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The Jenkins Controller is preparing for shutdown. No new builds can be started.
Skipping 993 KB.. Full Log Body 48 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 49] rotatex: 135.00000 0.00000 0.00000
Body 49 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 50] translate: 2.00000 1.00000 1.00000
Body 50 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 51] udprim: naca Thickness 0.12000 Camber -0.04000 sharpte 0.00000 (compiled code)
Body 51 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 52] rotatex: 135.00000 0.00000 0.00000
Body 52 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 53] translate: 2.00000 0.00000 0.00000
Body 53 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 54] udprim: naca Thickness 0.12000 Camber -0.04000 sharpte 0.00000 (compiled code)
Body 54 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 55] rotatex: 45.00000 0.00000 0.00000
Body 55 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 56] translate: 2.00000 -1.00000 1.00000
Body 56 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 57] udprim: naca Thickness 0.12000 Camber -0.04000 sharpte 0.00000 (compiled code)
Body 57 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 58] rotatex: 45.00000 0.00000 0.00000
Body 58 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 59] translate: 2.00000 0.00000 0.00000
. Body 59 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
finalizing:
==> Profile information
Branch type ncall time (sec) pct
box 18 0.019 0.2
udprim 39 0.244 2.7
extrude 6 0.048 0.5
intersect 6 8.345 93.3
subtract 12 0.166 1.9
translate 45 0.059 0.7
rotatex 33 0.039 0.4
rotatey 6 0.007 0.1
rotatez 12 0.015 0.2
Total 177 8.942
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Error: Only one of numSpanTotal and numSpanPerSection can be non-zero!
numSpanTotal = 24
numSpanPerSection = 12
Error: Premature exit in get_vlmSurface, status = -311
Error: Premature exit in AVL preAnalysis() status = -311
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
************************************************************
Error: numSpan is depricated.
Please use numSpanTotal or numSpanPerSection instead.
************************************************************
Error: Premature exit in get_vlmSurface, status = -311
Error: Premature exit in AVL preAnalysis() status = -311
Analysis object with the name, avlAIM, has already been initilized
('An altName of', 'avlAIM_4', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Writing surface - VTail1 (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 2)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
('An altName of', 'avlAIM_5', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Running avl......
. Cleaning up avlInstance - 0
Cleaning up avlInstance - 1
Cleaning up avlInstance - 2
Cleaning up avlInstance - 3
Cleaning up avlInstance - 4
Cleaning up avlInstance - 5
EGADS Info: 82 Objects, 103 Reference in Use (of 3382) at Close!
EGADS Info: 5 unattached Objects (103 References) removed!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
Analysis directory does not currently exist - it will be made automatically
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
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] set: cmean sqrt(area/aspect)
cmean = 2.82843 0.00000
executing [ 2] set: span cmean*aspect
span = 14.14214 0.00000
executing [ 3] set: sspan span/2
sspan = 7.07107 0.00000
executing [ 4] set: croot 2*cmean/(1+taper)
croot = 3.77124 0.00000
executing [ 5] set: ctip croot*taper
ctip = 1.88562 0.00000
executing [ 6] set: xtip sspan*tand(lesweep)
xtip = 4.08248 0.00000
executing [ 7] set: ytip sspan*tand(dihedral)
ytip = 0.12343 0.00000
executing [ 8] set: ybot -0.1*croot
ybot = -0.37712 0.00000
executing [ 9] set: ytop +0.2*croot+ytip
ytop = 0.87767 0.00000
executing [ 10] set: extend 0.02*cmean
extend = 0.05657 0.00000
executing [ 11] mark:
Mark created
executing [ 12] udprim: naca Series 8412.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 13] scale: 3.77124 0.00000 0.00000 0.00000
Body 2 created (toler= 3.7712e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 14] udprim: naca Series 20.00000 (compiled code)
Body 3 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 15] scale: 1.88562 0.00000 0.00000 0.00000
Body 4 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 16] rotatez: -15.00000 0.00000 0.00000
Body 5 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 17] translate: 4.08248 0.12343 -7.07107
Body 6 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 18] rule: 0.00000 0.00000
ruling 2 Xsects with 3 Strips each...
Body 7 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 19] store: HalfWing 0.00000 0.00000
Body 7 stored
executing [ 20] restore: HalfWing 0.00000
Body 8 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 21] restore: HalfWing 0.00000
Body 9 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 22] mirror: 0.00000 0.00000 1.00000 0.00000
Body 10 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 23] join: 0.00000 0.00000
Body 11 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 24] rotatex: 90.00000 0.00000 0.00000
Body 12 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 25] store: Wing 0.00000 0.00000
Body 12 stored
executing [ 26] restore: Wing 0.00000
Body 13 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 27] restore: Wing 0.00000
Body 14 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 28] scale: 0.40000 0.00000 0.00000 0.00000
Body 15 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 29] translate: 10.00000 0.00000 0.00000
Body 16 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 30] sphere: 0.00000 0.00000 0.00000 80.00000
Body 17 created (toler= 1.0000e-05, nnode= 2, nedge= 6, nface= 2)
finalizing:
==> Profile information
Branch type ncall time (sec) pct
sphere 1 0.002 0.6
udprim 2 0.016 4.0
restore 4 0.003 0.7
rule 1 0.061 15.5
join 1 0.081 20.5
translate 2 0.072 18.3
rotatex 1 0.068 17.2
rotatez 1 0.001 0.3
scale 3 0.071 18.1
mirror 1 0.019 4.9
set 10 0.000 0.0
store 2 0.000 0.0
mark 1 0.000 0.0
Total 30 0.394
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Tessellating body
Number of nodes = 9617
Number of elements = 19230
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19230
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 3)
Tessellating body
Number of nodes = 6090
Number of elements = 12176
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 12176
Number of quadrilateral elements = 0
Getting surface mesh for body 3 (of 3)
Tessellating body
Number of nodes = 108
Number of elements = 212
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 212
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 15815
Total number of elements = 31618
.Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] set: cmean sqrt(area/aspect)
cmean = 2.82843 0.00000
executing [ 2] set: span cmean*aspect
span = 14.14214 0.00000
executing [ 3] set: sspan span/2
sspan = 7.07107 0.00000
executing [ 4] set: croot 2*cmean/(1+taper)
croot = 3.77124 0.00000
executing [ 5] set: ctip croot*taper
ctip = 1.88562 0.00000
executing [ 6] set: xtip sspan*tand(lesweep)
xtip = 4.08248 0.00000
executing [ 7] set: ytip sspan*tand(dihedral)
ytip = 0.12343 0.00000
executing [ 8] set: ybot -0.1*croot
ybot = -0.37712 0.00000
executing [ 9] set: ytop +0.2*croot+ytip
ytop = 0.87767 0.00000
executing [ 10] set: extend 0.02*cmean
extend = 0.05657 0.00000
executing [ 11] mark:
Mark created
executing [ 12] udprim: naca Series 8412.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 13] scale: 3.77124 0.00000 0.00000 0.00000
Body 2 created (toler= 3.7712e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 14] udprim: naca Series 20.00000 (compiled code)
Body 3 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 15] scale: 1.88562 0.00000 0.00000 0.00000
Body 4 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 16] rotatez: -15.00000 0.00000 0.00000
Body 5 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 17] translate: 4.08248 0.12343 -7.07107
Body 6 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 18] rule: 0.00000 0.00000
ruling 2 Xsects with 3 Strips each...
Body 7 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 19] store: HalfWing 0.00000 0.00000
Body 7 stored
executing [ 20] restore: HalfWing 0.00000
Body 8 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 21] restore: HalfWing 0.00000
Body 9 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 22] mirror: 0.00000 0.00000 1.00000 0.00000
Body 10 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 23] join: 0.00000 0.00000
Body 11 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 24] rotatex: 90.00000 0.00000 0.00000
Body 12 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 25] store: Wing 0.00000 0.00000
Body 12 stored
executing [ 26] box: -40.00000 -40.00000 -40.00000 80.00000 80.00000 80.00000
Body 13 created (toler= 1.0000e-07, nnode= 8, nedge= 12, nface= 6)
executing [ 27] restore: Wing 0.00000
Body 14 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 28] subtract: none 1.00000 0.0000e+00
Body 15 created (toler= 1.0000e-07, nnode= 17, nedge= 27, nface= 14)
executing [ 29] select: body
putting Branch Attributes on Body
finalizing:
==> Profile information
Branch type ncall time (sec) pct
box 1 0.001 0.3
udprim 2 0.014 3.9
restore 3 0.002 0.6
rule 1 0.064 17.7
subtract 1 0.103 28.4
join 1 0.086 23.8
translate 1 0.001 0.3
rotatex 1 0.065 17.8
rotatez 1 0.001 0.3
scale 2 0.003 0.8
mirror 1 0.022 6.1
set 10 0.000 0.1
select 1 0.000 0.0
store 2 0.000 0.0
mark 1 0.000 0.0
Total 29 0.363
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Tessellating body
Number of nodes = 9629
Number of elements = 19250
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19250
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9629
Total number of elements = 19250
.Analysis directory does not currently exist - it will be made automatically
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
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] set: meshingAIMs $pointwiseAIM;aflr4AIM;egadsTessAIM
meshingAIMs = $pointwiseAIM;aflr4AIM;egadsTessAIM
executing [ 2] box: 0.00000 -0.50000 -0.50000 1.00000 1.00000 1.00000
Body 1 created (toler= 1.0000e-07, nnode= 8, nedge= 12, nface= 6)
executing [ 3] select: edge 1
putting Branch Attributes on Edge 1
executing [ 4] box: 2.00000 0.00000 0.00000 1.00000 0.00000 0.50000
Body 2 created (toler= 1.0000e-07, nnode= 4, nedge= 4, nface= 1)
executing [ 5] revolve: 2.00000 0.00000 0.00000 1.00000 0.00000 0.00000 360.00000
WARNING:: jbody= 2, jnode= 1, ibody= 3, found= 1, dbest= 0.500000000 (revolve)
WARNING:: jbody= 2, jnode= 2, ibody= 3, found= 2, dbest= 0.500000000 (revolve)
Body 3 created (toler= 1.0000e-07, nnode= 2, nedge= 3, nface= 3)
executing [ 6] cone: 4.00000 0.00000 0.00000 5.00000 0.00000 0.00000 0.50000
Body 4 created (toler= 1.0000e-05, nnode= 3, nedge= 6, nface= 3)
executing [ 7] skbeg: 7.00000 0.00000 0.00000 0.00000
executing [ 8] linseg: 7.25000 0.00000 0.00000
executing [ 9] skend: 0.00000
Sketch 7 created with 1 Edges
executing [ 10] revolve: 7.00000 0.00000 0.00000 0.00000 1.00000 0.00000 360.00000
WARNING:: jbody= 7, jnode= 1, ibody= 8, found= 1, dbest= 0.250000000 (revolve)
Body 8 created (toler= 1.0000e-07, nnode= 1, nedge= 1, nface= 1)
executing [ 11] revolve: 6.50000 0.00000 0.00000 0.00000 0.00000 1.00000 360.00000
Body 9 created (toler= 1.0000e-07, nnode= 1, nedge= 2, nface= 1)
executing [ 12] select: edge 1
putting Branch Attributes on Edge 1
executing [ 13] select: edge 2
putting Branch Attributes on Edge 2
executing [ 14] sphere: 8.50000 0.00000 0.00000 0.50000
Body 10 created (toler= 1.0000e-05, nnode= 2, nedge= 6, nface= 2)
executing [ 15] box: 10.00000 -0.50000 -0.50000 1.00000 1.00000 1.00000
Body 11 created (toler= 1.0000e-07, nnode= 8, nedge= 12, nface= 6)
executing [ 16] cylinder: 10.50000 0.00000 -1.00000 10.50000 0.00000 1.00000 0.25000
Body 12 created (toler= 1.0000e-05, nnode= 4, nedge= 6, nface= 4)
executing [ 17] subtract: none 1.00000 0.0000e+00
Body 13 created (toler= 1.0000e-05, nnode= 12, nedge= 18, nface= 8)
executing [ 18] box: 10.50000 0.00000 -1.00000 1.00000 0.00000 2.00000
Body 14 created (toler= 1.0000e-07, nnode= 4, nedge= 4, nface= 1)
executing [ 19] subtract: none 1.00000 0.0000e+00
Body 15 created (toler= 1.0000e-05, nnode= 14, nedge= 23, nface= 9)
executing [ 20] select: body
putting Branch Attributes on Body
executing [ 21] select: face
putting Branch Attributes on Face 1
putting Branch Attributes on Face 2
putting Branch Attributes on Face 3
putting Branch Attributes on Face 4
putting Branch Attributes on Face 5
putting Branch Attributes on Face 6
putting Branch Attributes on Face 7
putting Branch Attributes on Face 8
putting Branch Attributes on Face 9
executing [ 22] set: fs:radius 0.5
fs:radius = 0.50000 0.00000
executing [ 23] set: fs:nose:radius 0.25
fs:nose:radius = 0.25000 0.00000
executing [ 24] set: fs:nose:ogive_radius 10.0
fs:nose:ogive_radius = 10.00000 0.00000
executing [ 25] skbeg: 12.00000 0.00000 0.00000 1.00000
executing [ 26] skvar: xy 0.00000 0.00000 0.00000 ...
-> creating ::x[1] = 0.00000
-> creating ::y[1] = 0.00000
-> creating ::x[2] = 0.07000
-> creating ::y[2] = -0.12000
-> creating ::d[2] = 0.02000
-> creating ::x[3] = 1.00000
-> creating ::y[3] = -0.50000
-> creating ::d[3] = 0.09000
-> creating ::x[4] = 1.00000
-> creating ::y[4] = 0.00000
executing [ 27] skcon: X 1 -1 0
executing [ 28] skcon: Y 1 -1 0
executing [ 29] skcon: P 1 -1 0
executing [ 30] skcon: R 1 2 fs:nose:radius
executing [ 31] skcon: T 2 -1 0
executing [ 32] skcon: R 2 3 fs:nose:ogive_radius
executing [ 33] skcon: V 3 4 0
executing [ 34] skcon: P 4 -1 0
executing [ 35] skcon: L 3 4 fs:radius
executing [ 36] skcon: H 4 1 0
-> solving iter = 0, f0max = 8.5532e+00 accepting, omega= 0.30000
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:46965)
trying Levenberg-Marquardt solver
-> solving iter = 0, f0max = 8.5532e+00
-> solving iter = 1, f0max = 1.6117e+01
-> solving iter = 2, f0max = 1.7448e+01
-> solving iter = 3, f0max = 1.9375e+01
-> solving iter = 4, f0max = 2.2607e+01
-> solving iter = 5, f0max = 3.0533e+01
-> solving iter = 6, f0max = 1.0148e+02
-> solving iter = 7, f0max = 1.6544e+01
-> solving iter = 8, f0max = 2.5075e-01
-> solving iter = 9, f0max = 2.3231e-01
-> solving iter = 10, f0max = 2.0847e-01
-> solving iter = 11, f0max = 1.8155e-01
-> solving iter = 12, f0max = 1.5222e-01
-> solving iter = 13, f0max = 1.2009e-01
-> solving iter = 14, f0max = 9.7602e-02
-> solving iter = 15, f0max = 6.4364e-02
-> solving iter = 16, f0max = 4.0512e-02
-> solving iter = 17, f0max = 2.1157e-02
-> solving iter = 18, f0max = 7.5481e-03
-> solving iter = 19, f0max = 1.7629e-03
-> solving iter = 20, f0max = 2.3639e-04
-> solving iter = 21, f0max = 1.6881e-05
-> solving iter = 22, f0max = 6.2000e-07
-> solving iter = 23, f0max = 1.1572e-08
-> solving iter = 24, f0max = 1.0905e-10
-> updating ::x[1] = -0.00000
-> updating ::y[1] = 0.00000
-> updating ::x[2] = 0.18062
-> updating ::y[2] = -0.24018
-> updating ::d[2] = 0.05019
-> updating ::x[3] = 1.33041
-> updating ::y[3] = -0.50000
-> updating ::d[3] = 0.01738
-> updating ::x[4] = 1.33041
-> updating ::y[4] = -0.00000
executing [ 37] arc: 0.18062 -0.24018 0.00000 0.05019 xy
executing [ 38] arc: 1.33041 -0.50000 0.00000 0.01738 xy
executing [ 39] linseg: 1.33041 -0.00000 0.00000
executing [ 40] linseg: -0.00000 0.00000 0.00000
executing [ 41] skend: 0.00000
Sketch 21 created with 4 Edges
executing [ 42] revolve: 0.00000 0.00000 0.00000 1.00000 0.00000 0.00000 360.00000
WARNING:: jbody=21, jnode= 4, ibody=22, found= 3, dbest= 0.500000000 (revolve)
Body 22 created (toler= 1.0000e-07, nnode= 3, nedge= 5, nface= 3)
executing [ 43] select: body
putting Branch Attributes on Body
executing [ 44] select: face
putting Branch Attributes on Face 1
putting Branch Attributes on Face 2
putting Branch Attributes on Face 3
executing [ 45] box: -1.00000 -2.00000 -2.00000 15.00000 4.00000 4.00000
Body 23 created (toler= 1.0000e-07, nnode= 8, nedge= 12, nface= 6)
finalizing:
==> Profile information
Branch type ncall time (sec) pct
box 5 0.005 2.5
sphere 1 0.002 1.1
cone 1 0.002 1.1
cylinder 1 0.003 1.6
revolve 4 0.030 14.8
subtract 2 0.143 69.8
skbeg 2 0.000 0.0
skvar 1 0.000 0.1
skcon 10 0.000 0.0
linseg 3 0.000 0.0
arc 2 0.000 0.0
skend 2 0.002 0.9
set 4 0.000 0.0
select 7 0.016 7.9
Total 45 0.204
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 8)
Tessellating body
Number of nodes = 1538
Number of elements = 3072
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 8)
Tessellating body
Number of nodes = 906
Number of elements = 1808
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1808
Number of quadrilateral elements = 0
Getting surface mesh for body 3 (of 8)
Tessellating body
Number of nodes = 1332
Number of elements = 2660
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2660
Number of quadrilateral elements = 0
Getting surface mesh for body 4 (of 8)
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
Number of nodes = 2048
Number of elements = 4096
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Getting surface mesh for body 5 (of 8)
Tessellating body
Number of nodes = 847
Number of elements = 1690
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1690
Number of quadrilateral elements = 0
Getting surface mesh for body 6 (of 8)
Tessellating body
70000D065000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
70000D065000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FFF9744A380 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FFF9744A380 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Number of nodes = 1958
Number of elements = 3916
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3916
Number of quadrilateral elements = 0
Getting surface mesh for body 7 (of 8)
Tessellating body
Number of nodes = 946
Number of elements = 1888
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1888
Number of quadrilateral elements = 0
Getting surface mesh for body 8 (of 8)
Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 83305
Total number of elements = 166586
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_1', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Tessellating body
Number of nodes = 1538
Number of elements = 3072
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75268
Total number of elements = 150528
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_2', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Tessellating body
70000D065000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
70000D065000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FFF9744A380 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FFF9744A380 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Number of nodes = 1958
Number of elements = 3916
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3916
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75688
Total number of elements = 151372
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_3', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Tessellating body
Number of nodes = 946
Number of elements = 1888
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1888
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74676
Total number of elements = 149344
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_4', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Tessellating body
Number of nodes = 1332
Number of elements = 2660
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2660
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75062
Total number of elements = 150116
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_5', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Tessellating body
Number of nodes = 906
Number of elements = 1808
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1808
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74636
Total number of elements = 149264
.Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] set: cmean sqrt(area/aspect)
cmean = 2.82843 0.00000
executing [ 2] set: span cmean*aspect
span = 14.14214 0.00000
executing [ 3] set: sspan span/2
sspan = 7.07107 0.00000
executing [ 4] set: croot 2*cmean/(1+taper)
croot = 3.77124 0.00000
executing [ 5] set: ctip croot*taper
ctip = 1.88562 0.00000
executing [ 6] set: xtip sspan*tand(lesweep)
xtip = 4.08248 0.00000
executing [ 7] set: ytip sspan*tand(dihedral)
ytip = 0.12343 0.00000
executing [ 8] set: ybot -0.1*croot
ybot = -0.37712 0.00000
executing [ 9] set: ytop +0.2*croot+ytip
ytop = 0.87767 0.00000
executing [ 10] set: extend 0.02*cmean
extend = 0.05657 0.00000
executing [ 11] mark:
Mark created
executing [ 12] udprim: naca Series 8412.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 13] scale: 3.77124 0.00000 0.00000 0.00000
Body 2 created (toler= 3.7712e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 14] udprim: naca Series 20.00000 (compiled code)
Body 3 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 15] scale: 1.88562 0.00000 0.00000 0.00000
Body 4 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 16] rotatez: -15.00000 0.00000 0.00000
Body 5 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 17] translate: 4.08248 0.12343 -7.07107
Body 6 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 18] rule: 0.00000 0.00000
ruling 2 Xsects with 3 Strips each...
Body 7 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 19] store: HalfWing 0.00000 0.00000
Body 7 stored
executing [ 20] restore: HalfWing 0.00000
Body 8 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 21] restore: HalfWing 0.00000
Body 9 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 22] mirror: 0.00000 0.00000 1.00000 0.00000
Body 10 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 23] join: 0.00000 0.00000
Body 11 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 24] rotatex: 90.00000 0.00000 0.00000
Body 12 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 25] store: Wing 0.00000 0.00000
Body 12 stored
executing [ 26] box: -40.00000 -40.00000 -40.00000 80.00000 80.00000 80.00000
Body 13 created (toler= 1.0000e-07, nnode= 8, nedge= 12, nface= 6)
executing [ 27] restore: Wing 0.00000
Body 14 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 28] subtract: none 1.00000 0.0000e+00
Body 15 created (toler= 1.0000e-07, nnode= 17, nedge= 27, nface= 14)
executing [ 29] select: body
putting Branch Attributes on Body
finalizing:
==> Profile information
Branch type ncall time (sec) pct
box 1 0.001 0.4
udprim 2 0.013 4.1
restore 3 0.002 0.6
rule 1 0.053 16.4
subtract 1 0.101 31.3
join 1 0.073 22.5
translate 1 0.002 0.5
rotatex 1 0.057 17.7
rotatez 1 0.001 0.3
scale 2 0.002 0.6
mirror 1 0.017 5.3
set 10 0.000 0.1
select 1 0.000 0.0
store 2 0.000 0.0
mark 1 0.000 0.0
Total 29 0.324
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
**********************************************************
Mesh_Length_Factor is: -1.000000
Mesh_Length_Factor must be a positive number.
**********************************************************
Error: egadsTessAIM (instance = 0) status -311
.Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] set: cmean sqrt(area/aspect)
cmean = 2.82843 0.00000
executing [ 2] set: span cmean*aspect
span = 14.14214 0.00000
executing [ 3] set: sspan span/2
sspan = 7.07107 0.00000
executing [ 4] set: croot 2*cmean/(1+taper)
croot = 3.77124 0.00000
executing [ 5] set: ctip croot*taper
ctip = 1.88562 0.00000
executing [ 6] set: xtip sspan*tand(lesweep)
xtip = 4.08248 0.00000
executing [ 7] set: ytip sspan*tand(dihedral)
ytip = 0.12343 0.00000
executing [ 8] set: ybot -0.1*croot
ybot = -0.37712 0.00000
executing [ 9] set: ytop +0.2*croot+ytip
ytop = 0.87767 0.00000
executing [ 10] set: extend 0.02*cmean
extend = 0.05657 0.00000
executing [ 11] mark:
Mark created
executing [ 12] udprim: naca Series 8412.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 13] scale: 3.77124 0.00000 0.00000 0.00000
Body 2 created (toler= 3.7712e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 14] udprim: naca Series 20.00000 (compiled code)
Body 3 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 15] scale: 1.88562 0.00000 0.00000 0.00000
Body 4 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 16] rotatez: -15.00000 0.00000 0.00000
Body 5 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 17] translate: 4.08248 0.12343 -7.07107
Body 6 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 18] rule: 0.00000 0.00000
ruling 2 Xsects with 3 Strips each...
Body 7 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 19] store: HalfWing 0.00000 0.00000
Body 7 stored
executing [ 20] restore: HalfWing 0.00000
Body 8 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 21] restore: HalfWing 0.00000
Body 9 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 22] mirror: 0.00000 0.00000 1.00000 0.00000
Body 10 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 23] join: 0.00000 0.00000
Body 11 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 24] rotatex: 90.00000 0.00000 0.00000
Body 12 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 25] store: Wing 0.00000 0.00000
Body 12 stored
executing [ 26] box: -40.00000 -40.00000 -40.00000 80.00000 80.00000 80.00000
Body 13 created (toler= 1.0000e-07, nnode= 8, nedge= 12, nface= 6)
executing [ 27] restore: Wing 0.00000
Body 14 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 28] subtract: none 1.00000 0.0000e+00
Body 15 created (toler= 1.0000e-07, nnode= 17, nedge= 27, nface= 14)
executing [ 29] select: body
putting Branch Attributes on Body
finalizing:
==> Profile information
Branch type ncall time (sec) pct
box 1 0.001 0.2
udprim 2 0.012 3.4
restore 3 0.002 0.5
rule 1 0.052 14.7
subtract 1 0.137 38.6
join 1 0.073 20.5
translate 1 0.001 0.4
rotatex 1 0.056 15.8
rotatez 1 0.001 0.3
scale 2 0.002 0.6
mirror 1 0.017 4.8
set 10 0.000 0.1
select 1 0.000 0.0
store 2 0.000 0.0
mark 1 0.000 0.0
Total 29 0.355
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Tessellating body
Number of nodes = 9629
Number of elements = 19250
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19250
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9629
Total number of elements = 19250
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Tessellating body
Number of nodes = 7146
Number of elements = 14284
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 14284
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7146
Total number of elements = 14284
.Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_6', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Tessellating body
Number of nodes = 847
Number of elements = 1690
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1690
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74577
Total number of elements = 149146
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_7', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
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
Number of nodes = 2048
Number of elements = 4096
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75778
Total number of elements = 151552
. Cleaning up egadsInstance - 0
Cleaning up egadsInstance - 1
Cleaning up egadsInstance - 2
Cleaning up egadsInstance - 3
Cleaning up egadsInstance - 4
Cleaning up egadsInstance - 5
Cleaning up egadsInstance - 6
Cleaning up egadsInstance - 7
EGADS Info: 0 Objects, 0 Reference in Use (of 1494) at Close!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
Analysis directory does not currently exist - it will be made automatically
CAPS Info: No symbol for aimExecute in fun3dAIM
CAPS Info: No symbol for aimCheck in fun3dAIM
CAPS Info: No symbol for aimData in fun3dAIM
CAPS Info: No symbol for aimSensitivity in fun3dAIM
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_1', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] set: cmean sqrt(area/aspect)
cmean = 2.82843 0.00000
executing [ 2] set: span cmean*aspect
span = 14.14214 0.00000
executing [ 3] set: sspan span/2
sspan = 7.07107 0.00000
executing [ 4] set: croot 2*cmean/(1+taper)
croot = 3.77124 0.00000
executing [ 5] set: ctip croot*taper
ctip = 1.88562 0.00000
executing [ 6] set: xtip sspan*tand(lesweep)
xtip = 4.08248 0.00000
executing [ 7] set: ytip sspan*tand(dihedral)
ytip = 0.12343 0.00000
executing [ 8] set: ybot -0.1*croot
ybot = -0.37712 0.00000
executing [ 9] set: ytop +0.2*croot+ytip
ytop = 0.87767 0.00000
executing [ 10] set: extend 0.02*cmean
extend = 0.05657 0.00000
executing [ 11] mark:
Mark created
executing [ 12] udprim: naca Series 8412.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 13] scale: 3.77124 0.00000 0.00000 0.00000
Body 2 created (toler= 3.7712e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 14] udprim: naca Series 20.00000 (compiled code)
Body 3 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 15] scale: 1.88562 0.00000 0.00000 0.00000
Body 4 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 16] rotatez: -15.00000 0.00000 0.00000
Body 5 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 17] translate: 4.08248 0.12343 -7.07107
Body 6 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 18] rule: 0.00000 0.00000
ruling 2 Xsects with 3 Strips each...
Body 7 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 19] store: HalfWing 0.00000 0.00000
Body 7 stored
executing [ 20] restore: HalfWing 0.00000
Body 8 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 21] restore: HalfWing 0.00000
Body 9 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 22] mirror: 0.00000 0.00000 1.00000 0.00000
Body 10 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 23] join: 0.00000 0.00000
Body 11 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 24] rotatex: 90.00000 0.00000 0.00000
Body 12 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 25] store: Wing 0.00000 0.00000
Body 12 stored
executing [ 26] restore: Wing 0.00000
Body 13 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 27] restore: Wing 0.00000
Body 14 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 28] scale: 0.40000 0.00000 0.00000 0.00000
Body 15 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 29] translate: 10.00000 0.00000 0.00000
Body 16 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 30] sphere: 0.00000 0.00000 0.00000 80.00000
Body 17 created (toler= 1.0000e-05, nnode= 2, nedge= 6, nface= 2)
finalizing:
==> Profile information
Branch type ncall time (sec) pct
sphere 1 0.003 0.8
udprim 2 0.013 3.6
restore 4 0.003 0.9
rule 1 0.067 17.8
join 1 0.073 19.5
translate 2 0.060 16.1
rotatex 1 0.057 15.2
rotatez 1 0.001 0.3
scale 3 0.066 17.6
mirror 1 0.030 8.1
set 10 0.000 0.1
store 2 0.000 0.0
mark 1 0.000 0.0
Total 30 0.374
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Warning: No boundary condition specified for capsGroup Wing2!
Warning: No boundary condition specified for capsGroup Farfield!
Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Using Python to write FUN3D namelist (fun3d.nml)
Reading fun3d.nml .....
Appending namelist
Done writing nml file with Python
.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_2', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Warning: No boundary condition specified for capsGroup Wing2!
Warning: No boundary condition specified for capsGroup Farfield!
Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Using Python to write FUN3D namelist (fun3d.nml)
Reading fun3d.nml .....
Traceback (most recent call last):
File "fun3dNamelist.pyx", line 88, in fun3dNamelist.fun3d_writeNMLPython
Error: Python error occurred while writing namelist file
File "fun3dNamelist.pyx", line 61, in fun3dNamelist.read_fun3d_nml
File "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP_venv/lib/python3.7/site-packages/f90nml/__init__.py", line 31, in read
return parser.read(nml_path)
File "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP_venv/lib/python3.7/site-packages/f90nml/parser.py", line 264, in read
return self._readstream(nml_file, nml_patch)
File "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP_venv/lib/python3.7/site-packages/f90nml/parser.py", line 352, in _readstream
self._update_tokens()
File "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP_venv/lib/python3.7/site-packages/f90nml/parser.py", line 761, in _update_tokens
next_token = next(self.tokens)
StopIteration
Premature exit in fun3dAIM preAnalysis status = -311
.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_3', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Warning: No boundary condition specified for capsGroup Wing2!
Warning: No boundary condition specified for capsGroup Farfield!
Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Using Python to write FUN3D namelist (fun3d.nml)
fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Getting CFD boundary conditions
Boundary condition name - Wing1
Warning: No boundary condition specified for capsGroup Wing2!
Warning: No boundary condition specified for capsGroup Farfield!
Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Using Python to write FUN3D namelist (fun3d.nml)
Reading fun3d.nml .....
Appending namelist
Done writing nml file with Python
.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_4', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Python library was linked, but will not be used!
