Skipping 957 KB..
Full LogRefining mesh...
Refinement seconds: 0.00052
Improving mesh...
Mesh improvement seconds: 0.000654
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000281
Total running seconds: 0.04179
Statistics:
Input points: 642
Input facets: 1280
Input segments: 1920
Input holes: 0
Input regions: 1
Mesh points: 642
Mesh tetrahedra: 1722
Mesh faces: 4084
Mesh faces on exterior boundary: 1280
Mesh faces on input facets: 1280
Mesh edges on input segments: 1920
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.159129
Creating surface mesh ...
Surface mesh seconds: 0.00262
Recovering boundaries...
Boundary recovery seconds: 0.009903
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.001872
Recovering Delaunayness...
Delaunay recovery seconds: 0.048521
Refining mesh...
Refinement seconds: 0.131978
Smoothing vertices...
Mesh smoothing seconds: 0.109886
Improving mesh...
Mesh improvement seconds: 0.001849
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000635
Total running seconds: 0.466571
Statistics:
Input points: 1066
Input facets: 2128
Input segments: 3192
Input holes: 0
Input regions: 2
Mesh points: 1307
Mesh tetrahedra: 4393
Mesh faces: 9850
Mesh faces on exterior boundary: 2128
Mesh faces on input facets: 2128
Mesh edges on input segments: 3192
Steiner points inside domain: 241
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.161584
Creating surface mesh ...
Surface mesh seconds: 0.002131
Recovering boundaries...
Boundary recovery seconds: 0.009613
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: 0.002079
Recovering Delaunayness...
Delaunay recovery seconds: 0.049116
Refining mesh...
Refinement seconds: 0.131518
Smoothing vertices...
Mesh smoothing seconds: 0.107053
Improving mesh...
Mesh improvement seconds: 0.00185
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000575
Total running seconds: 0.465645
Statistics:
Input points: 1066
Input facets: 2128
Input segments: 3192
Input holes: 0
Input regions: 3
Mesh points: 1302
Mesh tetrahedra: 4374
Mesh faces: 9812
Mesh faces on exterior boundary: 2128
Mesh faces on input facets: 2128
Mesh edges on input segments: 3192
Steiner points inside domain: 236
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.160191
Creating surface mesh ...
Surface mesh seconds: 0.001852
Recovering boundaries...
Boundary recovery seconds: 0.009178
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: 0.001762
Recovering Delaunayness...
Delaunay recovery seconds: 0.046663
Refining mesh...
Refinement seconds: 0.127666
Smoothing vertices...
Mesh smoothing seconds: 0.11134
Improving mesh...
Mesh improvement seconds: 0.001779
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000448
Total running seconds: 0.460994
Statistics:
Input points: 1066
Input facets: 2128
Input segments: 3192
Input holes: 0
Input regions: 4
Mesh points: 1313
Mesh tetrahedra: 4448
Mesh faces: 9960
Mesh faces on exterior boundary: 2128
Mesh faces on input facets: 2128
Mesh edges on input segments: 3192
Steiner points inside domain: 247
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.157109
Creating surface mesh ...
Surface mesh seconds: 0.001775
Recovering boundaries...
Boundary recovery seconds: 0.009218
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: 0.001898
Recovering Delaunayness...
Delaunay recovery seconds: 0.048204
Refining mesh...
Refinement seconds: 0.130468
Smoothing vertices...
Mesh smoothing seconds: 0.110291
Improving mesh...
Mesh improvement seconds: 0.001808
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000484
Total running seconds: 0.461438
Statistics:
Input points: 1066
Input facets: 2128
Input segments: 3192
Input holes: 0
Input regions: 5
Mesh points: 1306
Mesh tetrahedra: 4416
Mesh faces: 9896
Mesh faces on exterior boundary: 2128
Mesh faces on input facets: 2128
Mesh edges on input segments: 3192
Steiner points inside domain: 240
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 4393
Block: 'leg1_tet', blk_id 3, num_entries 4374
Block: 'leg2_tet', blk_id 4, num_entries 4448
Block: 'leg3_tet', blk_id 5, num_entries 4416
Sideset: 'leg0Side', set_id 1, num_entries 2128
Sideset: 'leg1Side', set_id 2, num_entries 2128
Sideset: 'leg2Side', set_id 3, num_entries 2128
Sideset: 'leg3Side', set_id 4, num_entries 2128
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 0m6.567s
user 0m3.844s
sys 0m0.515s
+ 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/DARWIN64/ESP/DARWIN64/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/DARWIN64/ESP/DARWIN64/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 = 3600
Number of elements = 7324
Number of triangle elements = 7324
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3600
Total number of elements = 7324
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 - 3600, elements - 7324
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.34277
Creating surface mesh ...
Surface mesh seconds: 0.007326
Recovering boundaries...
Boundary recovery seconds: 0.047677
Removing exterior tetrahedra ...
Warning: The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.003499
Recovering Delaunayness...
Delaunay recovery seconds: 0.285591
Refining mesh...
Refinement seconds: 0.466782
Smoothing vertices...
Mesh smoothing seconds: 0.586411
Improving mesh...
Mesh improvement seconds: 0.011263
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.002228
Total running seconds: 1.75403
Statistics:
Input points: 3600
Input facets: 7324
Input segments: 10922
Input holes: 0
Input regions: 3
Mesh points: 5637
Mesh tetrahedra: 29545
Mesh faces: 60704
Mesh faces on exterior boundary: 3228
Mesh faces on input facets: 7324
Mesh edges on input segments: 10922
Steiner points inside domain: 2037
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 12826
Block: 'b_tet', blk_id 2, num_entries 11151
Block: 'a_tet', blk_id 3, num_entries 5568
Sideset: 'box', set_id 1, num_entries 3228
Sideset: 'cyl1', set_id 2, num_entries 2120
Sideset: 'cyl2', set_id 3, num_entries 2314
Finished writing Exodus file
real 0m6.311s
user 0m3.639s
sys 0m0.492s
+ 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/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
plato_aflr_tetgen_table_PyTest.py test;
+ python -u plato_aflr_tetgen_table_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
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 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
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 Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes -5 8 7 -6
EGADS : 3 Yes 9 5 -10 -1
EGADS : 4 Yes -11 3 12 -7
EGADS : 5 Yes 4 11 -8 -9
EGADS : 6 Yes -2 10 6 -12
EGADS : 7 Yes -13 -14 15 16
EGADS : 8 Yes 17 14 -18 -16
EGADS : 9 Yes 13 18
EGADS : 10 Yes -15 -17
EGADS : 11 Yes -19 -20 21 22
EGADS : 12 Yes 23 20 -24 -22
EGADS : 13 Yes 19 24
EGADS : 14 Yes -21 -23
EGADS : 15 Yes -25 -26 27 28
EGADS : 16 Yes 29 26 -30 -28
EGADS : 17 Yes 25 30
EGADS : 18 Yes -27 -29
EGADS : 19 Yes -31 -32 33 34
EGADS : 20 Yes 35 32 -36 -34
EGADS : 21 Yes 31 36
EGADS : 22 Yes -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= 2245 4304 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Nodes, Trias,Quads= 2247 4308 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= 2248 4310 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= 2247 4308 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= 2244 4302 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= 20654 41288 2208
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 21567 43114
AFLR4 : Nodes, Trias = 22451 44882
AFLR4 : Nodes, Trias = 22543 45066
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= 2273 4356 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2276 4362 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= 2274 4358 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= 2271 4352 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2274 4358 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= 2271 4352 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2276 4362 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 = 2.951 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 = 5134
Number of elements = 10264
Number of triangle elements = 10264
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 5132
Number of elements = 10260
Number of triangle elements = 10260
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 5130
Number of elements = 10256
Number of triangle elements = 10256
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 5132
Number of elements = 10260
Number of triangle elements = 10260
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 - 5134, elements - 10264
Body 3 number of surface: nodes - 5132, elements - 10260
Body 4 number of surface: nodes - 5130, elements - 10256
Body 5 number of surface: nodes - 5132, elements - 10260
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.046857
Creating surface mesh ...
Surface mesh seconds: 0.007147
Recovering boundaries...
Boundary recovery seconds: 0.029144
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.003332
Recovering Delaunayness...
Delaunay recovery seconds: 0.009559
Refining mesh...
Refinement seconds: 0.057993
Smoothing vertices...
Mesh smoothing seconds: 0.100805
Improving mesh...
Mesh improvement seconds: 0.005164
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.002189
Total running seconds: 0.262686
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: 0.084089
Creating surface mesh ...
Surface mesh seconds: 0.010809
Recovering boundaries...
Boundary recovery seconds: 0.065264
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.029872
Recovering Delaunayness...
Delaunay recovery seconds: 0.029232
Refining mesh...
Refinement seconds: 0.202306
Smoothing vertices...
Mesh smoothing seconds: 0.207834
Improving mesh...
Mesh improvement seconds: 0.008264
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.004272
Total running seconds: 0.642239
Statistics:
Input points: 5134
Input facets: 10264
Input segments: 15396
Input holes: 0
Input regions: 2
Mesh points: 6599
Mesh tetrahedra: 23322
Mesh faces: 51776
Mesh faces on exterior boundary: 10264
Mesh faces on input facets: 10264
Mesh edges on input segments: 15396
Steiner points inside domain: 1465
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.085948
Creating surface mesh ...
Surface mesh seconds: 0.009853
Recovering boundaries...
Boundary recovery seconds: 0.067267
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: 0.030264
Recovering Delaunayness...
Delaunay recovery seconds: 0.028815
Refining mesh...
Refinement seconds: 0.205859
Smoothing vertices...
Mesh smoothing seconds: 0.206366
Improving mesh...
Mesh improvement seconds: 0.009332
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.004503
Total running seconds: 0.648469
Statistics:
Input points: 5132
Input facets: 10260
Input segments: 15390
Input holes: 0
Input regions: 3
Mesh points: 6597
Mesh tetrahedra: 23258
Mesh faces: 51646
Mesh faces on exterior boundary: 10260
Mesh faces on input facets: 10260
Mesh edges on input segments: 15390
Steiner points inside domain: 1465
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.089887
Creating surface mesh ...
Surface mesh seconds: 0.010241
Recovering boundaries...
Boundary recovery seconds: 0.070078
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: 0.029814
Recovering Delaunayness...
Delaunay recovery seconds: 0.028101
Refining mesh...
Refinement seconds: 0.204681
Smoothing vertices...
Mesh smoothing seconds: 0.210632
Improving mesh...
Mesh improvement seconds: 0.008545
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.003746
Total running seconds: 0.655985
Statistics:
Input points: 5130
Input facets: 10256
Input segments: 15384
Input holes: 0
Input regions: 4
Mesh points: 6610
Mesh tetrahedra: 23420
Mesh faces: 51968
Mesh faces on exterior boundary: 10256
Mesh faces on input facets: 10256
Mesh edges on input segments: 15384
Steiner points inside domain: 1480
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.086158
Creating surface mesh ...
Surface mesh seconds: 0.010048
Recovering boundaries...
Boundary recovery seconds: 0.059938
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: 0.029166
Recovering Delaunayness...
Delaunay recovery seconds: 0.025957
Refining mesh...
Refinement seconds: 0.197809
Smoothing vertices...
Mesh smoothing seconds: 0.209257
Improving mesh...
Mesh improvement seconds: 0.008502
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00486
Total running seconds: 0.63191
Statistics:
Input points: 5132
Input facets: 10260
Input segments: 15390
Input holes: 0
Input regions: 5
Mesh points: 6601
Mesh tetrahedra: 23353
Mesh faces: 51836
Mesh faces on exterior boundary: 10260
Mesh faces on input facets: 10260
Mesh edges on input segments: 15390
Steiner points inside domain: 1469
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 23322
Block: 'leg1_tet', blk_id 3, num_entries 23258
Block: 'leg2_tet', blk_id 4, num_entries 23420
Block: 'leg3_tet', blk_id 5, num_entries 23353
Sideset: 'leg0Side', set_id 1, num_entries 10264
Sideset: 'leg1Side', set_id 2, num_entries 10260
Sideset: 'leg2Side', set_id 3, num_entries 10256
Sideset: 'leg3Side', set_id 4, num_entries 10260
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 0m11.204s
user 0m7.596s
sys 0m0.705s
+ 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/DARWIN64/ESP/DARWIN64/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/DARWIN64/ESP/DARWIN64/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
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 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
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 Edges
EGADS : 1 Yes -1 4 3 -2
EGADS : 2 Yes 5 1 -6 -7
EGADS : 3 Yes 8 9
EGADS : 4 Yes 10 -12 -11 8
EGADS : 5 Yes -10 9 11 -13
EGADS : 6 Yes 7 14 -15 -16
EGADS : 7 Yes -17 15 18 -3
EGADS : 8 Yes -12 -13
EGADS : 9 Yes 16 17 -4 -5
EGADS : 10 Yes -14 6 2 -18
EGADS : 11 Yes -8 -9
EGADS : 12 Yes 19 20
EGADS : 13 Yes 21 -23 -22 19
EGADS : 14 Yes -21 20 22 -24
EGADS : 15 Yes 12 13
EGADS : 16 Yes -23 -24
EGADS : 17 Yes -19 -20
EGADS : 18 Yes 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= 134 226 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 135 228 0
AFLR4 : Nodes, Trias,Quads= 131 220 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= 13767 27786 1608
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 13767 27786
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 137 232 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= 711 1318 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1882 3598 0
AFLR4 : Nodes, Trias,Quads= 1883 3600 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1876 3586 0
AFLR4 : Nodes, Trias,Quads= 1882 3598 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= 499 894 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= 137 232 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= 14205 28662 1608
OVERALL : CPU Time = 0.449 seconds
Body 1 (of 1)
Number of nodes = 14205
Number of elements = 28662
Number of triangle elements = 28662
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14205
Total number of elements = 28662
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 - 14205, elements - 28662
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.253359
Creating surface mesh ...
Surface mesh seconds: 0.029797
Recovering boundaries...
Boundary recovery seconds: 0.146833
Removing exterior tetrahedra ...
Warning: The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.02015
Recovering Delaunayness...
Delaunay recovery seconds: 0.173279
Refining mesh...
Refinement seconds: 0.877553
Smoothing vertices...
Mesh smoothing seconds: 1.23333
Improving mesh...
Mesh improvement seconds: 0.046531
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.014117
Total running seconds: 2.79626
Statistics:
Input points: 14205
Input facets: 28662
Input segments: 42865
Input holes: 0
Input regions: 3
Mesh points: 22379
Mesh tetrahedra: 121977
Mesh faces: 247495
Mesh faces on exterior boundary: 7082
Mesh faces on input facets: 28662
Mesh edges on input segments: 42865
Steiner points inside domain: 8174
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 58303
Block: 'a_tet', blk_id 2, num_entries 36164
Block: 'c_tet', blk_id 3, num_entries 27510
Sideset: 'box', set_id 1, num_entries 7082
Sideset: 'cyl1', set_id 2, num_entries 15894
Sideset: 'cyl2', set_id 3, num_entries 10758
Finished writing Exodus file
real 0m9.445s
user 0m8.395s
sys 0m0.716s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest
++ ./execute_PyTestRegression.sh STRUCTURE
=================================================
Legacy Using python : /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/ESP/venv/bin/python
=================================================
Running.... STRUCTURE PyTests
=================================================
+ rm -rf masstran_PyTest
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting results mass properties.....
Area 3.428666259747
Mass 5383.006027803
Centroid [1.222256036874, 0.1634981473778, -4.234377369776e-11]
CG [1.222256036874, 0.1634981473778, -4.234490614246e-11]
Ixx 22133.97306033
Iyy 23448.30046709
Izz 1389.213122582
Ixy 164.2055275657
Ixz -7.454850140458e-06
Iyz 1.707682988152e-06
I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454850140458e-06, 1.707682988152e-06]
II [[22133.97306033, -164.2055275657, 7.454850140458e-06], [-164.2055275657, 23448.30046709, -1.707682988152e-06], [7.454850140458e-06, -1.707682988152e-06, 1389.213122582]]
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 0m7.227s
user 0m11.722s
sys 0m6.473s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
masstran_AGARD445_PyTest.py test;
+ python -u masstran_AGARD445_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 36
Number of elements = 25
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 25
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Getting results mass properties.....
Area 547.7004
Mass 0.01605224431138
Centroid [20.03586282449, 14.01686746988, 0.0]
CG [20.03586282449, 14.01686746988, 0.0]
Ixx 1.140246300554
Iyy 0.919317482675
Izz 2.059563783229
Ixy 0.7352134614013
Ixz 0.0
Iyz 0.0
I [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0]
II [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.138s
user 0m0.748s
sys 0m0.311s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.750s
user 0m1.252s
sys 0m0.213s
+ 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/DARWIN64/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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 51
Elemental Tria3 = 0
Elemental Quad4 = 27
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1313
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.03 0.00)
1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.03 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.03 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.03 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.07 0.00)
8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.10 0.00)
9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.00 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
iter dr dd dp rlx max
11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.10 0.00)
11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00)
12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00)
13* 0.336E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00)
15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.10 0.00)
16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00)
17 0.558E-15 0.304E-14 0.603E-15 1.000 ddx @ ( 1.00 0.00 0.00)
Converging n vectors ...
it = 1 dn = 0.193E+01 rlx = 1.000 ( 12 )
it = 2 dn = 0.435E-15 rlx = 1.000 ( 28 )
Converging e1,e2 vectors ...
it = 1 de = 0.285E+01 rlx = 0.351 ( 24 )
it = 2 de = 0.292E+01 rlx = 0.342 ( 34 )
it = 3 de = 0.226E+01 rlx = 0.442 ( 34 )
it = 4 de = 0.151E+01 rlx = 0.660 ( 34 )
it = 5 de = 0.665E+00 rlx = 1.000 ( 34 )
it = 6 de = 0.609E-01 rlx = 1.000 ( 34 )
it = 7 de = 0.573E-04 rlx = 1.000 ( 34 )
it = 8 de = 0.478E-13 rlx = 1.000 ( 34 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMCantileverPlate.dat
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.342s
user 0m1.029s
sys 0m0.199s
+ 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/DARWIN64/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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Wing, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 286
Number of elements = 386
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 92
Elemental Quad4 = 294
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 287
Combined Number of elements = 387
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 92
Combined Elemental Quad4 = 294
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 48
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Ribs
No "material" specified for Property tuple Ribs, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Property name - Spar1
No "material" specified for Property tuple Spar1, defaulting to an index of 1
Property name - Spar2
No "material" specified for Property tuple Spar2, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
30 automatic connections were made for capsConnect Rib_Root (node id 287)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m13.788s
user 0m21.281s
sys 0m5.359s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_AGARD445_PyTest.py test;
+ python -u astros_AGARD445_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 36
Number of elements = 25
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 25
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
Getting results natural frequencies.....
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 2
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Natural freq (Mode 1) = 5.78 (Hz)
Natural freq (Mode 2) = 30.66 (Hz)
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.356s
user 0m0.876s
sys 0m0.377s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_Composite_PyTest.py test;
+ python -u astros_Composite_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 15
Number of elements = 8
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 8
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - cantilever
No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
Running Astros......
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m2.049s
user 0m0.956s
sys 0m0.385s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = wing, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - wing
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = root, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = wing, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = wing, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 429
Number of elements = 817
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 817
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - wing
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - root
No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
Running Astros......
Done running Astros!
Getting results for natural frequencies.....
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 5.91949 (Hz)
Natural freq (Mode 2) = 29.79990 (Hz)
Natural freq (Mode 3) = 39.10550 (Hz)
Natural freq (Mode 4) = 77.71580 (Hz)
Natural freq (Mode 5) = 99.79550 (Hz)
Natural freq (Mode 6) = 146.97500 (Hz)
Natural freq (Mode 7) = 176.90300 (Hz)
Natural freq (Mode 8) = 235.53300 (Hz)
Natural freq (Mode 9) = 274.42600 (Hz)
Natural freq (Mode 10) = 311.35900 (Hz)
No variable name provided - all variables will be writen to file
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsBound.writeTecplot' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].writeTecplot'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 1m0.087s
user 0m49.680s
sys 0m1.373s
+ 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/DARWIN64/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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m2.168s
user 0m1.324s
sys 0m0.597s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 16
Number of elements = 9
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 9
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 5
Load name - load_0
Load name - load_1
Load name - load_2
Load name - load_3
Load name - load_4
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 5
Analysis name - load_0
Analysis name - load_1
Analysis name - load_2
Analysis name - load_3
Analysis name - load_4
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
Writing analysis cards
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m2.130s
user 0m1.095s
sys 0m0.449s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 293
Number of elements = 217
Number of triangle elements = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes = 293
Total number of elements = 217
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 293
Number of elements = 217
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 217
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
Getting results for natural frequencies.....
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02335 (Hz)
Natural freq (Mode 2) = 0.02335 (Hz)
Natural freq (Mode 3) = 0.11619 (Hz)
Natural freq (Mode 4) = 0.11619 (Hz)
Natural freq (Mode 5) = 0.14468 (Hz)
Natural freq (Mode 6) = 0.14468 (Hz)
Natural freq (Mode 7) = 0.23352 (Hz)
Natural freq (Mode 8) = 0.23352 (Hz)
Natural freq (Mode 9) = 0.30497 (Hz)
Natural freq (Mode 10) = 0.30497 (Hz)
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m24.027s
user 0m24.020s
sys 0m7.406s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 6
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 6
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m2.059s
user 0m0.969s
sys 0m0.433s
+ 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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ python -u astros_ThreeBarFreq_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
Getting results for natural frequencies.....
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 2
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Natural freq (Mode 1) = 86.13400 (Hz)
Natural freq (Mode 2) = 168.53300 (Hz)
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.396s
user 0m0.942s
sys 0m0.449s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_ThreeBarMultiLoad_PyTest
+ echo 'astros_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ python -u astros_ThreeBarMultiLoad_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 2
Constraint name - conOne
No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
Constraint name - conTwo
No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - loadOne
Load name - loadTwo
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 2
Analysis name - analysisOne
Analysis name - analysisTwo
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m2.369s
user 0m0.935s
sys 0m0.382s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_ThreeBar_PyTest
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
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/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.402s
user 0m0.920s
sys 0m0.408s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_Trim_15degree
+ echo 'astros_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ python -u astros_Trim_15degree.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - Body
Property name - Edge
Property name - Root
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - PointSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Getting FEA loads.......
Number of loads - 2
Load name - GravityLoad
No "groupName" specified for Load tuple GravityLoad, going to use load name
Load name - PointLoad
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m1.827s
user 0m1.260s
sys 0m0.543s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Legacy Did not run examples for:
Nastran
Mystran
=================================================
All tests pass!
=================================================
=================================================
[Execution node] check if [macys] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/STRUCTURE/DARWIN64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.8,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWIN64,buildnode=macys #660'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS
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