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Skipping 1,270 KB.. Full LogElemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards 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 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 Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 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 small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards .ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting surface mesh for body 1 (of 7) Getting surface mesh for body 2 (of 7) Getting surface mesh for body 3 (of 7) Getting surface mesh for body 4 (of 7) Getting surface mesh for body 5 (of 7) Getting surface mesh for body 6 (of 7) 1EFC EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1CCC EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1EFC EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1CCC EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 7 (of 7) Body 1 (of 7) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 2 (of 7) Number of nodes = 296 Number of elements = 588 Number of triangle elements = 588 Number of quadrilateral elements = 0 Body 3 (of 7) Number of nodes = 487 Number of elements = 970 Number of triangle elements = 970 Number of quadrilateral elements = 0 Body 4 (of 7) Number of nodes = 2048 Number of elements = 4096 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 7) Number of nodes = 139 Number of elements = 274 Number of triangle elements = 274 Number of quadrilateral elements = 0 Body 6 (of 7) Number of nodes = 624 Number of elements = 1248 Number of triangle elements = 1248 Number of quadrilateral elements = 0 Body 7 (of 7) Number of nodes = 489 Number of elements = 974 Number of triangle elements = 974 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4181 Total number of elements = 8342 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 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 Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 296, elements - 588 Body 3 number of surface: nodes - 487, elements - 970 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 139, elements - 274 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 489, elements - 974 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.002 Creating surface mesh ... Surface mesh seconds: 0.001 Recovering boundaries... Boundary recovery seconds: 0.001 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0 Recovering Delaunayness... Delaunay recovery seconds: 0.001 Refining mesh... Refinement seconds: 0.002 Smoothing vertices... Mesh smoothing seconds: 0.004 Improving mesh... Mesh improvement seconds: 0 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0 Total running seconds: 0.011 Statistics: Input points: 98 Input facets: 192 Input segments: 288 Input holes: 0 Input regions: 0 Mesh points: 102 Mesh tetrahedra: 248 Mesh faces: 592 Mesh faces on exterior boundary: 192 Mesh faces on input facets: 192 Mesh edges on input segments: 288 Steiner points inside domain: 4 Done meshing using TetGen! Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.02 Creating surface mesh ... Surface mesh seconds: 0.001 Recovering boundaries... Boundary recovery seconds: 0.003 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.001 Recovering Delaunayness... Delaunay recovery seconds: 0.005 Refining mesh... Refinement seconds: 0.027 Smoothing vertices... Mesh smoothing seconds: 0.026 Improving mesh... Mesh improvement seconds: 0.002 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0 Total running seconds: 0.085 Statistics: Input points: 296 Input facets: 588 Input segments: 882 Input holes: 0 Input regions: 0 Mesh points: 351 Mesh tetrahedra: 1092 Mesh faces: 2478 Mesh faces on exterior boundary: 588 Mesh faces on input facets: 588 Mesh edges on input segments: 882 Steiner points inside domain: 55 Done meshing using TetGen! Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.073 Creating surface mesh ... Surface mesh seconds: 0.001 Recovering boundaries... Boundary recovery seconds: 0.008 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.003 Recovering Delaunayness... Delaunay recovery seconds: 0.021 Refining mesh... 649 insertions, added 166 points, 7051 tetrahedra in queue. 216 insertions, added 8 points, 5268 tetrahedra in queue. 288 insertions, added 8 points, 170 tetrahedra in queue. 383 insertions, added 9 points, 311 tetrahedra in queue. 511 insertions, added 12 points, 90 tetrahedra in queue. Refinement seconds: 0.255 Smoothing vertices... Mesh smoothing seconds: 0.072 Improving mesh... Mesh improvement seconds: 0.003 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0 Total running seconds: 0.437 Statistics: Input points: 487 Input facets: 970 Input segments: 1455 Input holes: 0 Input regions: 0 Mesh points: 693 Mesh tetrahedra: 2764 Mesh faces: 6013 Mesh faces on exterior boundary: 970 Mesh faces on input facets: 970 Mesh edges on input segments: 1455 Steiner points inside domain: 206 Done meshing using TetGen! Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.577 Creating surface mesh ... Surface mesh seconds: 0.008 Recovering boundaries... Boundary recovery seconds: 0.026 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.015 Recovering Delaunayness... Delaunay recovery seconds: 0.145 Refining mesh... Refinement seconds: 0.717 Smoothing vertices... Mesh smoothing seconds: 0.34 Improving mesh... Mesh improvement seconds: 0.014 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.006 Total running seconds: 1.849 Statistics: Input points: 2048 Input facets: 4096 Input segments: 6144 Input holes: 0 Input regions: 0 Mesh points: 2918 Mesh tetrahedra: 11384 Mesh faces: 24816 Mesh faces on exterior boundary: 4096 Mesh faces on input facets: 4096 Mesh edges on input segments: 6144 Steiner points inside domain: 870 Done meshing using TetGen! Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0 Creating surface mesh ... Surface mesh seconds: 0.001 Recovering boundaries... Boundary recovery seconds: 0 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.001 Recovering Delaunayness... Delaunay recovery seconds: 0.001 Refining mesh... 185 insertions, added 42 points, 701 tetrahedra in queue. Refinement seconds: 0.007 Smoothing vertices... Mesh smoothing seconds: 0.005 Improving mesh... Mesh improvement seconds: 0.001 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001 Total running seconds: 0.017 Statistics: Input points: 139 Input facets: 274 Input segments: 411 Input holes: 0 Input regions: 0 Mesh points: 181 Mesh tetrahedra: 629 Mesh faces: 1395 Mesh faces on exterior boundary: 274 Mesh faces on input facets: 274 Mesh edges on input segments: 411 Steiner points inside domain: 42 Done meshing using TetGen! Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.056 Creating surface mesh ... Surface mesh seconds: 0.002 Recovering boundaries... Boundary recovery seconds: 0.006 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.002 Recovering Delaunayness... Delaunay recovery seconds: 0.008 Refining mesh... 831 insertions, added 210 points, 6107 tetrahedra in queue. 276 insertions, added 8 points, 0 tetrahedra in queue. Refinement seconds: 0.1 Smoothing vertices... Mesh smoothing seconds: 0.091 Improving mesh... Mesh improvement seconds: 0.005 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.002 Total running seconds: 0.272 Statistics: Input points: 624 Input facets: 1248 Input segments: 1872 Input holes: 0 Input regions: 0 Mesh points: 842 Mesh tetrahedra: 3132 Mesh faces: 6888 Mesh faces on exterior boundary: 1248 Mesh faces on input facets: 1248 Mesh edges on input segments: 1872 Steiner points inside domain: 218 Done meshing using TetGen! Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.054 Creating surface mesh ... Surface mesh seconds: 0.002 Recovering boundaries... Boundary recovery seconds: 0.051 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.001 Suppressing Steiner points ... Steiner suppression seconds: 0 Recovering Delaunayness... Delaunay recovery seconds: 0.019 Refining mesh... Refinement seconds: 0.056 Smoothing vertices... Mesh smoothing seconds: 0.036 Improving mesh... Mesh improvement seconds: 0.003 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001 Total running seconds: 0.225 Statistics: Input points: 489 Input facets: 974 Input segments: 1461 Input holes: 0 Input regions: 0 Mesh points: 678 Mesh tetrahedra: 2544 Mesh faces: 5575 Mesh faces on exterior boundary: 974 Mesh faces on input facets: 974 Mesh edges on input segments: 1461 Steiner points inside domain: 189 Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 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 Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 296, elements - 588 Body 3 number of surface: nodes - 487, elements - 970 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 139, elements - 274 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 489, elements - 974 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.003 Creating surface mesh ... Surface mesh seconds: 0 Recovering boundaries... Boundary recovery seconds: 0.001 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.001 Recovering Delaunayness... Delaunay recovery seconds: 0.001 Refining mesh... Refinement seconds: 0.001 Smoothing vertices... Mesh smoothing seconds: 0.003 Improving mesh... Mesh improvement seconds: 0 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001 Total running seconds: 0.011 Statistics: Input points: 98 Input facets: 192 Input segments: 288 Input holes: 0 Input regions: 1 Mesh points: 102 Mesh tetrahedra: 248 Mesh faces: 592 Mesh faces on exterior boundary: 192 Mesh faces on input facets: 192 Mesh edges on input segments: 288 Steiner points inside domain: 4 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.02 Creating surface mesh ... Surface mesh seconds: 0.001 Recovering boundaries... Boundary recovery seconds: 0.003 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.001 Recovering Delaunayness... Delaunay recovery seconds: 0.005 Refining mesh... Refinement seconds: 0.027 Smoothing vertices... Mesh smoothing seconds: 0.026 Improving mesh... Mesh improvement seconds: 0.002 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0 Total running seconds: 0.085 Statistics: Input points: 296 Input facets: 588 Input segments: 882 Input holes: 0 Input regions: 2 Mesh points: 351 Mesh tetrahedra: 1092 Mesh faces: 2478 Mesh faces on exterior boundary: 588 Mesh faces on input facets: 588 Mesh edges on input segments: 882 Steiner points inside domain: 55 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.074 Creating surface mesh ... Surface mesh seconds: 0.001 Recovering boundaries... Boundary recovery seconds: 0.009 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.003 Recovering Delaunayness... Delaunay recovery seconds: 0.018 Refining mesh... 649 insertions, added 166 points, 7051 tetrahedra in queue. 216 insertions, added 8 points, 5268 tetrahedra in queue. 288 insertions, added 8 points, 170 tetrahedra in queue. 383 insertions, added 9 points, 311 tetrahedra in queue. 511 insertions, added 12 points, 90 tetrahedra in queue. Refinement seconds: 0.209 Smoothing vertices... Mesh smoothing seconds: 0.073 Improving mesh... Mesh improvement seconds: 0.003 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001 Total running seconds: 0.391 Statistics: Input points: 487 Input facets: 970 Input segments: 1455 Input holes: 0 Input regions: 3 Mesh points: 693 Mesh tetrahedra: 2764 Mesh faces: 6013 Mesh faces on exterior boundary: 970 Mesh faces on input facets: 970 Mesh edges on input segments: 1455 Steiner points inside domain: 206 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.558 Creating surface mesh ... Surface mesh seconds: 0.007 Recovering boundaries... Boundary recovery seconds: 0.015 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.007 Recovering Delaunayness... Delaunay recovery seconds: 0.139 Refining mesh... Refinement seconds: 0.379 Smoothing vertices... Mesh smoothing seconds: 0.276 Improving mesh... Mesh improvement seconds: 0.013 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.002 Total running seconds: 1.396 Statistics: Input points: 2048 Input facets: 4096 Input segments: 6144 Input holes: 0 Input regions: 4 Mesh points: 2900 Mesh tetrahedra: 11327 Mesh faces: 24702 Mesh faces on exterior boundary: 4096 Mesh faces on input facets: 4096 Mesh edges on input segments: 6144 Steiner points inside domain: 852 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0 Creating surface mesh ... Surface mesh seconds: 0.001 Recovering boundaries... Boundary recovery seconds: 0 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.001 Recovering Delaunayness... Delaunay recovery seconds: 0.001 Refining mesh... 185 insertions, added 42 points, 701 tetrahedra in queue. Refinement seconds: 0.007 Smoothing vertices... Mesh smoothing seconds: 0.005 Improving mesh... Mesh improvement seconds: 0 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001 Total running seconds: 0.016 Statistics: Input points: 139 Input facets: 274 Input segments: 411 Input holes: 0 Input regions: 5 Mesh points: 181 Mesh tetrahedra: 629 Mesh faces: 1395 Mesh faces on exterior boundary: 274 Mesh faces on input facets: 274 Mesh edges on input segments: 411 Steiner points inside domain: 42 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.056 Creating surface mesh ... Surface mesh seconds: 0.001 Recovering boundaries... Boundary recovery seconds: 0.006 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Warning: The 5-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.002 Recovering Delaunayness... Delaunay recovery seconds: 0.008 Refining mesh... 831 insertions, added 210 points, 6107 tetrahedra in queue. 276 insertions, added 8 points, 0 tetrahedra in queue. Refinement seconds: 0.091 Smoothing vertices... Mesh smoothing seconds: 0.067 Improving mesh... Mesh improvement seconds: 0.003 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001 Total running seconds: 0.235 Statistics: Input points: 624 Input facets: 1248 Input segments: 1872 Input holes: 0 Input regions: 6 Mesh points: 842 Mesh tetrahedra: 3132 Mesh faces: 6888 Mesh faces on exterior boundary: 1248 Mesh faces on input facets: 1248 Mesh edges on input segments: 1872 Steiner points inside domain: 218 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.049 Creating surface mesh ... Surface mesh seconds: 0.002 Recovering boundaries... Boundary recovery seconds: 0.05 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Warning: The 5-th region point lies outside the convex hull. Warning: The 6-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.002 Suppressing Steiner points ... Steiner suppression seconds: 0 Recovering Delaunayness... Delaunay recovery seconds: 0.019 Refining mesh... Refinement seconds: 0.054 Smoothing vertices... Mesh smoothing seconds: 0.036 Improving mesh... Mesh improvement seconds: 0.003 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001 Total running seconds: 0.218 Statistics: Input points: 489 Input facets: 974 Input segments: 1461 Input holes: 0 Input regions: 7 Mesh points: 678 Mesh tetrahedra: 2544 Mesh faces: 5575 Mesh faces on exterior boundary: 974 Mesh faces on input facets: 974 Mesh edges on input segments: 1461 Steiner points inside domain: 189 Done meshing using TetGen! EMapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9625, elements - 19242 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9625, elements - 19242 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9625, elements - 19242 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9625, elements - 19242 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9625, elements - 19242 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! 57 File(s) copied Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 3 File(s) copied 1 File(s) copied Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7130, elements - 14252 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9625 Number of elements = 19242 Number of triangle elements = 19242 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9625 Total number of elements = 19242 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9625, elements - 19242 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary STL file .... Finished writing Binary STL file Writing Binary VTK file .... Finished writing Binary VTK file Writing FAST file .... Finished writing FAST file Writing ASCII STL file .... Finished writing ASCII STL file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9625, elements - 19242 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary STL file .... Finished writing Binary STL file Writing Binary VTK file .... Finished writing Binary VTK file Writing FAST file .... Finished writing FAST file Writing ASCII STL file .... Finished writing ASCII STL file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing vtk file .... Writing vtk general file .... Finished writing vtk file . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL .Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL .Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL .Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL .Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL .Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL .Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL .Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL .Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL 39 File(s) copied 4 File(s) copied Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL ..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 = Rib_Root_Point, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1220 Number of elements = 2680 Number of triangle elements = 2680 Number of quadrilateral elements = 0 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 = 1221 Total number of elements = 2680 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 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 = Rib_Root_Point, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1220 Number of elements = 2680 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 2680 Elemental Quad4 = 0 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 = 1221 Combined Number of elements = 2681 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 2680 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 6 Property name - Rib_Root Property name - Rib_Root_Point Property name - Ribs Property name - Skin Property name - Spar1 Property name - Spar2 Done getting FEA properties Updating mesh element types based on properties input 'Smart_Restart' is ON Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting vortex lattice control surface data VLM control surface name - CntrlLE VLM control surface name - CntrlTE Done getting vortex lattice control surface data Getting FEA vortex lattice mesh Getting ZAERO UAIC Configurations....... Number of UAIC Configurations - 2 UAIC Configuration: climb, id = 1 - Mach Number : 0.200000 - Reduced Freq: [0.020000, ... , 0.250000] UAIC Configuration: cruise, id = 2 - Mach Number : 0.700000 - Reduced Freq: [0.040000, ... , 0.350000] Getting ZAERO Analysis Subcases....... Number of Analysis Subcases - 2 Analysis Subcase: FlutterCruise, id = 1 - Discipline : flutter - UAIC : cruise Analysis Subcase: Trim, id = 2 - Discipline : Trim - UAIC : climb Getting ZAERO Trim Variables....... Number of Trim Variables - 2 Trim Variable: ANGLEA - Label : ALPHA - Value : free Trim Variable: URDD3 - Label : NZ - Value : 1.0 Updating StaticAeroelastic subcase: Trim - vectorToCG -> [0.345898, 1.652951, -0.041403] - weight -> 476456.149985 - weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813292, 6179.981375, 19723.152207, 370546.335524] . ====================================================================== ERROR: test_journal (test_aflr2.TestAFLR2.test_journal) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr2.py", line 226, in test_journal line_total = self.run_journal(myProblem, -1) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr2.py", line 175, in run_journal aflr2.runAnalysis(); line += 1 ^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x0000000D00000016 ====================================================================== ERROR: test_phase (test_aflr2.TestAFLR2.test_phase) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr2.py", line 115, in test_phase NumberOfNode_1 = aflr2.output.NumberOfNode ^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1950, in __getattr__ return self._capsItems[name].value ^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1880, in value return self._valObj.getValue() ^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 1968, in getValue if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr2AIM.c:377 in aimUpdateState(): Error: No Bodies! ================================================================================ ====================================================================== ERROR: test_reenter (test_aflr2.TestAFLR2.test_reenter) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr2.py", line 73, in test_reenter myAnalysis.input.Mesh_Format = Mesh_Formats ^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1705, in __setattr__ self._capsItems[name].value = value ^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1573, in value self._valObj.setValue(val) File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2281, in setValue _raiseStatus(stat, msg="Trying to set value for: {!r}".format(name), errors=capsErrs(nErr, errs)) File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SHAPEERR: Trying to set value for: 'Mesh_Format': ================================================================================ ================================================================================ ====================================================================== ERROR: test_setInput (test_aflr2.TestAFLR2.test_setInput) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr2.py", line 61, in test_setInput myAnalysis.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x0000000100000000 ====================================================================== ERROR: test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 175, in test_Multiple_Mesh aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_all (test_aflr3.TestAFLR3.test_all) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 395, in test_all aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_box (test_aflr3.TestAFLR3.test_box) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 207, in test_box aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0xFFFFFFFFFFFFFFFF ====================================================================== ERROR: test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 343, in test_boxhole aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_bullet (test_aflr3.TestAFLR3.test_bullet) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 370, in test_bullet aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0xFFFFFFFFFFFFFFE3 ====================================================================== ERROR: test_cone (test_aflr3.TestAFLR3.test_cone) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 262, in test_cone aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 235, in test_cylinder aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 420, in test_faceMatch aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0xFFFFFFFFFFFFFFFF ====================================================================== ERROR: test_journal (test_aflr3.TestAFLR3.test_journal) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 679, in test_journal line_total = self.run_journal(myProblem, -1) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 632, in run_journal aflr3.runAnalysis(); line += 1 ^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0xFFFFFFFFFFFFFFFF ====================================================================== ERROR: test_phase (test_aflr3.TestAFLR3.test_phase) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 544, in test_phase VolNumberOfNode_1 = aflr3.output.NumberOfNode ^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1950, in __getattr__ return self._capsItems[name].value ^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1880, in value return self._valObj.getValue() ^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 1964, in getValue stat = _caps.caps_getValue(self._obj, ctypes.byref(vtype), ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0xFFFFFFFFFFFFFFFF ====================================================================== ERROR: test_reenter (test_aflr3.TestAFLR3.test_reenter) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 82, in test_reenter aflr3.input.Mesh_Format = Mesh_Formats ^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1705, in __setattr__ self._capsItems[name].value = value ^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1573, in value self._valObj.setValue(val) File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2281, in setValue _raiseStatus(stat, msg="Trying to set value for: {!r}".format(name), errors=capsErrs(nErr, errs)) File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SHAPEERR: Trying to set value for: 'Mesh_Format': ================================================================================ ================================================================================ ====================================================================== ERROR: test_sphere (test_aflr3.TestAFLR3.test_sphere) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 316, in test_sphere aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0xFFFFFFFFFFFFFFFF ====================================================================== ERROR: test_torus (test_aflr3.TestAFLR3.test_torus) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 289, in test_torus aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0xFFFFFFFFFFFFFFFF ====================================================================== ERROR: test_transp (test_aflr3.TestAFLR3.test_transp) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 133, in test_transp aflr3.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0xFFFFFFFFFFFFFFFF ====================================================================== ERROR: test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 122, in test_MultiBody_quad myAnalysis.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! ================================================================================ ====================================================================== ERROR: test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 94, in test_SingleBody_output myAnalysis.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! ================================================================================ ====================================================================== ERROR: test_all (test_aflr4.TestAFLR4.test_all) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 305, in test_all aflr4.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x0000002900000028 ====================================================================== ERROR: test_box (test_aflr4.TestAFLR4.test_box) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 175, in test_box aflr4.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! ================================================================================ ====================================================================== ERROR: test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 265, in test_boxhole aflr4.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x0000013100000130 ====================================================================== ERROR: test_bullet (test_aflr4.TestAFLR4.test_bullet) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 285, in test_bullet aflr4.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! ================================================================================ ====================================================================== ERROR: test_cone (test_aflr4.TestAFLR4.test_cone) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 209, in test_cone aflr4.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x000002D7000002D6 ====================================================================== ERROR: test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 192, in test_cylinder aflr4.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! ================================================================================ ====================================================================== ERROR: test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 328, in test_faceMatch aflr4.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x000002100000020F ====================================================================== ERROR: test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 53, in test_invalid_Mesh_Lenght_Scale myAnalysis.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x000002100000020F ====================================================================== ERROR: test_journal (test_aflr4.TestAFLR4.test_journal) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 577, in test_journal line_total = self.run_journal(myProblem, -1) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 531, in run_journal aflr4.runAnalysis(); line += 1 ^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x000002100000020F ====================================================================== ERROR: test_phase (test_aflr4.TestAFLR4.test_phase) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 477, in test_phase NumberOfNode_1 = aflr4.output.NumberOfNode ^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1950, in __getattr__ return self._capsItems[name].value ^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1880, in value return self._valObj.getValue() ^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 1964, in getValue stat = _caps.caps_getValue(self._obj, ctypes.byref(vtype), ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x000002100000020F ====================================================================== ERROR: test_reenter (test_aflr4.TestAFLR4.test_reenter) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 149, in test_reenter myAnalysis.input.Mesh_Format = Mesh_Formats ^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1705, in __setattr__ self._capsItems[name].value = value ^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 1573, in value self._valObj.setValue(val) File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2281, in setValue _raiseStatus(stat, msg="Trying to set value for: {!r}".format(name), errors=capsErrs(nErr, errs)) File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SHAPEERR: Trying to set value for: 'Mesh_Format': ================================================================================ ================================================================================ ====================================================================== ERROR: test_sphere (test_aflr4.TestAFLR4.test_sphere) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 246, in test_sphere aflr4.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2899, in execute stat = _caps.caps_execute(self._obj, ctypes.byref(status), ctypes.byref(nErr), ctypes.byref(errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ OSError: exception: access violation reading 0x000002100000020F ====================================================================== ERROR: test_torus (test_aflr4.TestAFLR4.test_torus) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 227, in test_torus aflr4.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! ================================================================================ ====================================================================== ERROR: test_Output (test_cbaero.TestCBAERO.test_Output) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_cbaero.py", line 95, in test_Output cbaero.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_inputs (test_cbaero.TestCBAERO.test_inputs) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_cbaero.py", line 78, in test_inputs cbaero.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_inputs (test_su2.TestSU2.test_inputs) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 102, in test_inputs self.myAnalysis.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 transferValues for Mesh from Volume_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_journal (test_su2.TestSU2.test_journal) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 357, in test_journal line_total = self.run_journal(myProblem, -1) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 310, in run_journal su2.preAnalysis(); line += 1 ^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 transferValues for Mesh from Volume_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_phase (test_su2.TestSU2.test_phase) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 226, in test_phase su2.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 transferValues for Mesh from Volume_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_reenter (test_su2.TestSU2.test_reenter) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 152, in test_reenter self.myAnalysis.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 transferValues for Mesh from Volume_Mesh = -330 ================================================================================ ====================================================================== ERROR: test_units (test_su2.TestSU2.test_units) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 194, in test_units myAnalysis.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ aflr4AIM.c:996 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 transferValues for Mesh from Volume_Mesh = -330 ================================================================================ ====================================================================== ERROR: tearDownClass (test_su2.TestSU2) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 48, in tearDownClass cls.cleanUp() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 56, in cleanUp shutil.rmtree(dir) File "C:\Users\jenkins\ESP_Python-3.11.6\Lib\shutil.py", line 759, in rmtree return _rmtree_unsafe(path, onerror) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\ESP_Python-3.11.6\Lib\shutil.py", line 617, in _rmtree_unsafe _rmtree_unsafe(fullname, onerror) File "C:\Users\jenkins\ESP_Python-3.11.6\Lib\shutil.py", line 617, in _rmtree_unsafe _rmtree_unsafe(fullname, onerror) File "C:\Users\jenkins\ESP_Python-3.11.6\Lib\shutil.py", line 622, in _rmtree_unsafe onerror(os.unlink, fullname, sys.exc_info()) File "C:\Users\jenkins\ESP_Python-3.11.6\Lib\shutil.py", line 620, in _rmtree_unsafe os.unlink(fullname) PermissionError: [WinError 32] The process cannot access the file because it is being used by another process: 'su2_problem\\Scratch\\capsRestart\\capsJournal' ====================================================================== ERROR: test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_tetgen.py", line 126, in test_Multiple_Mesh tetgen.runAnalysis() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_IOERR: ================================================================================ tetgenAIM.cpp:1011 in aimPostAnalysis(): Error: Failed to open 'tetgen_0.txt'! ================================================================================ ====================================================================== FAIL: test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 142, in test_invalidBoundary self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND") AssertionError: 'CAPS_SOURCEERR' != 'CAPS_NOTFOUND' - CAPS_SOURCEERR + CAPS_NOTFOUND ====================================================================== FAIL: test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ---------------------------------------------------------------------- Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_Beta\7.8\WIN64.2022\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 124, in test_invalidBoundaryName self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND") AssertionError: 'CAPS_SOURCEERR' != 'CAPS_NOTFOUND' - CAPS_SOURCEERR + CAPS_NOTFOUND ---------------------------------------------------------------------- Ran 140 tests in 774.642s FAILED (failures=2, errors=42, skipped=26) NMAKE : fatal error U1077: 'python -u -m unittest discover' : return code '0x1' Stop. Build step 'Conditional step (single)' marked build as failure [GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE' [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Skipped based on build state FAILURE Finished: FAILURE