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Skipping 1,215 KB.. Full Log
	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
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... 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)
 7FD224F02740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7FD224F02740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7FD2037FE700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7FD2037FE700 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    = 152
Number of elements = 300
Number of triangle elements      = 300
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    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4193
Total number of elements = 8366
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 - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
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 = pYq1.500/0.000QT1.00e-16A
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 = pYq1.500/0.000QT1.00e-16A
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 = pYq1.500/0.000QT1.00e-16A
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 = pYq1.500/0.000QT1.00e-16A
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 = pYq1.500/0.000QT1.00e-16A
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 = pYq1.500/0.000QT1.00e-16A
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 = pYq1.500/0.000QT1.00e-16A
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 - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 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
Number of surface: nodes - 4193, elements - 8366
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 374
Number of elements = 744
Number of triangle elements      = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 472
Total number of elements = 936
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 386
Number of elements = 768
Number of triangle elements      = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 351
Number of elements = 698
Number of triangle elements      = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 491
Total number of elements = 970
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 376
Number of elements = 748
Number of triangle elements      = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 454
Total number of elements = 896
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 126
Number of elements = 252
Number of triangle elements      = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 109
Number of elements = 214
Number of triangle elements      = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 48
Number of elements = 96
Number of triangle elements      = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 12
Number of elements = 20
Number of triangle elements      = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 169
Total number of elements = 330
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 536
Number of elements = 1072
Number of triangle elements      = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 544
Number of elements = 1084
Number of triangle elements      = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes    = 1352
Number of elements = 2684
Number of triangle elements      = 2684
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes    = 288
Number of elements = 572
Number of triangle elements      = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes    = 173
Number of elements = 342
Number of triangle elements      = 342
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes    = 26
Number of elements = 48
Number of triangle elements      = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes    = 482
Number of elements = 960
Number of triangle elements      = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

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 = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/cyl_seam.csm
 caps_filter Warning: No bodies with capsAIM = tetgenAIM!
   Body 1 capsAIM = aflr4AIM;aflr3AIM;platoAIM
   Body 2 capsAIM = aflr4AIM;aflr3AIM;platoAIM
 caps_filter Warning: No bodies with capsAIM = egadsTessAIM!
   Body 1 capsAIM = aflr4AIM;aflr3AIM;platoAIM
   Body 2 capsAIM = aflr4AIM;aflr3AIM;platoAIM
ERROR
test_journal (test_tetgen.TestTETGEN.test_journal) ... 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 - 9626, elements - 19244
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 - 9626, elements - 19244
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 - 9626, elements - 19244
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 - 9626, elements - 19244
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
ok
test_phase (test_tetgen.TestTETGEN.test_phase) ... 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 - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ERROR
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... 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    = 9626
Number of elements = 19244
Number of triangle elements      = 19244
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9626
Total number of elements = 19244
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing FAST file ....
Finished writing FAST file


Writing Binary STL file ....
Finished writing Binary STL file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing SU2 file ....
Finished writing SU2 file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing FAST file ....
Finished writing FAST file


Writing Binary STL file ....
Finished writing Binary STL file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing SU2 file ....
Finished writing SU2 file

ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ERROR
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ERROR
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ERROR
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ERROR
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ERROR
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ERROR
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ERROR
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ERROR
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ERROR
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1220
Number of elements = 2680
Number of triangle elements      = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1221
Total number of elements = 2680
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1220
	Number of elements = 2680
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 2680
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1221
	Combined Number of elements = 2681
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 2680
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 6
	Property name - Rib_Root
	Property name - Rib_Root_Point
	Property name - Ribs
	Property name - Skin
	Property name - Spar1
	Property name - Spar2
	Done getting FEA properties
Updating mesh element types based on properties input

'Smart_Restart' is ON
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh

Getting ZAERO UAIC Configurations.......
	Number of UAIC Configurations - 2

	UAIC Configuration: climb, id = 1
	- Mach Number : 0.200000
	- Reduced Freq: [0.020000, ... , 0.250000]

	UAIC Configuration: cruise, id = 2
	- Mach Number : 0.700000
	- Reduced Freq: [0.040000, ... , 0.350000]

Getting ZAERO Analysis Subcases.......
	Number of Analysis Subcases - 2

	Analysis Subcase: FlutterCruise, id = 1
	- Discipline : flutter
	- UAIC       : cruise

	Analysis Subcase: Trim, id = 2
	- Discipline : Trim
	- UAIC       : climb

Getting ZAERO Trim Variables.......
	Number of Trim Variables - 2

	Trim Variable: ANGLEA
	- Label : ALPHA
	- Value : free

	Trim Variable: URDD3
	- Label : NZ
	- Value : 1.0

	Updating StaticAeroelastic subcase: Trim
	- vectorToCG -> [0.345898, 1.652951, -0.041403]
	- weight -> 476456.149985
	- weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813292, 6179.981375, 19723.152207, 370546.335524]
ok

======================================================================
ERROR: test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_aflr3.py", line 613, in test_faceMatch_MultiDomain
    aflr3.runAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis
    self._analysisObj.execute()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 103238 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 103238
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 103238
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 103238
================================================================================


======================================================================
ERROR: test_phase (test_aflr3.TestAFLR3.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_aflr3.py", line 650, in test_phase
    myProblem = pyCAPS.Problem(problemName, phaseName="Phase1", phaseStart="Phase0", outLevel=0)
                ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 449, in __init__
    problemObj = caps.open(problemName, phaseName, flag, ptr, outLevel)
                 ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1123, in open
    _raiseStatus(stat, msg=msg, errors=capsErrs(nErr, errs))
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: EGADS_REFERCE: Failed to open Problem with prName='workDir_aflr3Test_Phase', phName='Phase1', flag=3, and ptr='Phase0':
================================================================================
Copy directory = -11 (caps_open)
================================================================================


======================================================================
ERROR: test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_aflr4.py", line 456, in test_faceMatch_MultiDomain
    aflr4.runAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis
    self._analysisObj.execute()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 103238 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 103238
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 103238
  Problem during AFLR4 surface meshing
================================================================================


======================================================================
ERROR: test_phase (test_aflr4.TestAFLR4.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_aflr4.py", line 485, in test_phase
    myProblem = pyCAPS.Problem(problemName, phaseName="Phase1", phaseStart="Phase0", outLevel=0)
                ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 449, in __init__
    problemObj = caps.open(problemName, phaseName, flag, ptr, outLevel)
                 ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1123, in open
    _raiseStatus(stat, msg=msg, errors=capsErrs(nErr, errs))
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: EGADS_REFERCE: Failed to open Problem with prName='workDir_aflr4Test_Phase', phName='Phase1', flag=3, and ptr='Phase0':
================================================================================
Copy directory = -11 (caps_open)
================================================================================


======================================================================
ERROR: test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_avl.py", line 1020, in test_MassProp_Units
    avl.runAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis
    self._analysisObj.execute()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_avl.py", line 940, in test_MassProp_noUnits
    avl.runAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis
    self._analysisObj.execute()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_avl.py", line 112, in test_alpha_custom_increment
    CLtot = avl.output.CLtot
            ^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_geom_change (test_avl.TestAVL.test_geom_change)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_avl.py", line 873, in test_geom_change
    CLtot = avl.output.CLtot
            ^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_phase (test_avl.TestAVL.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_avl.py", line 1089, in test_phase
    CLtot = avl.output.CLtot
            ^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_avl.py", line 713, in test_wing_Vtail
    Alpha = avl.output.Alpha
            ^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_wing_tail (test_avl.TestAVL.test_wing_tail)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_avl.py", line 325, in test_wing_tail
    self.assertAlmostEqual(AlphaTrue , avl.output["Alpha" ].value, 4)
                                       ^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_avl.py", line 828, in test_wing_tail_control
    self.assertAlmostEqual(AlphaTrue , avl.output["Alpha" ].value, 4)
                                       ^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_Output (test_cbaero.TestCBAERO.test_Output)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_cbaero.py", line 95, in test_Output
    cbaero.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../aflr4/aflr4_CAPS_0.fast.msh' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_cbaero/Scratch/cbaeroAIM0/cbaero_CAPS.msh'
cbaeroAIM.c:1517 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_inputs (test_cbaero.TestCBAERO.test_inputs)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_cbaero.py", line 78, in test_inputs
    cbaero.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../aflr4/aflr4_CAPS_0.fast.msh' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_cbaero/Scratch/cbaeroAIM1/cbaero_CAPS.msh'
cbaeroAIM.c:1517 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_phase (test_egadsTess.TestEGADS.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_egadsTess.py", line 332, in test_phase
    myProblem = pyCAPS.Problem(problemName, phaseName="Phase1", phaseStart="Phase0", outLevel=0)
                ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 449, in __init__
    problemObj = caps.open(problemName, phaseName, flag, ptr, outLevel)
                 ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1123, in open
    _raiseStatus(stat, msg=msg, errors=capsErrs(nErr, errs))
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: EGADS_REFERCE: Failed to open Problem with prName='workDir_egadsTest_Phase', phName='Phase1', flag=3, and ptr='Phase0':
================================================================================
Copy directory = -11 (caps_open)
================================================================================


