Skipping 1,318 KB..
Full LogEGADS : 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 = 0.053 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 1.24
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 = 1.442 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 1.24
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 = 0.650 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 1.24
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= 199 366 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= 1592 3176 428
OVERALL : CPU Time = 0.042 seconds
Body 1 (of 2)
Number of nodes = 372
Number of elements = 740
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 740
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 = 1592
Total number of elements = 3176
.
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 1.24
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 = 0.091 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 = 120
Number of elements = 236
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 236
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 15853
Total number of elements = 31694
.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:60313)
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)
1DACB5000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1DACB5000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
16F9DF000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
16F9DF000 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)
16F9DF000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
16F9DF000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1DACB5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1DACB5000 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 = 7137
Number of elements = 14266
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 14266
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7137
Total number of elements = 14266
. 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 = 7802
Number of elements = 15600
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 15600
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 = 545
Number of elements = 1086
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1086
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14253
Total number of elements = 28494
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 - 14253, elements - 28494
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.253321
Creating surface mesh ...
Surface mesh seconds: 0.034466
Recovering boundaries...
Boundary recovery seconds: 0.124479
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.044751
Recovering Delaunayness...
Delaunay recovery seconds: 0.066866
Refining mesh...
18999 insertions, added 13806 points, 712098 tetrahedra in queue.
6326 insertions, added 2564 points, 586841 tetrahedra in queue.
8433 insertions, added 1779 points, 64950 tetrahedra in queue.
Refinement seconds: 3.2152
Smoothing vertices...
Mesh smoothing seconds: 3.04042
Improving mesh...
Mesh improvement seconds: 0.130798
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.016013
Total running seconds: 6.92704
Statistics:
Input points: 14253
Input facets: 28494
Input segments: 42741
Input holes: 2
Input regions: 0
Mesh points: 33071
Mesh tetrahedra: 159280
Mesh faces: 332807
Mesh faces on exterior boundary: 28494
Mesh faces on input facets: 28494
Mesh edges on input segments: 42741
Steiner points inside domain: 18818
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_UndefinedCaps/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_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml .....
Error: Python error occurred while writing namelist file
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 378, in _readstream
self._update_tokens()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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 = 7802
Number of elements = 15600
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 15600
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 = 545
Number of elements = 1086
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1086
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14253
Total number of elements = 28494
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 - 14253, elements - 28494
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.262435
Creating surface mesh ...
Surface mesh seconds: 0.044344
Recovering boundaries...
Boundary recovery seconds: 0.13953
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.05399
Recovering Delaunayness...
Delaunay recovery seconds: 0.078526
Refining mesh...
18999 insertions, added 13806 points, 712098 tetrahedra in queue.
6326 insertions, added 2564 points, 586841 tetrahedra in queue.
8433 insertions, added 1779 points, 64950 tetrahedra in queue.
Refinement seconds: 2.90822
Smoothing vertices...
Mesh smoothing seconds: 3.03225
Improving mesh...
Mesh improvement seconds: 0.135918
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.012574
Total running seconds: 6.66912
Statistics:
Input points: 14253
Input facets: 28494
Input segments: 42741
Input holes: 2
Input regions: 0
Mesh points: 33071
Mesh tetrahedra: 159280
Mesh faces: 332807
Mesh faces on exterior boundary: 28494
Mesh faces on input facets: 28494
Mesh edges on input segments: 42741
Steiner points inside domain: 18818
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 116.757s
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 0m0.156s
user 0m0.079s
sys 0m0.011s
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aimTransferUtilTest passed (as expected)
=============================================
+ expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest
+ /Users/jenkins/workspace/ESP_UndefinedCaps/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 0m0.129s
user 0m0.064s
sys 0m0.009s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest passed (as expected)
=============================================
+ expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest
+ /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest
vlmUtils Tests passed!
real 0m0.137s
user 0m0.073s
sys 0m0.009s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest passed (as expected)
=============================================
+ rm -rf aimTest
+ expectCSuccess '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm'
+ /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm
Root Path = /Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/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 = 1986!
testingAIM/aimDiscr: npts = 1052!
testingAIM/aimDiscr: tname = Interface, instance = 0!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 6 matches Interface!
testingAIM/aimDiscr: ntris = 794!
testingAIM/aimDiscr: npts = 444!
testingAIM/aimTransfer name = scalar instance = 0 npts = 444/1!
CAPS Info: Bound 'Interface' Normalized Integrated 'scalar'
Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 1.563194e-13
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:44937 jenkins 2023/12/26 00:18:05 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 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:44937 jenkins 2023/12/26 00:18:05 2
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 2
value = 0.000000 (null)
Param has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 3
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 3
value = 99 (null)
num has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 6
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 1
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 6
value = 8.000000 (null)
x has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 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:44937 jenkins 2023/12/26 00:18:05 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 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:44937 jenkins 2023/12/26 00:18:05 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 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:44937 jenkins 2023/12/26 00:18:05 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 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:44937 jenkins 2023/12/26 00:18:05 7
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 1
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 7
linked to ParamName
pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 16
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 16
value = 34.641525 (null)
cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 16
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 16
value = 7.296560 (null)
testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 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:44937 jenkins 2023/12/26 00:18:05 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 8
value = 5.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 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:44937 jenkins 2023/12/26 00:18:05 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 8
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 8
value (0x0) = NULL with len = 0 writer
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 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:44937 jenkins 2023/12/26 00:18:15 18
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 18
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 18
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 9
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:15 18
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 18
value = 42 (null)
testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:15 28
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:15 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:44937 jenkins 2023/12/26 00:18:05 10
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 10
value = 6.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 12
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 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:44937 jenkins 2023/12/26 00:18:06 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 13
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:06 23
linked to tessOut
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 10
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 10
value (0x0) = NULL with len = 0 writer
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 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:44937 jenkins 2023/12/26 00:18:15 28
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 11
testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0!
tessPtr = 600003bbc200
value = 600003bbc200 ego
lazy: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:15 28
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 11
testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:15 28
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:15 28
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:15 28
value = 42 (null)
Interface has type BOUND, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 14
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
2 Connecteds, 0 UnConnecteds
testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
5 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
1052 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
1052 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:15 26
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 15
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:15 26
1052 points, rank=1, units=(null)
testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
6 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
444 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 23
444 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 25
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:07 25
444 points, rank=1, units=(null)
vector has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:44937 jenkins 2023/12/26 00:18:05 0
testingAIM/aimTransfer name = vector instance = 0 npts = 444/3!
444 points, rank=3, units=(null)
1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
8: 14.400000 14.400000 14.400000 14.378831 14.400000 14.400000 14.400000
15: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
22: 14.400000 14.400000 14.400000 14.383512 14.400000 14.400000 14.400000
29: 14.400000 14.390686 14.400000 14.400000 14.400000 14.400000 14.400000
36: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
43: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
50: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
57: 14.400000 14.400000 14.400000 14.400000 14.377096 14.400000 14.378002
64: 14.400000 14.378425 14.400000 14.380488 14.400000 14.400000 14.400000
71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
78: 14.400000 14.386209 14.400000 14.400000 14.400000 14.400000 14.384098
85: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
92: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
99: 14.400000 14.400000 14.386071 14.400000 14.384936 14.400000 14.400000
106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
155: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
162: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
169: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
176: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
183: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
190: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
197: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
204: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
211: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
218: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
225: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
232: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
239: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
246: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
253: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
260: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
267: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
274: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
281: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
288: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
295: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
302: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
309: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
316: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
323: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
330: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
337: 14.400000 14.400000 14.400000 14.400000 14.356558 14.400000 14.400000
344: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
351: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
358: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
365: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
372: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
379: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
386: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
393: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
400: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
407: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
414: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
421: 14.400000 14.364389 14.400000 14.400000 14.400000 14.400000 14.400000
428: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
435: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
442: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
449: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
456: 14.400000 14.400000 14.361360 14.400000 14.400000 14.400000 14.400000
463: 14.400000 14.361740 14.400000 14.400000 14.400000 14.400000 14.361165
470: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
477: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.360532
484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
491: 14.363802 14.400000 14.400000 14.361619 14.400000 14.368179 14.400000
498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
505: 14.400000 14.400000 14.362304 14.400000 14.400000 14.400000 14.400000
512: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
519: 14.400000 14.400000 14.373001 14.400000 14.400000 14.365765 14.400000
526: 14.364059 14.360074 14.400000 14.400000 14.364067 14.400000 14.366792
533: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
540: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
547: 14.400000 14.366792 14.400000 14.365283 14.370506 14.400000 14.400000
554: 14.400000 14.368606 14.400000 14.400000 14.400000 14.400000 14.400000
561: 14.400000 14.400000 14.400000 14.400000 14.366173 14.400000 14.400000
568: 14.400000 14.400000 14.400000 14.400000 14.368001 14.400000 14.400000
575: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
582: 14.400000 14.369112 14.400000 14.400000 14.371298 14.400000 14.368001
589: 14.400000 14.400000 14.372161 14.400000 14.400000 14.368488 14.400000
596: 14.400000 14.367602 14.400000 14.400000 14.400000 14.400000 14.400000
603: 14.400000 14.400000 14.400000 14.368001 14.366391 14.400000 14.400000
610: 14.371426 14.400000 14.400000 14.369447 14.400000 14.400000 14.400000
617: 14.400000 14.400000 14.400000 14.377309 14.400000 14.400000 14.400000
624: 14.368789 14.400000 14.400000 14.400000 14.370365 14.400000 14.367429
631: 14.400000 14.368910 14.400000 14.373079 14.400000 14.400000 14.400000
638: 14.400000 14.400000 14.400000 14.400000 14.400000 14.377329 14.400000
645: 14.376154 14.400000 14.400000 14.367922 14.400000 14.373272 14.400000
652: 14.378235 14.400000 14.400000 14.400000 14.400000 14.366804 14.400000
659: 14.368813 14.400000 14.377324 14.372228 14.400000 14.373478 14.375283
666: 14.400000 14.378016 14.400000 14.400000 14.371143 14.400000 14.372419
673: 14.400000 14.376808 14.400000 14.400000 14.400000 14.400000 14.400000
680: 14.400000 14.377703 14.400000 14.379051 14.372699 14.379817 14.400000
687: 14.400000 14.400000 14.400000 14.377610 14.375648 14.400000 14.400000
694: 14.369238 14.400000 14.369944 14.400000 14.371318 14.400000 14.375746
701: 14.375803 14.400000 14.400000 14.400000 14.400000 14.400000 14.372846
708: 14.400000 14.372368 14.378170 14.400000 14.374755 14.378030 14.400000
715: 14.400000 14.400000 14.374706 14.400000 14.400000 14.371318 14.400000
722: 14.375898 14.400000 14.370149 14.400000 14.400000 14.374805 14.377143
729: 14.373864 14.400000 14.379637 14.400000 14.400000 14.382610 14.379415
736: 14.400000 14.379571 14.381325 14.400000 14.373140 14.378638 14.400000
743: 14.400000 14.400000 14.370559 14.400000 14.375085 14.372229 14.372229
750: 14.400000 14.382920 14.375972 14.400000 14.374657 14.381204 14.371275
757: 14.379781 14.374921 14.400000 14.380608 14.382356 14.374971 14.400000
764: 14.400000 14.378465 14.400000 14.400000 14.400000 14.400000 14.400000
771: 14.400000 14.400000 14.400000 14.375852 14.383099 14.373140 14.373018
778: 14.400000 14.382099 14.382909 14.400000 14.379692 14.400000 14.400000
785: 14.384926 14.400000 14.388861 14.400000 14.400000 14.383987 14.383981
792: 14.400000 14.375970 14.400000 14.370583 14.381998 14.400000 14.400000
799: 14.400000 14.383910 14.400000 14.378728 14.388120 14.378271 14.400000
806: 14.375163 14.375173 14.400000 14.370338 14.382454 14.379061 14.380211
813: 14.384486 14.378136 14.400000 14.383500 14.381847 14.382863 14.400000
820: 14.400000 14.377101 14.375595 14.400000 14.373292 14.379779 14.380376
827: 14.400000 14.373874 14.400000 14.383686 14.380422 14.400000 14.400000
834: 14.383166 14.379052 14.383605 14.380344 14.400000 14.400000 14.382794
841: 14.375125 14.400000 14.382029 14.383056 14.400000 14.400000 14.378276
848: 14.400000 14.381153 14.400000 14.375008 14.377799 14.374541 14.381405
855: 14.374929 14.400000 14.400000 14.381218 14.379742 14.383231 14.400000
862: 14.381834 14.384969 14.384922 14.375179 14.400000 14.381622 14.379954
869: 14.383733 14.378833 14.400000 14.382551 14.400000 14.376921 14.374541
876: 14.400000 14.400000 14.400000 14.400000 14.400000 14.373804 14.376151
883: 14.400000 14.400000 14.385119 14.400000 14.384771 14.385277 14.400000
890: 14.384683 14.400000 14.383245 14.384658 14.385167 14.384820 14.400000
897: 14.381917 14.384748 14.381022 14.384180 14.376570 14.400000 14.376181
904: 14.400000 14.382409 14.383895 14.377432 14.376314 14.385461 14.385212
911: 14.383287 14.381870 14.382994 14.385890 14.385447 14.386114 14.385828
918: 14.385723 14.385871 14.400000 14.383085 14.400000 14.381737 14.383942
925: 14.384917 14.400000 14.381285 14.382095 14.400000 14.400000 14.376314
932: 14.376070 14.400000 14.382758 14.379454 14.378857 14.383739 14.386359
939: 14.380880 14.379472 14.380483 14.384546 14.387537 14.382787 14.385066
946: 14.400000 14.378835 14.386778 14.383010 14.383809 14.381921 14.386550
953: 14.378436 14.400000 14.381287 14.400000 14.385729 14.382203 14.400000
960: 14.400000 14.381514 14.400000 14.385837 14.383749 14.385373 14.381900
967: 14.400000 14.387191 14.381810 14.384633 14.386224 14.386188 14.382724
974: 14.384664 14.388330 14.386817 14.400000 14.400000 14.400000 14.380427
981: 14.387139 14.400000 14.387627 14.379233 14.389580 14.382421 14.378624
988: 14.380128 14.382483 14.383381 14.385844 14.382032 14.378711 14.381543
995: 14.389314 14.386279 14.381344 14.400000 14.386188 14.386800 14.386835
1002: 14.387324 14.384153 14.382603 14.386700 14.386676 14.386861 14.389231
1009: 14.384737 14.378482 14.379803 14.381706 14.400000 14.400000 14.378115
1016: 14.380762 14.381783 14.383927 14.382199 14.385896 14.386358 14.379724
1023: 14.385043 14.383526 14.383287 14.390892 14.381998 14.391005 14.381743
1030: 14.384274 14.381269 14.378385 14.386201 14.400000 14.382556 14.387124
1037: 14.400000 14.384367 14.387065 14.387284 14.379386 14.384733 14.383957
1044: 14.385662 14.388355 14.387666 14.387284 14.379803 14.384597 14.381439
1051: 14.385888 14.381269
source getTriangles = 0, nGtris = 1986, nGsegs = 5958, Ds = 0 0
destin getTriangles = 0, nGtris = 794, nGsegs = 2382, Ds = 0 0
In caps_outputObjects:
2 Analyses found
1 Bounds found
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m10.447s
user 0m10.225s
sys 0m0.222s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm passed (as expected)
=============================================
+ rm -rf source.vs destin.vs
+ expectCSuccess '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm'
+ /Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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 0m1.200s
user 0m1.028s
sys 0m0.137s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm passed (as expected)
=============================================
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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] Obtaining reference build from same job (7.7,CAPS/unit,DARWIN_ARM64,viggen)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #191' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[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_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #192'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS
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