Skipping 448 KB..
Full Log 358: 14.400000 14.400001 14.400001 14.400001 14.399999 14.400002 14.400001
365: 14.400001 14.400002 14.400000 14.400001 14.357384 14.400000 14.399999
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477: 14.400001 14.400006 14.400001 14.400000 14.400001 14.400000 14.400001
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554: 14.367007 14.367819 14.399999 14.369566 14.400001 14.399999 14.399999
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589: 14.372211 14.400002 14.400000 14.400002 14.400002 14.400003 14.400000
596: 14.400004 14.400004 14.373403 14.368774 14.400000 14.400000 14.399999
603: 14.400001 14.400002 14.370406 14.367007 14.400001 14.372363 14.400001
610: 14.370598 14.400000 14.399999 14.400002 14.400004 14.372320 14.400000
617: 14.400000 14.368054 14.400004 14.400000 14.378759 14.400000 14.366320
624: 14.400000 14.400000 14.400004 14.370366 14.370760 14.400002 14.400004
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652: 14.400002 14.367680 14.400000 14.400004 14.400000 14.400003 14.400003
659: 14.367301 14.400000 14.371052 14.400000 14.400004 14.375426 14.372158
666: 14.400000 14.370146 14.399999 14.400004 14.399999 14.368248 14.400000
673: 14.400003 14.369989 14.370548 14.368054 14.377207 14.400000 14.369613
680: 14.368333 14.400004 14.400001 14.377741 14.400003 14.400000 14.400004
687: 14.400003 14.400003 14.400000 14.377967 14.399999 14.376780 14.370538
694: 14.373367 14.400000 14.400003 14.400004 14.370294 14.371052 14.400000
701: 14.400003 14.370426 14.400004 14.400001 14.400001 14.376281 14.375920
708: 14.377357 14.400000 14.376914 14.400001 14.400002 14.400002 14.400002
715: 14.400003 14.379840 14.370996 14.400003 14.400003 14.370673 14.400000
722: 14.363653 14.362250 14.373534 14.400003 14.379510 14.400000 14.374657
729: 14.400003 14.400004 14.400002 14.379679 14.400000 14.379827 14.372479
736: 14.400002 14.380745 14.379344 14.379423 14.400003 14.380718 14.372490
743: 14.376209 14.400000 14.400000 14.400000 14.400000 14.400000 14.400003
750: 14.375014 14.373465 14.400000 14.400003 14.380638 14.400002 14.400002
757: 14.400000 14.376150 14.400003 14.400003 14.370382 14.379062 14.379044
764: 14.382714 14.371636 14.380688 14.372490 14.400004 14.380301 14.400003
771: 14.400003 14.400003 14.400003 14.381338 14.400003 14.400000 14.375566
778: 14.383460 14.400000 14.400000 14.382573 14.378742 14.378784 14.400002
785: 14.400003 14.377962 14.400003 14.388515 14.372960 14.400003 14.373659
792: 14.400000 14.376226 14.400000 14.400000 14.373627 14.400000 14.400002
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813: 14.400002 14.400002 14.400002 14.400002 14.400002 14.400003 14.400003
820: 14.375490 14.374772 14.400003 14.375179 14.376681 14.379475 14.400003
827: 14.374392 14.379479 14.377005 14.387430 14.400002 14.382223 14.400003
834: 14.374371 14.383997 14.382259 14.386520 14.400000 14.400002 14.384358
841: 14.381380 14.373136 14.380004 14.382103 14.400002 14.400000 14.376043
848: 14.400000 14.381875 14.400002 14.377417 14.379456 14.400000 14.379534
855: 14.400002 14.400003 14.400000 14.400003 14.400000 14.400000 14.382400
862: 14.384944 14.376706 14.383227 14.400002 14.380291 14.400002 14.382257
869: 14.400003 14.384774 14.384820 14.382273 14.373450 14.400000 14.400003
876: 14.375908 14.378550 14.400000 14.377290 14.382472 14.379168 14.383016
883: 14.385491 14.382723 14.400003 14.400002 14.378971 14.385404 14.380466
890: 14.384576 14.400003 14.377221 14.400000 14.381355 14.383645 14.384247
897: 14.385287 14.383280 14.375114 14.400002 14.400000 14.400000 14.400000
904: 14.382426 14.382735 14.400002 14.382499 14.387660 14.382883 14.400002
911: 14.383520 14.387020 14.383842 14.382243 14.400000 14.378098 14.383884
918: 14.383573 14.384907 14.386099 14.400002 14.383499 14.385888 14.400002
925: 14.377060 14.378436 14.381620 14.380706 14.400000 14.373575 14.383742
932: 14.381255 14.382997 14.384659 14.382920 14.400000 14.400002 14.377577
939: 14.400000 14.386915 14.386123 14.384593 14.381816 14.381745 14.385286
946: 14.385286 14.382005 14.385759 14.385133 14.388988 14.381642 14.387570
953: 14.386633 14.386532 14.381505 14.386235 14.385447 14.400000 14.380013
960: 14.400000 14.382953 14.400002 14.383380 14.385229 14.383810 14.382999
967: 14.385309 14.400002 14.400002 14.382711 14.383198 14.385759 14.387667
974: 14.385183 14.384109 14.387476 14.400002 14.384433 14.388306 14.400002
981: 14.400002 14.383798 14.386396 14.386806 14.383774 14.389577 14.400000
988: 14.379854 14.381554 14.377995 14.375728 14.378018 14.382139 14.386343
995: 14.386055 14.378954 14.383869 14.400002 14.383263 14.385113 14.381831
1002: 14.400002 14.386892 14.388833 14.386742 14.385055 14.385000 14.381934
1009: 14.381408 14.380687 14.379175 14.380043 14.381323 14.375969 14.381364
1016: 14.384193 14.380959 14.400002 14.400002 14.400002 14.385962 14.400002
1023: 14.386889 14.381389 14.400002 14.379351 14.387189 14.400000 14.382624
1030: 14.400002 14.387047 14.400002 14.386889 14.379175 14.377388 14.389345
1037: 14.400002 14.400000 14.400000 14.381891 14.380687 14.400002 14.400000
1044: 14.383688 14.400002 14.400002 14.400002 14.383791 14.400000 14.400002
1051: 14.400003 14.400000 14.376605 14.400002 14.400000 14.376130 14.400003
1058: 14.383633 14.400002 14.400000 14.378191 14.384880
source getTriangles = 0, nGtris = 2006, nGsegs = 6018, Ds = 0 0
destin getTriangles = 0, nGtris = 772, nGsegs = 2316, Ds = 0 0
In caps_outputObjects:
2 Analyses found
1 Bounds found
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m11.821s
user 0m11.266s
sys 0m0.274s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm passed (as expected)
=============================================
+ rm -rf source.vs destin.vs
+ expectCSuccess '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm'
+ /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm
testingAIM/aimInitialize instance = 0 unitSys = m!
testingAIM/aimInputs instance = 0 index = 1!
testingAIM/aimInputs instance = 0 index = 2!
testingAIM/aimInputs instance = 0 index = 3!
testingAIM/aimInputs instance = 0 index = 4!
testingAIM/aimOutputs instance = 0 index = 1!
testingAIM/aimOutputs instance = 0 index = 2!
testingAIM/aimOutputs instance = 0 index = 3!
testingAIM/aimInitialize instance = 1 unitSys = (null)!
testingAIM/aimInputs instance = 1 index = 1!
testingAIM/aimInputs instance = 1 index = 2!
testingAIM/aimInputs instance = 1 index = 3!
testingAIM/aimInputs instance = 1 index = 4!
testingAIM/aimOutputs instance = 1 index = 1!
testingAIM/aimOutputs instance = 1 index = 2!
testingAIM/aimOutputs instance = 1 index = 3!
Intent = child
APath = /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/test/autoExecTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 2
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
testingAIM/aimUpdateState instance = 0!
tess is NULL!
testingAIM/aimPreAnalysis instance = 0!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
getDiscr = -303
meshRef = NULL
testingAIM/aimExecute instance = 0!
testingAIM/aimPostAnalysis instance = 0 restart = 0!
testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0!
aim_getDiscr 0 on Interface = -303
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
testingAIM/aimUpdateState instance = 1!
tess is NULL!
testingAIM/aimPreAnalysis instance = 1!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
mesh file = /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/test/autoExecTest/Scratch/testingAIM0/meshFile
symLink = 0
getDiscr = -303
testingAIM/aimExecute instance = 1!
testingAIM/aimPostAnalysis instance = 1 restart = 0!
testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0!
aim_getDiscr 1 on Interface = -303
*** testingAIMout (child) = 12.340000 1 1 ***
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m0.468s
user 0m0.318s
sys 0m0.257s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm passed (as expected)
=============================================
/Library/Developer/CommandLineTools/usr/bin/make -C aim/skeleton test
python -u case.py
Loading file into our Problem
Default num = 8.0
Current num = 16.0
aim_newGeometry = 0!
GeometryIn:
1: num 2 (1,1)
2: x 2 (8,1)
3: ymin 2 (8,1)
4: zmin 2 (8,1)
5: zmax 2 (8,1)
GeometryOut:
1: pVol 6 (1,1)
2: cVol 6 (1,1)
AnalysisIn:
1: InputVariable 0 (1,1) (null)
2: num 2 (1,1) (null)
3: Mach 2 (1,1) (null)
4: Mesh_Format 3 (1,1) (null)
5: Table 4 (1,3) (null)
Computed sqrtNum = 4.0
# pyCAPS Unit tests (and legacy)
/Library/Developer/CommandLineTools/usr/bin/make -C pyCAPS/unitTest test
python --version
Python 3.11.6
python -u -m unittest discover
..Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 143
Number of elements = 282
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 282
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 155
Number of elements = 306
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 306
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 298
Combined Number of elements = 588
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 588
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library - d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 209
Number of elements = 414
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 414
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 186
Number of elements = 368
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 368
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 395
Combined Number of elements = 782
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 782
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
..........--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. 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!
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!
. 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!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. 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!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. CAPS Info: Hit last success -- going live!
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
----------------------------------------------------------------------
Ran 100 tests in 8.954s
OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
/Library/Developer/CommandLineTools/usr/bin/make -C legacy/unitTest test
python --version
Python 3.11.6
python -u -m unittest discover
......sAnalysis Info:
Name = UnitTest_fun3dAIM
Intent = None
AnalysisDir = /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM
Version = 1.25
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
Analysis Info:
Name = UnitTest_fun3dAIM
Intent = None
AnalysisDir = /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM
Version = 1.25
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_1 will be used!
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_2 will be used!
Analysis Info:
Name = UnitTest7_fun3dAIM
Intent = None
AnalysisDir = /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest7_fun3dAIM
Version = 1.25
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_3 will be used!
Analysis Info:
Name = UnitTest8_fun3dAIM
Intent = None
AnalysisDir = /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest8_fun3dAIM
Version = 1.25
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_4 will be used!
Analysis Info:
Name = UnitTest9_fun3dAIM
Intent = STRUCTURE
AnalysisDir = /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest9_fun3dAIM
Version = 1.25
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_5 will be used!
Analysis Info:
Name = UnitTest10_fun3dAIM
Intent = ['CFD', 'STRUCTURE']
AnalysisDir = /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest10_fun3dAIM
Version = 1.25
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
...Error: Invalid attribute level! Defaulting to 'Face'
..
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_6 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_7 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_8 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_9 will be used!
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_1 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_10 will be used!
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_2 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_11 will be used!
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_3 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_12 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_13 will be used!
...No data transfer method (transferMethod) provided - defaulting to "Interpolate"
No data transfer method (transferMethod) provided - defaulting to "Interpolate"
.No data transfer method (transferMethod) provided - defaulting to "Interpolate"
....No data transfer method (transferMethod) provided - defaulting to "Interpolate"
.No data transfer method (transferMethod) provided - defaulting to "Interpolate"
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.s. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
...Error: Invalid attribute level! Defaulting to 'Face'
........ EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
.... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.s... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.Linked Parameter Beta to analysis fun3d input Beta
Linked Parameter Alpha to analysis fun3d input Alpha
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
16F6AB000 Odd Degenerate test for side 1: 9!
1E2491C40 Odd Degenerate test for side 2: 9!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 395
Number of elements = 786
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 786
Elemental Quad4 = 0
16F6AB000 Odd Degenerate test for side 1: 9!
16F6AB000 Odd Degenerate test for side 2: 9!
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 623
Number of elements = 1242
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1242
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 1018
Combined Number of elements = 2028
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 2028
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
................
----------------------------------------------------------------------
Ran 72 tests in 3.876s
OK (skipped=3)
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.addAttribute' is deprecated. Please use 'Analysis.attr.create'!
WARNING: 'capsAnalysis.getAttribute' is deprecated. Please use 'Analysis.attr["name"].value'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsAnalysis.getAttributeVal' is deprecated. Please use 'Analysis.geometry.attrList'!
WARNING: 'capsAnalysis.getBoundingBox' is deprecated. Please use 'Analysis.bodies'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.saveGeometry' is deprecated. Please use 'Analysis.geometry.save'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.buildGeometry' is deprecated. Please use 'Problem.geometry.build'!
WARNING: 'capsGeometry.getAttributeMap' is deprecated. Please use 'Problem.geometry.attrMap'!
WARNING: 'capsGeometry.getAttributeVal' is deprecated. Please use 'Problem.geometry.attrList'!
WARNING: 'capsGeometry.getBoundingBox' is deprecated. Please use 'Problem.geometry.bodies'!
WARNING: 'capsGeometry.getGeometryOutVal' is deprecated. Please use 'Problem.geometry.outpmtr["varname"].value'!
WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.saveGeometry' is deprecated. Please use 'Problem.geometry.save'!
WARNING: 'capsGeometry.viewGeometry' is deprecated. Please use 'Problem.geometry.view'!
WARNING: 'capsProblem.addAttribute' is deprecated. Please use 'Problem.attr.create'!
WARNING: 'capsProblem.getAttribute' is deprecated. Please use 'Problem.attr["name"].value'!
WARNING: 'capsProblem.createValue' is deprecated. Please use 'Problem.parameter.create'!
WARNING: '_capsValue.__init__' is deprecated. Please use 'Problem.parameter.create'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
WARNING: 'capsProblem.autoLinkValue' is deprecated. Please use 'Problem.autoLinkParameter'!
Legacy pyCAPS unit testing done!
# CAPS Minimal examples (one per aim)
/Library/Developer/CommandLineTools/usr/bin/make -C examples test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
(make -C cCAPS -f avlTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/frictionTest' is up to date.
(make -C cCAPS -f fun3d.make)
make[2]: Nothing to be done for `fun3d'.
(make -C cCAPS -f hsm.make)
make[2]: `hsm' is up to date.
(make -C cCAPS -f interferenceTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/pointwiseTest' is up to date.
(cd /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests
All tests pass!
=================================================
=================================================
(cd /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest; ./execute_PyTestRegression.sh MINIMAL)
=================================================
Using python : /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
CXtot 0.0006119078685800925
CYtot -6.292592518559147e-15
CZtot -0.3012861394881712
Cltot -4.783069014642483e-14
Cmtot -0.1945055953448147
Cntot -2.338890054396671e-15
Cl'tot -4.786422456048383e-14
Cn'tot -1.50377318550154e-15
CLtot 0.3012509314146395
CDtot 0.00464635348821979
CDvis 0.0
CLff 0.3009503023516151
CYff -7.7198870803959e-15
CDind 0.00464635348821979
CDff 0.004968969500894849
e 0.9669902146155998
StripForces
Wing cl = [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407]
Wing cd = [-0.004234137763148, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946456, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372442, -0.004494543653152, -0.00423413776453]
real 0m0.510s
user 0m0.546s
sys 0m0.182s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Cl = [1.05475230551148, 1.36488869373725, 1.56607214272246, 2.03059709357768, 1.9727108312095, 1.87307153172323, 1.76050475760053]
Cd = [0.0131991208831308, 0.0166540240605859, 0.0200551482562657, 0.0458671341873005, 0.0754256009397268, 0.0994469174479059, 0.127479430989221]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.49604411072842, 0.461377732041756, 0.442376568202227, 0.361251636144409, 0.276104140854608, 0.214381239321802, 0.132988264746433]
real 0m2.011s
user 0m2.243s
sys 0m0.073s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Cl = 0.3783791085548177
Cd = 0.007775858417209677
Cm = 0.005262636995835036
real 0m2.154s
user 0m2.144s
sys 0m0.106s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'awave_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
awave_PyTest.py test;
+ python -u awave_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Writing Awave input file
Body Section, Body ID 1
XCG: 1.571025 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 2
XCG: 2.539271 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 3
XCG: 1.571025 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Body Section, Body ID 4
XCG: 2.539271 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Lifting Surface Section, Body ID 5
XLE: 1.571946 -3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 0
Lifting Surface Section, Body ID 6
XLE: 0.000000 0.000000 0.000000
CHORD: 1.614013
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 7
XLE: 1.571946 3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 8
XLE: 5.484123 0.000000 1.468246
CHORD: 0.726185
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 9
XLE: 5.000000 0.000000 0.500000
CHORD: 1.210308
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 10
XLE: 5.484123 -0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 0
Lifting Surface Section, Body ID 11
XLE: 5.484123 0.000000 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Lifting Surface Section, Body ID 12
XLE: 5.484123 0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Body Section, Body ID 13
XCG: -2.000000 0.000000 0.000000
AREA: 0.000000
RAD: 0.000000
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 14
XCG: 0.000000 -0.000000 -0.000000
AREA: 0.818123
RAD: 0.510310
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Warning: capsGroup not found on body 15!
Body Section, Body ID 15
XCG: 1.613743 -0.000000 -0.000000
AREA: 0.327249
RAD: 0.322749
ATTRIB:Fuse
NAME :(null)
Awave TYPE: 2
Body Section, Body ID 16
XCG: 5.000000 -0.000000 0.500000
AREA: 0.081812
RAD: 0.161374
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 17
XCG: 6.210307 -0.000000 0.500000
AREA: 0.000818
RAD: 0.016137
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
AwaveTypes: 2 5 4 2 2
Points for all four fuselage sections :: 5 0 0 0
Number of Mach-Alpha cases = 2
CdWave = [1.13333237, 0.216380283]
real 0m0.463s
user 0m0.587s
sys 0m0.080s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
real 0m0.374s
user 0m0.462s
sys 0m0.079s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go. Other input will terminate the job.
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG
Cl = 0.933407
Cd = 0.000284
Cd Wave = 0.0
Cm = -0.203436
Cp _Critcal = -1.303869
real 0m0.326s
user 0m0.428s
sys 0m0.060s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Getting mesh sizing parameters
Mesh sizing name - Airfoil
Mesh sizing name - AirfoilTE
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m0.578s
user 0m0.630s
sys 0m0.357s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting mesh sizing parameters
Mesh sizing name - LeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes = 3793
Number of elements = 4001
Number of triangle elements = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 76
Number of elements = 55
Number of triangle elements = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes = 100
Number of elements = 73
Number of triangle elements = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes = 3970
Total number of elements = 4129
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m3.857s
user 0m9.380s
sys 0m3.940s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Darwin 22.6.0 arm64
AFLR2 : Compile Date 08/01/23 @ 11:39PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 316 634
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 681 1018
AFLR2 GGp: Nodes, Faces = 1013 1682
AFLR2 GGp: Nodes, Faces = 1339 2334
AFLR2 GGp: Nodes, Faces = 1652 2960
AFLR2 GGp: Nodes, Faces = 1957 3570
AFLR2 GGp: Nodes, Faces = 2252 4160
AFLR2 GGp: Nodes, Faces = 2526 4708
AFLR2 GGp: Nodes, Faces = 2809 5274
AFLR2 GGp: Nodes, Faces = 3083 5822
AFLR2 GGp: Nodes, Faces = 3327 6310
AFLR2 GGp: Nodes, Faces = 3564 6784
AFLR2 GGp: Nodes, Faces = 3788 7232
AFLR2 GGp: Nodes, Faces = 3995 7646
AFLR2 GGp: Nodes, Faces = 4194 8044
AFLR2 GGp: Nodes, Faces = 4394 8444
AFLR2 GGp: Nodes, Faces = 4585 8826
AFLR2 GGp: Nodes, Faces = 4772 9200
AFLR2 GGp: Nodes, Faces = 4943 9542
AFLR2 GGp: Nodes, Faces = 5129 9914
AFLR2 GGp: Nodes, Faces = 5293 10242
AFLR2 GGp: Nodes, Faces = 5447 10550
AFLR2 GGp: Nodes, Faces = 5594 10844
AFLR2 GGp: Nodes, Faces = 5716 11088
AFLR2 GGp: Nodes, Faces = 5830 11316
AFLR2 GGp: Nodes, Faces = 5909 11474
AFLR2 GGp: Nodes, Faces = 5964 11584
AFLR2 GGp: Nodes, Faces = 6006 11668
AFLR2 GGp: Nodes, Faces = 6025 11706
AFLR2 GGp: Nodes, Faces = 6034 11724
AFLR2 : CPU Time = 0.010 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 6034 11724
AFLR2 QI : Nodes, Faces = 6033 454
AFLR2 QI : Nodes, Faces = 6033 5634
AFLR2 QI : Nodes, Faces = 6033 11722
AFLR2 QI : Nodes, Faces = 6032 462
AFLR2 QI : Nodes, Faces = 6032 5629
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 456
AFLR2 QI : Nodes, Faces = 6032 5632
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 474
AFLR2 QI : Nodes, Faces = 6032 5623
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6031 486
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 QI : Nodes, Faces = 6031 488
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 : CPU Time = 0.004 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
real 0m0.523s
user 0m0.698s
sys 0m0.304s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Darwin 22.6.0 arm64
AFLR2 : Compile Date 08/01/23 @ 11:39PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.9
AFLR4 : Version Date 08/14/23 @ 12:27AM
AFLR4 : Compile OS Darwin 22.6.0 arm64
AFLR4 : Compile Date 08/14/23 @ 12:31AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 150333
Number of elements = 450865
Number of triangles = 14380
Number of quadrilatarals = 0
Number of tetrahedrals = 215433
Number of pyramids = 427
Number of prisms = 220625
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m8.595s
user 0m7.786s
sys 0m0.282s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
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 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 = 2236
Number of elements = 4468
Number of triangle elements = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 636
Number of elements = 1268
Number of triangle elements = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 258
Number of elements = 512
Number of triangle elements = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3130
Total number of elements = 6248
Writing Tecplot file ....
Finished writing Tecplot file
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 - 3130, elements - 6248
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.01509
Creating surface mesh ...
Surface mesh seconds: 0.002984
Recovering boundaries...
Boundary recovery seconds: 0.049584
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.002608
Suppressing Steiner points ...
Steiner suppression seconds: 6e-06
Recovering Delaunayness...
Delaunay recovery seconds: 0.005274
Refining mesh...
4177 insertions, added 2159 points, 136953 tetrahedra in queue.
1390 insertions, added 372 points, 139199 tetrahedra in queue.
1853 insertions, added 454 points, 136118 tetrahedra in queue.
2470 insertions, added 521 points, 118263 tetrahedra in queue.
3293 insertions, added 464 points, 66933 tetrahedra in queue.
4389 insertions, added 406 points, 1337 tetrahedra in queue.
5851 insertions, added 599 points, 33 tetrahedra in queue.
Refinement seconds: 0.399392
Smoothing vertices...
Mesh smoothing seconds: 0.216332
Improving mesh...
Mesh improvement seconds: 0.007115
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00081
Total running seconds: 0.699431
Statistics:
Input points: 3130
Input facets: 6248
Input segments: 9372
Input holes: 2
Input regions: 0
Mesh points: 8156
Mesh tetrahedra: 40155
Mesh faces: 83435
Mesh faces on exterior boundary: 6250
Mesh faces on input facets: 6250
Mesh edges on input segments: 9373
Steiner points on input segments: 1
Steiner points inside domain: 5025
Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.
Writing Tecplot file ....
Finished writing Tecplot file
real 0m1.577s
user 0m1.779s
sys 0m0.158s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Darwin 22.6.0 arm64
AFLR2 : Compile Date 08/01/23 @ 11:39PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 545 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 545 545
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 110 222
AFLR2 IG : Nodes, Faces = 220 442
AFLR2 IG : Nodes, Faces = 330 662
AFLR2 IG : Nodes, Faces = 440 882
AFLR2 IG : Nodes, Faces = 517 1036
AFLR2 IG : Nodes, Faces = 545 1092
AFLR2 IG : Nodes, Faces = 549 1092
AFLR2 IG : Nodes, Faces = 545 545
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 545 545
AFLR2 GGp: Nodes, Faces = 1083 1621
AFLR2 GGp: Nodes, Faces = 1616 2687
AFLR2 GGp: Nodes, Faces = 2144 3743
AFLR2 GGp: Nodes, Faces = 2661 4777
AFLR2 GGp: Nodes, Faces = 3171 5797
AFLR2 GGp: Nodes, Faces = 3672 6799
AFLR2 GGp: Nodes, Faces = 4158 7771
AFLR2 GGp: Nodes, Faces = 4653 8761
AFLR2 GGp: Nodes, Faces = 5142 9739
AFLR2 GGp: Nodes, Faces = 5608 10671
AFLR2 GGp: Nodes, Faces = 6055 11565
AFLR2 GGp: Nodes, Faces = 6482 12419
AFLR2 GGp: Nodes, Faces = 6880 13215
AFLR2 GGp: Nodes, Faces = 7257 13969
AFLR2 GGp: Nodes, Faces = 7614 14683
AFLR2 GGp: Nodes, Faces = 7947 15349
AFLR2 GGp: Nodes, Faces = 8276 16007
AFLR2 GGp: Nodes, Faces = 8575 16605
AFLR2 GGp: Nodes, Faces = 8869 17193
AFLR2 GGp: Nodes, Faces = 9140 17735
AFLR2 GGp: Nodes, Faces = 9401 18257
AFLR2 GGp: Nodes, Faces = 9654 18763
AFLR2 GGp: Nodes, Faces = 9887 19229
AFLR2 GGp: Nodes, Faces = 10110 19675
AFLR2 GGp: Nodes, Faces = 10315 20085
AFLR2 GGp: Nodes, Faces = 10497 20449
AFLR2 GGp: Nodes, Faces = 10656 20767
AFLR2 GGp: Nodes, Faces = 10791 21037
AFLR2 GGp: Nodes, Faces = 10919 21293
AFLR2 GGp: Nodes, Faces = 11022 21499
AFLR2 GGp: Nodes, Faces = 11092 21639
AFLR2 GGp: Nodes, Faces = 11145 21745
AFLR2 GGp: Nodes, Faces = 11156 21767
AFLR2 : CPU Time = 0.022 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 11156 21767
AFLR2 QI : Nodes, Faces = 11155 819
AFLR2 QI : Nodes, Faces = 11155 10473
AFLR2 QI : Nodes, Faces = 11155 21765
AFLR2 QI : Nodes, Faces = 11154 811
AFLR2 QI : Nodes, Faces = 11154 10476
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11154 805
AFLR2 QI : Nodes, Faces = 11154 10479
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11154 911
AFLR2 QI : Nodes, Faces = 11154 10426
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11153 915
AFLR2 QI : Nodes, Faces = 11153 10423
AFLR2 QI : Nodes, Faces = 11153 917
AFLR2 QI : Nodes, Faces = 11153 10423
AFLR2 : CPU Time = 0.008 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 49.3184| 90|
| CV Face Area Aspect Ratio| 1.00035| 33.4982|
| CV Sub-Volume Ratio| 1.00001| 7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11153| 1/1.00| 10|
| 1| 2702| 1/4.13| 7.38309|
| 2| 549| 1/4.92| 4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 5.8149e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.5507e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.4402e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.4331e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.4155e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 5.3965e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 5.3703e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 5.3621e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 5.3504e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 5.3580e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.22124| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file |surface_flow_pyCAPS_su2_aflr2.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary |flow_pyCAPS_su2_aflr2.szplt |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.072253 Cd = -0.01151
Cmz = 0.070975
Cx = -0.01151 Cy = 0.072253
Pressure Contribution
Cl_p = 0.072253 Cd_p = -0.01151
Cmz_p = 0.070975
Cx_p = -0.01151 Cy_p = 0.072253
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m1.603s
user 0m1.499s
sys 0m0.600s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
./execute_PyTestRegression.sh: line 198: ulimit: stack size: cannot modify limit: Operation not permitted
=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 3.796888
Tessellating body 1 with MaxEdge = 0.094922 Sag = 0.003797 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9 > autoInputs.out
Executing: ./aero.csh > aero.out
C_A 0.023693377
C_Y -0.0012129282
C_N 0.065395002
C_D 0.025961197
C_S -0.0012129282
C_L 0.064528278
C_l 0.0510971
C_m 0.000248187
C_n -0.017525
C_M_x 0.0504544
C_M_y 0.000248187
C_M_z -0.0192976
real 0m9.446s
user 0m16.196s
sys 0m0.428s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
real 0m0.593s
user 0m0.635s
sys 0m0.118s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
real 0m0.708s
user 0m0.804s
sys 0m0.208s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
+ python -u masstran_PyTest.py -outLevel=0
Getting results mass properties.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Area 3.428666259749
Mass 5383.006027806
Centroid [1.222256036872, 0.1634981473779, -4.647736192456e-11]
CG [1.222256036872, 0.1634981473779, -4.647907951721e-11]
Ixx 22133.97306031
Iyy 23448.30046704
Izz 1389.213122564
Ixy 164.2055275655
Ixz -7.485782319314e-06
Iyz 1.710545499156e-06
I [22133.97306031, 23448.30046704, 1389.213122564, 164.2055275655, -7.485782319314e-06, 1.710545499156e-06]
II [[22133.97306031, -164.2055275655, 7.485782319314e-06], [-164.2055275655, 23448.30046704, -1.710545499156e-06], [7.485782319314e-06, -1.710545499156e-06, 1389.213122564]]
real 0m4.117s
user 0m5.696s
sys 0m10.664s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
real 0m0.483s
user 0m0.655s
sys 0m0.062s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
+ echo '../corsairlite/qp.py test;'
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt
Objective
---------
-21.56250 dimensionless
Variables
---------
x : 1.62500 [-] The X variable
y : 1.37500 [-] The Y variable
Constants
---------
c : 3 [-] A constant
c2 : 2 [-] A constant
Sensitivities
-------------
c : + 0.46957 A constant
c2 : - 0.22338 A constant
Solve Report
------------
Solve Method : Quadratic Program
Classification : Convex
Solver : cvxopt
real 0m5.840s
user 0m1.445s
sys 0m0.135s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
Mystran
=================================================
All tests pass!
=================================================
=================================================
(cd legacy/examples/regressionTest; ./execute_PyTestRegression.sh MINIMAL)
=================================================
Legacy Using python : /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/ESP/venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ rm -rf avl_PyTest
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ echo 'avl_PyTest.py test;'
avl_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u avl_PyTest.py -verbosity=0 -workDir=runDirectory
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Running AVL
CXtot 0.0006119078685800925
CYtot -6.292592518559147e-15
CZtot -0.3012861394881712
Cltot -4.783069014642483e-14
Cmtot -0.1945055953448147
Cntot -2.338890054396671e-15
Cl'tot -4.786422456048383e-14
Cn'tot -1.50377318550154e-15
CLtot 0.3012509314146395
CDtot 0.00464635348821979
CDvis 0.0
CLff 0.3009503023516151
CYff -7.7198870803959e-15
CDind 0.00464635348821979
CDff 0.004968969500894849
e 0.9669902146155998
StripForces
Wing cl = [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407]
Wing cd = [-0.004234137763148, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946456, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372442, -0.004494543653152, -0.00423413776453]
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.488s
user 0m0.555s
sys 0m0.221s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf xfoil_PyTest
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Running xFoil......
Cl = [1.05475230551148, 1.36488869373725, 1.56607214272246, 2.03059709357768, 1.9727108312095, 1.87307153172323, 1.76050475760053]
Cd = [0.0131991208831308, 0.0166540240605859, 0.0200551482562657, 0.0458671341873005, 0.0754256009397268, 0.0994469174479059, 0.127479430989221]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.49604411072842, 0.461377732041756, 0.442376568202227, 0.361251636144409, 0.276104140854608, 0.214381239321802, 0.132988264746433]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m3.567s
user 0m2.868s
sys 0m0.124s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf awave_PyTest
+ echo 'awave_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
awave_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u awave_PyTest.py -verbosity=0 -workDir=runDirectory
Writing Awave input file
Body Section, Body ID 1
XCG: 1.571025 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 2
XCG: 2.539271 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 3
XCG: 1.571025 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Body Section, Body ID 4
XCG: 2.539271 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Lifting Surface Section, Body ID 5
XLE: 1.571946 -3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 0
Lifting Surface Section, Body ID 6
XLE: 0.000000 0.000000 0.000000
CHORD: 1.614013
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 7
XLE: 1.571946 3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 8
XLE: 5.484123 0.000000 1.468246
CHORD: 0.726185
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 9
XLE: 5.000000 0.000000 0.500000
CHORD: 1.210308
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 10
XLE: 5.484123 -0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 0
Lifting Surface Section, Body ID 11
XLE: 5.484123 0.000000 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Lifting Surface Section, Body ID 12
XLE: 5.484123 0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Body Section, Body ID 13
XCG: -2.000000 0.000000 0.000000
AREA: 0.000000
RAD: 0.000000
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 14
XCG: 0.000000 -0.000000 -0.000000
AREA: 0.818123
RAD: 0.510310
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Warning: capsGroup not found on body 15!
Body Section, Body ID 15
XCG: 1.613743 -0.000000 -0.000000
AREA: 0.327249
RAD: 0.322749
ATTRIB:Fuse
NAME :(null)
Awave TYPE: 2
Body Section, Body ID 16
XCG: 5.000000 -0.000000 0.500000
AREA: 0.081812
RAD: 0.161374
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 17
XCG: 6.210307 -0.000000 0.500000
AREA: 0.000818
RAD: 0.016137
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
AwaveTypes: 2 5 4 2 2
Points for all four fuselage sections :: 5 0 0 0
Number of Mach-Alpha cases = 2
Running AWAVE
Running Post Analysis
CdWave = [1.13333237, 0.216380283]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.623s
user 0m0.627s
sys 0m0.122s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf aflr2_PyTest
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Darwin 22.6.0 arm64
AFLR2 : Compile Date 08/01/23 @ 11:39PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 316 634
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 681 1018
AFLR2 GGp: Nodes, Faces = 1013 1682
AFLR2 GGp: Nodes, Faces = 1339 2334
AFLR2 GGp: Nodes, Faces = 1652 2960
AFLR2 GGp: Nodes, Faces = 1957 3570
AFLR2 GGp: Nodes, Faces = 2252 4160
AFLR2 GGp: Nodes, Faces = 2526 4708
AFLR2 GGp: Nodes, Faces = 2809 5274
AFLR2 GGp: Nodes, Faces = 3083 5822
AFLR2 GGp: Nodes, Faces = 3327 6310
AFLR2 GGp: Nodes, Faces = 3564 6784
AFLR2 GGp: Nodes, Faces = 3788 7232
AFLR2 GGp: Nodes, Faces = 3995 7646
AFLR2 GGp: Nodes, Faces = 4194 8044
AFLR2 GGp: Nodes, Faces = 4394 8444
AFLR2 GGp: Nodes, Faces = 4585 8826
AFLR2 GGp: Nodes, Faces = 4772 9200
AFLR2 GGp: Nodes, Faces = 4943 9542
AFLR2 GGp: Nodes, Faces = 5129 9914
AFLR2 GGp: Nodes, Faces = 5293 10242
AFLR2 GGp: Nodes, Faces = 5447 10550
AFLR2 GGp: Nodes, Faces = 5594 10844
AFLR2 GGp: Nodes, Faces = 5716 11088
AFLR2 GGp: Nodes, Faces = 5830 11316
AFLR2 GGp: Nodes, Faces = 5909 11474
AFLR2 GGp: Nodes, Faces = 5964 11584
AFLR2 GGp: Nodes, Faces = 6006 11668
AFLR2 GGp: Nodes, Faces = 6025 11706
AFLR2 GGp: Nodes, Faces = 6034 11724
AFLR2 : CPU Time = 0.010 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 6034 11724
AFLR2 QI : Nodes, Faces = 6033 454
AFLR2 QI : Nodes, Faces = 6033 5634
AFLR2 QI : Nodes, Faces = 6033 11722
AFLR2 QI : Nodes, Faces = 6032 462
AFLR2 QI : Nodes, Faces = 6032 5629
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 456
AFLR2 QI : Nodes, Faces = 6032 5632
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 474
AFLR2 QI : Nodes, Faces = 6032 5623
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6031 486
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 QI : Nodes, Faces = 6031 488
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 : CPU Time = 0.005 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.748s
user 0m0.709s
sys 0m0.368s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf delaundo_PyTest
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Getting mesh sizing parameters
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Running Delaundo......
Reading delaundo mesh file - delaundoMesh.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.672s
user 0m0.684s
sys 0m0.377s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_ThreeBar_PyTest
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.621s
user 0m0.691s
sys 0m0.186s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf astros_Flutter_15degree
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.937s
user 0m0.895s
sys 0m0.286s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ rm -rf masstran_PyTest
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting results mass properties.....
Area 3.428666259749
Mass 5383.006027806
Centroid [1.222256036872, 0.1634981473779, -4.647736192456e-11]
CG [1.222256036872, 0.1634981473779, -4.647907951721e-11]
Ixx 22133.97306031
Iyy 23448.30046704
Izz 1389.213122564
Ixy 164.2055275655
Ixz -7.485782319314e-06
Iyz 1.710545499156e-06
I [22133.97306031, 23448.30046704, 1389.213122564, 164.2055275655, -7.485782319314e-06, 1.710545499156e-06]
II [[22133.97306031, -164.2055275655, 7.485782319314e-06], [-164.2055275655, 23448.30046704, -1.710545499156e-06], [7.485782319314e-06, -1.710545499156e-06, 1389.213122564]]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m4.903s
user 0m6.386s
sys 0m9.868s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ rm -rf hsm_SingleLoadCase_PyTest
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
real 0m0.398s
user 0m0.626s
sys 0m0.061s
+ status=0
+ set +x
=================================================
Legacy CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
*************************************************
*************************************************
All tests pass!
=================================================
=================================================
[Execution node] check if [viggen] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[MSBuild] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64')
[MSBuild] -> found 0 issues (skipped 0 duplicates)
[MSBuild] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64')
[MSBuild] -> found 0 issues (skipped 0 duplicates)
[MSBuild] Successfully parsed console log
[MSBuild] -> found 0 issues (skipped 0 duplicates)
[MSBuild] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64')
[MSBuild] Skipping post processing
[MSBuild] No filter has been set, publishing all 0 issues
[MSBuild] 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] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Commit/7.7/DARWIN_ARM64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] 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_Commit/7.7/DARWIN_ARM64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Commit/CASREV=7.7,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #7558'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS
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