The Jenkins Controller is preparing for shutdown. No new builds can be started.
Skipping 532 KB.. Full LogWarning: 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 = 49 Number of elements = 36 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 36 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 Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Warning: No loads specified for case EigenAnalysis!!!! Writing mass increment cards Writing analysis cards, 0 Writing combined constraint cards Writing constraint cards Writing material cards Writing property cards Writing coordinate system cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.447s user 0m0.515s sys 0m0.584s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_Composite_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_Flutter_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_Flutter_15degree.py test; + python -u nastran_Flutter_15degree.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 133 Number of elements = 108 Number of triangle elements = 0 Number of quadrilateral elements = 108 Body 2 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 134 Total number of elements = 108 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 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 = 133 Number of elements = 108 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 108 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 = 134 Combined Number of elements = 109 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 108 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 = 133 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 7 automatic connections were made for capsConnect Root (node id 134) Done getting FEA connections Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Flutter Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No loads specified for case Flutter!!!! Writing mass increment cards Writing aero card Writing analysis cards, 0 Writing constraint ADD cards Writing constraint cards Writing material cards Writing property cards Writing aeroelastic cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.589s user 0m0.567s sys 0m0.624s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_Flutter_15degree.py passed (as expected) ================================================= ================================================= + echo 'nastran_MultiLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_MultiLoadCase_PyTest.py test; + python -u nastran_MultiLoadCase_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, 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 = 49 Number of elements = 36 Number of triangle elements = 0 Number of quadrilateral elements = 36 ---------------------------- Total number of nodes = 49 Total number of elements = 36 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 = 49 Number of elements = 36 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 36 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 Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 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 Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran 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 mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing combined constraint cards Writing load ADD cards Writing combined constraint cards Writing load ADD cards Writing combined constraint cards Writing load ADD cards Writing combined constraint cards Writing load ADD cards Writing combined constraint cards Writing load cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.460s user 0m0.613s sys 0m0.660s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_MultiLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_OptimizationMultiLoad_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_OptimizationMultiLoad_PyTest.py test; + python -u nastran_OptimizationMultiLoad_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, 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 = 49 Number of elements = 36 Number of triangle elements = 0 Number of quadrilateral elements = 36 ---------------------------- Total number of nodes = 49 Total number of elements = 36 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 = 49 Number of elements = 36 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 36 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 - 2 Load name - load_0 Load name - load_1 Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - materialDV Design_Variable name - propertyDV Design_Variable_Relation name - materialDVR Name madeupium not found in attribute map!!!! Design_Variable_Relation name - propertyDVR Number of design variable relations - 2 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 2 Design_Constraint name - stress1 Design_Constraint name - stress2 Done getting FEA design constraints Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 2 Analysis name - load_0 Analysis name - load_1 Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran 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!!!! Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing combined constraint cards Writing design constraint ADD cards Writing load ADD cards Writing combined constraint cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running NASTRAN! real 0m1.245s user 0m0.547s sys 0m0.628s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_OptimizationMultiLoad_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt + echo 'nastran_PlateMisc_PyTest.py test;' nastran_PlateMisc_PyTest.py test; + python -u nastran_PlateMisc_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, 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 = 49 Number of elements = 36 Number of triangle elements = 0 Number of quadrilateral elements = 36 ---------------------------- Total number of nodes = 49 Total number of elements = 36 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 = 49 Number of elements = 36 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 36 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 - 3 Load name - moment Load name - pressure Load name - thermal Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - pltvar Number of design variable relations - 0 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 1 Design_Constraint name - pltcon Done getting FEA design constraints Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.291s user 0m0.588s sys 0m0.633s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_PlateMisc_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt + echo 'nastran_PyTest.py test;' nastran_PyTest.py test; + python -u nastran_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt 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 = 2091 Number of elements = 1845 Number of triangle elements = 0 Number of quadrilateral elements = 1845 ---------------------------- Total number of nodes = 2091 Total number of elements = 1845 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 = 2091 Number of elements = 1845 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 1845 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 Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Warning: No loads specified for case EigenAnalysis!!!! Writing mass increment cards Writing analysis cards, 0 Writing combined constraint cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! Getting results for natural frequencies..... Reading Nastran FO6 file - extracting Eigen-Values! Number of Eigen-Values = 18 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 Loading Eigen-Value = 10 Loading Eigen-Value = 10 Loading Eigen-Value = 10 Loading Eigen-Value = 10 Loading Eigen-Value = 10 Loading Eigen-Value = 10 Loading Eigen-Value = 10 Loading Eigen-Value = 10 Natural freq (Mode 1) = 0.02165 (Hz) Natural freq (Mode 2) = 0.02165 (Hz) Natural freq (Mode 3) = 0.10665 (Hz) Natural freq (Mode 4) = 0.10665 (Hz) Natural freq (Mode 5) = 0.13547 (Hz) Natural freq (Mode 6) = 0.13547 (Hz) Natural freq (Mode 7) = 0.23092 (Hz) Natural freq (Mode 8) = 0.23092 (Hz) Natural freq (Mode 9) = 0.27609 (Hz) Natural freq (Mode 10) = 0.27609 (Hz) Natural freq (Mode 11) = 0.00000 (Hz) Natural freq (Mode 12) = 0.00000 (Hz) Natural freq (Mode 13) = 0.00000 (Hz) Natural freq (Mode 14) = 0.00000 (Hz) Natural freq (Mode 15) = 0.00000 (Hz) Natural freq (Mode 16) = 0.00000 (Hz) Natural freq (Mode 17) = 0.00000 (Hz) Natural freq (Mode 18) = 0.00000 (Hz) real 0m9.637s user 0m11.450s sys 0m3.049s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_SingleLoadCase_PyTest.py test; + python -u nastran_SingleLoadCase_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, 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 = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 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 = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 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 Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.221s user 0m0.572s sys 0m0.613s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBarDesign_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_ThreeBarDesign_PyTest.py test; + python -u nastran_ThreeBarDesign_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 0 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 Getting FEA design variables....... Number of design variables - 3 Design_Variable name - Bar1A Design_Variable name - Bar2A Design_Variable name - Bar3A Design_Variable_Relation name - Bar1A Design_Variable_Relation name - Bar2A Design_Variable_Relation name - Bar3A Number of design variable relations - 3 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 3 Design_Constraint name - stress1 Design_Constraint name - stress2 Design_Constraint name - stress3 Done getting FEA design constraints Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.272s user 0m0.516s sys 0m0.675s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBarDesign_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBarFreq_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_ThreeBarFreq_PyTest.py test; + python -u nastran_ThreeBarFreq_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 0 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 Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Warning: No loads specified for case EigenAnalysis!!!! Writing mass increment cards Writing analysis cards, 0 Writing combined constraint cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.236s user 0m0.531s sys 0m0.606s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBarFreq_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBarLinkDesign_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_ThreeBarLinkDesign_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt + python -u nastran_ThreeBarLinkDesign_PyTest.py -outLevel=0 -noAnalysis WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 0 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 Getting FEA design variables....... Number of design variables - 3 Design_Variable name - Bar1A Design_Variable name - Bar2A Design_Variable name - Bar3A Design_Variable_Relation name - Bar1A Design_Variable_Relation name - Bar2A Design_Variable_Relation name - Bar3A Number of design variable relations - 3 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 3 Design_Constraint name - stress1 Design_Constraint name - stress2 Design_Constraint name - stress3 Done getting FEA design constraints Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.349s user 0m0.563s sys 0m0.616s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBarLinkDesign_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBarMultiLoad_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_ThreeBarMultiLoad_PyTest.py test; + python -u nastran_ThreeBarMultiLoad_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 0 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 Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 2 Analysis name - caseOne Analysis name - caseTwo Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.275s user 0m0.547s sys 0m0.607s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBarMultiLoad_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_ThreeBar_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_ThreeBar_PyTest.py test; + python -u nastran_ThreeBar_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 4 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4 Total number of elements = 0 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 Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.367s user 0m0.528s sys 0m0.653s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_ThreeBar_PyTest.py passed (as expected) ================================================= ================================================= + echo 'nastran_Trim_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt nastran_Trim_15degree.py test; + python -u nastran_Trim_15degree.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 117 Number of elements = 96 Number of triangle elements = 0 Number of quadrilateral elements = 96 Body 2 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 118 Total number of elements = 96 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 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 = 117 Number of elements = 96 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 96 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 = 118 Combined Number of elements = 97 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 96 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 = 117 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 9 automatic connections were made for capsConnect Root (node id 118) Done getting FEA connections Getting FEA loads....... Number of loads - 2 Load name - GravityLoad No "groupName" specified for Load tuple GravityLoad, going to use load name Load name - PointLoad Done getting FEA loads Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim Done getting FEA analyses Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing mass increment set Writing Nastran instruction file.... Warning: No loads specified for case Trim, assuming all loads are applied!!!! Writing mass increment cards Writing aeros card Writing aestat cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Done writing aeroelastic cards Done writing files Running Nastran...... Done running Nastran! real 0m1.251s user 0m0.601s sys 0m0.616s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case nastran_Trim_15degree.