======================================================================
ERROR: test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 345, in test_Design_SensFile
    self.fun3d.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM1/Flow/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 220, in test_Design_Sensitivity
    self.fun3d.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM2/Flow/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 431, in test_Mesh_Morph_Sensitivity
    self.fun3d.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:434 in aim_cpFile():
  Error: Could not execute: cp '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM3/tetgen_CAPS.lb8.ugrid'
aimMesh.c:1427 in aim_storeMeshRef(): Error status = -332
fun3dAIM.c:1401 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 500, in test_cythonNML
    self.fun3d.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 522, in test_cythonNMLReentrance
    self.fun3d.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_journal (test_fun3d.TestFUN3D.test_journal)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 789, in test_journal
    line_total = self.run_journal(myProblem, -1)
                 ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 710, in run_journal
    fun3d.preAnalysis(); line += 1
    ^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest2/Scratch/fun3dAIM0/Flow/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_moving_body (test_fun3d.TestFUN3D.test_moving_body)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 183, in test_moving_body
    self.fun3d.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM9/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 161, in test_overwriteNML
    self.fun3d.preAnalysis() # Don't except a config file because Overwrite_NML = False
    ^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM10/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_phase (test_fun3d.TestFUN3D.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 596, in test_phase
    fun3d.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest_Phase/Phase0/fun3d/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_reenter (test_fun3d.TestFUN3D.test_reenter)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 125, in test_reenter
    self.myAnalysis.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM0/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_symmetry (test_fun3d.TestFUN3D.test_symmetry)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 114, in test_symmetry
    self.fun3d.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
aimUtil.c:604 in aim_symLink():
  Error: Could not execute: ln -s '../tetgen/tetgen_CAPS.lb8.ugrid' '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM11/fun3d_CAPS.lb8.ugrid'
fun3dAIM.c:1520 in aimPreAnalysis(): Error status = -332
================================================================================


======================================================================
ERROR: test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_mses.py", line 173, in test_Cheby_Modes
    Cl_mod   = self.mses.output["CL"].deriv("Cheby_Modes")
               ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1910, in deriv
    return self._valObj.getDeriv(name)
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2649, in getDeriv
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
msesAIM.c:1275 in aimPreAnalysis(): Error status = -335
  Failed to execute: mset airfoil noplot < msetInput.txt > msetOutput.txt
================================================================================


======================================================================
ERROR: test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_mses.py", line 219, in test_Cheby_Modes_Symmetric
    Cheby_Modes = mses.output.Cheby_Modes
                  ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
msesAIM.c:1275 in aimPreAnalysis(): Error status = -335
  Failed to execute: mset airfoil noplot < msetInput.txt > msetOutput.txt
================================================================================


======================================================================
ERROR: test_execute (test_mses.TestMSES_Kulfan.test_execute)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_mses.py", line 97, in test_execute
    Alpha = self.mses.output.Alpha
            ^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
msesAIM.c:1275 in aimPreAnalysis(): Error status = -335
  Failed to execute: mset airfoil noplot < msetInput.txt > msetOutput.txt
================================================================================


======================================================================
ERROR: test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_mses.py", line 254, in test_sensitivity_AnalysisIn
    Cl = self.mses.output.CL
         ^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
msesAIM.c:1275 in aimPreAnalysis(): Error status = -335
  Failed to execute: mset airfoil noplot < msetInput.txt > msetOutput.txt
================================================================================


======================================================================
ERROR: test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_mses.py", line 572, in test_Cheby_Modes_Symmetric
    Cheby_Modes = self.mses.output.Cheby_Modes
                  ^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
msesAIM.c:1275 in aimPreAnalysis(): Error status = -335
  Failed to execute: mset airfoil noplot < msetInput.txt > msetOutput.txt
================================================================================


======================================================================
ERROR: test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_mses.py", line 597, in test_geom_sensitivity_CL
    Cl = self.mses.output.CL
         ^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
msesAIM.c:1275 in aimPreAnalysis(): Error status = -335
  Failed to execute: mset airfoil noplot < msetInput.txt > msetOutput.txt
================================================================================


======================================================================
ERROR: test_journal (test_mses.TestMSES_NACA.test_journal)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_mses.py", line 725, in test_journal
    line_total = self.run_journal(myProblem, -1)
                 ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_mses.py", line 679, in run_journal
    Cheby_Modes_thick = mses.output["Cheby_Modes"].deriv("thick"); line += 1
                        ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1910, in deriv
    return self._valObj.getDeriv(name)
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2649, in getDeriv
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
msesAIM.c:1275 in aimPreAnalysis(): Error status = -335
  Failed to execute: mset airfoil noplot < msetInput.txt > msetOutput.txt
================================================================================


======================================================================
ERROR: test_inputs (test_su2.TestSU2.test_inputs)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 102, in test_inputs
    self.myAnalysis.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_journal (test_su2.TestSU2.test_journal)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 357, in test_journal
    line_total = self.run_journal(myProblem, -1)
                 ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 310, in run_journal
    su2.preAnalysis(); line += 1
    ^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_phase (test_su2.TestSU2.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 226, in test_phase
    su2.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_reenter (test_su2.TestSU2.test_reenter)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 152, in test_reenter
    self.myAnalysis.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_units (test_su2.TestSU2.test_units)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 194, in test_units
    myAnalysis.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
    self._analysisObj.preAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
  Error: AFLR4 mesh generation failed...
  An EGADS file with all AFLR4 parameters
  has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
  Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================


======================================================================
ERROR: test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_tetgen.py", line 167, in test_faceMatch_MultiDomain
    tetgen.runAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis
    self._analysisObj.execute()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_SOURCEERR:
================================================================================
egadsTessAIM.c:420 in aimUpdateState():
  Error: No Bodies!
transferValues for Surface_Mesh from Surface_Mesh = -330
================================================================================


======================================================================
ERROR: test_phase (test_tetgen.TestTETGEN.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_tetgen.py", line 204, in test_phase
    myProblem = pyCAPS.Problem(problemName, phaseName="Phase1", phaseStart="Phase0", outLevel=0)
                ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 449, in __init__
    problemObj = caps.open(problemName, phaseName, flag, ptr, outLevel)
                 ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1123, in open
    _raiseStatus(stat, msg=msg, errors=capsErrs(nErr, errs))
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: EGADS_REFERCE: Failed to open Problem with prName='workDir_tetgenTest_Phase', phName='Phase1', flag=3, and ptr='Phase0':
================================================================================
Copy directory = -11 (caps_open)
================================================================================


======================================================================
ERROR: test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_xfoil.py", line 445, in test_Cl
    Alpha = self.xfoil.output.Alpha
            ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_xfoil.py", line 404, in test_alpha_custom_increment
    Alpha = self.xfoil.output.Alpha
            ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_xfoil.py", line 238, in test_CL_uniform_increment
    Alpha = self.xfoil.output.Alpha
            ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_Cl (test_xfoil.Testxfoil_NACA.test_Cl)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_xfoil.py", line 208, in test_Cl
    Alpha = self.xfoil.output.Alpha
            ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_xfoil.py", line 126, in test_alpha_custom_increment
    Alpha = self.xfoil.output.Alpha
            ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_xfoil.py", line 167, in test_alpha_uniform_inrement
    Alpha = self.xfoil.output.Alpha
            ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_append (test_xfoil.Testxfoil_NACA.test_append)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_xfoil.py", line 280, in test_append
    self.xfoil.runAnalysis()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis
    self._analysisObj.execute()
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_normalize (test_xfoil.Testxfoil_NACA.test_normalize)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_xfoil.py", line 79, in test_normalize
    AlphaTrue = self.xfoil.output.Alpha
                ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
ERROR: test_phase (test_xfoil.Testxfoil_NACA.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_xfoil.py", line 337, in test_phase
    CL = xfoil.output.CL
         ^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
           ^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


======================================================================
FAIL: test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 142, in test_invalidBoundary
    self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND")
AssertionError: 'UNKNOWN_ERROR' != 'CAPS_NOTFOUND'
- UNKNOWN_ERROR
+ CAPS_NOTFOUND


======================================================================
FAIL: test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 124, in test_invalidBoundaryName
    self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND")
AssertionError: 'UNKNOWN_ERROR' != 'CAPS_NOTFOUND'
- UNKNOWN_ERROR
+ CAPS_NOTFOUND


----------------------------------------------------------------------
Ran 143 tests in 255.356s

FAILED (failures=2, errors=49, skipped=26)
 CAPS Error: Cannot open /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/su2_problem/Scratch/capsRestart/Problem!
 CAPS Warning: caps_writeProblem = -333 (caps_close)!
 CAPS Error: Cannot open /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/capsRestart/Problem!
 CAPS Warning: caps_writeProblem = -333 (caps_close)!
Makefile:3: recipe for target 'test' failed
make: *** [test] Error 1
Build step 'Conditional step (single)' marked build as failure
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE