Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - cantilever
No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Warning: No loads specified for case EigenAnalysis!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing combined constraint cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.431s
user 0m0.563s
sys 0m0.666s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_Composite_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_Flutter_15degree.py test;
+ python -u nastran_Flutter_15degree.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 133
Number of elements = 108
Number of triangle elements = 0
Number of quadrilateral elements = 108
Body 2 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 134
Total number of elements = 108
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 133
Number of elements = 108
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 108
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 134
Combined Number of elements = 109
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 108
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 133
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
7 automatic connections were made for capsConnect Root (node id 134)
Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No loads specified for case Flutter!!!!
Writing mass increment cards
Writing aero card
Writing analysis cards, 0
Writing constraint ADD cards
Writing constraint cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.479s
user 0m0.627s
sys 0m0.668s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_MultiLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_MultiLoadCase_PyTest.py test;
+ python -u nastran_MultiLoadCase_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 49
Number of elements = 36
Number of triangle elements = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes = 49
Total number of elements = 36
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 5
Load name - load_0
Load name - load_1
Load name - load_2
Load name - load_3
Load name - load_4
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 5
Analysis name - load_0
Analysis name - load_1
Analysis name - load_2
Analysis name - load_3
Analysis name - load_4
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing combined constraint cards
Writing load ADD cards
Writing combined constraint cards
Writing load ADD cards
Writing combined constraint cards
Writing load ADD cards
Writing combined constraint cards
Writing load ADD cards
Writing combined constraint cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.344s
user 0m0.583s
sys 0m0.579s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_MultiLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_OptimizationMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_OptimizationMultiLoad_PyTest.py test;
+ python -u nastran_OptimizationMultiLoad_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 49
Number of elements = 36
Number of triangle elements = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes = 49
Total number of elements = 36
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - load_0
Load name - load_1
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - materialDV
Design_Variable name - propertyDV
Design_Variable_Relation name - materialDVR
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - propertyDVR
Number of design variable relations - 2
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 2
Design_Constraint name - stress1
Design_Constraint name - stress2
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 2
Analysis name - load_0
Analysis name - load_1
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing combined constraint cards
Writing design constraint ADD cards
Writing load ADD cards
Writing combined constraint cards
Writing design constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Writing design constraints and responses cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running NASTRAN!
real 0m1.997s
user 0m0.574s
sys 0m0.609s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_OptimizationMultiLoad_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_PlateMisc_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_PlateMisc_PyTest.py test;
+ python -u nastran_PlateMisc_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 49
Number of elements = 36
Number of triangle elements = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes = 49
Total number of elements = 36
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 3
Load name - moment
Load name - pressure
Load name - thermal
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - pltvar
Number of design variable relations - 0
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 1
Design_Constraint name - pltcon
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing design constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design constraints and responses cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m2.550s
user 0m0.556s
sys 0m0.655s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_PlateMisc_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_PyTest.py test;
+ python -u nastran_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 2091
Number of elements = 1845
Number of triangle elements = 0
Number of quadrilateral elements = 1845
----------------------------
Total number of nodes = 2091
Total number of elements = 1845
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2091
Number of elements = 1845
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 1845
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Warning: No loads specified for case EigenAnalysis!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing combined constraint cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
Getting results for natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02165 (Hz)
Natural freq (Mode 2) = 0.02165 (Hz)
Natural freq (Mode 3) = 0.10665 (Hz)
Natural freq (Mode 4) = 0.10665 (Hz)
Natural freq (Mode 5) = 0.13547 (Hz)
Natural freq (Mode 6) = 0.13547 (Hz)
Natural freq (Mode 7) = 0.23092 (Hz)
Natural freq (Mode 8) = 0.23092 (Hz)
Natural freq (Mode 9) = 0.27609 (Hz)
Natural freq (Mode 10) = 0.27609 (Hz)
real 0m10.378s
user 0m11.305s
sys 0m3.447s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_SingleLoadCase_PyTest.py test;
+ python -u nastran_SingleLoadCase_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.091s
user 0m0.465s
sys 0m0.522s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_ThreeBarDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarDesign_PyTest.py test;
+ python -u nastran_ThreeBarDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 3
Design_Variable name - Bar1A
Design_Variable name - Bar2A
Design_Variable name - Bar3A
Design_Variable_Relation name - Bar1A
Design_Variable_Relation name - Bar2A
Design_Variable_Relation name - Bar3A
Number of design variable relations - 3
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 3
Design_Constraint name - stress1
Design_Constraint name - stress2
Design_Constraint name - stress3
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing design constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Writing design constraints and responses cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.234s
user 0m0.525s
sys 0m0.548s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarDesign_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarFreq_PyTest.py test;
+ python -u nastran_ThreeBarFreq_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Warning: No loads specified for case EigenAnalysis!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing combined constraint cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.121s
user 0m0.508s
sys 0m0.540s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarLinkDesign_PyTest.py test;
+ python -u nastran_ThreeBarLinkDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 3
Design_Variable name - Bar1A
Design_Variable name - Bar2A
Design_Variable name - Bar3A
Design_Variable_Relation name - Bar1A
Design_Variable_Relation name - Bar2A
Design_Variable_Relation name - Bar3A
Number of design variable relations - 3
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 3
Design_Constraint name - stress1
Design_Constraint name - stress2
Design_Constraint name - stress3
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing design constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Writing design constraints and responses cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.096s
user 0m0.502s
sys 0m0.507s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarLinkDesign_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarMultiLoad_PyTest.py test;
+ python -u nastran_ThreeBarMultiLoad_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 2
Constraint name - conOne
No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
Constraint name - conTwo
No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - loadOne
Load name - loadTwo
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 2
Analysis name - caseOne
Analysis name - caseTwo
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.074s
user 0m0.516s
sys 0m0.539s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_ThreeBar_PyTest.py test;
+ python -u nastran_ThreeBar_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.124s
user 0m0.469s
sys 0m0.530s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
nastran_Trim_15degree.py test;
+ python -u nastran_Trim_15degree.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 117
Number of elements = 96
Number of triangle elements = 0
Number of quadrilateral elements = 96
Body 2 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 118
Total number of elements = 96
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 117
Number of elements = 96
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 96
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 118
Combined Number of elements = 97
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 96
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 117
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - Body
Property name - Edge
Property name - Root
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - PointSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
9 automatic connections were made for capsConnect Root (node id 118)
Done getting FEA connections
Getting FEA loads.......
Number of loads - 2
Load name - GravityLoad
No "groupName" specified for Load tuple GravityLoad, going to use load name
Load name - PointLoad
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No loads specified for case Trim, assuming all loads are applied!!!!
Writing mass increment cards
Writing aeros card
Writing aestat cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.616s
user 0m0.590s
sys 0m0.542s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_Trim_15degree.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
Nastran
Mystran
Plato
=================================================
All tests pass!
=================================================
=================================================
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest
++ ./execute_PyTestRegression.sh STRUCTURE
=================================================
Legacy Using python : /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/ESP/venv/bin/python
=================================================
Running.... STRUCTURE PyTests
=================================================
+ rm -rf masstran_PyTest
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting results mass properties.....
Area 3.428666259747
Mass 5383.006027803
Centroid [1.222256036874, 0.1634981473778, -4.234492548615e-11]
CG [1.222256036874, 0.1634981473778, -4.234574416087e-11]
Ixx 22133.97306033
Iyy 23448.30046709
Izz 1389.213122582
Ixy 164.2055275657
Ixz -7.454849830627e-06
Iyz 1.707682983295e-06
I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454849830627e-06, 1.707682983295e-06]
II [[22133.97306033, -164.2055275657, 7.454849830627e-06], [-164.2055275657, 23448.30046709, -1.707682983295e-06], [7.454849830627e-06, -1.707682983295e-06, 1389.213122582]]
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m8.618s
user 0m10.676s
sys 0m2.630s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf masstran_AGARD445_PyTest
+ echo 'masstran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
masstran_AGARD445_PyTest.py test;
+ python -u masstran_AGARD445_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 36
Number of elements = 25
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 25
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Getting results mass properties.....
Area 547.7004
Mass 0.01605224431138
Centroid [20.03586282449, 14.01686746988, 0.0]
CG [20.03586282449, 14.01686746988, 0.0]
Ixx 1.140246300554
Iyy 0.919317482675
Izz 2.059563783229
Ixy 0.7352134614013
Ixz 0.0
Iyz 0.0
I [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0]
II [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.497s
user 0m0.571s
sys 0m0.401s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf hsm_SingleLoadCase_PyTest
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.574s
user 0m0.924s
sys 0m0.323s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf hsm_CantileverPlate_PyTest
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ echo 'hsm_CantileverPlate_PyTest.py test;'
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 51
Elemental Tria3 = 0
Elemental Quad4 = 27
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1313
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.03 0.00)
1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.03 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.03 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.03 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.07 0.00)
8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.10 0.00)
9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.00 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
iter dr dd dp rlx max
11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.10 0.00)
11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00)
12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00)
13* 0.336E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00)
15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.10 0.00)
16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00)
17 0.558E-15 0.304E-14 0.603E-15 1.000 ddx @ ( 1.00 0.00 0.00)
Converging n vectors ...
it = 1 dn = 0.193E+01 rlx = 1.000 ( 12 )
it = 2 dn = 0.435E-15 rlx = 1.000 ( 28 )
Converging e1,e2 vectors ...
it = 1 de = 0.285E+01 rlx = 0.351 ( 24 )
it = 2 de = 0.292E+01 rlx = 0.342 ( 34 )
it = 3 de = 0.226E+01 rlx = 0.442 ( 34 )
it = 4 de = 0.151E+01 rlx = 0.660 ( 34 )
it = 5 de = 0.665E+00 rlx = 1.000 ( 34 )
it = 6 de = 0.609E-01 rlx = 1.000 ( 34 )
it = 7 de = 0.573E-04 rlx = 1.000 ( 34 )
it = 8 de = 0.478E-13 rlx = 1.000 ( 34 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMCantileverPlate.dat
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.566s
user 0m0.816s
sys 0m0.325s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_Aeroelastic_PyTest
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ echo 'astros_Aeroelastic_PyTest.py test;'
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Wing, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 286
Number of elements = 386
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 92
Elemental Quad4 = 294
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 287
Combined Number of elements = 387
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 92
Combined Elemental Quad4 = 294
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 48
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Ribs
No "material" specified for Property tuple Ribs, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Property name - Spar1
No "material" specified for Property tuple Spar1, defaulting to an index of 1
Property name - Spar2
No "material" specified for Property tuple Spar2, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
30 automatic connections were made for capsConnect Rib_Root (node id 287)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m24.195s
user 0m22.813s
sys 0m3.229s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_AGARD445_PyTest
+ echo 'astros_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_AGARD445_PyTest.py test;
+ python -u astros_AGARD445_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 36
Number of elements = 25
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 25
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
Getting results natural frequencies.....
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 2
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Natural freq (Mode 1) = 5.78 (Hz)
Natural freq (Mode 2) = 30.66 (Hz)
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.407s
user 0m0.648s
sys 0m0.436s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_Composite_PyTest
+ echo 'astros_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_Composite_PyTest.py test;
+ python -u astros_Composite_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 15
Number of elements = 8
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 8
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - cantilever
No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
Running Astros......
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.273s
user 0m0.705s
sys 0m0.453s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_Composite_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_CompositeWingFreq_PyTest
+ echo 'astros_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = wing, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - wing
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = root, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = wing, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = wing, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 429
Number of elements = 817
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 817
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - wing
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - root
No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
Running Astros......
Done running Astros!
Getting results for natural frequencies.....
