Skipping 807 KB..
Full LogWarning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Warning: The 4-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.002515
Recovering Delaunayness...
Delaunay recovery seconds: 0.046641
Refining mesh...
Refinement seconds: 0.121204
Smoothing vertices...
Mesh smoothing seconds: 0.113082
Improving mesh...
Mesh improvement seconds: 0.001719
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00054
Total running seconds: 0.456473
Statistics:
Input points: 1070
Input facets: 2136
Input segments: 3204
Input holes: 0
Input regions: 5
Mesh points: 1321
Mesh tetrahedra: 4502
Mesh faces: 10072
Mesh faces on exterior boundary: 2136
Mesh faces on input facets: 2136
Mesh edges on input segments: 3204
Steiner points inside domain: 251
Done meshing using TetGen!
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing exodus file ....
Block: 'tableTop_tet', blk_id 1, num_entries 1722
Block: 'leg0_tet', blk_id 2, num_entries 4467
Block: 'leg1_tet', blk_id 3, num_entries 4468
Block: 'leg2_tet', blk_id 4, num_entries 4517
Block: 'leg3_tet', blk_id 5, num_entries 4502
Sideset: 'leg0Side', set_id 1, num_entries 2136
Sideset: 'leg1Side', set_id 2, num_entries 2136
Sideset: 'leg2Side', set_id 3, num_entries 2136
Sideset: 'leg3Side', set_id 4, num_entries 2136
Sideset: 'tableTopSide', set_id 5, num_entries 1280
Nodeset: 'edge', set_id 1, num_entries 17
Nodeset: 'face1', set_id 2, num_entries 99
Nodeset: 'face2', set_id 3, num_entries 99
Nodeset: 'node', set_id 4, num_entries 1
Finished writing Exodus file
real 0m4.802s
user 0m3.734s
sys 0m0.253s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case plato_tetgen_table_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'plato_tetgen_cyli_box_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
plato_tetgen_cyli_box_PyTest.py test;
+ python -u plato_tetgen_cyli_box_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
EGADS Warning: Loop 2 marked with -1
EGADS Warning: Loop 2 marked with -1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = box, index = 1
Name = cyl2, index = 2
Name = box;cyl2, index = 3
Name = cyl1, index = 4
Name = cyl1;box;cyl2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 3591
Number of elements = 7306
Number of triangle elements = 7306
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3591
Total number of elements = 7306
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = box, index = 1
Name = cyl2, index = 2
Name = box;cyl2, index = 3
Name = cyl1, index = 4
Name = cyl1;box;cyl2, index = 5
Number of surface: nodes - 3591, elements - 7306
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.343084
Creating surface mesh ...
Surface mesh seconds: 0.002237
Recovering boundaries...
Boundary recovery seconds: 0.034299
Removing exterior tetrahedra ...
Warning: The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.00122
Recovering Delaunayness...
Delaunay recovery seconds: 0.225705
Refining mesh...
Refinement seconds: 0.413253
Smoothing vertices...
Mesh smoothing seconds: 0.535682
Improving mesh...
Mesh improvement seconds: 0.005602
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000504
Total running seconds: 1.56178
Statistics:
Input points: 3591
Input facets: 7306
Input segments: 10895
Input holes: 0
Input regions: 3
Mesh points: 5613
Mesh tetrahedra: 29362
Mesh faces: 60329
Mesh faces on exterior boundary: 3210
Mesh faces on input facets: 7306
Mesh edges on input segments: 10895
Steiner points inside domain: 2022
Done meshing using TetGen!
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing exodus file ....
Block: 'c_tet', blk_id 1, num_entries 12754
Block: 'b_tet', blk_id 2, num_entries 11091
Block: 'a_tet', blk_id 3, num_entries 5517
Sideset: 'box', set_id 1, num_entries 3210
Sideset: 'cyl1', set_id 2, num_entries 2116
Sideset: 'cyl2', set_id 3, num_entries 2310
Finished writing Exodus file
real 0m3.607s
user 0m3.179s
sys 0m0.231s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case plato_tetgen_cyli_box_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'plato_aflr_tetgen_table_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
plato_aflr_tetgen_table_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
+ python -u plato_aflr_tetgen_table_PyTest.py -outLevel=0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = tableTopSide, index = 1
Name = leg0Side, index = 2
Name = leg1Side, index = 3
Name = leg2Side, index = 4
Name = leg3Side, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Darwin 22.6.0 arm64
AFLR2 : Compile Date 08/01/23 @ 11:39PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.9
AFLR4 : Version Date 08/14/23 @ 12:27AM
AFLR4 : Compile OS Darwin 22.6.0 arm64
AFLR4 : Compile Date 08/14/23 @ 12:31AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 5 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 6 Faces
EGADS : Body 0 has 12 Edges
EGADS : Body 0 has 6 Loops
EGADS : Body 0 has 8 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 4 Faces
EGADS : Body 1 has 6 Edges
EGADS : Body 1 has 4 Loops
EGADS : Body 1 has 4 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 4 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 4 Loops
EGADS : Body 2 has 4 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 4 Faces
EGADS : Body 3 has 6 Edges
EGADS : Body 3 has 4 Loops
EGADS : Body 3 has 4 Nodes
EGADS : Body 4 is a SolidBody
EGADS : Body 4 has 1 Shells
EGADS : Body 4 has 4 Faces
EGADS : Body 4 has 6 Edges
EGADS : Body 4 has 4 Loops
EGADS : Body 4 has 4 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 3 4 5 6
EGADS : 2 Yes 0 0 1 0 1 3 4 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 5 6
EGADS : 4 Yes 0 0 1 0 1 1 2 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 3 4
EGADS : 6 Yes 0 0 1 0 1 1 2 3 4
EGADS : 7 Yes 1 0 1 0 1 8 9 10
EGADS : 8 Yes 1 0 1 0 1 7 9 10
EGADS : 9 Yes 1 0 1 0 1 7 8
EGADS : 10 Yes 1 0 1 0 1 7 8
EGADS : 11 Yes 2 0 1 0 1 12 13 14
EGADS : 12 Yes 2 0 1 0 1 11 13 14
EGADS : 13 Yes 2 0 1 0 1 11 12
EGADS : 14 Yes 2 0 1 0 1 11 12
EGADS : 15 Yes 3 0 1 0 1 16 17 18
EGADS : 16 Yes 3 0 1 0 1 15 17 18
EGADS : 17 Yes 3 0 1 0 1 15 16
EGADS : 18 Yes 3 0 1 0 1 15 16
EGADS : 19 Yes 4 0 1 0 1 20 21 22
EGADS : 20 Yes 4 0 1 0 1 19 21 22
EGADS : 21 Yes 4 0 1 0 1 19 20
EGADS : 22 Yes 4 0 1 0 1 19 20
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 -5 8 7 -6
EGADS : 3 9 5 -10 -1
EGADS : 4 -11 3 12 -7
EGADS : 5 4 11 -8 -9
EGADS : 6 -2 10 6 -12
EGADS : 7 -13 -14 15 16
EGADS : 8 17 14 -18 -16
EGADS : 9 13 18
EGADS : 10 -15 -17
EGADS : 11 -19 -20 21 22
EGADS : 12 23 20 -24 -22
EGADS : 13 19 24
EGADS : 14 -21 -23
EGADS : 15 -25 -26 27 28
EGADS : 16 29 26 -30 -28
EGADS : 17 25 30
EGADS : 18 -27 -29
EGADS : 19 -31 -32 33 34
EGADS : 20 35 32 -36 -34
EGADS : 21 31 36
EGADS : 22 -33 -35
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : 19 19
EGADS : 20 20
EGADS : 21 21
EGADS : 22 22
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 1 2 -3 -4
EGADS : 2 Yes 1 -5 8 7 -6
EGADS : 3 Yes 1 9 5 -10 -1
EGADS : 4 Yes 1 -11 3 12 -7
EGADS : 5 Yes 1 4 11 -8 -9
EGADS : 6 Yes 1 -2 10 6 -12
EGADS : 7 Yes 1 -13 -14 15 16
EGADS : 8 Yes 1 17 14 -18 -16
EGADS : 9 Yes 1 13 18
EGADS : 10 Yes 1 -15 -17
EGADS : 11 Yes 1 -19 -20 21 22
EGADS : 12 Yes 1 23 20 -24 -22
EGADS : 13 Yes 1 19 24
EGADS : 14 Yes 1 -21 -23
EGADS : 15 Yes 1 -25 -26 27 28
EGADS : 16 Yes 1 29 26 -30 -28
EGADS : 17 Yes 1 25 30
EGADS : 18 Yes 1 -27 -29
EGADS : 19 Yes 1 -31 -32 33 34
EGADS : 20 Yes 1 35 32 -36 -34
EGADS : 21 Yes 1 31 36
EGADS : 22 Yes 1 -33 -35
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 6 5 1 2 3
EGADS : 6 0 Yes 5 7 1 2 6
EGADS : 7 0 Yes 8 7 1 2 4
EGADS : 8 0 Yes 6 8 1 2 5
EGADS : 9 0 Yes 2 6 1 3 5
EGADS : 10 0 Yes 1 5 1 3 6
EGADS : 11 0 Yes 4 8 1 4 5
EGADS : 12 0 Yes 3 7 1 4 6
EGADS : 13 1 Yes 10 9 1 7 9
EGADS : 14 1 Yes 11 10 1 7 8
EGADS : 15 1 Yes 11 12 1 7 10
EGADS : 16 1 Yes 12 9 1 7 8
EGADS : 17 1 Yes 12 11 1 8 10
EGADS : 18 1 Yes 9 10 1 8 9
EGADS : 19 2 Yes 14 13 1 11 13
EGADS : 20 2 Yes 15 14 1 11 12
EGADS : 21 2 Yes 15 16 1 11 14
EGADS : 22 2 Yes 16 13 1 11 12
EGADS : 23 2 Yes 16 15 1 12 14
EGADS : 24 2 Yes 13 14 1 12 13
EGADS : 25 3 Yes 18 17 1 15 17
EGADS : 26 3 Yes 19 18 1 15 16
EGADS : 27 3 Yes 19 20 1 15 18
EGADS : 28 3 Yes 20 17 1 15 16
EGADS : 29 3 Yes 20 19 1 16 18
EGADS : 30 3 Yes 17 18 1 16 17
EGADS : 31 4 Yes 22 21 1 19 21
EGADS : 32 4 Yes 23 22 1 19 20
EGADS : 33 4 Yes 23 24 1 19 22
EGADS : 34 4 Yes 24 21 1 19 20
EGADS : 35 4 Yes 24 23 1 20 22
EGADS : 36 4 Yes 21 22 1 20 21
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0.5
EGADS : 2 Yes 0 0 0
EGADS : 3 Yes 0 0.1 0.5
EGADS : 4 Yes 0 0.1 0
EGADS : 5 Yes 0.5 0 0.5
EGADS : 6 Yes 0.5 0 0
EGADS : 7 Yes 0.5 0.1 0.5
EGADS : 8 Yes 0.5 0.1 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 0 0 0
EGADS : 11 Yes 0 0 0
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 0 0.26
EGADS : 14 Yes 0 0 0.46
EGADS : 15 Yes 0 0 0.46
EGADS : 16 Yes 0 0 0.26
EGADS : 17 Yes 0.36 0 0.26
EGADS : 18 Yes 0.36 0 0.46
EGADS : 19 Yes 0.36 0 0.46
EGADS : 20 Yes 0.36 0 0.26
EGADS : 21 Yes 0.36 0 0
EGADS : 22 Yes 0.36 0 0
EGADS : 23 Yes 0.36 0 0
EGADS : 24 Yes 0.36 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 1
AFLR4 : Min Bounding Box Length = 0.7
AFLR4 : Max Ref Bounding Box Length = 1
AFLR4 : Min Ref Bounding Box Length = 0.7
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.005
AFLR4 : Max Surf Spacing = 0.1
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : Case has 5 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6
AFLR4 : Component 2 includes Definitions 7 8 9 10
AFLR4 : Component 3 includes Definitions 11 12 13 14
AFLR4 : Component 4 includes Definitions 15 16 17 18
AFLR4 : Component 5 includes Definitions 19 20 21 22
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 34 34 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 34 34 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 229 400 0
AFLR4 : Nodes, Trias,Quads= 212 366 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 230 402 0
AFLR4 : Nodes, Trias,Quads= 212 366 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 34 34 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 34 34 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2258 4330 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2259 4332 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 515 964 0
AFLR4 : Nodes, Trias,Quads= 413 760 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 402 738 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2258 4330 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2259 4332 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 515 964 0
AFLR4 : Nodes, Trias,Quads= 413 760 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 402 738 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2258 4330 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2259 4332 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 515 964 0
AFLR4 : Nodes, Trias,Quads= 413 760 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 402 738 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2258 4330 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2259 4332 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 515 964 0
AFLR4 : Nodes, Trias,Quads= 413 760 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 402 738 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 20764 41508 2224
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 20764 41508
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Nodes, Trias,Quads= 30 28 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Nodes, Trias,Quads= 30 28 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 201 348 0
AFLR4 : Nodes, Trias,Quads= 193 332 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 204 354 0
AFLR4 : Nodes, Trias,Quads= 193 332 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Nodes, Trias,Quads= 30 28 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Nodes, Trias,Quads= 30 28 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 2245 4304 0
AFLR4 : Nodes, Trias,Quads= 2243 4300 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 496 926 0
AFLR4 : Nodes, Trias,Quads= 416 766 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 502 938 0
AFLR4 : Nodes, Trias,Quads= 408 750 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 2245 4304 0
AFLR4 : Nodes, Trias,Quads= 2244 4302 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Nodes, Trias,Quads= 2247 4308 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 496 926 0
AFLR4 : Nodes, Trias,Quads= 416 766 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 502 938 0
AFLR4 : Nodes, Trias,Quads= 408 750 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 2245 4304 0
AFLR4 : Nodes, Trias,Quads= 2244 4302 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Nodes, Trias,Quads= 2249 4312 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 496 926 0
AFLR4 : Nodes, Trias,Quads= 416 766 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 502 938 0
AFLR4 : Nodes, Trias,Quads= 408 750 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 2245 4304 0
AFLR4 : Nodes, Trias,Quads= 2243 4300 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Nodes, Trias,Quads= 2249 4312 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 496 926 0
AFLR4 : Nodes, Trias,Quads= 416 766 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 502 938 0
AFLR4 : Nodes, Trias,Quads= 408 750 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 20653 41286 2208
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 21566 43112
AFLR4 : Nodes, Trias = 22450 44880
AFLR4 : Nodes, Trias = 22542 45064
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 311 517 0
AFLR4 : Nodes, Trias,Quads= 309 513 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 313 521 0
AFLR4 : Nodes, Trias,Quads= 309 513 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3277 6339 0
AFLR4 : Nodes, Trias,Quads= 1431 2647 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1864 3566 0
AFLR4 : Nodes, Trias,Quads= 1736 3310 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 315 525 0
AFLR4 : Nodes, Trias,Quads= 307 509 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 318 530 0
AFLR4 : Nodes, Trias,Quads= 314 522 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 2301 4412 0
AFLR4 : Nodes, Trias,Quads= 2272 4354 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2273 4356 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 548 1028 0
AFLR4 : Nodes, Trias,Quads= 423 778 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 549 1030 0
AFLR4 : Nodes, Trias,Quads= 418 768 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 2301 4412 0
AFLR4 : Nodes, Trias,Quads= 2272 4354 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2273 4356 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 548 1028 0
AFLR4 : Nodes, Trias,Quads= 423 778 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 549 1030 0
AFLR4 : Nodes, Trias,Quads= 418 768 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 2301 4412 0
AFLR4 : Nodes, Trias,Quads= 2272 4354 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2277 4364 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 548 1028 0
AFLR4 : Nodes, Trias,Quads= 423 778 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 549 1030 0
AFLR4 : Nodes, Trias,Quads= 418 768 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 2301 4412 0
AFLR4 : Nodes, Trias,Quads= 2272 4354 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2277 4364 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 548 1028 0
AFLR4 : Nodes, Trias,Quads= 423 778 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 549 1030 0
AFLR4 : Nodes, Trias,Quads= 418 768 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 24537 49054 2818
OVERALL : CPU Time = 1.199 seconds
Body 1 (of 5)
Number of nodes = 4009
Number of elements = 8014
Number of triangle elements = 8014
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 5130
Number of elements = 10256
Number of triangle elements = 10256
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 5130
Number of elements = 10256
Number of triangle elements = 10256
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 5134
Number of elements = 10264
Number of triangle elements = 10264
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 5134
Number of elements = 10264
Number of triangle elements = 10264
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 24537
Total number of elements = 49054
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = tableTopSide, index = 1
Name = leg0Side, index = 2
Name = leg1Side, index = 3
Name = leg2Side, index = 4
Name = leg3Side, index = 5
Body 1 number of surface: nodes - 4009, elements - 8014
Body 2 number of surface: nodes - 5130, elements - 10256
Body 3 number of surface: nodes - 5130, elements - 10256
Body 4 number of surface: nodes - 5134, elements - 10264
Body 5 number of surface: nodes - 5134, elements - 10264
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.052561
Creating surface mesh ...
Surface mesh seconds: 0.002479
Recovering boundaries...
Boundary recovery seconds: 0.028291
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.003781
Recovering Delaunayness...
Delaunay recovery seconds: 0.005293
Refining mesh...
Refinement seconds: 0.040509
Smoothing vertices...
Mesh smoothing seconds: 0.076805
Improving mesh...
Mesh improvement seconds: 0.002583
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000635
Total running seconds: 0.213076
Statistics:
Input points: 4009
Input facets: 8014
Input segments: 12021
Input holes: 0
Input regions: 1
Mesh points: 4748
Mesh tetrahedra: 15739
Mesh faces: 35485
Mesh faces on exterior boundary: 8014
Mesh faces on input facets: 8014
Mesh edges on input segments: 12021
Steiner points inside domain: 739
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.061068
Creating surface mesh ...
Surface mesh seconds: 0.003953
Recovering boundaries...
Boundary recovery seconds: 0.050412
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.010937
Recovering Delaunayness...
Delaunay recovery seconds: 0.014205
Refining mesh...
Refinement seconds: 0.10435
Smoothing vertices...
Mesh smoothing seconds: 0.11064
Improving mesh...
Mesh improvement seconds: 0.003665
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00092
Total running seconds: 0.360265
Statistics:
Input points: 5130
Input facets: 10256
Input segments: 15384
Input holes: 0
Input regions: 2
Mesh points: 6596
Mesh tetrahedra: 23300
Mesh faces: 51728
Mesh faces on exterior boundary: 10256
Mesh faces on input facets: 10256
Mesh edges on input segments: 15384
Steiner points inside domain: 1466
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.065042
Creating surface mesh ...
Surface mesh seconds: 0.003871
Recovering boundaries...
Boundary recovery seconds: 0.063484
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.022897
Recovering Delaunayness...
Delaunay recovery seconds: 0.020341
Refining mesh...
Refinement seconds: 0.142637
Smoothing vertices...
Mesh smoothing seconds: 0.101207
Improving mesh...
Mesh improvement seconds: 0.003666
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000932
Total running seconds: 0.42425
Statistics:
Input points: 5130
Input facets: 10256
Input segments: 15384
Input holes: 0
Input regions: 3
Mesh points: 6576
Mesh tetrahedra: 23218
Mesh faces: 51564
Mesh faces on exterior boundary: 10256
Mesh faces on input facets: 10256
Mesh edges on input segments: 15384
Steiner points inside domain: 1446
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.048428
Creating surface mesh ...
Surface mesh seconds: 0.003286
Recovering boundaries...
Boundary recovery seconds: 0.050249
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.017358
Recovering Delaunayness...
Delaunay recovery seconds: 0.017392
Refining mesh...
Refinement seconds: 0.112904
Smoothing vertices...
Mesh smoothing seconds: 0.093372
Improving mesh...
Mesh improvement seconds: 0.004501
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.001025
Total running seconds: 0.34865
Statistics:
Input points: 5134
Input facets: 10264
Input segments: 15396
Input holes: 0
Input regions: 4
Mesh points: 6610
Mesh tetrahedra: 23465
Mesh faces: 52062
Mesh faces on exterior boundary: 10264
Mesh faces on input facets: 10264
Mesh edges on input segments: 15396
Steiner points inside domain: 1476
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.075626
Creating surface mesh ...
Surface mesh seconds: 0.003693
Recovering boundaries...
Boundary recovery seconds: 0.0548
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Warning: The 4-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.014067
Recovering Delaunayness...
Delaunay recovery seconds: 0.013591
Refining mesh...
Refinement seconds: 0.132817
Smoothing vertices...
Mesh smoothing seconds: 0.148495
Improving mesh...
Mesh improvement seconds: 0.004628
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.001017
Total running seconds: 0.44886
Statistics:
Input points: 5134
Input facets: 10264
Input segments: 15396
Input holes: 0
Input regions: 5
Mesh points: 6634
Mesh tetrahedra: 23569
Mesh faces: 52270
Mesh faces on exterior boundary: 10264
Mesh faces on input facets: 10264
Mesh edges on input segments: 15396
Steiner points inside domain: 1500
Done meshing using TetGen!
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing exodus file ....
Block: 'tableTop_tet', blk_id 1, num_entries 15739
Block: 'leg0_tet', blk_id 2, num_entries 23300
Block: 'leg1_tet', blk_id 3, num_entries 23218
Block: 'leg2_tet', blk_id 4, num_entries 23465
Block: 'leg3_tet', blk_id 5, num_entries 23569
Sideset: 'leg0Side', set_id 1, num_entries 10256
Sideset: 'leg1Side', set_id 2, num_entries 10256
Sideset: 'leg2Side', set_id 3, num_entries 10264
Sideset: 'leg3Side', set_id 4, num_entries 10264
Sideset: 'tableTopSide', set_id 5, num_entries 8014
Nodeset: 'edge', set_id 1, num_entries 41
Nodeset: 'face1', set_id 2, num_entries 610
Nodeset: 'face2', set_id 3, num_entries 617
Nodeset: 'node', set_id 4, num_entries 1
Finished writing Exodus file
real 0m5.469s
user 0m4.706s
sys 0m0.335s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case plato_aflr_tetgen_table_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'plato_aflr_tetgen_cyli_box_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
plato_aflr_tetgen_cyli_box_PyTest.py test;
+ python -u plato_aflr_tetgen_cyli_box_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
EGADS Warning: Loop 2 marked with -1
EGADS Warning: Loop 2 marked with -1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = box, index = 1
Name = cyl2, index = 2
Name = box;cyl2, index = 3
Name = cyl1, index = 4
Name = cyl1;box;cyl2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Darwin 22.6.0 arm64
AFLR2 : Compile Date 08/01/23 @ 11:39PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.9
AFLR4 : Version Date 08/14/23 @ 12:27AM
AFLR4 : Compile OS Darwin 22.6.0 arm64
AFLR4 : Compile Date 08/14/23 @ 12:31AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SheetBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 14 Faces
EGADS : Body 0 has 24 Edges
EGADS : Body 0 has 18 Loops
EGADS : Body 0 has 16 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 6 7 8
EGADS : 2 Yes 0 0 1 0 1 1 3 4 5 7 8 9
EGADS : 3 Yes 0 0 1 0 1 2 4 6 9 12
EGADS : 4 Yes 0 0 1 0 1 2 3 6 9 12
EGADS : 5 Yes 0 0 1 0 1 2 6 7 8
EGADS : 6 Yes 0 0 1 0 1 1 3 4 5 7 8 12
EGADS : 7 Yes 0 0 1 0 1 1 2 5 6
EGADS : 8 Yes 0 0 1 0 1 1 2 5 6
EGADS : 9 Yes 0 0 1 0 1 2 3 4 10 11 13
EGADS : 10 Yes 0 0 1 0 1 9 11 12 13 14
EGADS : 11 Yes 0 0 1 0 1 9 10 12 13 14
EGADS : 12 Yes 0 0 1 0 1 3 4 6 10 11 14
EGADS : 13 Yes 0 0 1 0 1 9 10 11
EGADS : 14 Yes 0 0 1 0 1 10 11 12
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 4 3 -2
EGADS : 2 5 1 -6 -7 8 9
EGADS : 3 10 -12 -11 8
EGADS : 4 -10 9 11 -13
EGADS : 5 7 14 -15 -16
EGADS : 6 -17 15 18 -3 -12 -13
EGADS : 7 16 17 -4 -5
EGADS : 8 -14 6 2 -18
EGADS : 9 -8 -9 19 20
EGADS : 10 21 -23 -22 19
EGADS : 11 -21 20 22 -24
EGADS : 12 12 13 -23 -24
EGADS : 13 -19 -20
EGADS : 14 23 24
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2 3
EGADS : 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7 8
EGADS : 7 9
EGADS : 8 10
EGADS : 9 11 12
EGADS : 10 13
EGADS : 11 14
EGADS : 12 15 16
EGADS : 13 17
EGADS : 14 18
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 -1 4 3 -2
EGADS : 2 Yes 1 5 1 -6 -7
EGADS : 3 Yes 1 8 9
EGADS : 4 Yes 1 10 -12 -11 8
EGADS : 5 Yes 1 -10 9 11 -13
EGADS : 6 Yes 1 7 14 -15 -16
EGADS : 7 Yes 1 -17 15 18 -3
EGADS : 8 Yes 1 -12 -13
EGADS : 9 Yes 1 16 17 -4 -5
EGADS : 10 Yes 1 -14 6 2 -18
EGADS : 11 Yes 1 -8 -9
EGADS : 12 Yes 1 19 20
EGADS : 13 Yes 1 21 -23 -22 19
EGADS : 14 Yes 1 -21 20 22 -24
EGADS : 15 Yes 1 12 13
EGADS : 16 Yes 1 -23 -24
EGADS : 17 Yes 1 -19 -20
EGADS : 18 Yes 1 23 24
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 8
EGADS : 3 0 Yes 4 3 1 1 6
EGADS : 4 0 Yes 2 4 1 1 7
EGADS : 5 0 Yes 5 2 1 2 7
EGADS : 6 0 Yes 6 1 1 2 8
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 7 8 1 2 3 9
EGADS : 9 0 Yes 8 7 1 2 4 9
EGADS : 10 0 Yes 8 9 1 3 4
EGADS : 11 0 Yes 7 10 1 3 4
EGADS : 12 0 Yes 10 9 1 3 6 12
EGADS : 13 0 Yes 9 10 1 4 6 12
EGADS : 14 0 Yes 6 11 1 5 8
EGADS : 15 0 Yes 12 11 1 5 6
EGADS : 16 0 Yes 5 12 1 5 7
EGADS : 17 0 Yes 12 4 1 6 7
EGADS : 18 0 Yes 11 3 1 6 8
EGADS : 19 0 Yes 13 14 1 9 10 13
EGADS : 20 0 Yes 14 13 1 9 11 13
EGADS : 21 0 Yes 14 15 1 10 11
EGADS : 22 0 Yes 13 16 1 10 11
EGADS : 23 0 Yes 16 15 1 10 12 14
EGADS : 24 0 Yes 15 16 1 11 12 14
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0.5 0 0.5
EGADS : 2 Yes 0.5 0 0
EGADS : 3 Yes 0.5 0.5 0.5
EGADS : 4 Yes 0.5 0.5 0
EGADS : 5 Yes 0 0 0
EGADS : 6 Yes 0 0 0.5
EGADS : 7 Yes 0 0 0.2
EGADS : 8 Yes 0 0 0
EGADS : 9 Yes 0 0.5 0
EGADS : 10 Yes 0 0.5 0.2
EGADS : 11 Yes 0 0.5 0.5
EGADS : 12 Yes 0 0.5 0
EGADS : 13 Yes 0 0 0.1
EGADS : 14 Yes 0 0 0
EGADS : 15 Yes 0 0.5 0
EGADS : 16 Yes 0 0.5 0.1
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 1
AFLR4 : Min Bounding Box Length = 1
AFLR4 : Max Ref Bounding Box Length = 1
AFLR4 : Min Ref Bounding Box Length = 1
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.005
AFLR4 : Max Surf Spacing = 0.1
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 TRANSP
AFLR4 : 4 CAD geometry 0 TRANSP
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 TRANSP
AFLR4 : 11 CAD geometry 0 TRANSP
AFLR4 : 12 CAD geometry 0 STD
AFLR4 : 13 CAD geometry 0 STD
AFLR4 : 14 CAD geometry 0 STD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 486 868 0
AFLR4 : Nodes, Trias,Quads= 477 850 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1904 3642 0
AFLR4 : Nodes, Trias,Quads= 1889 3612 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1904 3642 0
AFLR4 : Nodes, Trias,Quads= 1889 3612 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 486 868 0
AFLR4 : Nodes, Trias,Quads= 476 848 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 135 228 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 582 1036 0
AFLR4 : Nodes, Trias,Quads= 576 1024 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 3745 7224 0
AFLR4 : Nodes, Trias,Quads= 3741 7216 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 3745 7224 0
AFLR4 : Nodes, Trias,Quads= 3741 7216 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 582 1036 0
AFLR4 : Nodes, Trias,Quads= 576 1024 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 402 738 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 515 964 0
AFLR4 : Nodes, Trias,Quads= 413 760 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 13768 27788 1608
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 13768 27788
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 507 910 0
AFLR4 : Nodes, Trias,Quads= 712 1320 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1877 3588 0
AFLR4 : Nodes, Trias,Quads= 1882 3598 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1876 3586 0
AFLR4 : Nodes, Trias,Quads= 1883 3600 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 506 908 0
AFLR4 : Nodes, Trias,Quads= 710 1316 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 576 1024 0
AFLR4 : Nodes, Trias,Quads= 576 1024 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 3736 7206 0
AFLR4 : Nodes, Trias,Quads= 3727 7188 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 3735 7204 0
AFLR4 : Nodes, Trias,Quads= 3730 7194 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 576 1024 0
AFLR4 : Nodes, Trias,Quads= 576 1024 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 406 746 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 498 930 0
AFLR4 : Nodes, Trias,Quads= 416 766 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 14206 28664 1608
OVERALL : CPU Time = 0.281 seconds
Body 1 (of 1)
Number of nodes = 14206
Number of elements = 28664
Number of triangle elements = 28664
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14206
Total number of elements = 28664
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = box, index = 1
Name = cyl2, index = 2
Name = box;cyl2, index = 3
Name = cyl1, index = 4
Name = cyl1;box;cyl2, index = 5
Number of surface: nodes - 14206, elements - 28664
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.229219
Creating surface mesh ...
Surface mesh seconds: 0.025515
Recovering boundaries...
Boundary recovery seconds: 0.130483
Removing exterior tetrahedra ...
Warning: The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.017217
Recovering Delaunayness...
Delaunay recovery seconds: 0.169805
Refining mesh...
Refinement seconds: 0.59539
Smoothing vertices...
Mesh smoothing seconds: 0.924834
Improving mesh...
Mesh improvement seconds: 0.034514
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.009742
Total running seconds: 2.13706
Statistics:
Input points: 14206
Input facets: 28664
Input segments: 42868
Input holes: 0
Input regions: 3
Mesh points: 22419
Mesh tetrahedra: 122162
Mesh faces: 247866
Mesh faces on exterior boundary: 7084
Mesh faces on input facets: 28664
Mesh edges on input segments: 42868
Steiner points inside domain: 8213
Done meshing using TetGen!
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing exodus file ....
Block: 'b_tet', blk_id 1, num_entries 58372
Block: 'c_tet', blk_id 2, num_entries 27468
Block: 'a_tet', blk_id 3, num_entries 36322
Sideset: 'box', set_id 1, num_entries 7084
Sideset: 'cyl1', set_id 2, num_entries 15894
Sideset: 'cyl2', set_id 3, num_entries 10758
Finished writing Exodus file
real 0m5.538s
user 0m4.511s
sys 0m0.325s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case plato_aflr_tetgen_cyli_box_PyTest.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
Nastran
Mystran
=================================================
All tests pass!
=================================================
=================================================
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest
++ ./execute_PyTestRegression.sh STRUCTURE
=================================================
Legacy Using python : /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/ESP/venv/bin/python
=================================================
Running.... STRUCTURE PyTests
=================================================
+ rm -rf masstran_PyTest
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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 3.428666259749
Mass 5383.006027806
Centroid [1.222256036872, 0.1634981473779, -4.647736192456e-11]
CG [1.222256036872, 0.1634981473779, -4.647907951721e-11]
Ixx 22133.97306031
Iyy 23448.30046704
Izz 1389.213122564
Ixy 164.2055275655
Ixz -7.485782319314e-06
Iyz 1.710545499156e-06
I [22133.97306031, 23448.30046704, 1389.213122564, 164.2055275655, -7.485782319314e-06, 1.710545499156e-06]
II [[22133.97306031, -164.2055275655, 7.485782319314e-06], [-164.2055275655, 23448.30046704, -1.710545499156e-06], [7.485782319314e-06, -1.710545499156e-06, 1389.213122564]]
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 0m5.311s
user 0m6.306s
sys 0m7.276s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 36
Number of elements = 25
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 25
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Getting results mass properties.....
Area 547.7004
Mass 0.01605224431138
Centroid [20.03586282449, 14.01686746988, 0.0]
CG [20.03586282449, 14.01686746988, 0.0]
Ixx 1.140246300554
Iyy 0.919317482675
Izz 2.059563783229
Ixy 0.7352134614013
Ixz 0.0
Iyz 0.0
I [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0]
II [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.508s
user 0m0.544s
sys 0m0.112s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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 0m1.291s
user 0m0.823s
sys 0m0.107s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf hsm_CantileverPlate_PyTest
+ echo 'hsm_CantileverPlate_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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 0.10 0.00)
1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 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 0.00 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 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 0.03 0.00)
3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 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 0.03 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 0.07 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 0.00 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 0.07 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00)
8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 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 0.00 0.00)
9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 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 0.10 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
iter dr dd dp rlx max
11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.00 0.00)
11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.00 0.00)
12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.07 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 0.10 0.00)
14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.10 0.00)
15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00)
16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.00 0.00)
17 0.148E-15 0.575E-15 0.104E-14 1.000 dps @ ( 1.00 0.10 0.00)
Converging n vectors ...
it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 )
it = 2 dn = 0.423E-15 rlx = 1.000 ( 31 )
Converging e1,e2 vectors ...
it = 1 de = 0.285E+01 rlx = 0.351 ( 24 )
it = 2 de = 0.269E+01 rlx = 0.372 ( 14 )
it = 3 de = 0.202E+01 rlx = 0.494 ( 40 )
it = 4 de = 0.122E+01 rlx = 0.820 ( 40 )
it = 5 de = 0.378E+00 rlx = 1.000 ( 40 )
it = 6 de = 0.127E-01 rlx = 1.000 ( 14 )
it = 7 de = 0.524E-06 rlx = 1.000 ( 40 )
it = 8 de = 0.938E-16 rlx = 1.000 ( 22 )
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 0m1.327s
user 0m0.836s
sys 0m0.132s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_Aeroelastic_PyTest
+ echo 'astros_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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
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 0m23.941s
user 0m15.706s
sys 0m3.297s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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 0m1.248s
user 0m0.627s
sys 0m0.215s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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 0m1.460s
user 0m0.828s
sys 0m0.220s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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 = 443
Number of elements = 845
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 845
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) = 5.90553 (Hz)
Natural freq (Mode 2) = 29.72860 (Hz)
Natural freq (Mode 3) = 39.11840 (Hz)
Natural freq (Mode 4) = 77.46400 (Hz)
Natural freq (Mode 5) = 99.53050 (Hz)
Natural freq (Mode 6) = 146.35200 (Hz)
Natural freq (Mode 7) = 178.74700 (Hz)
Natural freq (Mode 8) = 234.29900 (Hz)
Natural freq (Mode 9) = 278.97300 (Hz)
Natural freq (Mode 10) = 313.52300 (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 = 443 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 = 443 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 = 443 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 = 443 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 = 443 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 0m55.475s
user 0m40.766s
sys 0m1.458s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
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 0m1.261s
user 0m1.021s
sys 0m0.312s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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
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 0m0.919s
user 0m0.931s
sys 0m0.168s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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 0m16.785s
user 0m14.028s
sys 0m4.589s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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
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 0m0.892s
user 0m0.792s
sys 0m0.165s
+ 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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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 0m0.875s
user 0m0.734s
sys 0m0.171s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_ThreeBarLinkDesign_PyTest
+ echo 'astros_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarLinkDesign_PyTest.py test;
+ python -u astros_ThreeBarLinkDesign_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
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 Astros......
Done running Astros!
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py", line 212, in <module>
nastranAIM.postAnalysis()
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/problem.py", line 2159, in postAnalysis
self._analysisObj.postAnalysis()
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/caps.py", line 2913, in postAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
nastranAIM.c:3037 in aimPostAnalysis():
Error: Unable to open file: threebar_nastran_Test.f06
================================================================================
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'!
real 0m0.722s
user 0m0.604s
sys 0m0.155s
+ status=1
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBarLinkDesign_PyTest.py failed (as NOT expected)
=================================================
=================================================
+ rm -rf astros_ThreeBarMultiLoad_PyTest
+ echo 'astros_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u astros_ThreeBarMultiLoad_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 - 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 0m0.893s
user 0m0.804s
sys 0m0.173s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_ThreeBar_PyTest
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ echo 'astros_ThreeBar_PyTest.py test;'
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.880s
user 0m0.815s
sys 0m0.174s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_Trim_15degree
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ echo 'astros_Trim_15degree.py test;'
astros_Trim_15degree.py test;
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN_ARM64/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
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 0m1.225s
user 0m0.953s
sys 0m0.261s
+ 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
=================================================
=================================================
Legacy Summary of examples NOT finished as expected
astros_ThreeBarLinkDesign_PyTest.py
See pyCAPSlog.txt for more details.
=================================================
=================================================
=================================================
Build step 'Conditional step (single)' marked build as failure
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE