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
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)
1FA0 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1E1C EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1FA0 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E1C 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: 0.003
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
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
Total running seconds: 0.01
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: 0.002
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.001
Recovering Delaunayness...
Delaunay recovery seconds: 0.006
Refining mesh...
Refinement seconds: 0.024
Smoothing vertices...
Mesh smoothing seconds: 0.024
Improving mesh...
Mesh improvement seconds: 0.002
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0
Total running seconds: 0.08
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: 0.081
Creating surface mesh ...
Surface mesh seconds: 0.002
Recovering boundaries...
Boundary recovery seconds: 0.012
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.002
Recovering Delaunayness...
Delaunay recovery seconds: 0.024
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: 0.2
Smoothing vertices...
Mesh smoothing seconds: 0.073
Improving mesh...
Mesh improvement seconds: 0.004
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.001
Total running seconds: 0.399
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: 0.473
Creating surface mesh ...
Surface mesh seconds: 0.006
Recovering boundaries...
Boundary recovery seconds: 0.018
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.007
Recovering Delaunayness...
Delaunay recovery seconds: 0.206
Refining mesh...
Refinement seconds: 0.479
Smoothing vertices...
Mesh smoothing seconds: 0.506
Improving mesh...
Mesh improvement seconds: 0.013
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.003
Total running seconds: 1.711
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: 0.001
Creating surface mesh ...
Surface mesh seconds: 0.001
Recovering boundaries...
Boundary recovery seconds: 0.002
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0
Recovering Delaunayness...
Delaunay recovery seconds: 0.001
Refining mesh...
185 insertions, added 42 points, 701 tetrahedra in queue.
Refinement seconds: 0.011
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: 0.024
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: 0.055
Creating surface mesh ...
Surface mesh seconds: 0.002
Recovering boundaries...
Boundary recovery seconds: 0.009
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.004
Recovering Delaunayness...
Delaunay recovery seconds: 0.014
Refining mesh...
831 insertions, added 210 points, 6107 tetrahedra in queue.
276 insertions, added 8 points, 0 tetrahedra in queue.
Refinement seconds: 0.271
Smoothing vertices...
Mesh smoothing seconds: 0.103
Improving mesh...
Mesh improvement seconds: 0.003
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.004
Total running seconds: 0.467
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: 0.063
Creating surface mesh ...
Surface mesh seconds: 0.001
Recovering boundaries...
Boundary recovery seconds: 0.054
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: 0.037
Improving mesh...
Mesh improvement seconds: 0.003
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.001
Total running seconds: 0.237
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: 0.018
Creating surface mesh ...
Surface mesh seconds: 0.001
Recovering boundaries...
Boundary recovery seconds: 0.002
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: 0.024
Smoothing vertices...
Mesh smoothing seconds: 0.023
Improving mesh...
Mesh improvement seconds: 0.002
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0
Total running seconds: 0.076
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: 0.07
Creating surface mesh ...
Surface mesh seconds: 0.002
Recovering boundaries...
Boundary recovery seconds: 0.008
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: 0.016
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: 0.191
Smoothing vertices...
Mesh smoothing seconds: 0.068
Improving mesh...
Mesh improvement seconds: 0.003
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0
Total running seconds: 0.361
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: 0.489
Creating surface mesh ...
Surface mesh seconds: 0.008
Recovering boundaries...
Boundary recovery seconds: 0.014
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: 0.01
Recovering Delaunayness...
Delaunay recovery seconds: 0.139
Refining mesh...
Refinement seconds: 0.372
Smoothing vertices...
Mesh smoothing seconds: 0.31
Improving mesh...
Mesh improvement seconds: 0.023
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.004
Total running seconds: 1.37
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: 0.001
Creating surface mesh ...
Surface mesh seconds: 0.001
Recovering boundaries...
Boundary recovery seconds: 0.001
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: 0.002
Recovering Delaunayness...
Delaunay recovery seconds: 0.002
Refining mesh...
185 insertions, added 42 points, 701 tetrahedra in queue.
Refinement seconds: 0.009
Smoothing vertices...
Mesh smoothing seconds: 0.006
Improving mesh...
Mesh improvement seconds: 0.001
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.001
Total running seconds: 0.025
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: 0.146
Creating surface mesh ...
Surface mesh seconds: 0.002
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: 0.004
Recovering Delaunayness...
Delaunay recovery seconds: 0.007
Refining mesh...
831 insertions, added 210 points, 6107 tetrahedra in queue.
276 insertions, added 8 points, 0 tetrahedra in queue.
Refinement seconds: 0.585
Smoothing vertices...
Mesh smoothing seconds: 0.081
Improving mesh...
Mesh improvement seconds: 0.012
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.001
Total running seconds: 0.845
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: 0.003
Recovering boundaries...
Boundary recovery seconds: 0.06
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: 0.004
Suppressing Steiner points ...
Steiner suppression seconds: 0
Recovering Delaunayness...
Delaunay recovery seconds: 0.02
Refining mesh...
Refinement seconds: 0.057
Smoothing vertices...
Mesh smoothing seconds: 0.052
Improving mesh...
Mesh improvement seconds: 0.003
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0
Total running seconds: 0.25
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
.. Information: Dynamic Loader Error for zaeroAIM.DLL
E EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
======================================================================
ERROR: test_journal (test_aflr2.TestAFLR2.test_journal)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_phase (test_aflr2.TestAFLR2.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1950, in __getattr__
return self._capsItems[name].value
^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1880, in value
return self._valObj.getValue()
^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 1968, in getValue
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1705, in __setattr__
self._capsItems[name].value = value
^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1573, in value
self._valObj.setValue(val)
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr2.py", line 61, in test_setInput
myAnalysis.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 175, in test_Multiple_Mesh
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 395, in test_all
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 207, in test_box
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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 0x000000BA000000B9
======================================================================
ERROR: test_boxhole (test_aflr3.TestAFLR3.test_boxhole)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 343, in test_boxhole
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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 0x000000BA000000B9
======================================================================
ERROR: test_bullet (test_aflr3.TestAFLR3.test_bullet)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 370, in test_bullet
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_cone (test_aflr3.TestAFLR3.test_cone)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 262, in test_cone
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 235, in test_cylinder
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 420, in test_faceMatch
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_journal (test_aflr3.TestAFLR3.test_journal)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_phase (test_aflr3.TestAFLR3.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1950, in __getattr__
return self._capsItems[name].value
^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1880, in value
return self._valObj.getValue()
^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 1968, in getValue
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_reenter (test_aflr3.TestAFLR3.test_reenter)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1705, in __setattr__
self._capsItems[name].value = value
^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1573, in value
self._valObj.setValue(val)
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 316, in test_sphere
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_torus (test_aflr3.TestAFLR3.test_torus)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 289, in test_torus
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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 0x000000BA000000B9
======================================================================
ERROR: test_transp (test_aflr3.TestAFLR3.test_transp)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr3.py", line 133, in test_transp
aflr3.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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 0x000000BA000000B9
======================================================================
ERROR: test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 122, in test_MultiBody_quad
myAnalysis.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 94, in test_SingleBody_output
myAnalysis.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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 0x000000000000006C
======================================================================
ERROR: test_all (test_aflr4.TestAFLR4.test_all)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 305, in test_all
aflr4.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_box (test_aflr4.TestAFLR4.test_box)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 175, in test_box
aflr4.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 265, in test_boxhole
aflr4.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_bullet (test_aflr4.TestAFLR4.test_bullet)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 285, in test_bullet
aflr4.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 209, in test_cone
aflr4.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_cylinder (test_aflr4.TestAFLR4.test_cylinder)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 192, in test_cylinder
aflr4.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 328, in test_faceMatch
aflr4.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_journal (test_aflr4.TestAFLR4.test_journal)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_phase (test_aflr4.TestAFLR4.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1950, in __getattr__
return self._capsItems[name].value
^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1880, in value
return self._valObj.getValue()
^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 1968, in getValue
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_reenter (test_aflr4.TestAFLR4.test_reenter)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1705, in __setattr__
self._capsItems[name].value = value
^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 1573, in value
self._valObj.setValue(val)
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 246, in test_sphere
aflr4.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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_torus (test_aflr4.TestAFLR4.test_torus)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 227, in test_torus
aflr4.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_cbaero.py", line 95, in test_Output
cbaero.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_cbaero.py", line 78, in test_inputs
cbaero.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 102, in test_inputs
self.myAnalysis.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2860, in preAnalysis
stat = _caps.caps_preAnalysis(self._obj, ctypes.byref(nErr), ctypes.byref(errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
OSError: exception: access violation reading 0xFFFFFFFF00000041
======================================================================
ERROR: test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 140, in test_invalidBoundary
self.su2.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2860, in preAnalysis
stat = _caps.caps_preAnalysis(self._obj, ctypes.byref(nErr), ctypes.byref(errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
OSError: exception: access violation reading 0xFFFFFFFF00000041
======================================================================
ERROR: test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 122, in test_invalidBoundaryName
self.su2.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2860, in preAnalysis
stat = _caps.caps_preAnalysis(self._obj, ctypes.byref(nErr), ctypes.byref(errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
OSError: exception: access violation reading 0xFFFFFFFF00000041
======================================================================
ERROR: test_journal (test_su2.TestSU2.test_journal)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2860, in preAnalysis
stat = _caps.caps_preAnalysis(self._obj, ctypes.byref(nErr), ctypes.byref(errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
OSError: exception: access violation reading 0x000000BA000000B9
======================================================================
ERROR: test_phase (test_su2.TestSU2.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 226, in test_phase
su2.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2861, in preAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 152, in test_reenter
self.myAnalysis.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2860, in preAnalysis
stat = _caps.caps_preAnalysis(self._obj, ctypes.byref(nErr), ctypes.byref(errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
OSError: exception: access violation reading 0xFFFFFFFF00000041
======================================================================
ERROR: test_units (test_su2.TestSU2.test_units)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 194, in test_units
myAnalysis.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2860, in preAnalysis
stat = _caps.caps_preAnalysis(self._obj, ctypes.byref(nErr), ctypes.byref(errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
OSError: exception: access violation reading 0xFFFFFFFF00000041
======================================================================
ERROR: tearDownClass (test_su2.TestSU2)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_su2.py", line 48, in tearDownClass
cls.cleanUp()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_tetgen.py", line 126, in test_Multiple_Mesh
tetgen.runAnalysis()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 2900, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\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'!
================================================================================
======================================================================
ERROR: test_inputs (test_zaero.TestZAERO.test_inputs)
----------------------------------------------------------------------
Traceback (most recent call last):
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_zaero.py", line 95, in test_inputs
zaero = self.capsProblem.analysis.create(aim = "zaeroAIM",autoExec=False,
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\problem.py", line 3134, in create
analysisObj = self._problemObj.makeAnalysis(aim,
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 1914, in makeAnalysis
_raiseStatus(stat, msg=msg, errors=capsErrs(nErr, errs))
File "C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\EngSketchPad\pyESP\pyCAPS\caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: EGADS_NULLOBJ: Failed to make AIM 'zaeroAIM':
================================================================================
================================================================================
======================================================================
FAIL: 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\7.7\WIN64.2019\EngSketchPad\src\CAPS\aim\unitTest\pyCAPS\test_aflr4.py", line 55, in test_invalid_Mesh_Lenght_Scale
self.assertEqual(e.exception.errorName, "CAPS_BADVALUE")
AssertionError: 'CAPS_SOURCEERR' != 'CAPS_BADVALUE'
- CAPS_SOURCEERR
+ CAPS_BADVALUE
----------------------------------------------------------------------
Ran 140 tests in 652.557s
FAILED (failures=1, errors=44, skipped=26)
NMAKE : fatal error U1077: 'C:\Users\jenkins\workspace\ESP_Beta\7.7\WIN64.2019\ESP_venv\Scripts\python.EXE' : 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
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