Skipping 1,273 KB..
Full LogEGADS : 3 Yes 0 0 2
EGADS : 4 Yes 0 0 0
EGADS : 5 Yes 0 2 2
EGADS : 6 Yes 0 2 0
EGADS : 7 Yes 14 0 2
EGADS : 8 Yes 14 0 0
EGADS : 9 Yes 14 2 2
EGADS : 10 Yes 14 2 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 15
AFLR4 : Min Bounding Box Length = 4
AFLR4 : Max Ref Bounding Box Length = 1
AFLR4 : Min Ref Bounding Box Length = 1
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 0.5
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.1
AFLR4 : Max Surf Spacing = 0.5
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 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 FARFIELD
AFLR4 : 8 CAD geometry 0 FARFIELD
AFLR4 : 9 CAD geometry 0 FARFIELD
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 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 103 173 0
AFLR4 : Nodes, Trias,Quads= 100 167 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 388 692 0
AFLR4 : Nodes, Trias,Quads= 388 692 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 105 177 0
AFLR4 : Nodes, Trias,Quads= 103 173 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1738 3468 512
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1738 3468
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 104 175 0
AFLR4 : Nodes, Trias,Quads= 99 165 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 388 692 0
AFLR4 : Nodes, Trias,Quads= 391 698 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 102 171 0
AFLR4 : Nodes, Trias,Quads= 102 171 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 91 148 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1739 3470 512
OVERALL : CPU Time = 0.159 seconds
Body 1 (of 2)
Number of nodes = 519
Number of elements = 1034
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1034
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1739
Total number of elements = 3470
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 2 Shells
EGADS : Body 0 has 14 Faces
EGADS : Body 0 has 27 Edges
EGADS : Body 0 has 14 Loops
EGADS : Body 0 has 17 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 NA NA 2 3 4 5
EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 8 9 10 11
EGADS : 8 Yes 0 0 1 0 1 7 10 11 12
EGADS : 9 Yes 0 0 1 0 1 7 12 13 14
EGADS : 10 Yes 0 0 1 0 1 7 8 11 13
EGADS : 11 Yes 0 0 1 0 1 7 8 10
EGADS : 12 Yes 0 0 1 0 1 8 9 13 14
EGADS : 13 Yes 0 0 1 0 1 9 10 12 14
EGADS : 14 Yes 0 0 1 0 1 9 12 13
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8
EGADS : 4 -10 3 8 -11
EGADS : 5 4 10 -12 -5
EGADS : 6 -6 12 11 -9
EGADS : 7 -13 14 15 -16
EGADS : 8 -17 18 13 -19
EGADS : 9 20 22 -21 -14
EGADS : 10 -15 23 17 -24
EGADS : 11 16 24 19
EGADS : 12 25 26 -20 -18
EGADS : 13 21 27 -25 -23
EGADS : 14 -22 -26 -27
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 : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 1 2 -3 -4
EGADS : 2 Yes 1 5 6 -7 -1
EGADS : 3 Yes 1 -2 7 9 -8
EGADS : 4 Yes 1 -10 3 8 -11
EGADS : 5 Yes 1 4 10 -12 -5
EGADS : 6 Yes 1 -6 12 11 -9
EGADS : 7 Yes 1 -13 14 15 -16
EGADS : 8 Yes 1 -17 18 13 -19
EGADS : 9 Yes 1 20 22 -21 -14
EGADS : 10 Yes 1 -15 23 17 -24
EGADS : 11 Yes 1 16 24 19
EGADS : 12 Yes 1 25 26 -20 -18
EGADS : 13 Yes 1 21 27 -25 -23
EGADS : 14 Yes 1 -22 -26 -27
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 NA 1 2
EGADS : 2 0 Yes 1 3 NA 1 3
EGADS : 3 0 Yes 4 3 NA 1 4
EGADS : 4 0 Yes 2 4 NA 1 5
EGADS : 5 0 Yes 2 5 NA 2 5
EGADS : 6 0 Yes 5 6 NA 2 6
EGADS : 7 0 Yes 1 6 NA 2 3
EGADS : 8 0 Yes 3 7 NA 3 4
EGADS : 9 0 Yes 6 7 NA 3 6
EGADS : 10 0 Yes 4 8 NA 4 5
EGADS : 11 0 Yes 8 7 NA 4 6
EGADS : 12 0 Yes 5 8 NA 5 6
EGADS : 13 0 Yes 9 10 1 7 8
EGADS : 14 0 Yes 9 11 1 7 9
EGADS : 15 0 Yes 11 12 1 7 10
EGADS : 16 0 Yes 10 12 1 7 11
EGADS : 17 0 Yes 13 14 1 8 10
EGADS : 18 0 Yes 13 9 1 8 12
EGADS : 19 0 Yes 14 10 1 8 11
EGADS : 20 0 Yes 9 15 1 9 12
EGADS : 21 0 Yes 11 16 1 9 13
EGADS : 22 0 Yes 15 16 1 9 14
EGADS : 23 0 Yes 11 13 1 10 13
EGADS : 24 0 Yes 12 14 1 10 11
EGADS : 25 0 Yes 13 17 1 12 13
EGADS : 26 0 Yes 17 15 1 12 14
EGADS : 27 0 Yes 16 17 1 13 14
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 40
EGADS : 2 Yes 0 0 0
EGADS : 3 Yes 0 40 40
EGADS : 4 Yes 0 40 0
EGADS : 5 Yes 40 0 0
EGADS : 6 Yes 40 0 40
EGADS : 7 Yes 40 40 40
EGADS : 8 Yes 40 40 0
EGADS : 9 Yes 3.77246052 0 0.00459131419
EGADS : 10 Yes 5.90487498 7.07106781 0
EGADS : 11 Yes 0 0 0
EGADS : 12 Yes 4.0824829 7.07106781 0.123425948
EGADS : 13 Yes 3.77001182 0 0
EGADS : 14 Yes 5.90282524 7.07106781 0
EGADS : 15 Yes 5.90487498 0 0
EGADS : 16 Yes 4.0824829 0 0.123425948
EGADS : 17 Yes 5.90282524 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 80
AFLR4 : Min Bounding Box Length = 80
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 2.82843
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 7.60986
AFLR4 : Abs Min Surf Spacing = 0.00707107
AFLR4 : Min Surf Spacing = 0.0141421
AFLR4 : Max Surf Spacing = 0.282843
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 FARFIELD
AFLR4 : 2 CAD geometry 0 FARFIELD
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
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 : 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= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 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= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 17055 33380 0
AFLR4 : Nodes, Trias,Quads= 7507 14284 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 182 241 0
AFLR4 : Nodes, Trias,Quads= 122 121 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 17164 33598 0
AFLR4 : Nodes, Trias,Quads= 7368 14006 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 14987 29245 0
AFLR4 : Nodes, Trias,Quads= 6879 13029 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 330 546 0
AFLR4 : Nodes, Trias,Quads= 322 530 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 182 241 0
AFLR4 : Nodes, Trias,Quads= 122 121 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 14793 28857 0
AFLR4 : Nodes, Trias,Quads= 6844 12959 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 328 542 0
AFLR4 : Nodes, Trias,Quads= 324 534 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 28462 56916 3616
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 28462 56916
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= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 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= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 15590 30449 0
AFLR4 : Nodes, Trias,Quads= 9447 18163 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 254 370 0
AFLR4 : Nodes, Trias,Quads= 136 134 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 15870 31009 0
AFLR4 : Nodes, Trias,Quads= 9439 18147 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 14689 28649 0
AFLR4 : Nodes, Trias,Quads= 9247 17765 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 346 577 0
AFLR4 : Nodes, Trias,Quads= 359 603 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 254 370 0
AFLR4 : Nodes, Trias,Quads= 136 134 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 14582 28435 0
AFLR4 : Nodes, Trias,Quads= 9309 17889 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 348 581 0
AFLR4 : Nodes, Trias,Quads= 361 607 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 37391 74774 3650
OVERALL : CPU Time = 1.115 seconds
Body 1 (of 1)
Number of nodes = 37391
Number of elements = 74774
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 74774
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 37391
Total number of elements = 74774
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 2 Shells
EGADS : Body 0 has 14 Faces
EGADS : Body 0 has 27 Edges
EGADS : Body 0 has 14 Loops
EGADS : Body 0 has 17 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 NA NA 2 3 4 5
EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 8 9 10 11
EGADS : 8 Yes 0 0 1 0 1 7 10 11 12
EGADS : 9 Yes 0 0 1 0 1 7 12 13 14
EGADS : 10 Yes 0 0 1 0 1 7 8 11 13
EGADS : 11 Yes 0 0 1 0 1 7 8 10
EGADS : 12 Yes 0 0 1 0 1 8 9 13 14
EGADS : 13 Yes 0 0 1 0 1 9 10 12 14
EGADS : 14 Yes 0 0 1 0 1 9 12 13
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8
EGADS : 4 -10 3 8 -11
EGADS : 5 4 10 -12 -5
EGADS : 6 -6 12 11 -9
EGADS : 7 -13 14 15 -16
EGADS : 8 -17 18 13 -19
EGADS : 9 20 22 -21 -14
EGADS : 10 -15 23 17 -24
EGADS : 11 16 24 19
EGADS : 12 25 26 -20 -18
EGADS : 13 21 27 -25 -23
EGADS : 14 -22 -26 -27
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 : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 1 2 -3 -4
EGADS : 2 Yes 1 5 6 -7 -1
EGADS : 3 Yes 1 -2 7 9 -8
EGADS : 4 Yes 1 -10 3 8 -11
EGADS : 5 Yes 1 4 10 -12 -5
EGADS : 6 Yes 1 -6 12 11 -9
EGADS : 7 Yes 1 -13 14 15 -16
EGADS : 8 Yes 1 -17 18 13 -19
EGADS : 9 Yes 1 20 22 -21 -14
EGADS : 10 Yes 1 -15 23 17 -24
EGADS : 11 Yes 1 16 24 19
EGADS : 12 Yes 1 25 26 -20 -18
EGADS : 13 Yes 1 21 27 -25 -23
EGADS : 14 Yes 1 -22 -26 -27
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 NA 1 2
EGADS : 2 0 Yes 1 3 NA 1 3
EGADS : 3 0 Yes 4 3 NA 1 4
EGADS : 4 0 Yes 2 4 NA 1 5
EGADS : 5 0 Yes 2 5 NA 2 5
EGADS : 6 0 Yes 5 6 NA 2 6
EGADS : 7 0 Yes 1 6 NA 2 3
EGADS : 8 0 Yes 3 7 NA 3 4
EGADS : 9 0 Yes 6 7 NA 3 6
EGADS : 10 0 Yes 4 8 NA 4 5
EGADS : 11 0 Yes 8 7 NA 4 6
EGADS : 12 0 Yes 5 8 NA 5 6
EGADS : 13 0 Yes 9 10 1 7 8
EGADS : 14 0 Yes 9 11 1 7 9
EGADS : 15 0 Yes 11 12 1 7 10
EGADS : 16 0 Yes 10 12 1 7 11
EGADS : 17 0 Yes 13 14 1 8 10
EGADS : 18 0 Yes 13 9 1 8 12
EGADS : 19 0 Yes 14 10 1 8 11
EGADS : 20 0 Yes 9 15 1 9 12
EGADS : 21 0 Yes 11 16 1 9 13
EGADS : 22 0 Yes 15 16 1 9 14
EGADS : 23 0 Yes 11 13 1 10 13
EGADS : 24 0 Yes 12 14 1 10 11
EGADS : 25 0 Yes 13 17 1 12 13
EGADS : 26 0 Yes 17 15 1 12 14
EGADS : 27 0 Yes 16 17 1 13 14
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 40
EGADS : 2 Yes 0 0 0
EGADS : 3 Yes 0 40 40
EGADS : 4 Yes 0 40 0
EGADS : 5 Yes 40 0 0
EGADS : 6 Yes 40 0 40
EGADS : 7 Yes 40 40 40
EGADS : 8 Yes 40 40 0
EGADS : 9 Yes 3.77246052 0 0.00459131419
EGADS : 10 Yes 5.90487498 7.07106781 0
EGADS : 11 Yes 0 0 0
EGADS : 12 Yes 4.0824829 7.07106781 0.123425948
EGADS : 13 Yes 3.77001182 0 0
EGADS : 14 Yes 5.90282524 7.07106781 0
EGADS : 15 Yes 5.90487498 0 0
EGADS : 16 Yes 4.0824829 0 0.123425948
EGADS : 17 Yes 5.90282524 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 80
AFLR4 : Min Bounding Box Length = 80
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 5.65685
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 7.62074
AFLR4 : Abs Min Surf Spacing = 0.0141421
AFLR4 : Min Surf Spacing = 0.0282843
AFLR4 : Max Surf Spacing = 0.565685
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 FARFIELD
AFLR4 : 2 CAD geometry 0 FARFIELD
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
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 : 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= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 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= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 6411 12401 0
AFLR4 : Nodes, Trias,Quads= 3253 6085 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 192 273 0
AFLR4 : Nodes, Trias,Quads= 110 109 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 6519 12617 0
AFLR4 : Nodes, Trias,Quads= 3180 5939 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5814 11207 0
AFLR4 : Nodes, Trias,Quads= 3048 5675 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 257 412 0
AFLR4 : Nodes, Trias,Quads= 256 410 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 192 273 0
AFLR4 : Nodes, Trias,Quads= 110 109 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5862 11303 0
AFLR4 : Nodes, Trias,Quads= 3028 5635 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 258 414 0
AFLR4 : Nodes, Trias,Quads= 256 410 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 12856 25704 2334
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 12856 25704
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= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 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= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 6200 11975 0
AFLR4 : Nodes, Trias,Quads= 4633 8841 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 226 328 0
AFLR4 : Nodes, Trias,Quads= 122 120 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 6154 11884 0
AFLR4 : Nodes, Trias,Quads= 4634 8844 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5942 11461 0
AFLR4 : Nodes, Trias,Quads= 4482 8541 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 263 424 0
AFLR4 : Nodes, Trias,Quads= 268 434 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 226 328 0
AFLR4 : Nodes, Trias,Quads= 122 120 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5975 11528 0
AFLR4 : Nodes, Trias,Quads= 4473 8524 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 265 428 0
AFLR4 : Nodes, Trias,Quads= 270 438 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 18601 37194 2370
OVERALL : CPU Time = 0.498 seconds
Body 1 (of 1)
Number of nodes = 18601
Number of elements = 37194
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 37194
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 18601
Total number of elements = 37194
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Analysis object with the name, aflr4AIM, has already been initilized
An altName of aflr4AIM_5 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 2 Faces
EGADS : Body 0 has 6 Edges
EGADS : Body 0 has 2 Loops
EGADS : Body 0 has 2 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 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
EGADS : 2 Yes 0 0 1 0 1 1
EGADS : 3 Yes 1 0 1 NA NA 5 6 7 8
EGADS : 4 Yes 1 0 1 NA NA 5 6 7 8
EGADS : 5 Yes 1 0 1 NA NA 3 4 7 8
EGADS : 6 Yes 1 0 1 NA NA 3 4 7 8
EGADS : 7 Yes 1 0 1 NA NA 3 4 5 6
EGADS : 8 Yes 1 0 1 NA NA 3 4 5 6
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 -2 3 4
EGADS : 2 -5 -4 6 2
EGADS : 3 7 8 -9 -10
EGADS : 4 -11 14 13 -12
EGADS : 5 15 11 -16 -7
EGADS : 6 -17 9 18 -13
EGADS : 7 10 17 -14 -15
EGADS : 8 -8 16 12 -18
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 : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 -1 -2 3 4
EGADS : 2 Yes 1 -5 -4 6 2
EGADS : 3 Yes 1 7 8 -9 -10
EGADS : 4 Yes 1 -11 14 13 -12
EGADS : 5 Yes 1 15 11 -16 -7
EGADS : 6 Yes 1 -17 9 18 -13
EGADS : 7 Yes 1 10 17 -14 -15
EGADS : 8 Yes 1 -8 16 12 -18
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 DEGEN 1 1 - 1
EGADS : 2 0 Yes 2 1 1 1 2
EGADS : 3 0 DEGEN 2 2 - 1
EGADS : 4 0 Yes 2 1 1 1 2
EGADS : 5 0 DEGEN 1 1 - 2
EGADS : 6 0 DEGEN 2 2 - 2
EGADS : 7 1 Yes 4 3 NA 3 5
EGADS : 8 1 Yes 3 5 NA 3 8
EGADS : 9 1 Yes 6 5 NA 3 6
EGADS : 10 1 Yes 4 6 NA 3 7
EGADS : 11 1 Yes 8 7 NA 4 5
EGADS : 12 1 Yes 7 9 NA 4 8
EGADS : 13 1 Yes 10 9 NA 4 6
EGADS : 14 1 Yes 8 10 NA 4 7
EGADS : 15 1 Yes 4 8 NA 5 7
EGADS : 16 1 Yes 3 7 NA 5 8
EGADS : 17 1 Yes 6 10 NA 6 7
EGADS : 18 1 Yes 5 9 NA 6 8
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 8.5 0 0.5
EGADS : 2 Yes 8.5 0 0
EGADS : 3 Yes 0 0 2
EGADS : 4 Yes 0 0 0
EGADS : 5 Yes 0 2 2
EGADS : 6 Yes 0 2 0
EGADS : 7 Yes 14 0 2
EGADS : 8 Yes 14 0 0
EGADS : 9 Yes 14 2 2
EGADS : 10 Yes 14 2 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 15
AFLR4 : Min Bounding Box Length = 4
AFLR4 : Max Ref Bounding Box Length = 1
AFLR4 : Min Ref Bounding Box Length = 1
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 0.5
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.1
AFLR4 : Max Surf Spacing = 0.5
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 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 FARFIELD
AFLR4 : 8 CAD geometry 0 FARFIELD
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 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 94 154 0
AFLR4 : Nodes, Trias,Quads= 202 370 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 94 154 0
AFLR4 : Nodes, Trias,Quads= 201 368 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1591 3174 432
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1591 3174
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 81 130 0
AFLR4 : Nodes, Trias,Quads= 203 374 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 81 130 0
AFLR4 : Nodes, Trias,Quads= 200 368 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 91 148 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1593 3178 428
OVERALL : CPU Time = 0.057 seconds
Body 1 (of 2)
Number of nodes = 373
Number of elements = 742
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 742
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1593
Total number of elements = 3178
.
Analysis object with the name, aflr4AIM, has already been initilized
An altName of aflr4AIM_6 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 1 Faces
EGADS : Body 0 has 2 Edges
EGADS : Body 0 has 1 Loops
EGADS : Body 0 has 1 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 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
EGADS : 2 Yes 1 0 1 NA NA 4 5 6 7
EGADS : 3 Yes 1 0 1 NA NA 4 5 6 7
EGADS : 4 Yes 1 0 1 NA NA 2 3 6 7
EGADS : 5 Yes 1 0 1 NA NA 2 3 6 7
EGADS : 6 Yes 1 0 1 NA NA 2 3 4 5
EGADS : 7 Yes 1 0 1 NA NA 2 3 4 5
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 1 -2
EGADS : 2 3 4 -5 -6
EGADS : 3 -7 10 9 -8
EGADS : 4 11 7 -12 -3
EGADS : 5 -13 5 14 -9
EGADS : 6 6 13 -10 -11
EGADS : 7 -4 12 8 -14
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 : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 -1 2 1 -2
EGADS : 2 Yes 1 3 4 -5 -6
EGADS : 3 Yes 1 -7 10 9 -8
EGADS : 4 Yes 1 11 7 -12 -3
EGADS : 5 Yes 1 -13 5 14 -9
EGADS : 6 Yes 1 6 13 -10 -11
EGADS : 7 Yes 1 -4 12 8 -14
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 1 1 1 1 1
EGADS : 2 0 Yes 1 1 1 1 1
EGADS : 3 1 Yes 3 2 NA 2 4
EGADS : 4 1 Yes 2 4 NA 2 7
EGADS : 5 1 Yes 5 4 NA 2 5
EGADS : 6 1 Yes 3 5 NA 2 6
EGADS : 7 1 Yes 7 6 NA 3 4
EGADS : 8 1 Yes 6 8 NA 3 7
EGADS : 9 1 Yes 9 8 NA 3 5
EGADS : 10 1 Yes 7 9 NA 3 6
EGADS : 11 1 Yes 3 7 NA 4 6
EGADS : 12 1 Yes 2 6 NA 4 7
EGADS : 13 1 Yes 5 9 NA 5 6
EGADS : 14 1 Yes 4 8 NA 5 7
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 7.25 0 0
EGADS : 2 Yes 0 0 2
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 0 2 2
EGADS : 5 Yes 0 2 0
EGADS : 6 Yes 14 0 2
EGADS : 7 Yes 14 0 0
EGADS : 8 Yes 14 2 2
EGADS : 9 Yes 14 2 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 15
AFLR4 : Min Bounding Box Length = 4
AFLR4 : Max Ref Bounding Box Length = 1.5
AFLR4 : Min Ref Bounding Box Length = 0.5
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 0.5
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.1
AFLR4 : Max Surf Spacing = 0.5
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 FARFIELD
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 FARFIELD
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 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 919 1710 0
AFLR4 : Nodes, Trias,Quads= 675 1222 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1831 3658 494
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1831 3658
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 930 1730 0
AFLR4 : Nodes, Trias,Quads= 728 1326 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 91 148 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1883 3762 496
OVERALL : CPU Time = 0.056 seconds
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 (of 2)
Number of nodes = 663
Number of elements = 1326
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1326
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1883
Total number of elements = 3762
.No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Rib_Root, index = 1
Name = Skin, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1
Number of elements = 1
Number of node elements = 1
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 46
Number of elements = 44
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes = 47
Total number of elements = 45
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 = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 46
Number of elements = 44
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 44
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 47
Combined Number of elements = 45
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 44
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 = 3
Surface 2: Number of points found for aero-spline = 6
(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 - 2
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, 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
8 automatic connections were made for capsConnect Rib_Root (node id 1)
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_UNDERFLOW_FLAG
Done running Astros!
.No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
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
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
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 ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
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 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 cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_1 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
Running avl......
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_2 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_3 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_4 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_5 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 0)
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Running avl......
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 9573
Number of elements = 19142
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19142
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 6160
Number of elements = 12316
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 12316
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 104
Number of elements = 204
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 204
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 15837
Total number of elements = 31662
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9583
Number of elements = 19158
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9583
Total number of elements = 19158
.ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 8)
Getting surface mesh for body 2 (of 8)
Getting surface mesh for body 3 (of 8)
Getting surface mesh for body 4 (of 8)
Getting surface mesh for body 5 (of 8)
Getting surface mesh for body 6 (of 8)
171457000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
171457000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 8)
Getting surface mesh for body 8 (of 8)
Body 1 (of 8)
Number of nodes = 1538
Number of elements = 3072
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Body 2 (of 8)
Number of nodes = 873
Number of elements = 1742
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1742
Number of quadrilateral elements = 0
Body 3 (of 8)
Number of nodes = 1315
Number of elements = 2626
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2626
Number of quadrilateral elements = 0
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 4 (of 8)
Number of nodes = 2048
Number of elements = 4096
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 5 (of 8)
Number of nodes = 822
Number of elements = 1640
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1640
Number of quadrilateral elements = 0
Body 6 (of 8)
Number of nodes = 1959
Number of elements = 3918
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3918
Number of quadrilateral elements = 0
Body 7 (of 8)
Number of nodes = 935
Number of elements = 1866
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1866
Number of quadrilateral elements = 0
Body 8 (of 8)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 83220
Total number of elements = 166416
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_1 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1538
Number of elements = 3072
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75268
Total number of elements = 150528
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_2 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
171457000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
171457000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1959
Number of elements = 3918
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3918
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75689
Total number of elements = 151374
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_3 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 935
Number of elements = 1866
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1866
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74665
Total number of elements = 149322
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_4 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1315
Number of elements = 2626
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2626
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75045
Total number of elements = 150082
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_5 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 873
Number of elements = 1742
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1742
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74603
Total number of elements = 149198
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9583
Number of elements = 19158
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9583
Total number of elements = 19158
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 7151
Number of elements = 14294
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 14294
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7151
Total number of elements = 14294
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_6 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 822
Number of elements = 1640
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1640
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74552
Total number of elements = 149096
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_7 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 (of 2)
Number of nodes = 2048
Number of elements = 4096
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75778
Total number of elements = 151552
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7800
Number of elements = 15596
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.114239
Creating surface mesh ...
Surface mesh seconds: 0.019618
Recovering boundaries...
Boundary recovery seconds: 0.097633
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.028325
Recovering Delaunayness...
Delaunay recovery seconds: 0.053846
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 1.60585
Smoothing vertices...
Mesh smoothing seconds: 1.70183
Improving mesh...
Mesh improvement seconds: 0.057736
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.018038
Total running seconds: 3.69743
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
Done meshing using TetGen!
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_1 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest4_fun3dAIM/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_2 will be used!
Getting CFD boundary conditions
Boundary condition name - Wing1
Warning: No boundary condition specified for capsGroup Wing2!
Warning: No boundary condition specified for capsGroup Farfield!
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml .....
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 378, in _readstream
Error: Python error occurred while writing namelist file
self._update_tokens()
File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 797, in _update_tokens
next_token = next(self.tokens)
^^^^^^^^^^^^^^^^^
StopIteration
During handling of the above exception, another exception occurred:
Traceback (most recent call last):
File "fun3dNamelist.pyx", line 103, in fun3dNamelist.fun3d_writeNMLPython
File "fun3dNamelist.pyx", line 65, in fun3dNamelist.read_fun3d_nml
File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/venv/lib/python3.11/site-packages/f90nml/__init__.py", line 31, in read
return parser.read(nml_path)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 281, in read
return self._readstream(nml_file, nml_patch)
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 380, in _readstream
raise ValueError(
ValueError: End-of-file before end of namelist group: '&badNamelist'
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_3 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_4 will be used!
Getting CFD boundary conditions
Boundary condition name - Wing1
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_5 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_6 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
.Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_7 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - Alpha
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 1
Objective name - LoD
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Reading rubber.data
.Closing fun3d!!!!
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 = 0
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 = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.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 = 0
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 = box1, index = 1
Face 3 TFI quading disabled with attribute .qParams
Face 6 TFI quading disabled with attribute .qParams
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4048
Number of elements = 6648
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5204
Elemental Quad4 = 1444
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.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 = 0
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 = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
.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 = 0
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 = box1, 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 = 400
Number of elements = 361
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 361
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7800
Number of elements = 15596
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.177096
Creating surface mesh ...
Surface mesh seconds: 0.04134
Recovering boundaries...
Boundary recovery seconds: 0.168031
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.048524
Recovering Delaunayness...
Delaunay recovery seconds: 0.063333
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 2.69747
Smoothing vertices...
Mesh smoothing seconds: 2.2442
Improving mesh...
Mesh improvement seconds: 0.057214
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.014674
Total running seconds: 5.51239
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
Done meshing using TetGen!
Analysis object with the name, su2AIM, has already been initilized
An altName of su2AIM_1 will be used!
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Wing1
.
Analysis object with the name, su2AIM, has already been initilized
An altName of su2AIM_2 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
.Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
Running xFoil......
.
----------------------------------------------------------------------
Ran 67 tests in 90.413s
OK (skipped=10)
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
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.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
Legacy AIM unit testing done!
(cd test; ./runUnitTest.sh)
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
aimTransferUtil Tests passed!
real 0m0.125s
user 0m0.066s
sys 0m0.005s
=============================================
+ expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aimTransferUtilTest passed (as expected)
=============================================
+ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 0.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of -2 must be greater than 1 for the input value 9.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 0 must be greater than 1 for the input value 9.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -1.000000E+100 with field with 7!
Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -9.900000E+99 with field with 7!
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 2 must be greater than 2 for the input value -1.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 1.000000E+00
Returning a 'NaN' string.
Error in convert_integerToString: Input 9999999 fails with requested fieldWidth of 6
Returning a 'NaN' string.
Error in convert_integerToString: Input -999999 fails with requested fieldWidth of 6
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth > 15 not verified
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0
Returning a 'NaN' string.
miscUtils Tests passed!
real 0m0.122s
user 0m0.073s
sys 0m0.006s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest passed (as expected)
=============================================
+ expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest
+ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest
vlmUtils Tests passed!
real 0m0.118s
user 0m0.065s
sys 0m0.005s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest passed (as expected)
=============================================
+ rm -rf aimTest
+ expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm'
+ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm
Root Path = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/test/aimTest/Scratch
testingAIM/aimInitialize instance = -1 unitSys = (null)!
caps_queryAnalysis = 0 4 3 1
testingAIM/aimInputs instance = -1 index = 1!
in 1: testingAIMin 0
testingAIM/aimInputs instance = -1 index = 2!
in 2: table 0
testingAIM/aimInputs instance = -1 index = 3!
in 3: tessIn 0
testingAIM/aimInputs instance = -1 index = 4!
in 4: meshFile 0
testingAIM/aimOutputs instance = -1 index = 1!
out 1: testingAIMout 0
testingAIM/aimOutputs instance = -1 index = 2!
out 2: tessOut 0
testingAIM/aimOutputs instance = -1 index = 3!
out 3: meshFile 0
testingAIM/aimInitialize instance = 0 unitSys = m!
testingAIM/aimInputs instance = 0 index = 1!
testingAIM/aimInputs instance = 0 index = 2!
testingAIM/aimInputs instance = 0 index = 3!
testingAIM/aimInputs instance = 0 index = 4!
testingAIM/aimOutputs instance = 0 index = 1!
testingAIM/aimOutputs instance = 0 index = 2!
testingAIM/aimOutputs instance = 0 index = 3!
testingAIM/aimBackdoor instance = 0: Input String!
Backdoor return string = aimBackdoor Output
testingAIM/aimInitialize instance = 1 unitSys = (null)!
testingAIM/aimInputs instance = 1 index = 1!
testingAIM/aimInputs instance = 1 index = 2!
testingAIM/aimInputs instance = 1 index = 3!
testingAIM/aimInputs instance = 1 index = 4!
testingAIM/aimOutputs instance = 1 index = 1!
testingAIM/aimOutputs instance = 1 index = 2!
testingAIM/aimOutputs instance = 1 index = 3!
Intent = child
APath = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/test/aimTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 1
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
Problem: # Dirty Analyses = 2!
Bound: # Dirty Analyses = 2!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 1!
testingAIM/aimUpdateState instance = 0!
tess is NULL!
testingAIM/aimPreAnalysis instance = 0!
testingAIM/aimPreAnalysis aim_getBounds = 0
Analysis in Bound = Interface
aim_newGeometry = 0!
getDiscr = 0
getDataSet = 0, rank = 1, method = 0
0 scalars!
meshRef = NULL
testingAIM/aimExecute instance = 0!
testingAIM/aimPostAnalysis instance = 0 restart = 0!
testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
After Execute on Parent
Problem: # Dirty Analyses = 1!
Bound: # Dirty Analyses = 1!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 0!
testingAIM/aimCalcOutput instance = 0 index = 2 tessOut 0!
tessPtr = 0
testingAIM/aimUpdateState instance = 1!
tess is NULL!
testingAIM/aimDiscr: tname = Interface, instance = 1!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 3 matches Interface!
testingAIM/aimDiscr: ntris = 2006!
testingAIM/aimDiscr: npts = 1062!
testingAIM/aimDiscr: tname = Interface, instance = 0!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 6 matches Interface!
testingAIM/aimDiscr: ntris = 772!
testingAIM/aimDiscr: npts = 433!
testingAIM/aimTransfer name = scalar instance = 0 npts = 433/1!
CAPS Info: Bound 'Interface' Normalized Integrated 'scalar'
Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 1.969212e-09
testingAIM/aimPreAnalysis instance = 1!
testingAIM/aimPreAnalysis aim_getBounds = 0
Analysis in Bound = Interface
aim_newGeometry = 0!
getDiscr = 0
getDataSet = -303, rank = 0, method = 0
vectors not setup yet!
testingAIM/aimExecute instance = 1!
testingAIM/aimPostAnalysis instance = 1 restart = 0!
Dirty = 0
Problem: # Dirty Analyses = 0!
Bound: # Dirty Analyses = 0!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 0!
Body 1 has length units = cm
Body 2 has length units = cm
aimTest has type PROBLEM, subtype PARAMETRIC with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds
ParamName has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 2
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 2
value = 0.000000 (null)
Param has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 3
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 3
value = 99 (null)
num has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 6
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 6
value = 8.000000 (null)
x has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
value (8x1) = 7.300000 8.400000 10.400000 11.300000 12.300000 13.800000 14.400000 17.200000 (null)
ymin has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
value (8x1) = -1.250000 -1.900000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 (null)
zmin has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
value (8x1) = -0.825000 -0.812500 -0.800000 -0.775000 -0.750000 -0.700000 -0.690000 -0.100000 (null)
zmax has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
value (8x1) = 0.825000 0.812500 0.800000 0.775000 0.750000 0.700000 0.690000 0.100000 (null)
unused has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 7
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 1
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 7
linked to ParamName
pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 16
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 16
value = 34.641525 (null)
cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 16
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 16
value = 7.296560 (null)
testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 18
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 8
value = 5.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 8
value (1x3) =
1: Entry1 -> Value1
2: Entry2 -> Value2
3: Entry3 -> Value3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 8
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 8
value (0x0) = NULL with len = 0 meter
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 9
testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0!
aim_getDiscr 0 on Interface = 0
aim_getDataSet 0 on Interface = -329
value = 12.340000 cm
lazy: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 18
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 18
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 18
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 9
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 18
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 18
value = 42 (null)
testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 28
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 28
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 10
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 10
value = 6.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 12
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 12
value (1x3) =
1: Entry1 -> newValue1
2: Entry2 -> newValue2
3: Entry3 -> newValue3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 13
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 23
linked to tessOut
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 10
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 10
value (0x0) = NULL with len = 0 meter
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 11
testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0!
aim_getDiscr 1 on Interface = 0
aim_getDataSet 1 on Interface = -329
value = 12.340000 cm
lazy: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 28
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 11
testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0!
tessPtr = 600003ce0600
value = 600003ce0600 ego
lazy: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 28
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 11
testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 28
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 28
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 28
value = 42 (null)
Interface has type BOUND, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 14
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
2 Connecteds, 0 UnConnecteds
testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
5 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
1062 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
1062 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 26
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 15
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:55 26
1062 points, rank=1, units=(null)
testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
6 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
433 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 23
433 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 25
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:28 25
433 points, rank=1, units=(null)
vector has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:20814 jenkins 2024/03/30 23:26:27 0
testingAIM/aimTransfer name = vector instance = 0 npts = 433/3!
433 points, rank=3, units=(null)
1: 14.400001 14.400001 14.400000 14.400001 14.400001 14.400000 14.400000
8: 14.400001 14.400000 14.400003 14.380571 14.400001 14.381441 14.400000
15: 14.400000 14.400002 14.400002 14.400000 14.400000 14.400002 14.400000
22: 14.400001 14.400001 14.400000 14.383000 14.400000 14.400000 14.400001
29: 14.400000 14.390397 14.400001 14.400000 14.400000 14.400002 14.400002
36: 14.400001 14.400001 14.390256 14.400001 14.389522 14.400002 14.400002
43: 14.400002 14.400000 14.400000 14.400002 14.400003 14.400003 14.400003
50: 14.400000 14.379777 14.400000 14.400001 14.378056 14.400000 14.400000
57: 14.400000 14.400001 14.376355 14.400002 14.400000 14.400000 14.400001
64: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400000 14.400001
71: 14.381349 14.400000 14.400002 14.400002 14.400002 14.400000 14.400000
78: 14.400000 14.400000 14.400001 14.400001 14.390810 14.400001 14.384482
85: 14.400000 14.400000 14.400001 14.400001 14.400001 14.400001 14.400000
92: 14.400002 14.400000 14.400000 14.400001 14.400001 14.400001 14.400000
99: 14.400000 14.400002 14.400000 14.400002 14.400000 14.400000 14.400000
106: 14.400002 14.400002 14.400002 14.400003 14.400003 14.400003 14.400003
113: 14.400003 14.400000 14.400000 14.400000 14.400001 14.400001 14.400001
120: 14.400002 14.400000 14.399999 14.400001 14.400002 14.400001 14.400002
127: 14.400001 14.400001 14.400000 14.400001 14.400001 14.400001 14.400002
134: 14.400002 14.400002 14.400002 14.400002 14.400003 14.400001 14.400001
141: 14.400002 14.400001 14.400002 14.400001 14.400002 14.400001 14.400002
148: 14.399999 14.400001 14.400001 14.400001 14.400001 14.400002 14.400001
155: 14.400001 14.400001 14.400001 14.400003 14.400001 14.400001 14.400001
162: 14.400001 14.400001 14.400002 14.400001 14.400001 14.400000 14.400001
169: 14.400001 14.400001 14.400001 14.400000 14.400001 14.400001 14.400002
176: 14.400000 14.400001 14.400001 14.400002 14.400002 14.400002 14.400002
183: 14.400001 14.400002 14.400002 14.400001 14.400001 14.400002 14.400001
190: 14.400001 14.400001 14.400002 14.399999 14.400001 14.400002 14.400002
197: 14.400001 14.400002 14.400001 14.400001 14.400002 14.400001 14.400001
204: 14.400002 14.400001 14.400001 14.400002 14.400002 14.400002 14.400002
211: 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001 14.400001
218: 14.400000 14.400001 14.400002 14.400001 14.400001 14.400002 14.400001
225: 14.400001 14.400001 14.400002 14.400002 14.400002 14.400001 14.400001
232: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400002 14.400000
239: 14.400000 14.400002 14.400000 14.400001 14.400001 14.400001 14.400002
246: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001
253: 14.400002 14.400002 14.400001 14.400001 14.400001 14.400001 14.400001
260: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001
267: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400001 14.400001
274: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400002
281: 14.400001 14.400001 14.400000 14.400001 14.399999 14.400001 14.400002
288: 14.400001 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001
295: 14.400003 14.400001 14.400001 14.400001 14.400002 14.400001 14.400001
302: 14.400002 14.400001 14.400001 14.400000 14.400001 14.400002 14.400000
309: 14.400002 14.400001 14.400001 14.400001 14.400002 14.400001 14.400000
316: 14.400001 14.400001 14.400001 14.400002 14.400001 14.400001 14.399999
323: 14.400001 14.400001 14.355208 14.400002 14.400002 14.400001 14.400001
330: 14.400000 14.400000 14.400001 14.399999 14.400001 14.400000 14.400001
337: 14.400001 14.400001 14.400003 14.400002 14.399999 14.400001 14.400000
344: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001
351: 14.400002 14.400001 14.400000 14.400006 14.400002 14.400001 14.400000
358: 14.400000 14.400001 14.400001 14.400001 14.399999 14.400002 14.400001
365: 14.400001 14.400002 14.400000 14.400001 14.357384 14.400000 14.399999
372: 14.400002 14.400002 14.400002 14.400001 14.400001 14.400001 14.399999
379: 14.400001 14.399999 14.400002 14.400002 14.400001 14.400001 14.400001
386: 14.400002 14.400000 14.399999 14.400001 14.400001 14.400000 14.400000
393: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400002 14.400001
400: 14.400002 14.400001 14.399999 14.400002 14.399999 14.400001 14.400001
407: 14.400000 14.400001 14.400002 14.400001 14.400002 14.400001 14.400001
414: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400004 14.359138
421: 14.400005 14.399999 14.400001 14.400000 14.400001 14.400001 14.400001
428: 14.400002 14.399999 14.400000 14.400000 14.400002 14.400001 14.400004
435: 14.400004 14.362514 14.362329 14.400001 14.399999 14.400001 14.400001
442: 14.400001 14.400001 14.400002 14.400003 14.399999 14.400001 14.400002
449: 14.400001 14.400001 14.400002 14.400001 14.399999 14.400001 14.399999
456: 14.400001 14.400002 14.400004 14.400000 14.399999 14.400000 14.400000
463: 14.400001 14.399999 14.362644 14.400001 14.400002 14.399999 14.399999
470: 14.400001 14.400001 14.400001 14.399999 14.400001 14.400001 14.366558
477: 14.400001 14.400006 14.400001 14.400000 14.400001 14.400000 14.400001
484: 14.400004 14.400001 14.400005 14.399999 14.400002 14.400001 14.400005
491: 14.399999 14.400002 14.399999 14.367443 14.400003 14.400001 14.400000
498: 14.400001 14.400001 14.362493 14.399999 14.400001 14.399999 14.400001
505: 14.399999 14.400005 14.399999 14.400004 14.400001 14.400004 14.363391
512: 14.400001 14.366127 14.400002 14.400004 14.399999 14.400001 14.400004
519: 14.399999 14.400001 14.399999 14.400001 14.364370 14.399999 14.400005
526: 14.400005 14.365691 14.399999 14.369927 14.400002 14.400001 14.400000
533: 14.400000 14.368701 14.400001 14.399999 14.400000 14.399999 14.364370
540: 14.360914 14.399999 14.400001 14.400005 14.400004 14.400002 14.399999
547: 14.400000 14.399999 14.366320 14.400001 14.400003 14.370716 14.367841
554: 14.367007 14.367819 14.399999 14.369566 14.400001 14.399999 14.399999
561: 14.366648 14.367456 14.400005 14.400002 14.366344 14.400000 14.369947
568: 14.400004 14.400004 14.367007 14.373369 14.400001 14.400000 14.400002
575: 14.365408 14.400004 14.400000 14.400004 14.399999 14.400005 14.400002
582: 14.399999 14.400002 14.400001 14.400004 14.400004 14.369590 14.400004
589: 14.372211 14.400002 14.400000 14.400002 14.400002 14.400003 14.400000
596: 14.400004 14.400004 14.373403 14.368774 14.400000 14.400000 14.399999
603: 14.400001 14.400002 14.370406 14.367007 14.400001 14.372363 14.400001
610: 14.370598 14.400000 14.399999 14.400002 14.400004 14.372320 14.400000
617: 14.400000 14.368054 14.400004 14.400000 14.378759 14.400000 14.366320
624: 14.400000 14.400000 14.400004 14.370366 14.370760 14.400002 14.400004
631: 14.400004 14.400004 14.369692 14.365169 14.400004 14.400004 14.400000
638: 14.399999 14.400005 14.368369 14.400001 14.400000 14.400000 14.400003
645: 14.400003 14.399999 14.400002 14.400001 14.370996 14.400001 14.400002
652: 14.400002 14.367680 14.400000 14.400004 14.400000 14.400003 14.400003
659: 14.367301 14.400000 14.371052 14.400000 14.400004 14.375426 14.372158
666: 14.400000 14.370146 14.399999 14.400004 14.399999 14.368248 14.400000
673: 14.400003 14.369989 14.370548 14.368054 14.377207 14.400000 14.369613
680: 14.368333 14.400004 14.400001 14.377741 14.400003 14.400000 14.400004
687: 14.400003 14.400003 14.400000 14.377967 14.399999 14.376780 14.370538
694: 14.373367 14.400000 14.400003 14.400004 14.370294 14.371052 14.400000
701: 14.400003 14.370426 14.400004 14.400001 14.400001 14.376281 14.375920
708: 14.377357 14.400000 14.376914 14.400001 14.400002 14.400002 14.400002
715: 14.400003 14.379840 14.370996 14.400003 14.400003 14.370673 14.400000
722: 14.363653 14.362250 14.373534 14.400003 14.379510 14.400000 14.374657
729: 14.400003 14.400004 14.400002 14.379679 14.400000 14.379827 14.372479
736: 14.400002 14.380745 14.379344 14.379423 14.400003 14.380718 14.372490
743: 14.376209 14.400000 14.400000 14.400000 14.400000 14.400000 14.400003
750: 14.375014 14.373465 14.400000 14.400003 14.380638 14.400002 14.400002
757: 14.400000 14.376150 14.400003 14.400003 14.370382 14.379062 14.379044
764: 14.382714 14.371636 14.380688 14.372490 14.400004 14.380301 14.400003
771: 14.400003 14.400003 14.400003 14.381338 14.400003 14.400000 14.375566
778: 14.383460 14.400000 14.400000 14.382573 14.378742 14.378784 14.400002
785: 14.400003 14.377962 14.400003 14.388515 14.372960 14.400003 14.373659
792: 14.400000 14.376226 14.400000 14.400000 14.373627 14.400000 14.400002
799: 14.379592 14.400001 14.384129 14.381281 14.380925 14.400002 14.400000
806: 14.376874 14.400003 14.400000 14.376488 14.400002 14.372785 14.382064
813: 14.400002 14.400002 14.400002 14.400002 14.400002 14.400003 14.400003
820: 14.375490 14.374772 14.400003 14.375179 14.376681 14.379475 14.400003
827: 14.374392 14.379479 14.377005 14.387430 14.400002 14.382223 14.400003
834: 14.374371 14.383997 14.382259 14.386520 14.400000 14.400002 14.384358
841: 14.381380 14.373136 14.380004 14.382103 14.400002 14.400000 14.376043
848: 14.400000 14.381875 14.400002 14.377417 14.379456 14.400000 14.379534
855: 14.400002 14.400003 14.400000 14.400003 14.400000 14.400000 14.382400
862: 14.384944 14.376706 14.383227 14.400002 14.380291 14.400002 14.382257
869: 14.400003 14.384774 14.384820 14.382273 14.373450 14.400000 14.400003
876: 14.375908 14.378550 14.400000 14.377290 14.382472 14.379168 14.383016
883: 14.385491 14.382723 14.400003 14.400002 14.378971 14.385404 14.380466
890: 14.384576 14.400003 14.377221 14.400000 14.381355 14.383645 14.384247
897: 14.385287 14.383280 14.375114 14.400002 14.400000 14.400000 14.400000
904: 14.382426 14.382735 14.400002 14.382499 14.387660 14.382883 14.400002
911: 14.383520 14.387020 14.383842 14.382243 14.400000 14.378098 14.383884
918: 14.383573 14.384907 14.386099 14.400002 14.383499 14.385888 14.400002
925: 14.377060 14.378436 14.381620 14.380706 14.400000 14.373575 14.383742
932: 14.381255 14.382997 14.384659 14.382920 14.400000 14.400002 14.377577
939: 14.400000 14.386915 14.386123 14.384593 14.381816 14.381745 14.385286
946: 14.385286 14.382005 14.385759 14.385133 14.388988 14.381642 14.387570
953: 14.386633 14.386532 14.381505 14.386235 14.385447 14.400000 14.380013
960: 14.400000 14.382953 14.400002 14.383380 14.385229 14.383810 14.382999
967: 14.385309 14.400002 14.400002 14.382711 14.383198 14.385759 14.387667
974: 14.385183 14.384109 14.387476 14.400002 14.384433 14.388306 14.400002
981: 14.400002 14.383798 14.386396 14.386806 14.383774 14.389577 14.400000
988: 14.379854 14.381554 14.377995 14.375728 14.378018 14.382139 14.386343
995: 14.386055 14.378954 14.383869 14.400002 14.383263 14.385113 14.381831
1002: 14.400002 14.386892 14.388833 14.386742 14.385055 14.385000 14.381934
1009: 14.381408 14.380687 14.379175 14.380043 14.381323 14.375969 14.381364
1016: 14.384193 14.380959 14.400002 14.400002 14.400002 14.385962 14.400002
1023: 14.386889 14.381389 14.400002 14.379351 14.387189 14.400000 14.382624
1030: 14.400002 14.387047 14.400002 14.386889 14.379175 14.377388 14.389345
1037: 14.400002 14.400000 14.400000 14.381891 14.380687 14.400002 14.400000
1044: 14.383688 14.400002 14.400002 14.400002 14.383791 14.400000 14.400002
1051: 14.400003 14.400000 14.376605 14.400002 14.400000 14.376130 14.400003
1058: 14.383633 14.400002 14.400000 14.378191 14.384880
source getTriangles = 0, nGtris = 2006, nGsegs = 6018, Ds = 0 0
destin getTriangles = 0, nGtris = 772, nGsegs = 2316, Ds = 0 0
In caps_outputObjects:
2 Analyses found
1 Bounds found
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m28.214s
user 0m15.296s
sys 0m0.370s
+ set +x
+ rm -rf source.vs destin.vs
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm passed (as expected)
=============================================
+ expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm'
+ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm
testingAIM/aimInitialize instance = 0 unitSys = m!
testingAIM/aimInputs instance = 0 index = 1!
testingAIM/aimInputs instance = 0 index = 2!
testingAIM/aimInputs instance = 0 index = 3!
testingAIM/aimInputs instance = 0 index = 4!
testingAIM/aimOutputs instance = 0 index = 1!
testingAIM/aimOutputs instance = 0 index = 2!
testingAIM/aimOutputs instance = 0 index = 3!
testingAIM/aimInitialize instance = 1 unitSys = (null)!
testingAIM/aimInputs instance = 1 index = 1!
testingAIM/aimInputs instance = 1 index = 2!
testingAIM/aimInputs instance = 1 index = 3!
testingAIM/aimInputs instance = 1 index = 4!
testingAIM/aimOutputs instance = 1 index = 1!
testingAIM/aimOutputs instance = 1 index = 2!
testingAIM/aimOutputs instance = 1 index = 3!
Intent = child
APath = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/test/autoExecTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 2
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
testingAIM/aimUpdateState instance = 0!
tess is NULL!
testingAIM/aimPreAnalysis instance = 0!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
getDiscr = -303
meshRef = NULL
testingAIM/aimExecute instance = 0!
testingAIM/aimPostAnalysis instance = 0 restart = 0!
testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0!
aim_getDiscr 0 on Interface = -303
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
testingAIM/aimUpdateState instance = 1!
tess is NULL!
testingAIM/aimPreAnalysis instance = 1!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
mesh file = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/test/autoExecTest/Scratch/testingAIM0/meshFile
symLink = 0
getDiscr = -303
testingAIM/aimExecute instance = 1!
testingAIM/aimPostAnalysis instance = 1 restart = 0!
testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0!
aim_getDiscr 1 on Interface = -303
*** testingAIMout (child) = 12.340000 1 1 ***
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m0.558s
user 0m0.363s
sys 0m0.146s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm passed (as expected)
=============================================
++ set +x
[Execution node] check if [viggen] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.7,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #627'.
[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
![[Jenkins]](/csi/static/a404d988/images/svgs/logo.svg){kind=logo}