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 5.91949 (Hz)
Natural freq (Mode 2) = 29.79990 (Hz)
Natural freq (Mode 3) = 39.10550 (Hz)
Natural freq (Mode 4) = 77.71580 (Hz)
Natural freq (Mode 5) = 99.79550 (Hz)
Natural freq (Mode 6) = 146.97500 (Hz)
Natural freq (Mode 7) = 176.90300 (Hz)
Natural freq (Mode 8) = 235.53300 (Hz)
Natural freq (Mode 9) = 274.42600 (Hz)
Natural freq (Mode 10) = 311.35900 (Hz)
No variable name provided - all variables will be writen to file
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsBound.writeTecplot' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].writeTecplot'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 1m24.071s
user 1m12.004s
sys 0m2.309s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_CompositeWingFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_Flutter_15degree
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u astros_Flutter_15degree.py -verbosity=0 -workDir=runDirectory
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m2.143s
user 0m1.276s
sys 0m0.749s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_MultipleLoadCase_PyTest
+ echo 'astros_MultipleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 16
Number of elements = 9
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 9
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 5
Load name - load_0
Load name - load_1
Load name - load_2
Load name - load_3
Load name - load_4
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 5
Analysis name - load_0
Analysis name - load_1
Analysis name - load_2
Analysis name - load_3
Analysis name - load_4
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
Writing analysis cards
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.628s
user 0m0.980s
sys 0m0.570s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_MultipleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_PyTest
+ echo 'astros_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 293
Number of elements = 217
Number of triangle elements = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes = 293
Total number of elements = 217
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 293
Number of elements = 217
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 217
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
Getting results for natural frequencies.....
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02335 (Hz)
Natural freq (Mode 2) = 0.02335 (Hz)
Natural freq (Mode 3) = 0.11619 (Hz)
Natural freq (Mode 4) = 0.11619 (Hz)
Natural freq (Mode 5) = 0.14468 (Hz)
Natural freq (Mode 6) = 0.14468 (Hz)
Natural freq (Mode 7) = 0.23352 (Hz)
Natural freq (Mode 8) = 0.23352 (Hz)
Natural freq (Mode 9) = 0.30497 (Hz)
Natural freq (Mode 10) = 0.30497 (Hz)
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m31.300s
user 0m29.956s
sys 0m4.049s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_SingleLoadCase_PyTest
+ echo 'astros_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 6
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 6
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m2.243s
user 0m1.034s
sys 0m0.804s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_ThreeBarFreq_PyTest
+ echo 'astros_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ python -u astros_ThreeBarFreq_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
Getting results for natural frequencies.....
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 2
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Natural freq (Mode 1) = 86.13400 (Hz)
Natural freq (Mode 2) = 168.53300 (Hz)
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m2.384s
user 0m0.870s
sys 0m0.835s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_ThreeBarMultiLoad_PyTest
+ echo 'astros_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ python -u astros_ThreeBarMultiLoad_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 2
Constraint name - conOne
No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
Constraint name - conTwo
No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - loadOne
Load name - loadTwo
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 2
Analysis name - analysisOne
Analysis name - analysisTwo
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.881s
user 0m0.909s
sys 0m0.707s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_ThreeBar_PyTest
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u astros_ThreeBar_PyTest.py -verbosity=0 -workDir=runDirectory
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.592s
user 0m0.809s
sys 0m0.630s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_Trim_15degree
+ echo 'astros_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u astros_Trim_15degree.py -verbosity=0 -workDir=runDirectory
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - Body
Property name - Edge
Property name - Root
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - PointSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Getting FEA loads.......
Number of loads - 2
Load name - GravityLoad
No "groupName" specified for Load tuple GravityLoad, going to use load name
Load name - PointLoad
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m2.122s
user 0m1.234s
sys 0m0.709s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Legacy Did not run examples for:
Nastran
Mystran
=================================================
All tests pass!
=================================================
=================================================
[Execution node] check if [macys_VM] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.7,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWIN64,buildnode=macys_VM #662'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS