
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - wing
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - root
No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 5.92088 (Hz)
Natural freq (Mode 2) = 29.77630 (Hz)
Natural freq (Mode 3) = 39.17100 (Hz)
Natural freq (Mode 4) = 77.68370 (Hz)
Natural freq (Mode 5) = 99.80360 (Hz)
Natural freq (Mode 6) = 145.83600 (Hz)
Natural freq (Mode 7) = 177.88500 (Hz)
Natural freq (Mode 8) = 237.90000 (Hz)
Natural freq (Mode 9) = 280.01500 (Hz)
Natural freq (Mode 10) = 305.57400 (Hz)
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 402 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 402 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 402 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 402 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 402 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
real 0m36.350s
user 0m27.482s
sys 0m0.710s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_CompositeWingFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
real 0m1.083s
user 0m0.959s
sys 0m0.296s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ echo 'astros_MultipleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 16
Number of elements = 9
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 9
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 5
Load name - load_0
Load name - load_1
Load name - load_2
Load name - load_3
Load name - load_4
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 5
Analysis name - load_0
Analysis name - load_1
Analysis name - load_2
Analysis name - load_3
Analysis name - load_4
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
Writing analysis cards
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
real 0m0.925s
user 0m0.825s
sys 0m0.183s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_MultipleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Getting results for natural frequencies.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 293
Number of elements = 217
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes = 293
Total number of elements = 217
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 293
Number of elements = 217
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 217
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02335 (Hz)
Natural freq (Mode 2) = 0.02335 (Hz)
Natural freq (Mode 3) = 0.11619 (Hz)
Natural freq (Mode 4) = 0.11619 (Hz)
Natural freq (Mode 5) = 0.14468 (Hz)
Natural freq (Mode 6) = 0.14468 (Hz)
Natural freq (Mode 7) = 0.23352 (Hz)
Natural freq (Mode 8) = 0.23352 (Hz)
Natural freq (Mode 9) = 0.30497 (Hz)
Natural freq (Mode 10) = 0.30497 (Hz)
real 0m17.085s
user 0m24.334s
sys 0m4.584s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 6
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 6
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
real 0m0.761s
user 0m0.756s
sys 0m0.180s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
+ python -u astros_ThreeBarFreq_PyTest.py -outLevel=0
Getting results for natural frequencies.....
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 2
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Natural freq (Mode 1) = 86.13400 (Hz)
Natural freq (Mode 2) = 168.53300 (Hz)
real 0m0.881s
user 0m0.762s
sys 0m0.202s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarLinkDesign_PyTest.py test;
+ python -u astros_ThreeBarLinkDesign_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Getting FEA design variables.......
Number of design variables - 3
Design_Variable name - Bar1A
Design_Variable name - Bar2A
Design_Variable name - Bar3A
Design_Variable_Relation name - Bar1A
Design_Variable_Relation name - Bar2A
Design_Variable_Relation name - Bar3A
Number of design variable relations - 3
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 3
Design_Constraint name - stress1
Design_Constraint name - stress2
Design_Constraint name - stress3
Done getting FEA design constraints
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing design constraint cards
Writing load cards
Writing material cards
Writing property cards
Writing design variable cards
Running Astros......
Done running Astros!
real 0m0.719s
user 0m0.781s
sys 0m0.150s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarLinkDesign_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ python -u astros_ThreeBarMultiLoad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 2
Constraint name - conOne
No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
Constraint name - conTwo
No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - loadOne
Load name - loadTwo
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 2
Analysis name - analysisOne
Analysis name - analysisTwo
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
real 0m0.652s
user 0m0.709s
sys 0m0.151s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
+ echo 'astros_ThreeBar_PyTest.py test;'
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
real 0m0.657s
user 0m0.722s
sys 0m0.153s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ python -u astros_Trim_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - Body
Property name - Edge
Property name - Root
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - PointSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Getting FEA loads.......
Number of loads - 2
Load name - GravityLoad
No "groupName" specified for Load tuple GravityLoad, going to use load name
Load name - PointLoad
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
real 0m0.892s
user 0m0.904s
sys 0m0.234s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
Nastran
Mystran
Plato
=================================================
All tests pass!
=================================================
=================================================
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.7,CAPS/STRUCTURE,DARWIN_ARM64,viggen)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #191' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #192'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS