sourceBoxDirection = 1.000000 0.000000 0.000000
sourceBoxAngle = 0.000000
sourceGrowthFactor = 10.000000
sourcePCDFile =
ModelSize = 0
writeGMA = 2.0
assembleTolMult = 2.0
modelOrientIntMeshVolume = 1
Elevate On Export
degree = Q1
costThreshold = 0.8
maxIncAngle = 175.0
relax = 0.05
smoothingPasses = 1000
WCNWeight = 0.5
WCNMode = Calculate
writeVTU = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 10
Computing maximum DB edge tolerance.
Quilt list has 9 entries.
Quilt quilt-1: edge tolerance = 2.40432e-07
Quilt quilt-2: edge tolerance = 2.40432e-07
Quilt quilt-3: edge tolerance = 2.40432e-07
Quilt quilt-4: edge tolerance = 5e-08
Quilt quilt-5: edge tolerance = 5e-08
Quilt quilt-6: edge tolerance = 5e-08
Quilt quilt-7: edge tolerance = 5e-08
Quilt quilt-8: edge tolerance = 5e-08
Quilt quilt-9: edge tolerance = 5e-08
Maximum DB edge tolerance = 2.40432e-07
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 4.808648e-07 due to model assembly tolerance
Looking for quilt names in geometry.
Quilt list has 9 entries.
Quilt list has 9 entries.
Original connector list has 15 entries.
Minimum connector length = 1
Tolerance = 2.40432e-07
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 15 entries.
Updating conData
Min Edge Tol: 5.000e-08 on con-5
Max Edge Tol: 2.404e-07 on con-1
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/15, name = con-1
Checking dimension for connector 2/15, name = con-2
Checking dimension for connector 3/15, name = con-4
Changing dimension for connector 3/15 from 6 to 3
Checking dimension for connector 4/15, name = con-5
Changing dimension for connector 4/15 from 6 to 3
Checking dimension for connector 5/15, name = con-6
Changing dimension for connector 5/15 from 6 to 3
Checking dimension for connector 6/15, name = con-7
Changing dimension for connector 6/15 from 6 to 3
Checking dimension for connector 7/15, name = con-8
Changing dimension for connector 7/15 from 6 to 3
Checking dimension for connector 8/15, name = con-9
Changing dimension for connector 8/15 from 6 to 3
Checking dimension for connector 9/15, name = con-10
Changing dimension for connector 9/15 from 6 to 3
Checking dimension for connector 10/15, name = con-11
Changing dimension for connector 10/15 from 6 to 3
Checking dimension for connector 11/15, name = con-12
Changing dimension for connector 11/15 from 6 to 3
Checking dimension for connector 12/15, name = con-13
Checking dimension for connector 13/15, name = con-15
Checking dimension for connector 14/15, name = con-17
Checking dimension for connector 15/15, name = con-19
Processing spacing values for connector 1/15, name = con-1
Processing spacing values for connector 2/15, name = con-2
Processing spacing values for connector 3/15, name = con-4
Processing spacing values for connector 4/15, name = con-5
Processing spacing values for connector 5/15, name = con-6
Processing spacing values for connector 6/15, name = con-7
Processing spacing values for connector 7/15, name = con-8
Processing spacing values for connector 8/15, name = con-9
Processing spacing values for connector 9/15, name = con-10
Processing spacing values for connector 10/15, name = con-11
Processing spacing values for connector 11/15, name = con-12
Processing spacing values for connector 12/15, name = con-13
Processing spacing values for connector 13/15, name = con-15
Processing spacing values for connector 14/15, name = con-17
Processing spacing values for connector 15/15, name = con-19
Number of unique endpoints = 10
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
Proximity test for connector 1/15, con-1.
Connector dimension changed from 6 to 8, avg. spacing changed from 0.628319 to 0.448799
Proximity test for connector 2/15, con-2.
Connector dimension changed from 6 to 8, avg. spacing changed from 0.628319 to 0.448799
Proximity test for connector 3/15, con-4.
Proximity test for connector 4/15, con-5.
Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8
Proximity test for connector 5/15, con-6.
Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8
Proximity test for connector 6/15, con-7.
Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8
Proximity test for connector 7/15, con-8.
Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8
Proximity test for connector 8/15, con-9.
Proximity test for connector 9/15, con-10.
Proximity test for connector 10/15, con-11.
Proximity test for connector 11/15, con-12.
Proximity test for connector 12/15, con-13.
Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Proximity test for connector 13/15, con-15.
Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Proximity test for connector 14/15, con-17.
Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Proximity test for connector 15/15, con-19.
Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 8
Connector con-2 current dim = 8
Connector con-4 current dim = 3
Connector con-5 current dim = 6
Connector con-6 current dim = 6
Connector con-7 current dim = 6
Connector con-8 current dim = 6
Connector con-9 current dim = 3
Connector con-10 current dim = 3
Connector con-11 current dim = 3
Connector con-12 current dim = 3
Connector con-13 current dim = 8
Connector con-15 current dim = 8
Connector con-17 current dim = 8
Connector con-19 current dim = 8
Domain list has 9 entries.
Looking for periodic domain attributes from geometry.
Tolerance = 2.40432e-07
Number of periodic target domains = 0
Unstructured domain 1 of 9:
boundary name = cylinder.
Creating boundary name cylinder
Unstructured domain 2 of 9:
boundary name = cylinder.
cylinder already in boundary name list.
Unstructured domain 3 of 9:
boundary name = cylinder.
cylinder already in boundary name list.
Unstructured domain 4 of 9:
boundary name = farfield.
Creating boundary name farfield
Unstructured domain 5 of 9:
boundary name = farfield.
farfield already in boundary name list.
Unstructured domain 6 of 9:
boundary name = farfield.
farfield already in boundary name list.
Unstructured domain 7 of 9:
boundary name = farfield.
farfield already in boundary name list.
Unstructured domain 8 of 9:
boundary name = farfield.
farfield already in boundary name list.
Unstructured domain 9 of 9:
boundary name = farfield.
farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 9 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 9 domains.
Block = auto-blk
Setting up unstructured block.
Retrieving block attributes from geometry.
Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Sat Jul 08 2023 3:13:38PM EDT
Run Time: 00 Hours 00 Minutes 01 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Sat Jul 08 2023 3:13:38PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 45 / 45 curves to EGADS originals
GMA contains 15 edge groups
GMA contains 9 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Sat Jul 08 2023 3:13:39PM EDT
Export Time: 00 Hours 00 Minutes 01 Seconds
Volume mesh:
Number of nodes = 430
Number of elements = 1960
Number of triangles = 348
Number of quadrilatarals = 0
Number of tetrahedrals = 1960
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Body = 1
Number of nodes = 38
Number of elements = 72
Number of tris = 72
Number of quad = 0
Body = 2
Number of nodes = 140
Number of elements = 276
Number of tris = 276
Number of quad = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
.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 = 1
Name = box, index = 1
Writing global Glyph inputs...
Writing egads file '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/BoxError/caps.egads'....
.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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Writing global Glyph inputs...
Writing egads file '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest3/Scratch/SingleBody2/caps.egads'....
Running pointwise......
Number of command line arguments = 2
Sat Jul 08 2023 3:13:41PM EDT
Pointwise V18.5
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
InitDim = 10
MaxDim = 12
MinDim = 3
TurnAngle = 0.000000
Deviation = 0.000000
SplitAngle = 0.000000
JoinCons = 0
ProxGrowthRate = 1.300000
SourceSpacing = 0
TurnAngleHard = 70.000000
EqualSpacing = 0
Domain level
Algorithm = Delaunay
FullLayers = 0
MaxLayers = 0
GrowthRate = 1.300000
IsoType = Triangle
TRexType = Triangle
TRexARLimit = 200.000000
TRexAngleBC = 0.000000
Decay = 0.500000
MinEdge = 0.000000
MaxEdge = 0.000000
Adapt = 0
WallSpacing = 0.000000
StrDomConvertARTrigger = 0.000000
Block level
Algorithm = Delaunay
VoxelLayers = 3
boundaryDecay = 0.500000
collisionBuffer = 0.500000
maxSkewAngle = 180.000000
TRexSkewDelay = 0
edgeMaxGrowthRate = 1.800000
fullLayers = 0
maxLayers = 0
growthRate = 1.300000
TRexType = TetPyramid
volInitialize = 1
General
SkipMeshing = 1
CAESolver = UGRID
outerBoxScale = 0
sourceBoxLengthScale = 0.000000
sourceBoxDirection = 1.000000 0.000000 0.000000
sourceBoxAngle = 0.000000
sourceGrowthFactor = 10.000000
sourcePCDFile =
ModelSize = 0
writeGMA = 2.0
assembleTolMult = 2.0
modelOrientIntMeshVolume = 1
Elevate On Export
degree = Q1
costThreshold = 0.8
maxIncAngle = 175.0
relax = 0.05
smoothingPasses = 1000
WCNWeight = 0.5
WCNMode = Calculate
writeVTU = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 100
Computing maximum DB edge tolerance.
Quilt list has 14 entries.
Quilt quilt-1: edge tolerance = 5e-07
Quilt quilt-2: edge tolerance = 5e-07
Quilt quilt-3: edge tolerance = 5e-07
Quilt quilt-4: edge tolerance = 5e-07
Quilt quilt-5: edge tolerance = 5e-07
Quilt quilt-6: edge tolerance = 5e-07
Quilt quilt-7: edge tolerance = 6.19984e-05
Quilt quilt-8: edge tolerance = 6.19984e-05
Quilt quilt-9: edge tolerance = 6.19984e-05
Quilt quilt-10: edge tolerance = 6.19984e-05
Quilt quilt-11: edge tolerance = 6.19984e-05
Quilt quilt-12: edge tolerance = 6.19984e-05
Quilt quilt-13: edge tolerance = 6.19984e-05
Quilt quilt-14: edge tolerance = 6.19984e-05
Maximum DB edge tolerance = 6.19984e-05
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.239969e-04 due to model assembly tolerance
Looking for quilt names in geometry.
Quilt list has 14 entries.
Quilt list has 14 entries.
Original connector list has 27 entries.
Minimum connector length = 0.00791958
Tolerance = 6.19984e-05
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 27 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-1
Max Edge Tol: 6.200e-05 on con-20
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/27, name = con-1
Checking dimension for connector 2/27, name = con-2
Checking dimension for connector 3/27, name = con-3
Checking dimension for connector 4/27, name = con-4
Checking dimension for connector 5/27, name = con-5
Checking dimension for connector 6/27, name = con-6
Checking dimension for connector 7/27, name = con-7
Checking dimension for connector 8/27, name = con-8
Checking dimension for connector 9/27, name = con-9
Checking dimension for connector 10/27, name = con-11
Checking dimension for connector 11/27, name = con-13
Checking dimension for connector 12/27, name = con-15
Checking dimension for connector 13/27, name = con-16
Changing dimension for connector 13/27 from 10 to 3
Checking dimension for connector 14/27, name = con-17
Changing dimension for connector 14/27 from 10 to 3
Checking dimension for connector 15/27, name = con-18
Changing dimension for connector 15/27 from 10 to 3
Checking dimension for connector 16/27, name = con-19
Changing dimension for connector 16/27 from 10 to 3
Checking dimension for connector 17/27, name = con-20
Changing dimension for connector 17/27 from 10 to 3
Checking dimension for connector 18/27, name = con-21
Changing dimension for connector 18/27 from 10 to 3
Checking dimension for connector 19/27, name = con-22
Checking dimension for connector 20/27, name = con-23
Changing dimension for connector 20/27 from 10 to 3
Checking dimension for connector 21/27, name = con-24
Checking dimension for connector 22/27, name = con-26
Changing dimension for connector 22/27 from 10 to 4
Checking dimension for connector 23/27, name = con-27
Checking dimension for connector 24/27, name = con-29
Changing dimension for connector 24/27 from 10 to 4
Checking dimension for connector 25/27, name = con-31
Checking dimension for connector 26/27, name = con-33
Checking dimension for connector 27/27, name = con-37
Processing spacing values for connector 1/27, name = con-1
Processing spacing values for connector 2/27, name = con-2
Processing spacing values for connector 3/27, name = con-3
Processing spacing values for connector 4/27, name = con-4
Processing spacing values for connector 5/27, name = con-5
Processing spacing values for connector 6/27, name = con-6
Processing spacing values for connector 7/27, name = con-7
Processing spacing values for connector 8/27, name = con-8
Processing spacing values for connector 9/27, name = con-9
Processing spacing values for connector 10/27, name = con-11
Processing spacing values for connector 11/27, name = con-13
Processing spacing values for connector 12/27, name = con-15
Processing spacing values for connector 13/27, name = con-16
Processing spacing values for connector 14/27, name = con-17
Processing spacing values for connector 15/27, name = con-18
Processing spacing values for connector 16/27, name = con-19
Processing spacing values for connector 17/27, name = con-20
Processing spacing values for connector 18/27, name = con-21
Processing spacing values for connector 19/27, name = con-22
Processing spacing values for connector 20/27, name = con-23
Processing spacing values for connector 21/27, name = con-24
Processing spacing values for connector 22/27, name = con-26
Processing spacing values for connector 23/27, name = con-27
Processing spacing values for connector 24/27, name = con-29
Processing spacing values for connector 25/27, name = con-31
Processing spacing values for connector 26/27, name = con-33
Processing spacing values for connector 27/27, name = con-37
Number of unique endpoints = 17
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
Proximity test for connector 1/27, con-1.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 2/27, con-2.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 3/27, con-3.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 4/27, con-4.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 5/27, con-5.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 6/27, con-6.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 7/27, con-7.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 8/27, con-8.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 9/27, con-9.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 10/27, con-11.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 11/27, con-13.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 12/27, con-15.
Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
Proximity test for connector 13/27, con-16.
Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
Proximity test for connector 14/27, con-17.
Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
Proximity test for connector 15/27, con-18.
Proximity test for connector 16/27, con-19.
Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
Proximity test for connector 17/27, con-20.
Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
Proximity test for connector 18/27, con-21.
Proximity test for connector 19/27, con-22.
Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244
Proximity test for connector 20/27, con-23.
Proximity test for connector 21/27, con-24.
Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224
Proximity test for connector 22/27, con-26.
Connector dimension changed from 4 to 12, avg. spacing changed from 1.33869 to 0.365097
Proximity test for connector 23/27, con-27.
Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354
Proximity test for connector 24/27, con-29.
Connector dimension changed from 4 to 12, avg. spacing changed from 1.26705 to 0.34556
Proximity test for connector 25/27, con-31.
Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244
Proximity test for connector 26/27, con-33.
Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224
Proximity test for connector 27/27, con-37.
Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 12
Connector con-2 current dim = 12
Connector con-3 current dim = 12
Connector con-4 current dim = 12
Connector con-5 current dim = 12
Connector con-6 current dim = 12
Connector con-7 current dim = 12
Connector con-8 current dim = 12
Connector con-9 current dim = 12
Connector con-11 current dim = 12
Connector con-13 current dim = 12
Connector con-15 current dim = 12
Connector con-16 current dim = 12
Connector con-17 current dim = 12
Connector con-18 current dim = 3
Connector con-19 current dim = 12
Connector con-20 current dim = 12
Connector con-21 current dim = 3
Connector con-22 current dim = 12
Connector con-23 current dim = 3
Connector con-24 current dim = 12
Connector con-26 current dim = 12
Connector con-27 current dim = 12
Connector con-29 current dim = 12
Connector con-31 current dim = 12
Connector con-33 current dim = 12
Connector con-37 current dim = 12
Domain list has 14 entries.
Looking for periodic domain attributes from geometry.
Tolerance = 6.19984e-05
Number of periodic target domains = 0
Unstructured domain 1 of 14:
boundary name = Farfield.
Creating boundary name Farfield
Unstructured domain 2 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 3 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 4 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 5 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 6 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 7 of 14:
boundary name = Wing1.
Creating boundary name Wing1
Unstructured domain 8 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 9 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 10 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 11 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 12 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 13 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 14 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 14 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 14 domains.
Block = auto-blk
Setting up unstructured block.
Retrieving block attributes from geometry.
Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Sat Jul 08 2023 3:13:44PM EDT
Run Time: 00 Hours 00 Minutes 03 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Sat Jul 08 2023 3:13:44PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 81 / 81 curves to EGADS originals
GMA contains 27 edge groups
GMA contains 14 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Sat Jul 08 2023 3:13:46PM EDT
Export Time: 00 Hours 00 Minutes 02 Seconds
Volume mesh:
Number of nodes = 9674
Number of elements = 54410
Number of triangles = 3012
Number of quadrilatarals = 0
Number of tetrahedrals = 54410
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Body = 1
Number of nodes = 1510
Number of elements = 3012
Number of tris = 3012
Number of quad = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Writing global Glyph inputs...
Writing egads file '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest3/Scratch/SingleBody2/caps.egads'....
Running pointwise......
Number of command line arguments = 2
Sat Jul 08 2023 3:13:47PM EDT
Pointwise V18.5
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
InitDim = 6
MaxDim = 8
MinDim = 3
TurnAngle = 0.000000
Deviation = 0.000000
SplitAngle = 0.000000
JoinCons = 0
ProxGrowthRate = 1.300000
SourceSpacing = 0
TurnAngleHard = 70.000000
EqualSpacing = 0
Domain level
Algorithm = Delaunay
FullLayers = 0
MaxLayers = 0
GrowthRate = 1.300000
IsoType = Triangle
TRexType = Triangle
TRexARLimit = 200.000000
TRexAngleBC = 0.000000
Decay = 0.500000
MinEdge = 0.000000
MaxEdge = 0.000000
Adapt = 0
WallSpacing = 0.000000
StrDomConvertARTrigger = 0.000000
Block level
Algorithm = Delaunay
VoxelLayers = 3
boundaryDecay = 0.500000
collisionBuffer = 0.500000
maxSkewAngle = 180.000000
TRexSkewDelay = 0
edgeMaxGrowthRate = 1.800000
fullLayers = 0
maxLayers = 0
growthRate = 1.300000
TRexType = TetPyramid
volInitialize = 1
General
SkipMeshing = 1
CAESolver = UGRID
outerBoxScale = 0
sourceBoxLengthScale = 0.000000
sourceBoxDirection = 1.000000 0.000000 0.000000
sourceBoxAngle = 0.000000
sourceGrowthFactor = 10.000000
sourcePCDFile =
ModelSize = 0
writeGMA = 2.0
assembleTolMult = 2.0
modelOrientIntMeshVolume = 1
Elevate On Export
degree = Q1
costThreshold = 0.8
maxIncAngle = 175.0
relax = 0.05
smoothingPasses = 1000
WCNWeight = 0.5
WCNMode = Calculate
writeVTU = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 100
Computing maximum DB edge tolerance.
Quilt list has 14 entries.
Quilt quilt-1: edge tolerance = 5e-07
Quilt quilt-2: edge tolerance = 5e-07
Quilt quilt-3: edge tolerance = 5e-07
Quilt quilt-4: edge tolerance = 5e-07
Quilt quilt-5: edge tolerance = 5e-07
Quilt quilt-6: edge tolerance = 5e-07
Quilt quilt-7: edge tolerance = 6.19984e-05
Quilt quilt-8: edge tolerance = 6.19984e-05
Quilt quilt-9: edge tolerance = 6.19984e-05
Quilt quilt-10: edge tolerance = 6.19984e-05
Quilt quilt-11: edge tolerance = 6.19984e-05
Quilt quilt-12: edge tolerance = 6.19984e-05
Quilt quilt-13: edge tolerance = 6.19984e-05
Quilt quilt-14: edge tolerance = 6.19984e-05
Maximum DB edge tolerance = 6.19984e-05
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.239969e-04 due to model assembly tolerance
Looking for quilt names in geometry.
Quilt list has 14 entries.
Quilt list has 14 entries.
Original connector list has 27 entries.
Minimum connector length = 0.00791958
Tolerance = 6.19984e-05
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 27 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-1
Max Edge Tol: 6.200e-05 on con-20
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/27, name = con-1
Checking dimension for connector 2/27, name = con-2
Checking dimension for connector 3/27, name = con-3
Checking dimension for connector 4/27, name = con-4
Checking dimension for connector 5/27, name = con-5
Checking dimension for connector 6/27, name = con-6
Checking dimension for connector 7/27, name = con-7
Checking dimension for connector 8/27, name = con-8
Checking dimension for connector 9/27, name = con-9
Checking dimension for connector 10/27, name = con-11
Checking dimension for connector 11/27, name = con-13
Checking dimension for connector 12/27, name = con-15
Checking dimension for connector 13/27, name = con-16
Changing dimension for connector 13/27 from 6 to 3
Checking dimension for connector 14/27, name = con-17
Changing dimension for connector 14/27 from 6 to 3
Checking dimension for connector 15/27, name = con-18
Changing dimension for connector 15/27 from 6 to 3
Checking dimension for connector 16/27, name = con-19
Changing dimension for connector 16/27 from 6 to 3
Checking dimension for connector 17/27, name = con-20
Changing dimension for connector 17/27 from 6 to 3
Checking dimension for connector 18/27, name = con-21
Changing dimension for connector 18/27 from 6 to 3
Checking dimension for connector 19/27, name = con-22
Checking dimension for connector 20/27, name = con-23
Changing dimension for connector 20/27 from 6 to 3
Checking dimension for connector 21/27, name = con-24
Checking dimension for connector 22/27, name = con-26
Changing dimension for connector 22/27 from 6 to 3
Checking dimension for connector 23/27, name = con-27
Checking dimension for connector 24/27, name = con-29
Changing dimension for connector 24/27 from 6 to 3
Checking dimension for connector 25/27, name = con-31
Checking dimension for connector 26/27, name = con-33
Checking dimension for connector 27/27, name = con-37
Processing spacing values for connector 1/27, name = con-1
Processing spacing values for connector 2/27, name = con-2
Processing spacing values for connector 3/27, name = con-3
Processing spacing values for connector 4/27, name = con-4
Processing spacing values for connector 5/27, name = con-5
Processing spacing values for connector 6/27, name = con-6
Processing spacing values for connector 7/27, name = con-7
Processing spacing values for connector 8/27, name = con-8
Processing spacing values for connector 9/27, name = con-9
Processing spacing values for connector 10/27, name = con-11
Processing spacing values for connector 11/27, name = con-13
Processing spacing values for connector 12/27, name = con-15
Processing spacing values for connector 13/27, name = con-16
Processing spacing values for connector 14/27, name = con-17
Processing spacing values for connector 15/27, name = con-18
Processing spacing values for connector 16/27, name = con-19
Processing spacing values for connector 17/27, name = con-20
Processing spacing values for connector 18/27, name = con-21
Processing spacing values for connector 19/27, name = con-22
Processing spacing values for connector 20/27, name = con-23
Processing spacing values for connector 21/27, name = con-24
Processing spacing values for connector 22/27, name = con-26
Processing spacing values for connector 23/27, name = con-27
Processing spacing values for connector 24/27, name = con-29
Processing spacing values for connector 25/27, name = con-31
Processing spacing values for connector 26/27, name = con-33
Processing spacing values for connector 27/27, name = con-37
Number of unique endpoints = 17
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
Proximity test for connector 1/27, con-1.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 2/27, con-2.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 3/27, con-3.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 4/27, con-4.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 5/27, con-5.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 6/27, con-6.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 7/27, con-7.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 8/27, con-8.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 9/27, con-9.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 10/27, con-11.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 11/27, con-13.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 12/27, con-15.
Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
Proximity test for connector 13/27, con-16.
Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495
Proximity test for connector 14/27, con-17.
Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495
Proximity test for connector 15/27, con-18.
Proximity test for connector 16/27, con-19.
Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495
Proximity test for connector 17/27, con-20.
Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495
Proximity test for connector 18/27, con-21.
Proximity test for connector 19/27, con-22.
Connector dimension changed from 6 to 8, avg. spacing changed from 1.47894 to 1.05638
Proximity test for connector 20/27, con-23.
Proximity test for connector 21/27, con-24.
Connector dimension changed from 6 to 8, avg. spacing changed from 1.47893 to 1.05638
Proximity test for connector 22/27, con-26.
Connector dimension changed from 3 to 8, avg. spacing changed from 2.00803 to 0.573724
Proximity test for connector 23/27, con-27.
Connector dimension changed from 6 to 8, avg. spacing changed from 1.63318 to 1.16656
Proximity test for connector 24/27, con-29.
Connector dimension changed from 3 to 8, avg. spacing changed from 1.90058 to 0.543022
Proximity test for connector 25/27, con-31.
Connector dimension changed from 6 to 8, avg. spacing changed from 1.47894 to 1.05638
Proximity test for connector 26/27, con-33.
Connector dimension changed from 6 to 8, avg. spacing changed from 1.47893 to 1.05638
Proximity test for connector 27/27, con-37.
Connector dimension changed from 6 to 8, avg. spacing changed from 1.63318 to 1.16656
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 8
Connector con-2 current dim = 8
Connector con-3 current dim = 8
Connector con-4 current dim = 8
Connector con-5 current dim = 8
Connector con-6 current dim = 8
Connector con-7 current dim = 8
Connector con-8 current dim = 8
Connector con-9 current dim = 8
Connector con-11 current dim = 8
Connector con-13 current dim = 8
Connector con-15 current dim = 8
Connector con-16 current dim = 8
Connector con-17 current dim = 8
Connector con-18 current dim = 3
Connector con-19 current dim = 8
Connector con-20 current dim = 8
Connector con-21 current dim = 3
Connector con-22 current dim = 8
Connector con-23 current dim = 3
Connector con-24 current dim = 8
Connector con-26 current dim = 8
Connector con-27 current dim = 8
Connector con-29 current dim = 8
Connector con-31 current dim = 8
Connector con-33 current dim = 8
Connector con-37 current dim = 8
Domain list has 14 entries.
Looking for periodic domain attributes from geometry.
Tolerance = 6.19984e-05
Number of periodic target domains = 0
Unstructured domain 1 of 14:
boundary name = Farfield.
Creating boundary name Farfield
Unstructured domain 2 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 3 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 4 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 5 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 6 of 14:
boundary name = Farfield.
Farfield already in boundary name list.
Unstructured domain 7 of 14:
boundary name = Wing1.
Creating boundary name Wing1
Unstructured domain 8 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 9 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 10 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 11 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 12 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 13 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 14 of 14:
boundary name = Wing1.
Wing1 already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 14 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 14 domains.
Block = auto-blk
Setting up unstructured block.
Retrieving block attributes from geometry.
Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Sat Jul 08 2023 3:13:50PM EDT
Run Time: 00 Hours 00 Minutes 03 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Sat Jul 08 2023 3:13:50PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 81 / 81 curves to EGADS originals
GMA contains 27 edge groups
GMA contains 14 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Sat Jul 08 2023 3:13:51PM EDT
Export Time: 00 Hours 00 Minutes 01 Seconds
Volume mesh:
Number of nodes = 7020
Number of elements = 40674
Number of triangles = 1278
Number of quadrilatarals = 0
Number of tetrahedrals = 40674
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Body = 1
Number of nodes = 643
Number of elements = 1278
Number of tris = 1278
Number of quad = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
.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
Writing global Glyph inputs...
Writing egads file '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/Sphere/caps.egads'....
Running pointwise......
Number of command line arguments = 2
Sat Jul 08 2023 3:13:52PM EDT
Pointwise V18.5
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
InitDim = 6
MaxDim = 8
MinDim = 3
TurnAngle = 0.000000
Deviation = 0.000000
SplitAngle = 0.000000
JoinCons = 0
ProxGrowthRate = 1.300000
SourceSpacing = 0
TurnAngleHard = 70.000000
EqualSpacing = 0
Domain level
Algorithm = Delaunay
FullLayers = 0
MaxLayers = 0
GrowthRate = 1.300000
IsoType = Triangle
TRexType = Triangle
TRexARLimit = 200.000000
TRexAngleBC = 0.000000
Decay = 0.500000
MinEdge = 0.000000
MaxEdge = 0.000000
Adapt = 0
WallSpacing = 0.000000
StrDomConvertARTrigger = 0.000000
Block level
Algorithm = Delaunay
VoxelLayers = 3
boundaryDecay = 0.500000
collisionBuffer = 0.500000
maxSkewAngle = 180.000000
TRexSkewDelay = 0
edgeMaxGrowthRate = 1.800000
fullLayers = 0
maxLayers = 0
growthRate = 1.300000
TRexType = TetPyramid
volInitialize = 1
General
SkipMeshing = 1
CAESolver = UGRID
outerBoxScale = 0
sourceBoxLengthScale = 0.000000
sourceBoxDirection = 1.000000 0.000000 0.000000
sourceBoxAngle = 0.000000
sourceGrowthFactor = 10.000000
sourcePCDFile =
ModelSize = 0
writeGMA = 2.0
assembleTolMult = 2.0
modelOrientIntMeshVolume = 1
Elevate On Export
degree = Q1
costThreshold = 0.8
maxIncAngle = 175.0
relax = 0.05
smoothingPasses = 1000
WCNWeight = 0.5
WCNMode = Calculate
writeVTU = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 10
Computing maximum DB edge tolerance.
Quilt list has 8 entries.
Quilt quilt-1: edge tolerance = 6.91474e-06
Quilt quilt-2: edge tolerance = 6.91474e-06
Quilt quilt-3: edge tolerance = 5e-08
Quilt quilt-4: edge tolerance = 5e-08
Quilt quilt-5: edge tolerance = 5e-08
Quilt quilt-6: edge tolerance = 5e-08
Quilt quilt-7: edge tolerance = 5e-08
Quilt quilt-8: edge tolerance = 5e-08
Maximum DB edge tolerance = 6.91474e-06
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.382948e-05 due to model assembly tolerance
Looking for quilt names in geometry.
Quilt list has 8 entries.
Quilt list has 8 entries.
Original connector list has 14 entries.
Minimum connector length = 1.5708
Tolerance = 6.91474e-06
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 14 entries.
Updating conData
Min Edge Tol: 5.000e-08 on con-3
Max Edge Tol: 6.915e-06 on con-1
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/14, name = con-1
Checking dimension for connector 2/14, name = con-2
Checking dimension for connector 3/14, name = con-3
Changing dimension for connector 3/14 from 6 to 3
Checking dimension for connector 4/14, name = con-4
Changing dimension for connector 4/14 from 6 to 3
Checking dimension for connector 5/14, name = con-5
Changing dimension for connector 5/14 from 6 to 3
Checking dimension for connector 6/14, name = con-6
Changing dimension for connector 6/14 from 6 to 3
Checking dimension for connector 7/14, name = con-7
Changing dimension for connector 7/14 from 6 to 3
Checking dimension for connector 8/14, name = con-8
Changing dimension for connector 8/14 from 6 to 3
Checking dimension for connector 9/14, name = con-9
Changing dimension for connector 9/14 from 6 to 3
Checking dimension for connector 10/14, name = con-10
Changing dimension for connector 10/14 from 6 to 3
Checking dimension for connector 11/14, name = con-11
Checking dimension for connector 12/14, name = con-13
Checking dimension for connector 13/14, name = con-15
Checking dimension for connector 14/14, name = con-17
Processing spacing values for connector 1/14, name = con-1
Processing spacing values for connector 2/14, name = con-2
Processing spacing values for connector 3/14, name = con-3
Processing spacing values for connector 4/14, name = con-4
Processing spacing values for connector 5/14, name = con-5
Processing spacing values for connector 6/14, name = con-6
Processing spacing values for connector 7/14, name = con-7
Processing spacing values for connector 8/14, name = con-8
Processing spacing values for connector 9/14, name = con-9
Processing spacing values for connector 10/14, name = con-10
Processing spacing values for connector 11/14, name = con-11
Processing spacing values for connector 12/14, name = con-13
Processing spacing values for connector 13/14, name = con-15
Processing spacing values for connector 14/14, name = con-17
Number of unique endpoints = 10
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
Proximity test for connector 1/14, con-1.
Proximity test for connector 2/14, con-2.
Proximity test for connector 3/14, con-3.
Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
Proximity test for connector 4/14, con-4.
Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
Proximity test for connector 5/14, con-5.
Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
Proximity test for connector 6/14, con-6.
Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
Proximity test for connector 7/14, con-7.
Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
Proximity test for connector 8/14, con-8.
Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
Proximity test for connector 9/14, con-9.
Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
Proximity test for connector 10/14, con-10.
Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
Proximity test for connector 11/14, con-11.
Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Proximity test for connector 12/14, con-13.
Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Proximity test for connector 13/14, con-15.
Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Proximity test for connector 14/14, con-17.
Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 6
Connector con-2 current dim = 6
Connector con-3 current dim = 4
Connector con-4 current dim = 4
Connector con-5 current dim = 4
Connector con-6 current dim = 4
Connector con-7 current dim = 5
Connector con-8 current dim = 5
Connector con-9 current dim = 5
Connector con-10 current dim = 5
Connector con-11 current dim = 8
Connector con-13 current dim = 8
Connector con-15 current dim = 8
Connector con-17 current dim = 8
Domain list has 8 entries.
Looking for periodic domain attributes from geometry.
Tolerance = 6.91474e-06
Number of periodic target domains = 0
Unstructured domain 1 of 8:
boundary name = sphere.
Creating boundary name sphere
Unstructured domain 2 of 8:
boundary name = sphere.
sphere already in boundary name list.
Unstructured domain 3 of 8:
boundary name = farfield.
Creating boundary name farfield
Unstructured domain 4 of 8:
boundary name = farfield.
farfield already in boundary name list.
Unstructured domain 5 of 8:
boundary name = farfield.
farfield already in boundary name list.
Unstructured domain 6 of 8:
boundary name = farfield.
farfield already in boundary name list.
Unstructured domain 7 of 8:
boundary name = farfield.
farfield already in boundary name list.
Unstructured domain 8 of 8:
boundary name = farfield.
farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 8 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 8 domains.
Block = auto-blk
Setting up unstructured block.
Retrieving block attributes from geometry.
Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Sat Jul 08 2023 3:13:54PM EDT
Run Time: 00 Hours 00 Minutes 02 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Sat Jul 08 2023 3:13:54PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 42 / 42 curves to EGADS originals
GMA contains 14 edge groups
GMA contains 8 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Sat Jul 08 2023 3:13:54PM EDT
Export Time: 00 Hours 00 Minutes 00 Seconds
Volume mesh:
Number of nodes = 602
Number of elements = 2985
Number of triangles = 356
Number of quadrilatarals = 0
Number of tetrahedrals = 2985
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Body = 1
Number of nodes = 49
Number of elements = 94
Number of tris = 94
Number of quad = 0
Body = 2
Number of nodes = 133
Number of elements = 262
Number of tris = 262
Number of quad = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
.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 = 7819
Number of elements = 15634
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 15634
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5889
Number of elements = 11774
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 516
Number of elements = 1028
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1028
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14224
Total number of elements = 28436
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 - 14224, elements - 28436
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.291345
Creating surface mesh ...
Surface mesh seconds: 0.057367
Recovering boundaries...
Boundary recovery seconds: 0.146481
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.073711
Recovering Delaunayness...
Delaunay recovery seconds: 0.079522
Refining mesh...
18960 insertions, added 14017 points, 701008 tetrahedra in queue.
6313 insertions, added 2494 points, 554976 tetrahedra in queue.
8415 insertions, added 1753 points, 70 tetrahedra in queue.
Refinement seconds: 3.95789
Smoothing vertices...
Mesh smoothing seconds: 3.84978
Improving mesh...
Mesh improvement seconds: 0.192319
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.024085
Total running seconds: 8.67356
Statistics:
Input points: 14224
Input facets: 28436
Input segments: 42654
Input holes: 2
Input regions: 0
Mesh points: 33058
Mesh tetrahedra: 159464
Mesh faces: 333146
Mesh faces on exterior boundary: 28436
Mesh faces on input facets: 28436
Mesh edges on input segments: 42654
Steiner points inside domain: 18834
Done meshing using TetGen!
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
.Getting CFD boundary conditions
Boundary condition name - Wing1
.Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
.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
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 - 14224, elements - 28436
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing SU2 file ....
Finished writing SU2 file
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 "BlackBird (7.5.1) "
Running SU2 1
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2 2
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
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
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 - 14224, elements - 28436
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing SU2 file ....
Finished writing SU2 file
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 "BlackBird (7.5.1) "
CAPS Info: Hit last success -- going live!
Running SU2 1
CAPS Info: Hit last success -- going live!
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
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
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
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
CAPS Info: Hit last success -- going live!
Running SU2 2
CAPS Info: Hit last success -- going live!
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
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
.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
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 - 15857, elements - 31702
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing SU2 file ....
Finished writing SU2 file
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 "BlackBird (7.5.1) "
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
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
.Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
.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 "BlackBird (7.5.1) "
.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 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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
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 capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
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
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
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
FERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:58432)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
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
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting surface mesh for body 1 (of 7)
Getting surface mesh for body 2 (of 7)
Getting surface mesh for body 3 (of 7)
Getting surface mesh for body 4 (of 7)
Getting surface mesh for body 5 (of 7)
Getting surface mesh for body 6 (of 7)
7FF848386640 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FF848386640 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000CC06000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000CC06000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes = 98
Number of elements = 192
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes = 297
Number of elements = 590
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 590
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes = 487
Number of elements = 970
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 970
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 7)
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 7)
Number of nodes = 152
Number of elements = 300
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes = 624
Number of elements = 1248
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes = 488
Number of elements = 972
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4194
Total number of elements = 8368
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
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
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 297, elements - 590
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.003174
Creating surface mesh ...
Surface mesh seconds: 0.000331
Recovering boundaries...
Boundary recovery seconds: 0.001337
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.000106
Recovering Delaunayness...
Delaunay recovery seconds: 0.001125
Refining mesh...
Refinement seconds: 0.002597
Smoothing vertices...
Mesh smoothing seconds: 0.003528
Improving mesh...
Mesh improvement seconds: 0.000283
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000136
Total running seconds: 0.012678
Statistics:
Input points: 98
Input facets: 192
Input segments: 288
Input holes: 0
Input regions: 0
Mesh points: 100
Mesh tetrahedra: 232
Mesh faces: 560
Mesh faces on exterior boundary: 192
Mesh faces on input facets: 192
Mesh edges on input segments: 288
Steiner points inside domain: 2
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.015842
Creating surface mesh ...
Surface mesh seconds: 0.000969
Recovering boundaries...
Boundary recovery seconds: 0.00294
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.000609
Recovering Delaunayness...
Delaunay recovery seconds: 0.004439
Refining mesh...
Refinement seconds: 0.027994
Smoothing vertices...
Mesh smoothing seconds: 0.025005
Improving mesh...
Mesh improvement seconds: 0.002802
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00028
Total running seconds: 0.08095
Statistics:
Input points: 297
Input facets: 590
Input segments: 885
Input holes: 0
Input regions: 0
Mesh points: 347
Mesh tetrahedra: 1044
Mesh faces: 2383
Mesh faces on exterior boundary: 590
Mesh faces on input facets: 590
Mesh edges on input segments: 885
Steiner points inside domain: 50
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.064037
Creating surface mesh ...
Surface mesh seconds: 0.001766
Recovering boundaries...
Boundary recovery seconds: 0.007991
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.001341
Recovering Delaunayness...
Delaunay recovery seconds: 0.016699
Refining mesh...
649 insertions, added 165 points, 7218 tetrahedra in queue.
216 insertions, added 8 points, 5722 tetrahedra in queue.
288 insertions, added 12 points, 3275 tetrahedra in queue.
383 insertions, added 10 points, 312 tetrahedra in queue.
511 insertions, added 11 points, 94 tetrahedra in queue.
Refinement seconds: 0.207893
Smoothing vertices...
Mesh smoothing seconds: 0.076084
Improving mesh...
Mesh improvement seconds: 0.003802
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000366
Total running seconds: 0.380089
Statistics:
Input points: 487
Input facets: 970
Input segments: 1455
Input holes: 0
Input regions: 0
Mesh points: 695
Mesh tetrahedra: 2810
Mesh faces: 6105
Mesh faces on exterior boundary: 970
Mesh faces on input facets: 970
Mesh edges on input segments: 1455
Steiner points inside domain: 208
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.4741
Creating surface mesh ...
Surface mesh seconds: 0.006901
Recovering boundaries...
Boundary recovery seconds: 0.015622
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.007692
Recovering Delaunayness...
Delaunay recovery seconds: 0.137505
Refining mesh...
Refinement seconds: 0.415706
Smoothing vertices...
Mesh smoothing seconds: 0.336744
Improving mesh...
Mesh improvement seconds: 0.015789
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.002088
Total running seconds: 1.41243
Statistics:
Input points: 2048
Input facets: 4096
Input segments: 6144
Input holes: 0
Input regions: 0
Mesh points: 2895
Mesh tetrahedra: 11267
Mesh faces: 24582
Mesh faces on exterior boundary: 4096
Mesh faces on input facets: 4096
Mesh edges on input segments: 6144
Steiner points inside domain: 847
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.00102
Creating surface mesh ...
Surface mesh seconds: 0.000623
Recovering boundaries...
Boundary recovery seconds: 0.000748
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.000269
Recovering Delaunayness...
Delaunay recovery seconds: 0.000842
Refining mesh...
202 insertions, added 46 points, 0 tetrahedra in queue.
Refinement seconds: 0.012172
Smoothing vertices...
Mesh smoothing seconds: 0.007319
Improving mesh...
Mesh improvement seconds: 0.000743
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00013
Total running seconds: 0.02393
Statistics:
Input points: 152
Input facets: 300
Input segments: 450
Input holes: 0
Input regions: 0
Mesh points: 198
Mesh tetrahedra: 672
Mesh faces: 1494
Mesh faces on exterior boundary: 300
Mesh faces on input facets: 300
Mesh edges on input segments: 450
Steiner points inside domain: 46
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.058846
Creating surface mesh ...
Surface mesh seconds: 0.002342
Recovering boundaries...
Boundary recovery seconds: 0.006628
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.001774
Recovering Delaunayness...
Delaunay recovery seconds: 0.008012
Refining mesh...
831 insertions, added 225 points, 6035 tetrahedra in queue.
Refinement seconds: 0.099069
Smoothing vertices...
Mesh smoothing seconds: 0.079822
Improving mesh...
Mesh improvement seconds: 0.004276
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000506
Total running seconds: 0.261391
Statistics:
Input points: 624
Input facets: 1248
Input segments: 1872
Input holes: 0
Input regions: 0
Mesh points: 856
Mesh tetrahedra: 3198
Mesh faces: 7020
Mesh faces on exterior boundary: 1248
Mesh faces on input facets: 1248
Mesh edges on input segments: 1872
Steiner points inside domain: 232
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.047643
Creating surface mesh ...
Surface mesh seconds: 0.001671
Recovering boundaries...
Boundary recovery seconds: 0.007676
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.000953
Recovering Delaunayness...
Delaunay recovery seconds: 0.039187
Refining mesh...
Refinement seconds: 0.067886
Smoothing vertices...
Mesh smoothing seconds: 0.046942
Improving mesh...
Mesh improvement seconds: 0.003336
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000476
Total running seconds: 0.215867
Statistics:
Input points: 488
Input facets: 972
Input segments: 1458
Input holes: 0
Input regions: 0
Mesh points: 676
Mesh tetrahedra: 2529
Mesh faces: 5544
Mesh faces on exterior boundary: 972
Mesh faces on input facets: 972
Mesh edges on input segments: 1458
Steiner points inside domain: 188
Done meshing using TetGen!
Writing AFLR3 file ....
Finished writing AFLR3 file
Writing AFLR3 file ....
Finished writing AFLR3 file
Writing AFLR3 file ....
Finished writing AFLR3 file
Writing AFLR3 file ....
Finished writing AFLR3 file
Writing AFLR3 file ....
Finished writing AFLR3 file
Writing AFLR3 file ....
Finished writing AFLR3 file
Writing AFLR3 file ....
Finished writing AFLR3 file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
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
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 297, elements - 590
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.003312
Creating surface mesh ...
Surface mesh seconds: 0.000355
Recovering boundaries...
Boundary recovery seconds: 0.001372
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.000109
Recovering Delaunayness...
Delaunay recovery seconds: 0.00127
Refining mesh...
Refinement seconds: 0.001075
Smoothing vertices...
Mesh smoothing seconds: 0.003495
Improving mesh...
Mesh improvement seconds: 0.000273
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 9e-05
Total running seconds: 0.011407
Statistics:
Input points: 98
Input facets: 192
Input segments: 288
Input holes: 0
Input regions: 1
Mesh points: 100
Mesh tetrahedra: 232
Mesh faces: 560
Mesh faces on exterior boundary: 192
Mesh faces on input facets: 192
Mesh edges on input segments: 288
Steiner points inside domain: 2
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.01649
Creating surface mesh ...
Surface mesh seconds: 0.001045
Recovering boundaries...
Boundary recovery seconds: 0.003185
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.000691
Recovering Delaunayness...
Delaunay recovery seconds: 0.004486
Refining mesh...
Refinement seconds: 0.025502
Smoothing vertices...
Mesh smoothing seconds: 0.025938
Improving mesh...
Mesh improvement seconds: 0.001285
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000286
Total running seconds: 0.078999
Statistics:
Input points: 297
Input facets: 590
Input segments: 885
Input holes: 0
Input regions: 2
Mesh points: 347
Mesh tetrahedra: 1044
Mesh faces: 2383
Mesh faces on exterior boundary: 590
Mesh faces on input facets: 590
Mesh edges on input segments: 885
Steiner points inside domain: 50
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.065752
Creating surface mesh ...
Surface mesh seconds: 0.001751
Recovering boundaries...
Boundary recovery seconds: 0.008221
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.001449
Recovering Delaunayness...
Delaunay recovery seconds: 0.017149
Refining mesh...
649 insertions, added 164 points, 7317 tetrahedra in queue.
216 insertions, added 10 points, 6108 tetrahedra in queue.
288 insertions, added 9 points, 3288 tetrahedra in queue.
383 insertions, added 12 points, 283 tetrahedra in queue.
511 insertions, added 12 points, 75 tetrahedra in queue.
Refinement seconds: 0.213721
Smoothing vertices...
Mesh smoothing seconds: 0.077447
Improving mesh...
Mesh improvement seconds: 0.003742
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00044
Total running seconds: 0.389777
Statistics:
Input points: 487
Input facets: 970
Input segments: 1455
Input holes: 0
Input regions: 3
Mesh points: 695
Mesh tetrahedra: 2796
Mesh faces: 6077
Mesh faces on exterior boundary: 970
Mesh faces on input facets: 970
Mesh edges on input segments: 1455
Steiner points inside domain: 208
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.478172
Creating surface mesh ...
Surface mesh seconds: 0.007002
Recovering boundaries...
Boundary recovery seconds: 0.017256
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.007166
Recovering Delaunayness...
Delaunay recovery seconds: 0.138816
Refining mesh...
Refinement seconds: 0.410519
Smoothing vertices...
Mesh smoothing seconds: 0.337466
Improving mesh...
Mesh improvement seconds: 0.015868
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.001976
Total running seconds: 1.41447
Statistics:
Input points: 2048
Input facets: 4096
Input segments: 6144
Input holes: 0
Input regions: 4
Mesh points: 2905
Mesh tetrahedra: 11306
Mesh faces: 24660
Mesh faces on exterior boundary: 4096
Mesh faces on input facets: 4096
Mesh edges on input segments: 6144
Steiner points inside domain: 857
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.001026
Creating surface mesh ...
Surface mesh seconds: 0.000591
Recovering boundaries...
Boundary recovery seconds: 0.000759
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Warning: The 4-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.000225
Recovering Delaunayness...
Delaunay recovery seconds: 0.000785
Refining mesh...
202 insertions, added 46 points, 0 tetrahedra in queue.
Refinement seconds: 0.010468
Smoothing vertices...
Mesh smoothing seconds: 0.007326
Improving mesh...
Mesh improvement seconds: 0.00079
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000171
Total running seconds: 0.022209
Statistics:
Input points: 152
Input facets: 300
Input segments: 450
Input holes: 0
Input regions: 5
Mesh points: 198
Mesh tetrahedra: 672
Mesh faces: 1494
Mesh faces on exterior boundary: 300
Mesh faces on input facets: 300
Mesh edges on input segments: 450
Steiner points inside domain: 46
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.058219
Creating surface mesh ...
Surface mesh seconds: 0.002324
Recovering boundaries...
Boundary recovery seconds: 0.006818
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Warning: The 4-th region point lies outside the convex hull.
Warning: The 5-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.001968
Recovering Delaunayness...
Delaunay recovery seconds: 0.008323
Refining mesh...
831 insertions, added 225 points, 6035 tetrahedra in queue.
Refinement seconds: 0.098116
Smoothing vertices...
Mesh smoothing seconds: 0.083533
Improving mesh...
Mesh improvement seconds: 0.004331
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000491
Total running seconds: 0.264249
Statistics:
Input points: 624
Input facets: 1248
Input segments: 1872
Input holes: 0
Input regions: 6
Mesh points: 856
Mesh tetrahedra: 3198
Mesh faces: 7020
Mesh faces on exterior boundary: 1248
Mesh faces on input facets: 1248
Mesh edges on input segments: 1872
Steiner points inside domain: 232
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.048717
Creating surface mesh ...
Surface mesh seconds: 0.00355
Recovering boundaries...
Boundary recovery seconds: 0.008238
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Warning: The 4-th region point lies outside the convex hull.
Warning: The 5-th region point lies outside the convex hull.
Warning: The 6-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.001153
Recovering Delaunayness...
Delaunay recovery seconds: 0.042803
Refining mesh...
Refinement seconds: 0.0727
Smoothing vertices...
Mesh smoothing seconds: 0.049031
Improving mesh...
Mesh improvement seconds: 0.003571
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000432
Total running seconds: 0.230313
Statistics:
Input points: 488
Input facets: 972
Input segments: 1458
Input holes: 0
Input regions: 7
Mesh points: 676
Mesh tetrahedra: 2544
Mesh faces: 5574
Mesh faces on exterior boundary: 972
Mesh faces on input facets: 972
Mesh edges on input segments: 1458
Steiner points inside domain: 188
Done meshing using TetGen!
Writing AFLR3 file ....
Finished writing AFLR3 file
.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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup 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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing TECPLOT file: test.dat ....
Finished writing TECPLOT file
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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup 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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 7161, elements - 14314
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing TECPLOT file: test.dat ....
Finished writing TECPLOT file
.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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
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 = 9605
Number of elements = 19202
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19202
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9605
Total number of elements = 19202
Writing TECPLOT file: test.dat ....
Finished writing TECPLOT file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing TECPLOT file: test.dat ....
Finished writing TECPLOT file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
Writing TECPLOT file: test.dat ....
Finished writing TECPLOT file
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.......Note: The following floating-point exceptions are signalling: IEEE_DENORMAL
..
======================================================================
ERROR: test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 427, in test_Mesh_Morph_Sensitivity
self.fun3d.preAnalysis()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 2861, in preAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: EGADS_NULLOBJ:
================================================================================
aimMesh.c:1542 in aim_morphMeshUpdate(): Error status = -2
fun3dAIM.c:1069 in aimUpdateState(): Error status = -2
================================================================================
======================================================================
FAIL: test_PlateSensFile (test_tacs.TestTACS)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/test_tacs.py", line 163, in test_PlateSensFile
self.assertAlmostEqual(Func1_plateLength, xyz[inode][0], 5)
AssertionError: 0.0 != 0.5 within 5 places (0.5 difference)
----------------------------------------------------------------------
Ran 123 tests in 907.166s
FAILED (failures=1, errors=1)
CAPS Error: Cannot open /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/capsRestart/Problem!
CAPS Warning: caps_writeProblem = -333 (caps_close)!
make[1]: *** [test] Error 1
make: *** [unitaim] Error 2
++ true
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWIN64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.6,CAPS/unit,DARWIN64,macys)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN64,buildnode=macys #183' 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=7.6,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN64,buildnode=macys #184'.
[Checks API] No suitable checks publisher found.
Build step 'Console output (build log) parsing' changed build result to FAILURE
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE
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