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: abaqus Nastran Mystran Plato ================================================= All tests pass! ================================================= ================================================= ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest ++ ./execute_PyTestRegression.sh STRUCTURE ================================================= Legacy Using python : /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/venv/bin/python ================================================= Running.... STRUCTURE PyTests ================================================= + rm -rf masstran_PyTest + echo 'masstran_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt No analysis directory provided - defaulting to altName 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 triangle elements = 0 Number of quadrilateral elements = 798 ---------------------------- Total number of nodes = 1159 Total number of elements = 798 No analysis directory provided - defaulting to altName 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 Getting results mass properties..... Area 3.428666259747 Mass 5383.006027803 Centroid [1.222256036874, 0.1634981473778, -4.234492548615e-11] CG [1.222256036874, 0.1634981473778, -4.234574416087e-11] Ixx 22133.97306033 Iyy 23448.30046709 Izz 1389.213122582 Ixy 164.2055275657 Ixz -7.454849830627e-06 Iyz 1.707682983295e-06 I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454849830627e-06, 1.707682983295e-06] II [[22133.97306033, -164.2055275657, 7.454849830627e-06], [-164.2055275657, 23448.30046709, -1.707682983295e-06], [7.454849830627e-06, -1.707682983295e-06, 1389.213122582]] WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m9.778s user 0m11.230s sys 0m2.775s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf masstran_AGARD445_PyTest + echo 'masstran_AGARD445_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt masstran_AGARD445_PyTest.py test; + python -u masstran_AGARD445_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt No analysis directory provided - defaulting to altName Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = constEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = yatesPlate, index = 1 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 Getting results mass properties..... 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]] WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.839s user 0m0.483s sys 0m0.342s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf hsm_SingleLoadCase_PyTest + echo 'hsm_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt hsm_SingleLoadCase_PyTest.py test; + python -u hsm_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.282s user 0m0.903s sys 0m0.231s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf hsm_CantileverPlate_PyTest + echo 'hsm_CantileverPlate_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt hsm_CantileverPlate_PyTest.py test; + python -u hsm_CantileverPlate_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = plate, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - plate Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plateTip, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Creating HSM BEM Getting quads for BEM! Number of nodal coordinates = 40 Number of elements = 51 Elemental Tria3 = 0 Elemental Quad4 = 27 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA loads....... Number of loads - 1 Load name - appliedLoad Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 9 MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 4 ->HSMSOL Matrix Non-zero Entries = 1313 Converging HSM equation system ... iter dr dd dp rlx max 1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00) 1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.03 0.00) 1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.03 0.00) 2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00) 3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00) 4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00) 5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.03 0.00) 6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.03 0.00) 7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.07 0.00) 8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.10 0.00) 9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.00 0.00) 10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) iter dr dd dp rlx max 11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.10 0.00) 11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00) 12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00) 13* 0.336E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00) 15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.10 0.00) 16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00) 17 0.558E-15 0.304E-14 0.603E-15 1.000 ddx @ ( 1.00 0.00 0.00) Converging n vectors ... it = 1 dn = 0.193E+01 rlx = 1.000 ( 12 ) it = 2 dn = 0.435E-15 rlx = 1.000 ( 28 ) Converging e1,e2 vectors ... it = 1 de = 0.285E+01 rlx = 0.351 ( 24 ) it = 2 de = 0.292E+01 rlx = 0.342 ( 34 ) it = 3 de = 0.226E+01 rlx = 0.442 ( 34 ) it = 4 de = 0.151E+01 rlx = 0.660 ( 34 ) it = 5 de = 0.665E+00 rlx = 1.000 ( 34 ) it = 6 de = 0.609E-01 rlx = 1.000 ( 34 ) it = 7 de = 0.573E-04 rlx = 1.000 ( 34 ) it = 8 de = 0.478E-13 rlx = 1.000 ( 34 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMCantileverPlate.dat WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.995s user 0m0.720s sys 0m0.227s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_Aeroelastic_PyTest + echo 'astros_Aeroelastic_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_Aeroelastic_PyTest.py test; + python -u astros_Aeroelastic_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Wing, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 286 Number of elements = 386 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 92 Elemental Quad4 = 294 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 = 287 Combined Number of elements = 387 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 92 Combined Elemental Quad4 = 294 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 48 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set 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 30 automatic connections were made for capsConnect Rib_Root (node id 287) 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 Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m17.104s user 0m22.290s sys 0m3.037s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_AGARD445_PyTest + echo 'astros_AGARD445_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_AGARD445_PyTest.py test; + python -u astros_AGARD445_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 = constEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping 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 Running Astros...... Done running Astros! Getting results natural frequencies..... 