Skipping 2,852 KB..
Full Log Body 26 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1303] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1304] udprim: editAttr filename tmp_OpenCSM_00/03 (compiled code)
processing: FACE ADJ2EDGE tagType=leadingEdge
processing: SET capsIgnore=true
processing:
processing: FACE HAS tagType=trailingEdge
processing: SET capsIgnore=true
processing:
processing: FACE ADJ2FACE tagType=trailingEdge
processing: ANDNOT HAS tagType=rib
processing: ANDNOT HAS tagType=tip
processing: SET capsIgnore=true
processing:
processing: FACE ADJ2EDGE tagType=trailingEdge
processing: SET capsIgnore=true
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 27 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1305] udprim: editAttr filename tmp_OpenCSM_00/04 (compiled code)
processing: FACE HAS tagComp=leftWing
processing: ANDNOT ADJ2EDGE tagType=leadingEdge
processing: ANDNOT ADJ2EDGE tagType=trailingEdge
processing: ANDNOT ADJ2FACE tagType=trailingEdge
processing: SET capsGroup=leftWingSkin
processing:
processing: FACE HAS tagComp=riteWing
processing: ANDNOT ADJ2EDGE tagType=leadingEdge
processing: ANDNOT ADJ2EDGE tagType=trailingEdge
processing: ANDNOT ADJ2FACE tagType=trailingEdge
processing: SET capsGroup=riteWingSkin
processing:
processing: FACE HAS tagType=rib
processing: SET capsGroup=wingRib
processing:
processing: FACE HAS tagType=tip
processing: SET capsGroup=wingRib
processing:
processing: FACE HAS tagType=spar tagIndex=1
processing: SET capsGroup=wingSpar1
processing: SET capsMesh=wingSpar1
processing:
processing: FACE HAS tagType=spar tagIndex=2
processing: SET capsGroup=wingSpar2
processing: SET capsMesh=wingSpar2
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 28 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1309] udprim: editAttr filename tmp_OpenCSM_00/06 (compiled code)
processing: FACE HAS tagType=upper
processing: SET capsBound=upperWing
processing:
processing: FACE HAS tagType=lower
processing: SET capsBound=lowerWing
processing:
processing: FACE HAS tagType=tip tagIndex=1
processing: SET capsBound=leftTip
processing:
processing: FACE HAS tagType=tip tagIndex=2
processing: SET capsBound=riteTip
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 29 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1310] udprim: editAttr filename tmp_OpenCSM_00/07 (compiled code)
processing: NODE ADJ2FACE tagComp=leftWing tagType=tip
processing: AND ADJ2FACE tagType=lower
processing: AND ADJ2FACE tagType=spar tagIndex=1
processing: SET capsLoad=leftPointLoad
processing:
processing: NODE ADJ2FACE tagComp=riteWing tagType=tip
processing: AND ADJ2FACE tagType=lower
processing: AND ADJ2FACE tagType=spar tagIndex=1
processing: SET capsLoad=ritePointLoad
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 30 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1311] select: edge tagType leadingEdge * * * *
executing [1312] dimension: leadingEdges 1.00000 8.00000
executing [1313] set: leadingEdges @sellist
leadingEdges[1,1] = 8.00000 0.00000
leadingEdges[1,2] = 31.00000 0.00000
leadingEdges[1,3] = 33.00000 0.00000
leadingEdges[1,4] = 62.00000 0.00000
leadingEdges[1,5] = 64.00000 0.00000
leadingEdges[1,6] = 94.00000 0.00000
leadingEdges[1,7] = 96.00000 0.00000
leadingEdges[1,8] = 121.00000 0.00000
executing [1314] patbeg: i 8.00000
pattern counter: i = 1
executing [1315] select: edge 8
putting Branch Attributes on Edge 8
executing [1316] patend:
pattern counter: i = 2
executing [1315] select: edge 31
putting Branch Attributes on Edge 31
executing [1316] patend:
pattern counter: i = 3
executing [1315] select: edge 33
putting Branch Attributes on Edge 33
executing [1316] patend:
pattern counter: i = 4
executing [1315] select: edge 62
putting Branch Attributes on Edge 62
executing [1316] patend:
pattern counter: i = 5
executing [1315] select: edge 64
putting Branch Attributes on Edge 64
executing [1316] patend:
pattern counter: i = 6
executing [1315] select: edge 94
putting Branch Attributes on Edge 94
executing [1316] patend:
pattern counter: i = 7
executing [1315] select: edge 96
putting Branch Attributes on Edge 96
executing [1316] patend:
pattern counter: i = 8
executing [1315] select: edge 121
putting Branch Attributes on Edge 121
executing [1316] patend:
executing [1317] udprim: editAttr filename tmp_OpenCSM_00/08 (compiled code)
processing: FACE ADJ2EDGE tagComp=leftWing
processing: SET tagTemp=leadingEdgeFace
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 31 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1318] udprim: editAttr filename tmp_OpenCSM_00/09 (compiled code)
processing: EDGE ADJ2FACE tagTemp=leadingEdgeFace
processing: AND ADJ2FACE tagComp=rootWing
processing: SET capsMesh=rootLeadingEdge
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 32 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1319] ifthen: 0.00000 EQ 1.00000 and ...
executing [1322] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1323] udprim: editAttr filename tmp_OpenCSM_00/11 (compiled code)
processing: FACE HAS tagComp=rootWing
processing: SET capsConnectLink=ribRoot
processing:
processing: EDGE ADJ2FACE tagComp=rootWing
processing: SET capsConnectLink=ribRoot
processing:
processing: NODE ADJ2FACE tagComp=rootWing
processing: SET capsConnectLink=ribRoot
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 33 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1325] udprim: editAttr filename tmp_OpenCSM_00/12 (compiled code)
processing: FACE HAS tagComp=leftWing tagType=upper
processing: AND ADJ2EDGE tagType=leadingEdge
processing: AND ADJ2FACE tagComp=riteWing
processing: SET tagCsys=leftWing
processing:
processing: FACE HAS tagComp=riteWing tagType=upper
processing: AND ADJ2EDGE tagType=leadingEdge
processing: AND ADJ2FACE tagComp=leftWing
processing: SET tagCsys=riteWing
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 34 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1326] select: face tagCsys leftWing * * * *
executing [1327] set: leftWingSkinCsys @sellist
leftWingSkinCsys = 27.00000 0.00000
executing [1328] select: face tagCsys riteWing * * * *
executing [1329] set: riteWingSkinCsys @sellist
riteWingSkinCsys = 8.00000 0.00000
executing [1330] store: WingStruct 0.00000 0.00000
Body 34 stored
executing [1331] restore: WingStruct 0.00000
Body 35 restored (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1332] store: WingStruct 0.00000 0.00000
WARNING:: storage WingStruct (0) is being overwritten
Body 35 stored
executing [1334] restore: WingStruct 0.00000
Body 36 restored (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1335] select: body
putting Branch Attributes on Body
executing [1336] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1337] point: 0.40344 0.00000 0.00000
Body 37 created
executing [1339] end:
executing [1341] ifthen: 0.00000 NE 0.00000 and ...
executing [1378] end:
finalizing:
==> Profile information
Branch type ncall time (sec) pct
dimension 1 0.005 0.0
point 1 0.027 0.2
udprim 14 1.461 11.0
restore 8 0.132 1.0
rule 1 0.159 1.2
intersect 1 1.072 8.1
subtract 1 2.780 20.9
union 1 5.719 43.0
join 1 0.217 1.6
extract 1 1.253 9.4
translate 2 0.029 0.2
rotatex 2 0.006 0.0
rotatey 1 0.003 0.0
scale 2 0.008 0.1
mirror 1 0.058 0.4
interface 3 0.002 0.0
end 3 0.020 0.2
set 60 0.087 0.7
udparg 3 0.003 0.0
select 23 0.153 1.1
store 6 0.010 0.1
patbeg 1 0.003 0.0
patend 8 0.040 0.3
ifthen 43 0.066 0.5
else 2 0.000 0.0
endif 43 0.000 0.0
catbeg 1 0.001 0.0
catend 1 0.000 0.0
mark 1 0.000 0.0
Total 236 13.314
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar1, index = 1
Name = riteWingSkin, index = 2
Name = wingRib, index = 3
Name = leftWingSkin, index = 4
Name = wingSpar2, index = 5
Name = ribSupport, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 2)
Tessellating body
capsIgnore attribute found for face - 3!!
capsIgnore attribute found for face - 8!!
capsIgnore attribute found for face - 15!!
capsIgnore attribute found for face - 16!!
capsIgnore attribute found for face - 17!!
capsIgnore attribute found for face - 18!!
capsIgnore attribute found for face - 26!!
capsIgnore attribute found for face - 27!!
capsIgnore attribute found for face - 33!!
capsIgnore attribute found for face - 36!!
capsIgnore attribute found for face - 37!!
capsIgnore attribute found for face - 38!!
capsIgnore attribute found for face - 39!!
capsIgnore attribute found for face - 40!!
capsIgnore attribute found for face - 41!!
capsIgnore attribute found for face - 42!!
capsIgnore attribute found for face - 50!!
capsIgnore attribute found for face - 51!!
capsIgnore attribute found for face - 52!!
capsIgnore attribute found for face - 58!!
capsIgnore attribute found for face - 61!!
capsIgnore attribute found for face - 62!!
capsIgnore attribute found for face - 63!!
capsIgnore attribute found for face - 64!!
capsIgnore attribute found for face - 65!!
capsIgnore attribute found for face - 66!!
capsIgnore attribute found for face - 73!!
capsIgnore attribute found for face - 74!!
capsIgnore attribute found for face - 75!!
capsIgnore attribute found for face - 81!!
capsIgnore attribute found for face - 83!!
capsIgnore attribute found for face - 84!!
capsIgnore attribute found for face - 85!!
capsIgnore attribute found for face - 86!!
capsIgnore attribute found for face - 89!!
capsIgnore attribute found for face - 90!!
capsIgnore attribute found for face - 91!!
capsIgnore attribute found for face - 96!!
capsIgnore attribute found for face - 97!!
capsIgnore attribute found for face - 98!!
Number of nodes = 299
Number of elements = 387
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 387
Getting surface mesh for body 2 (of 2)
Tessellating body
Number of nodes = 1
Number of elements = 1
Number of node elements = 1
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 300
Total number of elements = 388
Analysis directory does not currently exist - it will be made automatically
CAPS Info: No symbol for aimExecute in astrosAIM
CAPS Info: No symbol for aimCheck in astrosAIM
CAPS Info: No symbol for aimData in astrosAIM
CAPS Info: No symbol for aimSensitivity in astrosAIM
==> Running ASTROS pre-analysis...
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 = 1
Name = ribRootPoint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = lowerWing, index = 1
Name = upperWing, index = 2
Name = riteTip, index = 3
Name = leftTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = ribRoot, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Found link for attrMap (Attribute_Map) from parent
Found link for a Surface mesh from parent
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 64 (out of 299) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
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 = 236
Combined Number of elements = 228
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 227
Getting FEA materials.......
Number of materials - 2
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 6
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Property name - ribSupport
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - ribRoot
No "groupName" specified for Connection tuple ribRoot!
Looking for automatic connections from the use of capsConnectLink for ribRoot
19 automatic connections were made for capsConnect ribRoot (node id 300)
Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing support cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running Astros...
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_DENORMAL
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
--> Eigen-frequencies:
1 : 0.0357647
2 : 0.0533161
3 : 0.102451
4 : 0.102496
5 : 0.159637
6 : 0.211734
7 : 0.215446
8 : 0.223928
9 : 0.350115
10: 0.432754
--> temporary directory "tmp_OpenCSM_00" removed
Cleaning up egadsInstance - 0
Cleaning up astrosInstance - 0
EGADS Info: 861 Objects, 1379 Reference in Use (of 34601) at Close!
real 0m24.147s
user 0m0.155s
sys 0m0.405s
+ status=0
+ set +x
=================================================
data/session10/astros_2_ModalSupport.py passed (as expected)
=================================================
=================================================
astros_3_StaticClamped.py test;
+ python astros_3_StaticClamped.py
+ tee -a /c/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/training/WIN64.2017/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
CAPS Info: No symbol for aimDiscr in egadsTessAIM
CAPS Info: No symbol for aimFreeDiscr in egadsTessAIM
CAPS Info: No symbol for aimLocateElement in egadsTessAIM
CAPS Info: No symbol for aimUsesDataSet in egadsTessAIM
CAPS Info: No symbol for aimCheck in egadsTessAIM
CAPS Info: No symbol for aimTransfer in egadsTessAIM
CAPS Info: No symbol for aimInterpolation in egadsTessAIM
CAPS Info: No symbol for aimInterpolateBar in egadsTessAIM
CAPS Info: No symbol for aimIntegration in egadsTessAIM
CAPS Info: No symbol for aimIntegrateBar in egadsTessAIM
CAPS Info: No symbol for aimSensitivity in egadsTessAIM
==> Generating Mesh...
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] udprim: $/capsHeader (scripted code)
[ 2] interface: . ALL 0.00000
executing [ 3] set: makeFuseOml 0
makeFuseOml = 0.00000 0.00000
executing [ 4] set: makeFuseWaffle 0
makeFuseWaffle = 0.00000 0.00000
executing [ 5] set: makeFuseCmass 0
makeFuseCmass = 0.00000 0.00000
executing [ 6] set: makeWingOml 0
makeWingOml = 0.00000 0.00000
executing [ 7] set: makeWingHinge 0
makeWingHinge = 0.00000 0.00000
executing [ 8] set: makeWingWaffle 0
makeWingWaffle = 0.00000 0.00000
executing [ 9] set: makeWingCmass 0
makeWingCmass = 0.00000 0.00000
executing [ 10] set: makeHtailOml 0
makeHtailOml = 0.00000 0.00000
executing [ 11] set: makeHtailHinge 0
makeHtailHinge = 0.00000 0.00000
executing [ 12] set: makeHtailWaffle 0
makeHtailWaffle = 0.00000 0.00000
executing [ 13] set: makeHtailCmass 0
makeHtailCmass = 0.00000 0.00000
executing [ 14] set: makeVtailOml 0
makeVtailOml = 0.00000 0.00000
executing [ 15] set: makeVtailHinge 0
makeVtailHinge = 0.00000 0.00000
executing [ 16] set: makeVtailWaffle 0
makeVtailWaffle = 0.00000 0.00000
executing [ 17] set: makeVtailCmass 0
makeVtailCmass = 0.00000 0.00000
executing [ 18] set: makePylonOml 0
makePylonOml = 0.00000 0.00000
executing [ 19] set: makePodOml 0
makePodOml = 0.00000 0.00000
executing [ 20] set: SHARP_TE 0
SHARP_TE = 0.00000 0.00000
executing [ 21] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 24] ifthen: 0.00000 NE 0.00000 and ...
executing [ 40] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 43] ifthen: 0.00000 NE 0.00000 and ...
executing [ 51] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 54] ifthen: 0.00000 NE 0.00000 and ...
executing [ 65] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 68] ifthen: 0.00000 NE 0.00000 and ...
executing [ 79] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 82] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 85] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 88] ifthen: 1.00000 NE 0.00000 OR ...
executing [ 89] set: makeWingOml 1
makeWingOml = 1.00000 0.00000
executing [ 90] set: makeWingWaffle 1
makeWingWaffle = 1.00000 0.00000
executing [ 92] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 95] ifthen: 0.00000 NE 0.00000 and ...
executing [ 101] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 102] set: COMP:Fuse 0
COMP:Fuse = 0.00000 0.00000
executing [ 104] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 107] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 108] set: COMP:Htail 0
COMP:Htail = 0.00000 0.00000
executing [ 110] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 111] set: COMP:Vtail 0
COMP:Vtail = 0.00000 0.00000
executing [ 113] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 114] set: COMP:Pylon 0
COMP:Pylon = 0.00000 0.00000
executing [ 116] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 117] set: COMP:Pod 0
COMP:Pod = 0.00000 0.00000
executing [ 119] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 120] set: COMP:Control 0
COMP:Control = 0.00000 0.00000
executing [ 122] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 123] set: makeFuseOml 0
makeFuseOml = 0.00000 0.00000
executing [ 124] set: makeFuseWaffle 0
makeFuseWaffle = 0.00000 0.00000
executing [ 125] set: makeFuseCmass 0
makeFuseCmass = 0.00000 0.00000
executing [ 127] ifthen: 1.00000 EQ 0.00000 and ...
executing [ 133] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 134] set: makeHtailOml 0
makeHtailOml = 0.00000 0.00000
executing [ 135] set: makeHtailHinge 0
makeHtailHinge = 0.00000 0.00000
executing [ 136] set: makeHtailWaffle 0
makeHtailWaffle = 0.00000 0.00000
executing [ 137] set: makeHtailCmass 0
makeHtailCmass = 0.00000 0.00000
executing [ 139] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 140] set: makeVtailOml 0
makeVtailOml = 0.00000 0.00000
executing [ 141] set: makeVtailHinge 0
makeVtailHinge = 0.00000 0.00000
executing [ 142] set: makeVtailWaffle 0
makeVtailWaffle = 0.00000 0.00000
executing [ 143] set: makeVtailCmass 0
makeVtailCmass = 0.00000 0.00000
executing [ 145] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 146] set: makePylonOml 0
makePylonOml = 0.00000 0.00000
executing [ 148] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 149] set: makePodOml 0
makePodOml = 0.00000 0.00000
executing [ 151] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 152] set: makeWingHinge 0
makeWingHinge = 0.00000 0.00000
executing [ 153] set: makeHtailHinge 0
makeHtailHinge = 0.00000 0.00000
executing [ 154] set: makeVtailHinge 0
makeVtailHinge = 0.00000 0.00000
executing [ 156] end:
executing [ 157] set: wing:span sqrt(wing:aspect*wing:area)
wing:span = 7.74597 0.00000
executing [ 158] set: wing:chordr 2*wing:area/wing:span/(1+wing:taper)
wing:chordr = 1.61374 0.00000
executing [ 159] set: wing:chordt wing:chordr*wing:taper
wing:chordt = 0.96825 0.00000
executing [ 160] set: wing:ytip -wing:span/2
wing:ytip = -3.87298 0.00000
executing [ 161] set: wing:xtip -wing:ytip*tand(wing:sweep)
wing:xtip = 1.40965 0.00000
executing [ 162] set: wing:ztip -wing:ytip*tand(wing:dihedral)
wing:ztip = 0.27083 0.00000
executing [ 163] set: wing:mac sqrt(wing:area/wing:aspect)
wing:mac = 1.29099 0.00000
executing [ 164] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 165] mark:
Mark created
executing [ 166] udprim: naca thickness 0.12000 camber 0.06000 sharpte 0.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 167] scale: 1.61374 0.00000 0.00000 0.00000
Body 2 created (toler= 1.6137e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 168] rotatex: 90.00000 0.00000 0.00000
Body 3 created (toler= 1.6137e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 169] udprim: naca thickness 0.16000 camber 0.02000 sharpte 0.00000 (compiled code)
Body 4 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 170] scale: 0.96825 0.00000 0.00000 0.00000
Body 5 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 171] rotatex: 90.00000 0.00000 0.00000
Body 6 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 172] rotatey: -5.00000 0.00000 0.00000
Body 7 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 173] translate: 1.40965 -3.87298 0.27083
Body 8 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 174] rule: 0.00000 0.00000
ruling 2 Xsects with 3 Strips each...
Body 9 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 175] set: ruledBody @nbody
ruledBody = 9.00000 0.00000
executing [ 176] select: face 9 1
putting Branch Attributes on Face 4
executing [ 177] select: face 9 2
putting Branch Attributes on Face 5
executing [ 178] select: face 9 3
putting Branch Attributes on Face 1
executing [ 179] select: face 9 4
putting Branch Attributes on Face 2
executing [ 180] select: edge 9 3 9 4 1
putting Branch Attributes on Edge 3
executing [ 181] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 182] select: face 9 5
putting Branch Attributes on Face 3
executing [ 186] store: LeftWing 0.00000 1.00000
Body 9 stored
executing [ 187] restore: LeftWing 0.00000
Body 10 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 188] select: face tagType tip * * * *
putting Branch Attributes on Face 5
executing [ 189] select: edge tagType leadingEdge * * * *
executing [ 190] ifthen: 3.00000 GT 0.00000 and 0.00000 eq 0.00000
executing [ 191] select: edge tagType leadingEdge * * * *
putting Branch Attributes on Edge 3
executing [ 193] select: edge tagType trailingEdge * * * *
ERROR:: (edge_not_found) in Branch Brch_000193 at [[..\ESP\wing3.csm:103]]
SELECT specified nonexistant Edge
executing [ 197] catbeg: $edge_not_found
--> catching signal -223 (edge_not_found)
executing [ 199] mirror: 0.00000 1.00000 0.00000 0.00000
Body 11 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 200] join: 0.00000 0.00000
Body 12 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 201] select: edge 9 3 9 3 1
putting Branch Attributes on Edge 2
executing [ 202] select: edge 9 4 9 4 1
putting Branch Attributes on Edge 5
executing [ 203] store: WingOml 0.00000 0.00000
Body 12 stored
executing [ 205] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 206] restore: WingOml 0.00000
Body 13 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 207] set: xmin @xmin-0.1
xmin = -0.10102 0.00000
executing [ 208] set: xmax @xmax+0.1
xmax = 2.47425 0.00000
executing [ 209] set: ymin 0
ymin = 0.00000 0.00000
executing [ 210] set: ymax @ymax+0.1
ymax = 3.97298 0.00000
executing [ 211] set: zmin @zmin-0.1
zmin = -0.13316 0.00000
executing [ 212] set: zmax @zmax+0.1
zmax = 0.49998 0.00000
executing [ 213] store: . 0.00000 0.00000
Body 13 removed from stack
executing [ 214] udparg: waffle depth 3.00000
Body 14 created (NULL Body)
executing [ 215] udparg: waffle depth 0.20000
Body 15 created (NULL Body)
executing [ 216] udparg: waffle depth 0.70000
Body 16 created (NULL Body)
executing [ 217] udprim: waffle depth 0.63315 filename tmp_OpenCSM_00/00 (compiled code)
processing:
processing: # construction lines for spars
processing: CPOINT A AT 0+wing:spar1*wing:chordr 0
processing: CPOINT B AT wing:xtip+wing:spar1*wing:chordt -wing:ytip
processing: CPOINT C AT 0+wing:spar2*wing:chordr 0
processing: CPOINT D AT wing:xtip+wing:spar2*wing:chordt -wing:ytip
processing:
processing: CLINE AB A B
processing: CLINE CD C D
processing:
processing: # rite spars
processing: POINT E ON AB YLOC ymin
processing: POINT F ON AB YLOC ymax
processing: LINE EF E F tagComp=riteWing tagType=spar tagIndex=1
processing:
processing: POINT G ON CD YLOC ymin
processing: POINT H ON CD YLOC ymax
processing: LINE GH G H tagComp=riteWing tagType=spar tagIndex=2
processing:
processing: # rite ribs
processing: PATBEG irib wing:nrib
processing: CPOINT I AT xmin -wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=riteWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin -wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=riteWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin -wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=riteWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing:
processing: # root rib
processing: CPOINT I AT xmin 0
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=rootWing tagType=rib tagIndex=0
processing:
processing: # left spars
processing: POINT E AT x@E -y@E
processing: POINT F AT x@F -y@F
processing: LINE FE F E tagComp=leftWing tagType=spar tagIndex=1
processing:
processing: POINT G AT x@G -y@G
processing: POINT H AT x@H -y@H
processing: LINE HG H G tagComp=leftWing tagType=spar tagIndex=2
processing:
processing: # left ribs
processing: PATBEG irib wing:nrib
processing: CPOINT I AT xmin wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=leftWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=leftWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=leftWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
Body 17 created (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [ 218] translate: 0.00000 0.00000 -0.13316
Body 18 created (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [ 219] store: WingWaffle 0.00000 0.00000
Body 18 stored
executing [ 221] udprim: $/capsViews (scripted code)
[ 222] interface: . ALL 0.00000
executing [ 223] ifthen: 0.00000 NE 0.00000 and ...
executing [ 268] ifthen: 0.00000 NE 0.00000 and ...
executing [ 409] ifthen: 0.00000 NE 0.00000 and ...
executing [ 852] ifthen: 0.00000 NE 0.00000 and ...
executing [1290] ifthen: 1.00000 NE 0.00000 OR ...
executing [1291] udprim: $/viewStructure (scripted code)
[1292] interface: . ALL 0.00000
executing [1293] set: structAIMs $nastranAIM;astrosAIM;mystranAIM;egadsTessAIM
structAIMs = $nastranAIM;astrosAIM;mystranAIM;egadsTessAIM
executing [1294] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1295] restore: WingOml 0.00000
Body 19 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [1296] restore: WingWaffle 0.00000
Body 20 restored (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [1297] intersect: none 1.00000 0.0000e+00
Body 21 created (toler= 5.0000e-06, nnode= 57, nedge= 99, nface= 37)
executing [1298] restore: WingOml 0.00000
Body 22 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [1299] restore: WingWaffle 0.00000
Body 23 restored (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [1300] subtract: none 1.00000 0.0000e+00
Body 24 created (toler= 6.7429e-07, nnode= 63, nedge= 123, nface= 62)
executing [1301] extract: 0
Body 25 created (toler= 6.7429e-07, nnode= 63, nedge= 123, nface= 62)
executing [1302] union: 0.00000 0 0.0000e+00
Body 26 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1303] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1304] udprim: editAttr filename tmp_OpenCSM_00/03 (compiled code)
processing: FACE ADJ2EDGE tagType=leadingEdge
processing: SET capsIgnore=true
processing:
processing: FACE HAS tagType=trailingEdge
processing: SET capsIgnore=true
processing:
processing: FACE ADJ2FACE tagType=trailingEdge
processing: ANDNOT HAS tagType=rib
processing: ANDNOT HAS tagType=tip
processing: SET capsIgnore=true
processing:
processing: FACE ADJ2EDGE tagType=trailingEdge
processing: SET capsIgnore=true
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 27 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1305] udprim: editAttr filename tmp_OpenCSM_00/04 (compiled code)
processing: FACE HAS tagComp=leftWing
processing: ANDNOT ADJ2EDGE tagType=leadingEdge
processing: ANDNOT ADJ2EDGE tagType=trailingEdge
processing: ANDNOT ADJ2FACE tagType=trailingEdge
processing: SET capsGroup=leftWingSkin
processing:
processing: FACE HAS tagComp=riteWing
processing: ANDNOT ADJ2EDGE tagType=leadingEdge
processing: ANDNOT ADJ2EDGE tagType=trailingEdge
processing: ANDNOT ADJ2FACE tagType=trailingEdge
processing: SET capsGroup=riteWingSkin
processing:
processing: FACE HAS tagType=rib
processing: SET capsGroup=wingRib
processing:
processing: FACE HAS tagType=tip
processing: SET capsGroup=wingRib
processing:
processing: FACE HAS tagType=spar tagIndex=1
processing: SET capsGroup=wingSpar1
processing: SET capsMesh=wingSpar1
processing:
processing: FACE HAS tagType=spar tagIndex=2
processing: SET capsGroup=wingSpar2
processing: SET capsMesh=wingSpar2
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 28 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1309] udprim: editAttr filename tmp_OpenCSM_00/06 (compiled code)
processing: FACE HAS tagType=upper
processing: SET capsBound=upperWing
processing:
processing: FACE HAS tagType=lower
processing: SET capsBound=lowerWing
processing:
processing: FACE HAS tagType=tip tagIndex=1
processing: SET capsBound=leftTip
processing:
processing: FACE HAS tagType=tip tagIndex=2
processing: SET capsBound=riteTip
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 29 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1310] udprim: editAttr filename tmp_OpenCSM_00/07 (compiled code)
processing: NODE ADJ2FACE tagComp=leftWing tagType=tip
processing: AND ADJ2FACE tagType=lower
processing: AND ADJ2FACE tagType=spar tagIndex=1
processing: SET capsLoad=leftPointLoad
processing:
processing: NODE ADJ2FACE tagComp=riteWing tagType=tip
processing: AND ADJ2FACE tagType=lower
processing: AND ADJ2FACE tagType=spar tagIndex=1
processing: SET capsLoad=ritePointLoad
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 30 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1311] select: edge tagType leadingEdge * * * *
executing [1312] dimension: leadingEdges 1.00000 8.00000
executing [1313] set: leadingEdges @sellist
leadingEdges[1,1] = 8.00000 0.00000
leadingEdges[1,2] = 31.00000 0.00000
leadingEdges[1,3] = 33.00000 0.00000
leadingEdges[1,4] = 62.00000 0.00000
leadingEdges[1,5] = 64.00000 0.00000
leadingEdges[1,6] = 94.00000 0.00000
leadingEdges[1,7] = 96.00000 0.00000
leadingEdges[1,8] = 121.00000 0.00000
executing [1314] patbeg: i 8.00000
pattern counter: i = 1
executing [1315] select: edge 8
putting Branch Attributes on Edge 8
executing [1316] patend:
pattern counter: i = 2
executing [1315] select: edge 31
putting Branch Attributes on Edge 31
executing [1316] patend:
pattern counter: i = 3
executing [1315] select: edge 33
putting Branch Attributes on Edge 33
executing [1316] patend:
pattern counter: i = 4
executing [1315] select: edge 62
putting Branch Attributes on Edge 62
executing [1316] patend:
pattern counter: i = 5
executing [1315] select: edge 64
putting Branch Attributes on Edge 64
executing [1316] patend:
pattern counter: i = 6
executing [1315] select: edge 94
putting Branch Attributes on Edge 94
executing [1316] patend:
pattern counter: i = 7
executing [1315] select: edge 96
putting Branch Attributes on Edge 96
executing [1316] patend:
pattern counter: i = 8
executing [1315] select: edge 121
putting Branch Attributes on Edge 121
executing [1316] patend:
executing [1317] udprim: editAttr filename tmp_OpenCSM_00/08 (compiled code)
processing: FACE ADJ2EDGE tagComp=leftWing
processing: SET tagTemp=leadingEdgeFace
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 31 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1318] udprim: editAttr filename tmp_OpenCSM_00/09 (compiled code)
processing: EDGE ADJ2FACE tagTemp=leadingEdgeFace
processing: AND ADJ2FACE tagComp=rootWing
processing: SET capsMesh=rootLeadingEdge
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 32 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1319] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1320] udprim: editAttr filename tmp_OpenCSM_00/10 (compiled code)
processing: FACE HAS tagComp=rootWing
processing: SET capsConstraint=rootConstraint
processing:
processing: EDGE ADJ2FACE tagComp=rootWing
processing: SET capsConstraint=rootConstraint
processing:
processing: NODE ADJ2FACE tagComp=rootWing
processing: SET capsConstraint=rootConstraint
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 33 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1322] ifthen: 0.00000 EQ 1.00000 and ...
executing [1325] udprim: editAttr filename tmp_OpenCSM_00/12 (compiled code)
processing: FACE HAS tagComp=leftWing tagType=upper
processing: AND ADJ2EDGE tagType=leadingEdge
processing: AND ADJ2FACE tagComp=riteWing
processing: SET tagCsys=leftWing
processing:
processing: FACE HAS tagComp=riteWing tagType=upper
processing: AND ADJ2EDGE tagType=leadingEdge
processing: AND ADJ2FACE tagComp=leftWing
processing: SET tagCsys=riteWing
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 34 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1326] select: face tagCsys leftWing * * * *
executing [1327] set: leftWingSkinCsys @sellist
leftWingSkinCsys = 27.00000 0.00000
executing [1328] select: face tagCsys riteWing * * * *
executing [1329] set: riteWingSkinCsys @sellist
riteWingSkinCsys = 8.00000 0.00000
executing [1330] store: WingStruct 0.00000 0.00000
Body 34 stored
executing [1331] restore: WingStruct 0.00000
Body 35 restored (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1332] store: WingStruct 0.00000 0.00000
WARNING:: storage WingStruct (0) is being overwritten
Body 35 stored
executing [1334] restore: WingStruct 0.00000
Body 36 restored (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1335] select: body
putting Branch Attributes on Body
executing [1336] ifthen: 0.00000 EQ 1.00000 and ...
executing [1339] end:
executing [1341] ifthen: 0.00000 NE 0.00000 and ...
executing [1378] end:
finalizing:
==> Profile information
Branch type ncall time (sec) pct
dimension 1 0.000 0.0
udprim 14 1.527 11.2
restore 8 0.155 1.1
rule 1 0.121 0.9
intersect 1 1.059 7.8
subtract 1 2.613 19.2
union 1 6.256 46.0
join 1 0.133 1.0
extract 1 1.304 9.6
translate 2 0.025 0.2
rotatex 2 0.006 0.0
rotatey 1 0.003 0.0
scale 2 0.006 0.0
mirror 1 0.040 0.3
interface 3 0.002 0.0
end 3 0.000 0.0
set 60 0.136 1.0
udparg 3 0.002 0.0
select 23 0.148 1.1
store 6 0.005 0.0
patbeg 1 0.001 0.0
patend 8 0.003 0.0
ifthen 43 0.065 0.5
else 2 0.000 0.0
endif 43 0.000 0.0
catbeg 1 0.000 0.0
catend 1 0.000 0.0
mark 1 0.000 0.0
Total 235 13.610
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar1, index = 1
Name = riteWingSkin, index = 2
Name = wingRib, index = 3
Name = leftWingSkin, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Tessellating body
capsIgnore attribute found for face - 3!!
capsIgnore attribute found for face - 8!!
capsIgnore attribute found for face - 15!!
capsIgnore attribute found for face - 16!!
capsIgnore attribute found for face - 17!!
capsIgnore attribute found for face - 18!!
capsIgnore attribute found for face - 26!!
capsIgnore attribute found for face - 27!!
capsIgnore attribute found for face - 33!!
capsIgnore attribute found for face - 36!!
capsIgnore attribute found for face - 37!!
capsIgnore attribute found for face - 38!!
capsIgnore attribute found for face - 39!!
capsIgnore attribute found for face - 40!!
capsIgnore attribute found for face - 41!!
capsIgnore attribute found for face - 42!!
capsIgnore attribute found for face - 50!!
capsIgnore attribute found for face - 51!!
capsIgnore attribute found for face - 52!!
capsIgnore attribute found for face - 58!!
capsIgnore attribute found for face - 61!!
capsIgnore attribute found for face - 62!!
capsIgnore attribute found for face - 63!!
capsIgnore attribute found for face - 64!!
capsIgnore attribute found for face - 65!!
capsIgnore attribute found for face - 66!!
capsIgnore attribute found for face - 73!!
capsIgnore attribute found for face - 74!!
capsIgnore attribute found for face - 75!!
capsIgnore attribute found for face - 81!!
capsIgnore attribute found for face - 83!!
capsIgnore attribute found for face - 84!!
capsIgnore attribute found for face - 85!!
capsIgnore attribute found for face - 86!!
capsIgnore attribute found for face - 89!!
capsIgnore attribute found for face - 90!!
capsIgnore attribute found for face - 91!!
capsIgnore attribute found for face - 96!!
capsIgnore attribute found for face - 97!!
capsIgnore attribute found for face - 98!!
Number of nodes = 299
Number of elements = 387
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 387
----------------------------
Total number of nodes = 299
Total number of elements = 387
Analysis directory does not currently exist - it will be made automatically
CAPS Info: No symbol for aimExecute in astrosAIM
CAPS Info: No symbol for aimCheck in astrosAIM
CAPS Info: No symbol for aimData in astrosAIM
CAPS Info: No symbol for aimSensitivity in astrosAIM
==> Running ASTROS pre-analysis...
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = lowerWing, index = 1
Name = upperWing, index = 2
Name = riteTip, index = 3
Name = leftTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Found link for attrMap (Attribute_Map) from parent
Found link for a Surface mesh from parent
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 64 (out of 299) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
Getting FEA materials.......
Number of materials - 2
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftPointLoad
No "groupName" specified for Load tuple leftPointLoad, going to use load name
Load name - ritePointLoad
No "groupName" specified for Load tuple ritePointLoad, going to use load name
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running Astros...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
--> Maximum displacements:
--> Tmax 43461.879162311016
--> T1max 738.595
--> T2max 3686.25
--> T3max 43363.8
--> temporary directory "tmp_OpenCSM_00" removed
Cleaning up egadsInstance - 0
Cleaning up astrosInstance - 0
EGADS Info: 861 Objects, 1379 Reference in Use (of 34591) at Close!
real 0m16.784s
user 0m0.061s
sys 0m0.342s
+ status=0
+ set +x
=================================================
data/session10/astros_3_StaticClamped.py passed (as expected)
=================================================
=================================================
astros_4_Composite.py test;
+ python astros_4_Composite.py
+ tee -a /c/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/training/WIN64.2017/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
CAPS Info: No symbol for aimDiscr in egadsTessAIM
CAPS Info: No symbol for aimFreeDiscr in egadsTessAIM
CAPS Info: No symbol for aimLocateElement in egadsTessAIM
CAPS Info: No symbol for aimUsesDataSet in egadsTessAIM
CAPS Info: No symbol for aimCheck in egadsTessAIM
CAPS Info: No symbol for aimTransfer in egadsTessAIM
CAPS Info: No symbol for aimInterpolation in egadsTessAIM
CAPS Info: No symbol for aimInterpolateBar in egadsTessAIM
CAPS Info: No symbol for aimIntegration in egadsTessAIM
CAPS Info: No symbol for aimIntegrateBar in egadsTessAIM
CAPS Info: No symbol for aimSensitivity in egadsTessAIM
==> Generating Mesh...
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] udprim: $/capsHeader (scripted code)
[ 2] interface: . ALL 0.00000
executing [ 3] set: makeFuseOml 0
makeFuseOml = 0.00000 0.00000
executing [ 4] set: makeFuseWaffle 0
makeFuseWaffle = 0.00000 0.00000
executing [ 5] set: makeFuseCmass 0
makeFuseCmass = 0.00000 0.00000
executing [ 6] set: makeWingOml 0
makeWingOml = 0.00000 0.00000
executing [ 7] set: makeWingHinge 0
makeWingHinge = 0.00000 0.00000
executing [ 8] set: makeWingWaffle 0
makeWingWaffle = 0.00000 0.00000
executing [ 9] set: makeWingCmass 0
makeWingCmass = 0.00000 0.00000
executing [ 10] set: makeHtailOml 0
makeHtailOml = 0.00000 0.00000
executing [ 11] set: makeHtailHinge 0
makeHtailHinge = 0.00000 0.00000
executing [ 12] set: makeHtailWaffle 0
makeHtailWaffle = 0.00000 0.00000
executing [ 13] set: makeHtailCmass 0
makeHtailCmass = 0.00000 0.00000
executing [ 14] set: makeVtailOml 0
makeVtailOml = 0.00000 0.00000
executing [ 15] set: makeVtailHinge 0
makeVtailHinge = 0.00000 0.00000
executing [ 16] set: makeVtailWaffle 0
makeVtailWaffle = 0.00000 0.00000
executing [ 17] set: makeVtailCmass 0
makeVtailCmass = 0.00000 0.00000
executing [ 18] set: makePylonOml 0
makePylonOml = 0.00000 0.00000
executing [ 19] set: makePodOml 0
makePodOml = 0.00000 0.00000
executing [ 20] set: SHARP_TE 0
SHARP_TE = 0.00000 0.00000
executing [ 21] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 24] ifthen: 0.00000 NE 0.00000 and ...
executing [ 40] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 43] ifthen: 0.00000 NE 0.00000 and ...
executing [ 51] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 54] ifthen: 0.00000 NE 0.00000 and ...
executing [ 65] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 68] ifthen: 0.00000 NE 0.00000 and ...
executing [ 79] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 82] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 85] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 88] ifthen: 1.00000 NE 0.00000 OR ...
executing [ 89] set: makeWingOml 1
makeWingOml = 1.00000 0.00000
executing [ 90] set: makeWingWaffle 1
makeWingWaffle = 1.00000 0.00000
executing [ 92] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 95] ifthen: 0.00000 NE 0.00000 and ...
executing [ 101] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 102] set: COMP:Fuse 0
COMP:Fuse = 0.00000 0.00000
executing [ 104] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 107] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 108] set: COMP:Htail 0
COMP:Htail = 0.00000 0.00000
executing [ 110] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 111] set: COMP:Vtail 0
COMP:Vtail = 0.00000 0.00000
executing [ 113] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 114] set: COMP:Pylon 0
COMP:Pylon = 0.00000 0.00000
executing [ 116] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 117] set: COMP:Pod 0
COMP:Pod = 0.00000 0.00000
executing [ 119] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 120] set: COMP:Control 0
COMP:Control = 0.00000 0.00000
executing [ 122] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 123] set: makeFuseOml 0
makeFuseOml = 0.00000 0.00000
executing [ 124] set: makeFuseWaffle 0
makeFuseWaffle = 0.00000 0.00000
executing [ 125] set: makeFuseCmass 0
makeFuseCmass = 0.00000 0.00000
executing [ 127] ifthen: 1.00000 EQ 0.00000 and ...
executing [ 133] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 134] set: makeHtailOml 0
makeHtailOml = 0.00000 0.00000
executing [ 135] set: makeHtailHinge 0
makeHtailHinge = 0.00000 0.00000
executing [ 136] set: makeHtailWaffle 0
makeHtailWaffle = 0.00000 0.00000
executing [ 137] set: makeHtailCmass 0
makeHtailCmass = 0.00000 0.00000
executing [ 139] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 140] set: makeVtailOml 0
makeVtailOml = 0.00000 0.00000
executing [ 141] set: makeVtailHinge 0
makeVtailHinge = 0.00000 0.00000
executing [ 142] set: makeVtailWaffle 0
makeVtailWaffle = 0.00000 0.00000
executing [ 143] set: makeVtailCmass 0
makeVtailCmass = 0.00000 0.00000
executing [ 145] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 146] set: makePylonOml 0
makePylonOml = 0.00000 0.00000
executing [ 148] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 149] set: makePodOml 0
makePodOml = 0.00000 0.00000
executing [ 151] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 152] set: makeWingHinge 0
makeWingHinge = 0.00000 0.00000
executing [ 153] set: makeHtailHinge 0
makeHtailHinge = 0.00000 0.00000
executing [ 154] set: makeVtailHinge 0
makeVtailHinge = 0.00000 0.00000
executing [ 156] end:
executing [ 157] set: wing:span sqrt(wing:aspect*wing:area)
wing:span = 7.74597 0.00000
executing [ 158] set: wing:chordr 2*wing:area/wing:span/(1+wing:taper)
wing:chordr = 1.61374 0.00000
executing [ 159] set: wing:chordt wing:chordr*wing:taper
wing:chordt = 0.96825 0.00000
executing [ 160] set: wing:ytip -wing:span/2
wing:ytip = -3.87298 0.00000
executing [ 161] set: wing:xtip -wing:ytip*tand(wing:sweep)
wing:xtip = 1.40965 0.00000
executing [ 162] set: wing:ztip -wing:ytip*tand(wing:dihedral)
wing:ztip = 0.27083 0.00000
executing [ 163] set: wing:mac sqrt(wing:area/wing:aspect)
wing:mac = 1.29099 0.00000
executing [ 164] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 165] mark:
Mark created
executing [ 166] udprim: naca thickness 0.12000 camber 0.06000 sharpte 0.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 167] scale: 1.61374 0.00000 0.00000 0.00000
Body 2 created (toler= 1.6137e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 168] rotatex: 90.00000 0.00000 0.00000
Body 3 created (toler= 1.6137e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 169] udprim: naca thickness 0.16000 camber 0.02000 sharpte 0.00000 (compiled code)
Body 4 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 170] scale: 0.96825 0.00000 0.00000 0.00000
Body 5 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 171] rotatex: 90.00000 0.00000 0.00000
Body 6 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 172] rotatey: -5.00000 0.00000 0.00000
Body 7 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 173] translate: 1.40965 -3.87298 0.27083
Body 8 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 174] rule: 0.00000 0.00000
ruling 2 Xsects with 3 Strips each...
Body 9 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 175] set: ruledBody @nbody
ruledBody = 9.00000 0.00000
executing [ 176] select: face 9 1
putting Branch Attributes on Face 4
executing [ 177] select: face 9 2
putting Branch Attributes on Face 5
executing [ 178] select: face 9 3
putting Branch Attributes on Face 1
executing [ 179] select: face 9 4
putting Branch Attributes on Face 2
executing [ 180] select: edge 9 3 9 4 1
putting Branch Attributes on Edge 3
executing [ 181] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 182] select: face 9 5
putting Branch Attributes on Face 3
executing [ 186] store: LeftWing 0.00000 1.00000
Body 9 stored
executing [ 187] restore: LeftWing 0.00000
Body 10 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 188] select: face tagType tip * * * *
putting Branch Attributes on Face 5
executing [ 189] select: edge tagType leadingEdge * * * *
executing [ 190] ifthen: 3.00000 GT 0.00000 and 0.00000 eq 0.00000
executing [ 191] select: edge tagType leadingEdge * * * *
putting Branch Attributes on Edge 3
executing [ 193] select: edge tagType trailingEdge * * * *
ERROR:: (edge_not_found) in Branch Brch_000193 at [[..\ESP\wing3.csm:103]]
SELECT specified nonexistant Edge
executing [ 197] catbeg: $edge_not_found
--> catching signal -223 (edge_not_found)
executing [ 199] mirror: 0.00000 1.00000 0.00000 0.00000
Body 11 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 200] join: 0.00000 0.00000
Body 12 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 201] select: edge 9 3 9 3 1
putting Branch Attributes on Edge 2
executing [ 202] select: edge 9 4 9 4 1
putting Branch Attributes on Edge 5
executing [ 203] store: WingOml 0.00000 0.00000
Body 12 stored
executing [ 205] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 206] restore: WingOml 0.00000
Body 13 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 207] set: xmin @xmin-0.1
xmin = -0.10102 0.00000
executing [ 208] set: xmax @xmax+0.1
xmax = 2.47425 0.00000
executing [ 209] set: ymin 0
ymin = 0.00000 0.00000
executing [ 210] set: ymax @ymax+0.1
ymax = 3.97298 0.00000
executing [ 211] set: zmin @zmin-0.1
zmin = -0.13316 0.00000
executing [ 212] set: zmax @zmax+0.1
zmax = 0.49998 0.00000
executing [ 213] store: . 0.00000 0.00000
Body 13 removed from stack
executing [ 214] udparg: waffle depth 3.00000
Body 14 created (NULL Body)
executing [ 215] udparg: waffle depth 0.20000
Body 15 created (NULL Body)
executing [ 216] udparg: waffle depth 0.70000
Body 16 created (NULL Body)
executing [ 217] udprim: waffle depth 0.63315 filename tmp_OpenCSM_00/00 (compiled code)
processing:
processing: # construction lines for spars
processing: CPOINT A AT 0+wing:spar1*wing:chordr 0
processing: CPOINT B AT wing:xtip+wing:spar1*wing:chordt -wing:ytip
processing: CPOINT C AT 0+wing:spar2*wing:chordr 0
processing: CPOINT D AT wing:xtip+wing:spar2*wing:chordt -wing:ytip
processing:
processing: CLINE AB A B
processing: CLINE CD C D
processing:
processing: # rite spars
processing: POINT E ON AB YLOC ymin
processing: POINT F ON AB YLOC ymax
processing: LINE EF E F tagComp=riteWing tagType=spar tagIndex=1
processing:
processing: POINT G ON CD YLOC ymin
processing: POINT H ON CD YLOC ymax
processing: LINE GH G H tagComp=riteWing tagType=spar tagIndex=2
processing:
processing: # rite ribs
processing: PATBEG irib wing:nrib
processing: CPOINT I AT xmin -wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=riteWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin -wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=riteWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin -wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=riteWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing:
processing: # root rib
processing: CPOINT I AT xmin 0
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=rootWing tagType=rib tagIndex=0
processing:
processing: # left spars
processing: POINT E AT x@E -y@E
processing: POINT F AT x@F -y@F
processing: LINE FE F E tagComp=leftWing tagType=spar tagIndex=1
processing:
processing: POINT G AT x@G -y@G
processing: POINT H AT x@H -y@H
processing: LINE HG H G tagComp=leftWing tagType=spar tagIndex=2
processing:
processing: # left ribs
processing: PATBEG irib wing:nrib
processing: CPOINT I AT xmin wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=leftWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=leftWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=leftWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
Body 17 created (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [ 218] translate: 0.00000 0.00000 -0.13316
Body 18 created (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [ 219] store: WingWaffle 0.00000 0.00000
Body 18 stored
executing [ 221] udprim: $/capsViews (scripted code)
[ 222] interface: . ALL 0.00000
executing [ 223] ifthen: 0.00000 NE 0.00000 and ...
executing [ 268] ifthen: 0.00000 NE 0.00000 and ...
executing [ 409] ifthen: 0.00000 NE 0.00000 and ...
executing [ 852] ifthen: 0.00000 NE 0.00000 and ...
executing [1290] ifthen: 1.00000 NE 0.00000 OR ...
executing [1291] udprim: $/viewStructure (scripted code)
[1292] interface: . ALL 0.00000
executing [1293] set: structAIMs $nastranAIM;astrosAIM;mystranAIM;egadsTessAIM
structAIMs = $nastranAIM;astrosAIM;mystranAIM;egadsTessAIM
executing [1294] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1295] restore: WingOml 0.00000
Body 19 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [1296] restore: WingWaffle 0.00000
Body 20 restored (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [1297] intersect: none 1.00000 0.0000e+00
Body 21 created (toler= 5.0000e-06, nnode= 57, nedge= 99, nface= 37)
executing [1298] restore: WingOml 0.00000
Body 22 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [1299] restore: WingWaffle 0.00000
Body 23 restored (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [1300] subtract: none 1.00000 0.0000e+00
Body 24 created (toler= 6.7429e-07, nnode= 63, nedge= 123, nface= 62)
executing [1301] extract: 0
Body 25 created (toler= 6.7429e-07, nnode= 63, nedge= 123, nface= 62)
executing [1302] union: 0.00000 0 0.0000e+00
Body 26 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1303] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1304] udprim: editAttr filename tmp_OpenCSM_00/03 (compiled code)
processing: FACE ADJ2EDGE tagType=leadingEdge
processing: SET capsIgnore=true
processing:
processing: FACE HAS tagType=trailingEdge
processing: SET capsIgnore=true
processing:
processing: FACE ADJ2FACE tagType=trailingEdge
processing: ANDNOT HAS tagType=rib
processing: ANDNOT HAS tagType=tip
processing: SET capsIgnore=true
processing:
processing: FACE ADJ2EDGE tagType=trailingEdge
processing: SET capsIgnore=true
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 27 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1305] udprim: editAttr filename tmp_OpenCSM_00/04 (compiled code)
processing: FACE HAS tagComp=leftWing
processing: ANDNOT ADJ2EDGE tagType=leadingEdge
processing: ANDNOT ADJ2EDGE tagType=trailingEdge
processing: ANDNOT ADJ2FACE tagType=trailingEdge
processing: SET capsGroup=leftWingSkin
processing:
processing: FACE HAS tagComp=riteWing
processing: ANDNOT ADJ2EDGE tagType=leadingEdge
processing: ANDNOT ADJ2EDGE tagType=trailingEdge
processing: ANDNOT ADJ2FACE tagType=trailingEdge
processing: SET capsGroup=riteWingSkin
processing:
processing: FACE HAS tagType=rib
processing: SET capsGroup=wingRib
processing:
processing: FACE HAS tagType=tip
processing: SET capsGroup=wingRib
processing:
processing: FACE HAS tagType=spar tagIndex=1
processing: SET capsGroup=wingSpar1
processing: SET capsMesh=wingSpar1
processing:
processing: FACE HAS tagType=spar tagIndex=2
processing: SET capsGroup=wingSpar2
processing: SET capsMesh=wingSpar2
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 28 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1309] udprim: editAttr filename tmp_OpenCSM_00/06 (compiled code)
processing: FACE HAS tagType=upper
processing: SET capsBound=upperWing
processing:
processing: FACE HAS tagType=lower
processing: SET capsBound=lowerWing
processing:
processing: FACE HAS tagType=tip tagIndex=1
processing: SET capsBound=leftTip
processing:
processing: FACE HAS tagType=tip tagIndex=2
processing: SET capsBound=riteTip
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 29 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1310] udprim: editAttr filename tmp_OpenCSM_00/07 (compiled code)
processing: NODE ADJ2FACE tagComp=leftWing tagType=tip
processing: AND ADJ2FACE tagType=lower
processing: AND ADJ2FACE tagType=spar tagIndex=1
processing: SET capsLoad=leftPointLoad
processing:
processing: NODE ADJ2FACE tagComp=riteWing tagType=tip
processing: AND ADJ2FACE tagType=lower
processing: AND ADJ2FACE tagType=spar tagIndex=1
processing: SET capsLoad=ritePointLoad
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 30 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1311] select: edge tagType leadingEdge * * * *
executing [1312] dimension: leadingEdges 1.00000 8.00000
executing [1313] set: leadingEdges @sellist
leadingEdges[1,1] = 8.00000 0.00000
leadingEdges[1,2] = 31.00000 0.00000
leadingEdges[1,3] = 33.00000 0.00000
leadingEdges[1,4] = 62.00000 0.00000
leadingEdges[1,5] = 64.00000 0.00000
leadingEdges[1,6] = 94.00000 0.00000
leadingEdges[1,7] = 96.00000 0.00000
leadingEdges[1,8] = 121.00000 0.00000
executing [1314] patbeg: i 8.00000
pattern counter: i = 1
executing [1315] select: edge 8
putting Branch Attributes on Edge 8
executing [1316] patend:
pattern counter: i = 2
executing [1315] select: edge 31
putting Branch Attributes on Edge 31
executing [1316] patend:
pattern counter: i = 3
executing [1315] select: edge 33
putting Branch Attributes on Edge 33
executing [1316] patend:
pattern counter: i = 4
executing [1315] select: edge 62
putting Branch Attributes on Edge 62
executing [1316] patend:
pattern counter: i = 5
executing [1315] select: edge 64
putting Branch Attributes on Edge 64
executing [1316] patend:
pattern counter: i = 6
executing [1315] select: edge 94
putting Branch Attributes on Edge 94
executing [1316] patend:
pattern counter: i = 7
executing [1315] select: edge 96
putting Branch Attributes on Edge 96
executing [1316] patend:
pattern counter: i = 8
executing [1315] select: edge 121
putting Branch Attributes on Edge 121
executing [1316] patend:
executing [1317] udprim: editAttr filename tmp_OpenCSM_00/08 (compiled code)
processing: FACE ADJ2EDGE tagComp=leftWing
processing: SET tagTemp=leadingEdgeFace
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 31 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1318] udprim: editAttr filename tmp_OpenCSM_00/09 (compiled code)
processing: EDGE ADJ2FACE tagTemp=leadingEdgeFace
processing: AND ADJ2FACE tagComp=rootWing
processing: SET capsMesh=rootLeadingEdge
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 32 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1319] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1320] udprim: editAttr filename tmp_OpenCSM_00/10 (compiled code)
processing: FACE HAS tagComp=rootWing
processing: SET capsConstraint=rootConstraint
processing:
processing: EDGE ADJ2FACE tagComp=rootWing
processing: SET capsConstraint=rootConstraint
processing:
processing: NODE ADJ2FACE tagComp=rootWing
processing: SET capsConstraint=rootConstraint
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 33 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1322] ifthen: 0.00000 EQ 1.00000 and ...
executing [1325] udprim: editAttr filename tmp_OpenCSM_00/12 (compiled code)
processing: FACE HAS tagComp=leftWing tagType=upper
processing: AND ADJ2EDGE tagType=leadingEdge
processing: AND ADJ2FACE tagComp=riteWing
processing: SET tagCsys=leftWing
processing:
processing: FACE HAS tagComp=riteWing tagType=upper
processing: AND ADJ2EDGE tagType=leadingEdge
processing: AND ADJ2FACE tagComp=leftWing
processing: SET tagCsys=riteWing
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 34 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1326] select: face tagCsys leftWing * * * *
executing [1327] set: leftWingSkinCsys @sellist
leftWingSkinCsys = 27.00000 0.00000
executing [1328] select: face tagCsys riteWing * * * *
executing [1329] set: riteWingSkinCsys @sellist
riteWingSkinCsys = 8.00000 0.00000
executing [1330] store: WingStruct 0.00000 0.00000
Body 34 stored
executing [1331] restore: WingStruct 0.00000
Body 35 restored (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1332] store: WingStruct 0.00000 0.00000
WARNING:: storage WingStruct (0) is being overwritten
Body 35 stored
executing [1334] restore: WingStruct 0.00000
Body 36 restored (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1335] select: body
putting Branch Attributes on Body
executing [1336] ifthen: 0.00000 EQ 1.00000 and ...
executing [1339] end:
executing [1341] ifthen: 0.00000 NE 0.00000 and ...
executing [1378] end:
finalizing:
==> Profile information
Branch type ncall time (sec) pct
dimension 1 0.001 0.0
udprim 14 1.490 10.1
restore 8 0.138 0.9
rule 1 0.197 1.3
intersect 1 0.972 6.6
subtract 1 2.857 19.3
union 1 7.010 47.3
join 1 0.179 1.2
extract 1 1.548 10.4
translate 2 0.025 0.2
rotatex 2 0.007 0.0
rotatey 1 0.003 0.0
scale 2 0.007 0.0
mirror 1 0.040 0.3
interface 3 0.001 0.0
end 3 0.000 0.0
set 60 0.103 0.7
udparg 3 0.008 0.1
select 23 0.174 1.2
store 6 0.008 0.1
patbeg 1 0.002 0.0
patend 8 0.007 0.0
ifthen 43 0.039 0.3
else 2 0.000 0.0
endif 43 0.000 0.0
catbeg 1 0.001 0.0
catend 1 0.000 0.0
mark 1 0.001 0.0
Total 235 14.818
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar1, index = 1
Name = riteWingSkin, index = 2
Name = wingRib, index = 3
Name = leftWingSkin, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Tessellating body
capsIgnore attribute found for face - 3!!
capsIgnore attribute found for face - 8!!
capsIgnore attribute found for face - 15!!
capsIgnore attribute found for face - 16!!
capsIgnore attribute found for face - 17!!
capsIgnore attribute found for face - 18!!
capsIgnore attribute found for face - 26!!
capsIgnore attribute found for face - 27!!
capsIgnore attribute found for face - 33!!
capsIgnore attribute found for face - 36!!
capsIgnore attribute found for face - 37!!
capsIgnore attribute found for face - 38!!
capsIgnore attribute found for face - 39!!
capsIgnore attribute found for face - 40!!
capsIgnore attribute found for face - 41!!
capsIgnore attribute found for face - 42!!
capsIgnore attribute found for face - 50!!
capsIgnore attribute found for face - 51!!
capsIgnore attribute found for face - 52!!
capsIgnore attribute found for face - 58!!
capsIgnore attribute found for face - 61!!
capsIgnore attribute found for face - 62!!
capsIgnore attribute found for face - 63!!
capsIgnore attribute found for face - 64!!
capsIgnore attribute found for face - 65!!
capsIgnore attribute found for face - 66!!
capsIgnore attribute found for face - 73!!
capsIgnore attribute found for face - 74!!
capsIgnore attribute found for face - 75!!
capsIgnore attribute found for face - 81!!
capsIgnore attribute found for face - 83!!
capsIgnore attribute found for face - 84!!
capsIgnore attribute found for face - 85!!
capsIgnore attribute found for face - 86!!
capsIgnore attribute found for face - 89!!
capsIgnore attribute found for face - 90!!
capsIgnore attribute found for face - 91!!
capsIgnore attribute found for face - 96!!
capsIgnore attribute found for face - 97!!
capsIgnore attribute found for face - 98!!
Number of nodes = 299
Number of elements = 387
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 387
----------------------------
Total number of nodes = 299
Total number of elements = 387
Analysis directory does not currently exist - it will be made automatically
CAPS Info: No symbol for aimExecute in astrosAIM
CAPS Info: No symbol for aimCheck in astrosAIM
CAPS Info: No symbol for aimData in astrosAIM
CAPS Info: No symbol for aimSensitivity in astrosAIM
==> Running ASTROS pre-analysis...
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = lowerWing, index = 1
Name = upperWing, index = 2
Name = riteTip, index = 3
Name = leftTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Found link for attrMap (Attribute_Map) from parent
Found link for a Surface mesh from parent
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 64 (out of 299) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftPointLoad
No "groupName" specified for Load tuple leftPointLoad, going to use load name
Load name - ritePointLoad
No "groupName" specified for Load tuple ritePointLoad, going to use load name
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running Astros...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
--> Maximum displacements:
--> Tmax 12131.654370141774
--> T1max 275.241
--> T2max 1005.74
--> T3max 12103.5
--> temporary directory "tmp_OpenCSM_00" removed
Cleaning up egadsInstance - 0
Cleaning up astrosInstance - 0
EGADS Info: 861 Objects, 1379 Reference in Use (of 34591) at Close!
real 0m17.782s
user 0m0.109s
sys 0m0.311s
+ status=0
+ set +x
=================================================
data/session10/astros_4_Composite.py passed (as expected)
=================================================
=================================================
nastran_5_Flutter.py test;
+ python nastran_5_Flutter.py
+ tee -a /c/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/training/WIN64.2017/CAPS/training/training.log
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
CAPS Info: No symbol for aimDiscr in egadsTessAIM
CAPS Info: No symbol for aimFreeDiscr in egadsTessAIM
CAPS Info: No symbol for aimLocateElement in egadsTessAIM
CAPS Info: No symbol for aimUsesDataSet in egadsTessAIM
CAPS Info: No symbol for aimCheck in egadsTessAIM
CAPS Info: No symbol for aimTransfer in egadsTessAIM
CAPS Info: No symbol for aimInterpolation in egadsTessAIM
CAPS Info: No symbol for aimInterpolateBar in egadsTessAIM
CAPS Info: No symbol for aimIntegration in egadsTessAIM
CAPS Info: No symbol for aimIntegrateBar in egadsTessAIM
CAPS Info: No symbol for aimSensitivity in egadsTessAIM
==> Generating Mesh...
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] udprim: $/capsHeader (scripted code)
[ 2] interface: . ALL 0.00000
executing [ 3] set: makeFuseOml 0
makeFuseOml = 0.00000 0.00000
executing [ 4] set: makeFuseWaffle 0
makeFuseWaffle = 0.00000 0.00000
executing [ 5] set: makeFuseCmass 0
makeFuseCmass = 0.00000 0.00000
executing [ 6] set: makeWingOml 0
makeWingOml = 0.00000 0.00000
executing [ 7] set: makeWingHinge 0
makeWingHinge = 0.00000 0.00000
executing [ 8] set: makeWingWaffle 0
makeWingWaffle = 0.00000 0.00000
executing [ 9] set: makeWingCmass 0
makeWingCmass = 0.00000 0.00000
executing [ 10] set: makeHtailOml 0
makeHtailOml = 0.00000 0.00000
executing [ 11] set: makeHtailHinge 0
makeHtailHinge = 0.00000 0.00000
executing [ 12] set: makeHtailWaffle 0
makeHtailWaffle = 0.00000 0.00000
executing [ 13] set: makeHtailCmass 0
makeHtailCmass = 0.00000 0.00000
executing [ 14] set: makeVtailOml 0
makeVtailOml = 0.00000 0.00000
executing [ 15] set: makeVtailHinge 0
makeVtailHinge = 0.00000 0.00000
executing [ 16] set: makeVtailWaffle 0
makeVtailWaffle = 0.00000 0.00000
executing [ 17] set: makeVtailCmass 0
makeVtailCmass = 0.00000 0.00000
executing [ 18] set: makePylonOml 0
makePylonOml = 0.00000 0.00000
executing [ 19] set: makePodOml 0
makePodOml = 0.00000 0.00000
executing [ 20] set: SHARP_TE 0
SHARP_TE = 0.00000 0.00000
executing [ 21] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 24] ifthen: 0.00000 NE 0.00000 and ...
executing [ 40] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 43] ifthen: 1.00000 NE 0.00000 and 0.00000 eq 0.00000
executing [ 44] set: makeWingOml 1
makeWingOml = 1.00000 0.00000
executing [ 45] set: makeWingHinge 1
makeWingHinge = 1.00000 0.00000
executing [ 46] set: makeHtailOml 1
makeHtailOml = 1.00000 0.00000
executing [ 47] set: makeHtailHinge 1
makeHtailHinge = 1.00000 0.00000
executing [ 48] set: makeVtailOml 1
makeVtailOml = 1.00000 0.00000
executing [ 49] set: makeVtailHinge 1
makeVtailHinge = 1.00000 0.00000
executing [ 51] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 54] ifthen: 0.00000 NE 0.00000 and ...
executing [ 65] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 68] ifthen: 0.00000 NE 0.00000 and ...
executing [ 79] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 82] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 85] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 88] ifthen: 1.00000 NE 0.00000 OR ...
executing [ 89] set: makeWingOml 1
makeWingOml = 1.00000 0.00000
executing [ 90] set: makeWingWaffle 1
makeWingWaffle = 1.00000 0.00000
executing [ 92] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 95] ifthen: 0.00000 NE 0.00000 and ...
executing [ 101] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 102] set: COMP:Fuse 0
COMP:Fuse = 0.00000 0.00000
executing [ 104] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 107] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 108] set: COMP:Htail 0
COMP:Htail = 0.00000 0.00000
executing [ 110] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 111] set: COMP:Vtail 0
COMP:Vtail = 0.00000 0.00000
executing [ 113] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 114] set: COMP:Pylon 0
COMP:Pylon = 0.00000 0.00000
executing [ 116] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 117] set: COMP:Pod 0
COMP:Pod = 0.00000 0.00000
executing [ 119] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 120] set: COMP:Control 0
COMP:Control = 0.00000 0.00000
executing [ 122] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 123] set: makeFuseOml 0
makeFuseOml = 0.00000 0.00000
executing [ 124] set: makeFuseWaffle 0
makeFuseWaffle = 0.00000 0.00000
executing [ 125] set: makeFuseCmass 0
makeFuseCmass = 0.00000 0.00000
executing [ 127] ifthen: 1.00000 EQ 0.00000 and ...
executing [ 133] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 134] set: makeHtailOml 0
makeHtailOml = 0.00000 0.00000
executing [ 135] set: makeHtailHinge 0
makeHtailHinge = 0.00000 0.00000
executing [ 136] set: makeHtailWaffle 0
makeHtailWaffle = 0.00000 0.00000
executing [ 137] set: makeHtailCmass 0
makeHtailCmass = 0.00000 0.00000
executing [ 139] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 140] set: makeVtailOml 0
makeVtailOml = 0.00000 0.00000
executing [ 141] set: makeVtailHinge 0
makeVtailHinge = 0.00000 0.00000
executing [ 142] set: makeVtailWaffle 0
makeVtailWaffle = 0.00000 0.00000
executing [ 143] set: makeVtailCmass 0
makeVtailCmass = 0.00000 0.00000
executing [ 145] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 146] set: makePylonOml 0
makePylonOml = 0.00000 0.00000
executing [ 148] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 149] set: makePodOml 0
makePodOml = 0.00000 0.00000
executing [ 151] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 152] set: makeWingHinge 0
makeWingHinge = 0.00000 0.00000
executing [ 153] set: makeHtailHinge 0
makeHtailHinge = 0.00000 0.00000
executing [ 154] set: makeVtailHinge 0
makeVtailHinge = 0.00000 0.00000
executing [ 156] end:
executing [ 157] set: wing:span sqrt(wing:aspect*wing:area)
wing:span = 7.74597 0.00000
executing [ 158] set: wing:chordr 2*wing:area/wing:span/(1+wing:taper)
wing:chordr = 1.61374 0.00000
executing [ 159] set: wing:chordt wing:chordr*wing:taper
wing:chordt = 0.96825 0.00000
executing [ 160] set: wing:ytip -wing:span/2
wing:ytip = -3.87298 0.00000
executing [ 161] set: wing:xtip -wing:ytip*tand(wing:sweep)
wing:xtip = 1.40965 0.00000
executing [ 162] set: wing:ztip -wing:ytip*tand(wing:dihedral)
wing:ztip = 0.27083 0.00000
executing [ 163] set: wing:mac sqrt(wing:area/wing:aspect)
wing:mac = 1.29099 0.00000
executing [ 164] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 165] mark:
Mark created
executing [ 166] udprim: naca thickness 0.12000 camber 0.06000 sharpte 0.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 167] scale: 1.61374 0.00000 0.00000 0.00000
Body 2 created (toler= 1.6137e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 168] rotatex: 90.00000 0.00000 0.00000
Body 3 created (toler= 1.6137e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 169] udprim: naca thickness 0.16000 camber 0.02000 sharpte 0.00000 (compiled code)
Body 4 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 170] scale: 0.96825 0.00000 0.00000 0.00000
Body 5 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 171] rotatex: 90.00000 0.00000 0.00000
Body 6 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 172] rotatey: -5.00000 0.00000 0.00000
Body 7 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 173] translate: 1.40965 -3.87298 0.27083
Body 8 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 174] rule: 0.00000 0.00000
ruling 2 Xsects with 3 Strips each...
Body 9 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 175] set: ruledBody @nbody
ruledBody = 9.00000 0.00000
executing [ 176] select: face 9 1
putting Branch Attributes on Face 4
executing [ 177] select: face 9 2
putting Branch Attributes on Face 5
executing [ 178] select: face 9 3
putting Branch Attributes on Face 1
executing [ 179] select: face 9 4
putting Branch Attributes on Face 2
executing [ 180] select: edge 9 3 9 4 1
putting Branch Attributes on Edge 3
executing [ 181] ifthen: 0.00000 EQ 0.00000 and 0.00000 eq 0.00000
executing [ 182] select: face 9 5
putting Branch Attributes on Face 3
executing [ 186] store: LeftWing 0.00000 1.00000
Body 9 stored
executing [ 187] restore: LeftWing 0.00000
Body 10 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 188] select: face tagType tip * * * *
putting Branch Attributes on Face 5
executing [ 189] select: edge tagType leadingEdge * * * *
executing [ 190] ifthen: 3.00000 GT 0.00000 and 0.00000 eq 0.00000
executing [ 191] select: edge tagType leadingEdge * * * *
putting Branch Attributes on Edge 3
executing [ 193] select: edge tagType trailingEdge * * * *
ERROR:: (edge_not_found) in Branch Brch_000193 at [[..\ESP\wing3.csm:103]]
SELECT specified nonexistant Edge
executing [ 197] catbeg: $edge_not_found
--> catching signal -223 (edge_not_found)
executing [ 199] mirror: 0.00000 1.00000 0.00000 0.00000
Body 11 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 200] join: 0.00000 0.00000
Body 12 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 201] select: edge 9 3 9 3 1
putting Branch Attributes on Edge 2
executing [ 202] select: edge 9 4 9 4 1
putting Branch Attributes on Edge 5
executing [ 203] store: WingOml 0.00000 0.00000
Body 12 stored
executing [ 205] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 206] restore: WingOml 0.00000
Body 13 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 207] set: xmin @xmin-0.1
xmin = -0.10102 0.00000
executing [ 208] set: xmax @xmax+0.1
xmax = 2.47425 0.00000
executing [ 209] set: ymin 0
ymin = 0.00000 0.00000
executing [ 210] set: ymax @ymax+0.1
ymax = 3.97298 0.00000
executing [ 211] set: zmin @zmin-0.1
zmin = -0.13316 0.00000
executing [ 212] set: zmax @zmax+0.1
zmax = 0.49998 0.00000
executing [ 213] store: . 0.00000 0.00000
Body 13 removed from stack
executing [ 214] udparg: waffle depth 3.00000
Body 14 created (NULL Body)
executing [ 215] udparg: waffle depth 0.20000
Body 15 created (NULL Body)
executing [ 216] udparg: waffle depth 0.70000
Body 16 created (NULL Body)
executing [ 217] udprim: waffle depth 0.63315 filename tmp_OpenCSM_00/00 (compiled code)
processing:
processing: # construction lines for spars
processing: CPOINT A AT 0+wing:spar1*wing:chordr 0
processing: CPOINT B AT wing:xtip+wing:spar1*wing:chordt -wing:ytip
processing: CPOINT C AT 0+wing:spar2*wing:chordr 0
processing: CPOINT D AT wing:xtip+wing:spar2*wing:chordt -wing:ytip
processing:
processing: CLINE AB A B
processing: CLINE CD C D
processing:
processing: # rite spars
processing: POINT E ON AB YLOC ymin
processing: POINT F ON AB YLOC ymax
processing: LINE EF E F tagComp=riteWing tagType=spar tagIndex=1
processing:
processing: POINT G ON CD YLOC ymin
processing: POINT H ON CD YLOC ymax
processing: LINE GH G H tagComp=riteWing tagType=spar tagIndex=2
processing:
processing: # rite ribs
processing: PATBEG irib wing:nrib
processing: CPOINT I AT xmin -wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=riteWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin -wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=riteWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin -wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=riteWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing:
processing: # root rib
processing: CPOINT I AT xmin 0
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=rootWing tagType=rib tagIndex=0
processing:
processing: # left spars
processing: POINT E AT x@E -y@E
processing: POINT F AT x@F -y@F
processing: LINE FE F E tagComp=leftWing tagType=spar tagIndex=1
processing:
processing: POINT G AT x@G -y@G
processing: POINT H AT x@H -y@H
processing: LINE HG H G tagComp=leftWing tagType=spar tagIndex=2
processing:
processing: # left ribs
processing: PATBEG irib wing:nrib
processing: CPOINT I AT xmin wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=leftWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=leftWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
processing: CPOINT I AT xmin wing:ytip*irib/(wing:nrib+1)
processing: CPOINT J AT xmax y@I
processing: LINE . I J tagComp=leftWing tagType=rib tagIndex=!val2str(irib,0)
processing: PATEND
Body 17 created (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [ 218] translate: 0.00000 0.00000 -0.13316
Body 18 created (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [ 219] store: WingWaffle 0.00000 0.00000
Body 18 stored
executing [ 221] udprim: $/capsViews (scripted code)
[ 222] interface: . ALL 0.00000
executing [ 223] ifthen: 0.00000 NE 0.00000 and ...
executing [ 268] ifthen: 1.00000 NE 0.00000 and 0.00000 eq 0.00000
executing [ 269] udprim: $/viewVLM (scripted code)
[ 270] interface: . ALL 0.00000
executing [ 271] set: vlmAIMs $avlAIM;$astrosAIM;nastranAIM;egadsTessAIM
vlmAIMs = $avlAIM;$astrosAIM;nastranAIM;egadsTessAIM
executing [ 272] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 273] restore: WingOml 0.00000
Body 19 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 274] set: xmin @xmin-1
xmin = -1.00102 0.00000
executing [ 275] set: xmax @xmax+1
xmax = 3.37425 0.00000
executing [ 276] set: ymin @ymin+0.001
ymin = -3.87198 0.00000
executing [ 277] set: ymax @ymax-0.001
ymax = 3.87198 0.00000
executing [ 278] set: zmin @zmin-1
zmin = -1.03316 0.00000
executing [ 279] set: zmax @zmax+1
zmax = 1.39998 0.00000
executing [ 280] store: . 0.00000 0.00000
Body 19 removed from stack
executing [ 281] set: WingVlmNcut 3
WingVlmNcut = 3.00000 0.00000
executing [ 282] mark:
Mark created
executing [ 283] patbeg: icut 3.00000
pattern counter: icut = 1
executing [ 284] set: y ymin+(ymax-ymin)*(icut-1)/(WingVlmNcut-1)
y = -3.87198 0.00000
executing [ 285] box: -1.00102 -3.87198 -1.03316 4.37527 0.00000 2.43315
Body 20 created (toler= 1.0000e-07, nnode= 4, nedge= 4, nface= 1)
executing [ 286] restore: WingOml 0.00000
Body 21 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 287] intersect: none 1.00000 0.0000e+00
Body 22 created (toler= 5.0000e-06, nnode= 3, nedge= 3, nface= 1)
executing [ 288] select: face 1
putting Branch Attributes on Face 1
executing [ 289] patend:
pattern counter: icut = 2
executing [ 284] set: y ymin+(ymax-ymin)*(icut-1)/(WingVlmNcut-1)
y = 0.00000 0.00000
executing [ 285] box: -1.00102 0.00000 -1.03316 4.37527 0.00000 2.43315
Body 23 created (toler= 1.0000e-07, nnode= 4, nedge= 4, nface= 1)
executing [ 286] restore: WingOml 0.00000
Body 24 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 287] intersect: none 1.00000 0.0000e+00
Body 25 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 288] select: face 1
putting Branch Attributes on Face 1
executing [ 289] patend:
pattern counter: icut = 3
executing [ 284] set: y ymin+(ymax-ymin)*(icut-1)/(WingVlmNcut-1)
y = 3.87198 0.00000
executing [ 285] box: -1.00102 3.87198 -1.03316 4.37527 0.00000 2.43315
Body 26 created (toler= 1.0000e-07, nnode= 4, nedge= 4, nface= 1)
executing [ 286] restore: WingOml 0.00000
Body 27 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 287] intersect: none 1.00000 0.0000e+00
Body 28 created (toler= 5.0000e-06, nnode= 3, nedge= 3, nface= 1)
executing [ 288] select: face 1
putting Branch Attributes on Face 1
executing [ 289] patend:
executing [ 290] ifthen: 1.00000 EQ 0.00000 and ...
executing [ 299] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 321] group: 0.00000
Body 25 added to Group 28
Body 22 added to Group 28
executing [ 323] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 365] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 407] end:
executing [ 409] ifthen: 0.00000 NE 0.00000 and ...
executing [ 852] ifthen: 0.00000 NE 0.00000 and ...
executing [1290] ifthen: 1.00000 NE 0.00000 OR ...
executing [1291] udprim: $/viewStructure (scripted code)
[1292] interface: . ALL 0.00000
executing [1293] set: structAIMs $nastranAIM;astrosAIM;mystranAIM;egadsTessAIM
structAIMs = $nastranAIM;astrosAIM;mystranAIM;egadsTessAIM
executing [1294] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1295] restore: WingOml 0.00000
Body 29 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [1296] restore: WingWaffle 0.00000
Body 30 restored (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [1297] intersect: none 1.00000 0.0000e+00
Body 31 created (toler= 5.0000e-06, nnode= 57, nedge= 99, nface= 37)
executing [1298] restore: WingOml 0.00000
Body 32 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [1299] restore: WingWaffle 0.00000
Body 33 restored (toler= 1.0000e-07, nnode= 64, nedge= 106, nface= 37)
executing [1300] subtract: none 1.00000 0.0000e+00
Body 34 created (toler= 6.7429e-07, nnode= 63, nedge= 123, nface= 62)
executing [1301] extract: 0
Body 35 created (toler= 6.7429e-07, nnode= 63, nedge= 123, nface= 62)
executing [1302] union: 0.00000 0 0.0000e+00
Body 36 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1303] ifthen: 0.00000 EQ 1.00000 and ...
executing [1306] else:
executing [1307] udprim: editAttr filename tmp_OpenCSM_00/05 (compiled code)
processing: FACE HAS tagComp=leftWing
processing: SET capsGroup=leftWingSkin
processing:
processing: FACE HAS tagComp=riteWing
processing: SET capsGroup=riteWingSkin
processing:
processing: FACE HAS tagType=tip
processing: SET capsGroup=wingRib
processing:
processing: FACE HAS tagType=trailingEdge
processing: SET capsGroup=wingTE
processing:
processing: FACE HAS tagType=rib
processing: SET capsGroup=wingRib
processing:
processing: FACE HAS tagType=spar tagIndex=1
processing: SET capsGroup=wingSpar1
processing: SET capsMesh=wingSpar1
processing:
processing: FACE HAS tagType=spar tagIndex=2
processing: SET capsGroup=wingSpar2
processing: SET capsMesh=wingSpar2
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 37 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1309] udprim: editAttr filename tmp_OpenCSM_00/06 (compiled code)
processing: FACE HAS tagType=upper
processing: SET capsBound=upperWing
processing:
processing: FACE HAS tagType=lower
processing: SET capsBound=lowerWing
processing:
processing: FACE HAS tagType=tip tagIndex=1
processing: SET capsBound=leftTip
processing:
processing: FACE HAS tagType=tip tagIndex=2
processing: SET capsBound=riteTip
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 38 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1310] udprim: editAttr filename tmp_OpenCSM_00/07 (compiled code)
processing: NODE ADJ2FACE tagComp=leftWing tagType=tip
processing: AND ADJ2FACE tagType=lower
processing: AND ADJ2FACE tagType=spar tagIndex=1
processing: SET capsLoad=leftPointLoad
processing:
processing: NODE ADJ2FACE tagComp=riteWing tagType=tip
processing: AND ADJ2FACE tagType=lower
processing: AND ADJ2FACE tagType=spar tagIndex=1
processing: SET capsLoad=ritePointLoad
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 39 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1311] select: edge tagType leadingEdge * * * *
executing [1312] dimension: leadingEdges 1.00000 8.00000
executing [1313] set: leadingEdges @sellist
leadingEdges[1,1] = 8.00000 0.00000
leadingEdges[1,2] = 31.00000 0.00000
leadingEdges[1,3] = 33.00000 0.00000
leadingEdges[1,4] = 62.00000 0.00000
leadingEdges[1,5] = 64.00000 0.00000
leadingEdges[1,6] = 94.00000 0.00000
leadingEdges[1,7] = 96.00000 0.00000
leadingEdges[1,8] = 121.00000 0.00000
executing [1314] patbeg: i 8.00000
pattern counter: i = 1
executing [1315] select: edge 8
putting Branch Attributes on Edge 8
executing [1316] patend:
pattern counter: i = 2
executing [1315] select: edge 31
putting Branch Attributes on Edge 31
executing [1316] patend:
pattern counter: i = 3
executing [1315] select: edge 33
putting Branch Attributes on Edge 33
executing [1316] patend:
pattern counter: i = 4
executing [1315] select: edge 62
putting Branch Attributes on Edge 62
executing [1316] patend:
pattern counter: i = 5
executing [1315] select: edge 64
putting Branch Attributes on Edge 64
executing [1316] patend:
pattern counter: i = 6
executing [1315] select: edge 94
putting Branch Attributes on Edge 94
executing [1316] patend:
pattern counter: i = 7
executing [1315] select: edge 96
putting Branch Attributes on Edge 96
executing [1316] patend:
pattern counter: i = 8
executing [1315] select: edge 121
putting Branch Attributes on Edge 121
executing [1316] patend:
executing [1317] udprim: editAttr filename tmp_OpenCSM_00/08 (compiled code)
processing: FACE ADJ2EDGE tagComp=leftWing
processing: SET tagTemp=leadingEdgeFace
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 40 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1318] udprim: editAttr filename tmp_OpenCSM_00/09 (compiled code)
processing: EDGE ADJ2FACE tagTemp=leadingEdgeFace
processing: AND ADJ2FACE tagComp=rootWing
processing: SET capsMesh=rootLeadingEdge
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 41 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1319] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [1320] udprim: editAttr filename tmp_OpenCSM_00/10 (compiled code)
processing: FACE HAS tagComp=rootWing
processing: SET capsConstraint=rootConstraint
processing:
processing: EDGE ADJ2FACE tagComp=rootWing
processing: SET capsConstraint=rootConstraint
processing:
processing: NODE ADJ2FACE tagComp=rootWing
processing: SET capsConstraint=rootConstraint
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 42 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1322] ifthen: 0.00000 EQ 1.00000 and ...
executing [1325] udprim: editAttr filename tmp_OpenCSM_00/12 (compiled code)
processing: FACE HAS tagComp=leftWing tagType=upper
processing: AND ADJ2EDGE tagType=leadingEdge
processing: AND ADJ2FACE tagComp=riteWing
processing: SET tagCsys=leftWing
processing:
processing: FACE HAS tagComp=riteWing tagType=upper
processing: AND ADJ2EDGE tagType=leadingEdge
processing: AND ADJ2FACE tagComp=leftWing
processing: SET tagCsys=riteWing
WARNING:: toler = 5.0000e-06 for UDPRIM
Body 43 created (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1326] select: face tagCsys leftWing * * * *
executing [1327] set: leftWingSkinCsys @sellist
leftWingSkinCsys = 27.00000 0.00000
executing [1328] select: face tagCsys riteWing * * * *
executing [1329] set: riteWingSkinCsys @sellist
riteWingSkinCsys = 8.00000 0.00000
executing [1330] store: WingStruct 0.00000 0.00000
Body 43 stored
executing [1331] restore: WingStruct 0.00000
Body 44 restored (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1332] store: WingStruct 0.00000 0.00000
WARNING:: storage WingStruct (0) is being overwritten
Body 44 stored
executing [1334] restore: WingStruct 0.00000
Body 45 restored (toler= 5.0000e-06, nnode= 63, nedge= 137, nface= 99)
executing [1335] select: body
putting Branch Attributes on Body
executing [1336] ifthen: 0.00000 EQ 1.00000 and ...
executing [1339] end:
executing [1341] ifthen: 0.00000 NE 0.00000 and ...
executing [1378] end:
finalizing:
==> Profile information
Branch type ncall time (sec) pct
dimension 1 0.001 0.0
box 3 0.012 0.1
udprim 14 1.034 7.8
restore 12 0.147 1.1
rule 1 0.151 1.1
intersect 4 1.511 11.4
subtract 1 2.762 20.8
union 1 5.627 42.3
join 1 0.145 1.1
extract 1 1.494 11.2
translate 2 0.040 0.3
rotatex 2 0.008 0.1
rotatey 1 0.004 0.0
scale 2 0.009 0.1
mirror 1 0.037 0.3
interface 4 0.002 0.0
end 4 0.002 0.0
set 77 0.094 0.7
udparg 3 0.001 0.0
select 26 0.137 1.0
store 7 0.007 0.1
patbeg 2 0.002 0.0
patend 11 0.011 0.1
ifthen 48 0.049 0.4
else 2 0.001 0.0
endif 48 0.000 0.0
catbeg 1 0.000 0.0
catend 1 0.000 0.0
mark 2 0.002 0.0
group 1 0.001 0.0
Total 284 13.291
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Wing, index = 1
Name = wingSpar1, index = 2
Name = riteWingSkin, index = 3
Name = wingRib, index = 4
Name = leftWingSkin, index = 5
Name = wingSpar2, index = 6
Name = wingTE, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 4)
Tessellating body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Number of nodes = 7
Number of elements = 3
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 3
Getting surface mesh for body 2 (of 4)
Tessellating body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Number of nodes = 7
Number of elements = 3
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 3
Getting surface mesh for body 3 (of 4)
Tessellating body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Number of nodes = 7
Number of elements = 3
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 3
Getting surface mesh for body 4 (of 4)
Tessellating body
Number of nodes = 299
Number of elements = 387
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 387
----------------------------
Total number of nodes = 320
Total number of elements = 396
Analysis directory does not currently exist - it will be made automatically
CAPS Info: No symbol for aimExecute in nastranAIM
CAPS Info: No symbol for aimCheck in nastranAIM
CAPS Info: No symbol for aimSensitivity in nastranAIM
==> Running Nastran pre-analysis...
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = lowerWing, index = 1
Name = upperWing, index = 2
Name = riteTip, index = 3
Name = leftTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Found link for attrMap (Attribute_Map) from parent
Found link for a Surface mesh from parent
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 7
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 3
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 7
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 3
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 7
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 3
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 299
Number of elements = 387
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 387
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 320
Combined Number of elements = 396
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 396
Getting vortex lattice surface data
VLM surface name - upperWing
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 12
Surface 2: Number of points found for aero-spline = 12
Getting FEA materials.......
Number of materials - 2
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing Nastran instruction file....
SUBCASE = 0
Warning: No loads specified for case Flutter!!!!
Writing aero card
Writing analysis cards
Writing constraint ADD cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
Writing aeroelastic cards
==> Running Nastran...
'nastran' is not recognized as an internal or external command,
operable program or batch file.
--> temporary directory "tmp_OpenCSM_00" removed
Cleaning up egadsInstance - 0
Cleaning up nastranInstance - 0
EGADS Info: 906 Objects, 1436 Reference in Use (of 33673) at Close!
real 0m15.131s
user 0m0.109s
sys 0m0.374s
+ status=0
+ set +x
=================================================
data/session10/nastran_5_Flutter.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
session07
=================================================
All tests pass!
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>set err4=0
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>REM Check CAPS training examples
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>if training == training2018 mkdir C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\test\training2018 || exit /b 666
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>if training == training2018 cd C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\test\training2018 || exit /b 666
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>if training == training2018 xcopy C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training\2018\data\* /Q /Y || exit /b 666
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>if training == training2018 C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\ESP\WIN64\test\template_avl || set err4=1
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>if training == training2018 bash.exe -x -e -c "for i in `ls wing*.csm | sort -f`; do time python runAll.py $i; done" || set err4=1
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>REM Don't run examples because matplotlib actually plots, but nobody is there to close the window
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>REM if training==training2018 bash.exe -x -e -c "for i in `ls exercise*.py | sort -f`; do time python $i; done" || set err4=1
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>set err1=0
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>set err2=0
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>set err3=0
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>if CAPS == OpenCSM (if NOT training == pyOCSM (
set /p err1= 0<err1_tmp.out
set /p err2= 0<err2_tmp.out
if "" == "" (set /p err3= 0<err3_tmp.out ) else (set err3=0 )
) )
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>echo off
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>set /a "err=0+0+0+0"
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\training>exit /b 0
C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017\CAPS\aim\skeleton>exit 0
[GNU C Compiler (gcc)] Sleeping for 5 seconds due to JENKINS-32191...
[GNU C Compiler (gcc)] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017')
[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 mining
[Clang (LLVM based)] Sleeping for 5 seconds due to JENKINS-32191...
[Clang (LLVM based)] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\training\WIN64.2017')
[Clang (LLVM based)] Successfully parsed console log
[Clang (LLVM based)] -> found 0 issues (skipped 0 duplicates)
[Clang (LLVM based)] Skipping post processing
[Clang (LLVM based)] No filter has been set, publishing all 0 issues
[Clang (LLVM based)] Repository miner is not configured, skipping mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.4,WIN64.2017,windows10x64)
[Static Analysis] Using reference build 'ESP_QuickTestCaps/CASREV=7.4,ESP_ARCH=WIN64.2017,buildnode=windows10x64 #23' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality QualityGate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_QuickTestCaps/CASREV=7.4,ESP_ARCH=WIN64.2017,buildnode=windows10x64 #24'.
[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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