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) WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.368s user 0m0.672s sys 0m0.509s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_Composite_PyTest + echo 'astros_Composite_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_Composite_PyTest.py test; + python -u astros_Composite_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 Running Astros...... Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.560s user 0m0.811s sys 0m0.551s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_Composite_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_CompositeWingFreq_PyTest + echo 'astros_CompositeWingFreq_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_CompositeWingFreq_PyTest.py test; + python -u astros_CompositeWingFreq_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = wing, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - wing Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = wing, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = wing, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 429 Number of elements = 817 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 817 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Aluminum No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic" Material name - Graphite_epoxy Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - root No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards Running Astros...... Done running Astros! Getting results for natural frequencies..... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Natural freq (Mode 1) = 5.91949 (Hz) Natural freq (Mode 2) = 29.79990 (Hz) Natural freq (Mode 3) = 39.10550 (Hz) Natural freq (Mode 4) = 77.71580 (Hz) Natural freq (Mode 5) = 99.79550 (Hz) Natural freq (Mode 6) = 146.97500 (Hz) Natural freq (Mode 7) = 176.90300 (Hz) Natural freq (Mode 8) = 235.53300 (Hz) Natural freq (Mode 9) = 274.42600 (Hz) Natural freq (Mode 10) = 311.35900 (Hz) No variable name provided - all variables will be writen to file Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 429 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 429 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 429 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 429 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 429 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsBound.writeTecplot' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].writeTecplot'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 1m34.608s user 1m10.360s sys 0m2.743s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_CompositeWingFreq_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_Flutter_15degree + echo 'astros_Flutter_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_Flutter_15degree.py test; + python -u astros_Flutter_15degree.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m3.339s user 0m1.121s sys 0m0.692s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected) ================================================= ================================================= + rm -rf astros_MultipleLoadCase_PyTest + echo 'astros_MultipleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_MultipleLoadCase_PyTest.py test; + python -u astros_MultipleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m2.749s user 0m0.913s sys 0m0.537s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_MultipleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_PyTest + echo 'astros_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_PyTest.py test; + python -u astros_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt No analysis directory provided - defaulting to altName 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 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 Running Astros...... Done running Astros! Getting results for natural frequencies..... 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) WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m35.884s user 0m28.411s sys 0m3.799s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_SingleLoadCase_PyTest + echo 'astros_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_SingleLoadCase_PyTest.py test; + python -u astros_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.375s user 0m0.700s sys 0m0.451s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_ThreeBarFreq_PyTest + echo 'astros_ThreeBarFreq_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_ThreeBarFreq_PyTest.py test; + python -u astros_ThreeBarFreq_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Running Astros...... Done running Astros! Getting results for natural frequencies..... 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) WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.496s user 0m0.679s sys 0m0.462s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_ThreeBarMultiLoad_PyTest + echo 'astros_ThreeBarMultiLoad_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_ThreeBarMultiLoad_PyTest.py test; + python -u astros_ThreeBarMultiLoad_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 Running Astros...... Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m2.570s user 0m0.679s sys 0m0.486s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_ThreeBar_PyTest + echo 'astros_ThreeBar_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_ThreeBar_PyTest.py test; + python -u astros_ThreeBar_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 Running Astros...... Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.708s user 0m0.653s sys 0m0.433s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_Trim_15degree + echo 'astros_Trim_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_Trim_15degree.py test; + python -u astros_Trim_15degree.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/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 Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.742s user 0m1.042s sys 0m0.583s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Legacy Did not run examples for: Nastran Mystran ================================================= All tests pass! ================================================= ================================================= [Execution node] check if [macys_VM] is in [[windows10x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64') [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_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64') [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_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64') [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_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64') [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_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.7,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWIN64,buildnode=macys_VM #649'. [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