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Unrecognized "bcType" specified ("X") for Boundary_Condition tuple Wing1, current options (not all options are valid for this analysis tool - see AIM documentation) are " Inviscid, Viscous, Farfield, Extrapolate, Freestream, BackPressure, Symmetry, SubsonicInflow, SubsonicOutflow, MassflowIn, MassflowOut, MachOutflow, FixedInflow, FixedOutflow"
Premature exit in fun3dAIM preAnalysis status = -303
.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_5', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Python library was linked, but will not be used!
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Boundary condition name - X
BC name "X" not found in attrMap
Premature exit in fun3dAIM preAnalysis status = -303
.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_6', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Python library was linked, but will not be used!
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Warning: No boundary condition specified for capsGroup Wing2!
Warning: No boundary condition specified for capsGroup Farfield!
Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
.Python library was linked, but will not be used!
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Boundary condition name - Wing2
Boundary condition name - Farfield
Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Python library was linked, but will not be used!
Getting CFD boundary conditions
Boundary condition name - Wing1
Boundary condition name - Wing2
Boundary condition name - Farfield
Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
.Analysis directory does not currently exist - it will be made automatically
CAPS Info: No symbol for aimDiscr in aflr4AIM
CAPS Info: No symbol for aimFreeDiscr in aflr4AIM
CAPS Info: No symbol for aimLocateElement in aflr4AIM
CAPS Info: No symbol for aimUsesDataSet in aflr4AIM
CAPS Info: No symbol for aimCheck in aflr4AIM
CAPS Info: No symbol for aimTransfer in aflr4AIM
CAPS Info: No symbol for aimInterpolation in aflr4AIM
CAPS Info: No symbol for aimInterpolateBar in aflr4AIM
CAPS Info: No symbol for aimIntegration in aflr4AIM
CAPS Info: No symbol for aimIntegrateBar in aflr4AIM
CAPS Info: No symbol for aimSensitivity in aflr4AIM
CAPS Info: No symbol for aimDiscr in aflr3AIM
CAPS Info: No symbol for aimFreeDiscr in aflr3AIM
CAPS Info: No symbol for aimLocateElement in aflr3AIM
CAPS Info: No symbol for aimUsesDataSet in aflr3AIM
CAPS Info: No symbol for aimCheck in aflr3AIM
CAPS Info: No symbol for aimTransfer in aflr3AIM
CAPS Info: No symbol for aimInterpolation in aflr3AIM
CAPS Info: No symbol for aimInterpolateBar in aflr3AIM
CAPS Info: No symbol for aimIntegration in aflr3AIM
CAPS Info: No symbol for aimIntegrateBar in aflr3AIM
CAPS Info: No symbol for aimSensitivity in aflr3AIM
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_7', 'will be used!')
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
EGADS : EGADS CAD Geometry Setup
EGADS : Using EGADS Version 1.19
EGADS : Using OpenCASCADE Version ase with OpenCASCADE 7.4.1
EGADS : Model has 3 Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 BRep Shells
EGADS : Body 0 has 8 BRep Faces
EGADS : Body 0 has 15 BRep Edges
EGADS : Body 0 has 9 BRep Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 BRep Shells
EGADS : Body 1 has 8 BRep Faces
EGADS : Body 1 has 15 BRep Edges
EGADS : Body 1 has 9 BRep Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 BRep Shells
EGADS : Body 2 has 2 BRep Faces
EGADS : Body 2 has 6 BRep Edges
EGADS : Body 2 has 2 BRep Nodes
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 160
AFLR4 : Min Bounding Box Length = 160
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 56.5685
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 15.8264
AFLR4 : Abs Min Surf Spacing = 0.141421
AFLR4 : Min Surf Spacing = 0.282843
AFLR4 : Max Surf Spacing = 5.65685
AFLR4 : Check Grid BCs
AFLR4 : Grid BCs are OK
AFLR4 : Geometry Definition Information
AFLR4 : IER = Isolated Edge Refinement
AFLR4 : ER = Edge Refinement
AFLR4 : Definition Definition Composite Grid BC IER ER Scale
AFLR4 : ID Type ID Type Flag Weight Factor
AFLR4 : 0 glue-only composite - - - - -
AFLR4 : 1 CAD geometry 0 STD w/BL 1 1 1
AFLR4 : 2 CAD geometry 0 STD w/BL 1 1 1
AFLR4 : 3 CAD geometry 0 STD w/BL 1 1 1
AFLR4 : 4 CAD geometry 0 STD w/BL 1 1 1
AFLR4 : 5 CAD geometry 0 STD w/BL 1 1 1
AFLR4 : 6 CAD geometry 0 STD w/BL 1 1 1
AFLR4 : 7 CAD geometry 0 STD w/BL 1 1 1
AFLR4 : 8 CAD geometry 0 STD w/BL 1 1 1
AFLR4 : 9 CAD geometry 0 STD w/BL 1 0 10
AFLR4 : 10 CAD geometry 0 STD w/BL 1 0 10
AFLR4 : 11 CAD geometry 0 STD w/BL 1 0 10
AFLR4 : 12 CAD geometry 0 STD w/BL 1 0 10
AFLR4 : 13 CAD geometry 0 STD w/BL 1 0 10
AFLR4 : 14 CAD geometry 0 STD w/BL 1 0 10
AFLR4 : 15 CAD geometry 0 STD w/BL 1 0 10
AFLR4 : 16 CAD geometry 0 STD w/BL 1 0 10
AFLR4 : 17 CAD geometry 0 FARFIELD 1 0 1
AFLR4 : 18 CAD geometry 0 FARFIELD 1 0 1
AFLR4 : Definition Neighbor Map
AFLR4 : Definition Neighbor-Definitions
AFLR4 : 1 3 5 2 4
AFLR4 : 2 1 6 3 4
AFLR4 : 3 1 2 7 4
AFLR4 : 4 1 2 3
AFLR4 : 5 1 7 6 8
AFLR4 : 6 2 5 7 8
AFLR4 : 7 3 5 6 8
AFLR4 : 8 5 6 7
AFLR4 : 9 11 13 10 12
AFLR4 : 10 9 14 11 12
AFLR4 : 11 9 10 15 12
AFLR4 : 12 9 10 11
AFLR4 : 13 9 15 14 16
AFLR4 : 14 10 13 15 16
AFLR4 : 15 11 13 14 16
AFLR4 : 16 13 14 15
AFLR4 : 17 18
AFLR4 : 18 17
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes...
Definition 1 with ID/Label 1
Definition 2 with ID/Label 2
Definition 3 with ID/Label 3
Definition 4 with ID/Label 4
Definition 5 with ID/Label 5
Definition 6 with ID/Label 6
Definition 7 with ID/Label 7
Definition 8 with ID/Label 8
AFLR4 : Component 2 includes...
Definition 9 with ID/Label 9
Definition 10 with ID/Label 10
Definition 11 with ID/Label 11
Definition 12 with ID/Label 12
Definition 13 with ID/Label 13
Definition 14 with ID/Label 14
Definition 15 with ID/Label 15
Definition 16 with ID/Label 16
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 811 1487
AFLR4 : Nodes, Faces = 662 1189
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 808 1483
AFLR4 : Nodes, Faces = 643 1153
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 190 269
AFLR4 : Nodes, Faces = 110 109
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 182 282
AFLR4 : Nodes, Faces = 182 282
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 813 1491
AFLR4 : Nodes, Faces = 662 1189
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 804 1475
AFLR4 : Nodes, Faces = 644 1155
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 190 269
AFLR4 : Nodes, Faces = 110 109
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 182 282
AFLR4 : Nodes, Faces = 182 282
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Faces = 480 859
AFLR4 : Nodes, Faces = 436 771
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Faces = 331 561
AFLR4 : Nodes, Faces = 431 761
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Faces = 161 213
AFLR4 : Nodes, Faces = 108 107
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Faces = 181 280
AFLR4 : Nodes, Faces = 180 278
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Faces = 482 863
AFLR4 : Nodes, Faces = 438 775
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Faces = 290 479
AFLR4 : Nodes, Faces = 442 783
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Faces = 161 213
AFLR4 : Nodes, Faces = 108 107
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Faces = 181 280
AFLR4 : Nodes, Faces = 180 278
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Faces = 80 128
AFLR4 : Nodes, Faces = 183 334
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Faces = 80 128
AFLR4 : Nodes, Faces = 182 332
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes, Faces = 5003 9994
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 5003 9994
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 826 1503
AFLR4 : Nodes, Faces = 811 1473
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 847 1545
AFLR4 : Nodes, Faces = 785 1421
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 233 334
AFLR4 : Nodes, Faces = 130 128
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 180 278
AFLR4 : Nodes, Faces = 192 302
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 818 1487
AFLR4 : Nodes, Faces = 814 1479
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 847 1545
AFLR4 : Nodes, Faces = 786 1423
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 233 334
AFLR4 : Nodes, Faces = 130 128
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 182 282
AFLR4 : Nodes, Faces = 194 306
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Faces = 626 1142
AFLR4 : Nodes, Faces = 608 1106
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Faces = 609 1108
AFLR4 : Nodes, Faces = 597 1084
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Faces = 214 311
AFLR4 : Nodes, Faces = 115 113
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Faces = 182 284
AFLR4 : Nodes, Faces = 187 294
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Faces = 638 1165
AFLR4 : Nodes, Faces = 614 1117
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Faces = 600 1090
AFLR4 : Nodes, Faces = 599 1088
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Faces = 216 314
AFLR4 : Nodes, Faces = 116 114
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Faces = 180 280
AFLR4 : Nodes, Faces = 186 292
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Faces = 73 116
AFLR4 : Nodes, Faces = 180 330
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Faces = 73 116
AFLR4 : Nodes, Faces = 182 334
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes, Faces = 6272 12532
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
OVERALL : CPU Time = 0.247 seconds
AFLR4 : GET EGADS TESS FROM AFLR4 DATA
AFLR4 : EGADS TESS CREATED WITHOUT ERROR
AFLR4 : CHECK COORDINATES OF EGADS TESSELLATION
AFLR4 : CAD Definition= 1 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 2 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 3 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 4 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 5 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 6 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 7 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 8 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 1 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 2 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 3 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 4 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 5 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 6 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 7 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 8 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 1 Max Coordinate Deviation=0.000000e+00
AFLR4 : CAD Definition= 2 Max Coordinate Deviation=0.000000e+00
AFLR4 : COORDINATES OF EGADS TESSELLATION CHECKED WITHOUT ERROR
AFLR4 : CHECK AFLR4 AND EGADS TRIA-FACE ORDERING
AFLR4 : CAD Definition= 1 Ordering OK Reversed
AFLR4 : CAD Definition= 2 Ordering OK Reversed
AFLR4 : CAD Definition= 3 Ordering OK Reversed
AFLR4 : CAD Definition= 4 Ordering OK Reversed
AFLR4 : CAD Definition= 5 Ordering OK
AFLR4 : CAD Definition= 6 Ordering OK
AFLR4 : CAD Definition= 7 Ordering OK
AFLR4 : CAD Definition= 8 Ordering OK
AFLR4 : CAD Definition= 9 Ordering OK Reversed
AFLR4 : CAD Definition= 10 Ordering OK Reversed
AFLR4 : CAD Definition= 11 Ordering OK Reversed
AFLR4 : CAD Definition= 12 Ordering OK Reversed
AFLR4 : CAD Definition= 13 Ordering OK
AFLR4 : CAD Definition= 14 Ordering OK
AFLR4 : CAD Definition= 15 Ordering OK
AFLR4 : CAD Definition= 16 Ordering OK
AFLR4 : CAD Definition= 17 Ordering OK
AFLR4 : CAD Definition= 18 Ordering OK
AFLR4 : AFLR4 AND EGADS TRIA-FACE ORDERING CHECKED WITHOUT ERROR
Body = 1
Number of nodes = 3332
Number of elements = 6660
Number of tris = 6660
Number of quad = 0
Body = 2
Number of nodes = 2606
Number of elements = 5208
Number of tris = 5208
Number of quad = 0
Body = 3
Number of nodes = 334
Number of elements = 664
Number of tris = 664
Number of quad = 0
----------------------------
Total number of nodes = 6272
Total number of elements = 12532
Found link for groupMap (Attribute_Map) from parent
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Found link for a surface mesh (Surface_Mesh) from parent
Number of surface nodes - 6272
Number of surface elements - 12532
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.30.16
AFLR3 : Version Date 10/10/20 @ 03:34PM
AFLR3 : Compile OS Darwin 19.6.0 x86_64
AFLR3 : Compile Date 10/11/20 @ 12:50AM
AFLR3 : Copyright 1994-2020, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 6272 0
AFLR3 : CPU Time = 0.012 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 6272 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1256 7675
AFLR3 IG : Nodes, Elements = 2512 16487
AFLR3 IG : Nodes, Elements = 3768 25117
AFLR3 IG : Nodes, Elements = 5024 34383
AFLR3 IG : Nodes, Elements = 6279 43250
AFLR3 IG : Nodes, Elements = 6279 43173
AFLR3 IG : Nodes, Elements = 6279 43183
AFLR3 IG : Nodes, Elements = 6279 43171
AFLR3 IG : Nodes, Elements = 6279 43170
AFLR3 IG : Nodes, Elements = 6272 25585
AFLR3 IG : Nodes, Elements = 6272 25605
AFLR3 IG : Nodes, Elements = 6272 20878
AFLR3 IG : Nodes, Elements = 6272 18524
AFLR3 : CPU Time = 0.156 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6272 18524
AFLR3 GG : Nodes, Elements = 9141 27351
AFLR3 GG : Nodes, Elements = 9141 39101
AFLR3 GG : Nodes, Elements = 9141 36222
AFLR3 GG : Nodes, Elements = 9141 34761
AFLR3 GG : Nodes, Elements = 11743 42912
AFLR3 GG : Nodes, Elements = 11743 54201
AFLR3 GG : Nodes, Elements = 11743 51098
AFLR3 GG : Nodes, Elements = 11743 50260
AFLR3 GG : Nodes, Elements = 14611 59142
AFLR3 GG : Nodes, Elements = 14611 71558
AFLR3 GG : Nodes, Elements = 14611 68041
AFLR3 GG : Nodes, Elements = 14611 67160
AFLR3 GG : Nodes, Elements = 17636 76431
AFLR3 GG : Nodes, Elements = 17636 89789
AFLR3 GG : Nodes, Elements = 17636 86013
AFLR3 GG : Nodes, Elements = 17636 85164
AFLR3 GG : Nodes, Elements = 20795 94846
AFLR3 GG : Nodes, Elements = 20795 108553
AFLR3 GG : Nodes, Elements = 20795 104758
AFLR3 GG : Nodes, Elements = 20795 103868
AFLR3 GG : Nodes, Elements = 24143 114103
AFLR3 GG : Nodes, Elements = 24143 128399
AFLR3 GG : Nodes, Elements = 24143 124496
AFLR3 GG : Nodes, Elements = 24143 123622
AFLR3 GG : Nodes, Elements = 27578 134085
AFLR3 GG : Nodes, Elements = 27578 148825
AFLR3 GG : Nodes, Elements = 27578 144871
AFLR3 GG : Nodes, Elements = 27578 144095
AFLR3 GG : Nodes, Elements = 31062 154651
AFLR3 GG : Nodes, Elements = 31062 169473
AFLR3 GG : Nodes, Elements = 31062 165516
AFLR3 GG : Nodes, Elements = 31062 164721
AFLR3 GG : Nodes, Elements = 34579 175350
AFLR3 GG : Nodes, Elements = 34579 190320
AFLR3 GG : Nodes, Elements = 34579 186429
AFLR3 GG : Nodes, Elements = 34579 185651
AFLR3 GG : Nodes, Elements = 38117 196339
AFLR3 GG : Nodes, Elements = 38117 211235
AFLR3 GG : Nodes, Elements = 38117 207372
AFLR3 GG : Nodes, Elements = 38117 206679
AFLR3 GG : Nodes, Elements = 41546 217008
AFLR3 GG : Nodes, Elements = 41546 231612
AFLR3 GG : Nodes, Elements = 41546 227849
AFLR3 GG : Nodes, Elements = 41546 227098
AFLR3 GG : Nodes, Elements = 44816 236945
AFLR3 GG : Nodes, Elements = 44816 250860
AFLR3 GG : Nodes, Elements = 44816 247251
AFLR3 GG : Nodes, Elements = 44816 246555
AFLR3 GG : Nodes, Elements = 47997 256119
AFLR3 GG : Nodes, Elements = 47997 269545
AFLR3 GG : Nodes, Elements = 47997 266235
AFLR3 GG : Nodes, Elements = 47997 265599
AFLR3 GG : Nodes, Elements = 51063 274826
AFLR3 GG : Nodes, Elements = 51063 287600
AFLR3 GG : Nodes, Elements = 51063 284406
AFLR3 GG : Nodes, Elements = 51063 283837
AFLR3 GG : Nodes, Elements = 53943 292484
AFLR3 GG : Nodes, Elements = 53943 304592
AFLR3 GG : Nodes, Elements = 53943 301537
AFLR3 GG : Nodes, Elements = 53943 301039
AFLR3 GG : Nodes, Elements = 56663 309207
AFLR3 GG : Nodes, Elements = 56663 320639
AFLR3 GG : Nodes, Elements = 56663 317772
AFLR3 GG : Nodes, Elements = 56663 317298
AFLR3 GG : Nodes, Elements = 59285 325171
AFLR3 GG : Nodes, Elements = 59285 336094
AFLR3 GG : Nodes, Elements = 59285 333329
AFLR3 GG : Nodes, Elements = 59285 332965
AFLR3 GG : Nodes, Elements = 61664 340102
AFLR3 GG : Nodes, Elements = 61664 350059
AFLR3 GG : Nodes, Elements = 61664 347499
AFLR3 GG : Nodes, Elements = 61664 347178
AFLR3 GG : Nodes, Elements = 63775 353515
AFLR3 GG : Nodes, Elements = 63775 362373
AFLR3 GG : Nodes, Elements = 63775 360097
AFLR3 GG : Nodes, Elements = 63775 359845
AFLR3 GG : Nodes, Elements = 65488 364985
AFLR3 GG : Nodes, Elements = 65488 372358
AFLR3 GG : Nodes, Elements = 65488 370380
AFLR3 GG : Nodes, Elements = 65488 370151
AFLR3 GG : Nodes, Elements = 66827 374169
AFLR3 GG : Nodes, Elements = 66827 379876
AFLR3 GG : Nodes, Elements = 66827 378328
AFLR3 GG : Nodes, Elements = 66827 378171
AFLR3 GG : Nodes, Elements = 67794 381072
AFLR3 GG : Nodes, Elements = 67794 385093
AFLR3 GG : Nodes, Elements = 67794 384025
AFLR3 GG : Nodes, Elements = 67794 383942
AFLR3 GG : Nodes, Elements = 68434 385864
AFLR3 GG : Nodes, Elements = 68434 388601
AFLR3 GG : Nodes, Elements = 68434 387851
AFLR3 GG : Nodes, Elements = 68434 387773
AFLR3 GG : Nodes, Elements = 68796 388859
AFLR3 GG : Nodes, Elements = 68796 390447
AFLR3 GG : Nodes, Elements = 68796 389963
AFLR3 GG : Nodes, Elements = 68796 389933
AFLR3 GG : Nodes, Elements = 68972 390461
AFLR3 GG : Nodes, Elements = 68972 391210
AFLR3 GG : Nodes, Elements = 68972 390963
AFLR3 GG : Nodes, Elements = 68972 390952
AFLR3 GG : Nodes, Elements = 69050 391186
AFLR3 GG : Nodes, Elements = 69050 391558
AFLR3 GG : Nodes, Elements = 69050 391429
AFLR3 GG : Nodes, Elements = 69050 391423
AFLR3 GG : Nodes, Elements = 69065 391468
AFLR3 GG : Nodes, Elements = 69065 391533
AFLR3 GG : Nodes, Elements = 69065 391506
AFLR3 GG : Nodes, Elements = 69065 391507
AFLR3 GG : Nodes, Elements = 69069 391519
AFLR3 GG : Nodes, Elements = 69069 391536
AFLR3 GG : Nodes, Elements = 69069 391532
AFLR3 GG : Nodes, Elements = 69070 391535
AFLR3 GG : Nodes, Elements = 69070 391537
AFLR3 GG : Nodes, Elements = 69070 391536
AFLR3 GG : Nodes, Elements = 69071 391539
AFLR3 GG : Nodes, Elements = 69071 391543
AFLR3 GG : Nodes, Elements = 69071 391542
AFLR3 GG : Nodes, Elements = 69092 391605
AFLR3 GG : Nodes, Elements = 69092 391685
AFLR3 GG : Nodes, Elements = 69092 391658
AFLR3 GG : Nodes, Elements = 69092 391659
AFLR3 GG : Nodes, Elements = 69099 391680
AFLR3 GG : Nodes, Elements = 69099 391699
AFLR3 GG : Nodes, Elements = 69099 391694
AFLR3 GG : Nodes, Elements = 69099 391697
AFLR3 : CPU Time = 3.362 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 69099 391697
AFLR3 QI : Nodes, Elements = 67707 383766
AFLR3 QI : Nodes, Elements = 67488 382515
AFLR3 QI : Nodes, Elements = 67472 382422
AFLR3 QI : Nodes, Elements = 67472 386105
AFLR3 QI : Nodes, Elements = 67472 382216
AFLR3 QI : Nodes, Elements = 67472 381782
AFLR3 QI : Nodes, Elements = 67472 382185
AFLR3 QI : Nodes, Elements = 67472 381535
AFLR3 QI : Nodes, Elements = 67472 381323
AFLR3 QI : Nodes, Elements = 67472 381641
AFLR3 QI : Nodes, Elements = 67472 381293
AFLR3 QI : Nodes, Elements = 67472 381218
AFLR3 QI : Nodes, Elements = 67472 381493
AFLR3 QI : Nodes, Elements = 67472 381214
AFLR3 QI : Nodes, Elements = 67472 381162
AFLR3 QI : Nodes, Elements = 67472 381420
AFLR3 QI : Nodes, Elements = 67472 381183
AFLR3 QI : Nodes, Elements = 67472 381132
AFLR3 QI : Nodes, Elements = 67478 381161
AFLR3 QI : Nodes, Elements = 67478 381419
AFLR3 QI : Nodes, Elements = 67478 381185
AFLR3 QI : Nodes, Elements = 67478 381160
AFLR3 QI : Nodes, Elements = 67478 381441
AFLR3 QI : Nodes, Elements = 67478 381177
AFLR3 QI : Nodes, Elements = 67478 381133
AFLR3 QI : Nodes, Elements = 67478 381161
AFLR3 : CPU Time = 1.383 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 67478 381161
AFLR3 QRG: Nodes, Elements = 67477 381154
AFLR3 QRG: Nodes, Elements = 67476 381148
AFLR3 QRG: Nodes, Elements = 67476 381146
AFLR3 QRG: Nodes, Elements = 67477 381151
AFLR3 QRG: Nodes, Elements = 67488 381216
AFLR3 : CPU Time = 0.039 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 381216
UG3 : Min, Max Ang = 0.9236 174.6
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 72
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.11e+06
UG3 : No. Tet Elems = 381216
UG3 : Min Vol = 6.78e-10
UG3 : Average Vol = 5.53
UG3 : Total-Tet-Vol = 2.11e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 381216
UG3 : Min, Max Q = 0.0392 1
UG3 : Average Q = 0.892
UG3 : No. Q< 0.1 = 16
UG3 : No. Q< 0.01 = 0
Volume mesh:
Number of nodes = 67488
Number of elements = 393748
Number of triangles = 12532
Number of quadrilatarals = 0
Number of tetrahedrals = 381216
Number of pyramids= 0
Number of prisms= 0
Number of hexahedrals= 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
Python library was linked, but will not be used!
Found link for attrMap (Attribute_Map) from parent
Getting CFD boundary conditions
Boundary condition name - Wing1
Boundary condition name - Wing2
Boundary condition name - Farfield
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - Alpha
Done getting CFD design variables
Getting CFD objective.......
Number of design variables - 1
Objective name - ClCd
Done getting CFD objective
Found link for volume mesh (Volume_Mesh) from parent
Writing AFLR3 file ....
Finished writing AFLR3 file
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
No recognized data transfer names found!
Error: Premature exit in fun3d_dataTransfer status = -303
Creating FUN3D directory tree
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data
. Cleaning up fun3dInstance - 0
Cleaning up fun3dInstance - 1
Cleaning up fun3dInstance - 2
Cleaning up fun3dInstance - 3
Cleaning up fun3dInstance - 4
Cleaning up fun3dInstance - 5
Cleaning up fun3dInstance - 6
Cleaning up fun3dInstance - 7
Cleaning up aflr4Instance - 0
Cleaning up aflr3Instance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 2659) at Close!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
No analysis directory provided - defaulting to current working directory
CAPS Info: No symbol for aimDiscr in masstranAIM
CAPS Info: No symbol for aimFreeDiscr in masstranAIM
CAPS Info: No symbol for aimLocateElement in masstranAIM
CAPS Info: No symbol for aimUsesDataSet in masstranAIM
CAPS Info: No symbol for aimCheck in masstranAIM
CAPS Info: No symbol for aimTransfer in masstranAIM
CAPS Info: No symbol for aimInterpolation in masstranAIM
CAPS Info: No symbol for aimInterpolateBar in masstranAIM
CAPS Info: No symbol for aimIntegration in masstranAIM
CAPS Info: No symbol for aimIntegrateBar in masstranAIM
CAPS Info: No symbol for aimData in masstranAIM
CAPS Info: No symbol for aimSensitivity in masstranAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 5] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 6] box: 0.00000 0.00000 0.00000 1.00000 1.00000 1.00000
Body 1 created (toler= 1.0000e-07, nnode= 8, nedge= 12, nface= 6)
executing [ 7] select: body 1
putting Branch Attributes on Body
executing [ 9] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 16] ifthen: 0.00000 EQ 1.00000 and ...
finalizing:
==> Profile information
Branch type ncall time (sec) pct
box 1 0.001 90.4
select 1 0.000 4.1
ifthen 4 0.000 4.7
endif 4 0.000 0.8
Total 10 0.001
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Didn't find a Surface mesh (Surface_Mesh) from parent - checking for volume mesh
Didn't find a volume mesh (Volume_Mesh) from parent
Creating FEA BEM
Getting quads for BEM!
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
. EGADS Info: 0 Objects, 0 Reference in Use (of 135) at Close!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
No analysis directory provided - defaulting to current working directory
CAPS Info: No symbol for aimDiscr in masstranAIM
CAPS Info: No symbol for aimFreeDiscr in masstranAIM
CAPS Info: No symbol for aimLocateElement in masstranAIM
CAPS Info: No symbol for aimUsesDataSet in masstranAIM
CAPS Info: No symbol for aimCheck in masstranAIM
CAPS Info: No symbol for aimTransfer in masstranAIM
CAPS Info: No symbol for aimInterpolation in masstranAIM
CAPS Info: No symbol for aimInterpolateBar in masstranAIM
CAPS Info: No symbol for aimIntegration in masstranAIM
CAPS Info: No symbol for aimIntegrateBar in masstranAIM
CAPS Info: No symbol for aimData in masstranAIM
CAPS Info: No symbol for aimSensitivity in masstranAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 5] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 9] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 10] box: 2.00000 0.00000 0.00000 1.00000 1.00000 1.00000
Body 1 created (toler= 1.0000e-07, nnode= 8, nedge= 12, nface= 6)
executing [ 11] select: face 1
putting Branch Attributes on Face 1
executing [ 12] select: face 3
putting Branch Attributes on Face 3
executing [ 13] select: face 6
putting Branch Attributes on Face 6
executing [ 14] select: body 1
putting Branch Attributes on Body
executing [ 16] ifthen: 0.00000 EQ 1.00000 and ...
finalizing:
==> Profile information
Branch type ncall time (sec) pct
box 1 0.002 82.9
select 4 0.000 14.3
ifthen 4 0.000 2.7
endif 4 0.000 0.0
Total 13 0.002
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Didn't find a Surface mesh (Surface_Mesh) from parent - checking for volume mesh
Didn't find a volume mesh (Volume_Mesh) from parent
Creating FEA BEM
Face 3 quading disabled with attribute .qParams
Face 6 quading disabled with attribute .qParams
Getting quads for BEM!
capsIgnore attribute found for face - 1!!
Removing unused nodes...
Removed 324 (out of 4009) unused nodes!
Mesh for body = 0
Number of nodal coordinates = 3685
Number of elements = 6209
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5126
Elemental Quad4 = 1083
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
. EGADS Info: 0 Objects, 0 Reference in Use (of 135) at Close!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
No analysis directory provided - defaulting to current working directory
CAPS Info: No symbol for aimDiscr in masstranAIM
CAPS Info: No symbol for aimFreeDiscr in masstranAIM
CAPS Info: No symbol for aimLocateElement in masstranAIM
CAPS Info: No symbol for aimUsesDataSet in masstranAIM
CAPS Info: No symbol for aimCheck in masstranAIM
CAPS Info: No symbol for aimTransfer in masstranAIM
CAPS Info: No symbol for aimInterpolation in masstranAIM
CAPS Info: No symbol for aimInterpolateBar in masstranAIM
CAPS Info: No symbol for aimIntegration in masstranAIM
CAPS Info: No symbol for aimIntegrateBar in masstranAIM
CAPS Info: No symbol for aimData in masstranAIM
CAPS Info: No symbol for aimSensitivity in masstranAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 5] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 9] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 16] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 17] box: 4.00000 0.00000 0.00000 1.00000 1.00000 1.00000
Body 1 created (toler= 1.0000e-07, nnode= 8, nedge= 12, nface= 6)
executing [ 18] select: face 1
putting Branch Attributes on Face 1
executing [ 19] select: face 2
putting Branch Attributes on Face 2
executing [ 20] select: face 3
putting Branch Attributes on Face 3
executing [ 21] select: face 4
putting Branch Attributes on Face 4
executing [ 22] select: face 5
putting Branch Attributes on Face 5
executing [ 23] select: face 6
putting Branch Attributes on Face 6
executing [ 24] select: body 1
putting Branch Attributes on Body
finalizing:
==> Profile information
Branch type ncall time (sec) pct
box 1 0.001 56.8
select 7 0.001 39.6
ifthen 4 0.000 3.3
endif 4 0.000 0.3
Total 16 0.001
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Didn't find a Surface mesh (Surface_Mesh) from parent - checking for volume mesh
Didn't find a volume mesh (Volume_Mesh) from parent
Creating FEA BEM
Getting quads for BEM!
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
. EGADS Info: 0 Objects, 0 Reference in Use (of 135) at Close!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
No analysis directory provided - defaulting to current working directory
CAPS Info: No symbol for aimDiscr in masstranAIM
CAPS Info: No symbol for aimFreeDiscr in masstranAIM
CAPS Info: No symbol for aimLocateElement in masstranAIM
CAPS Info: No symbol for aimUsesDataSet in masstranAIM
CAPS Info: No symbol for aimCheck in masstranAIM
CAPS Info: No symbol for aimTransfer in masstranAIM
CAPS Info: No symbol for aimInterpolation in masstranAIM
CAPS Info: No symbol for aimInterpolateBar in masstranAIM
CAPS Info: No symbol for aimIntegration in masstranAIM
CAPS Info: No symbol for aimIntegrateBar in masstranAIM
CAPS Info: No symbol for aimData in masstranAIM
CAPS Info: No symbol for aimSensitivity in masstranAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] ifthen: 1.00000 EQ 1.00000 and 0.00000 eq 0.00000
executing [ 2] box: 0.00000 0.00000 0.00000 2.00000 3.00000 0.00000
Body 1 created (toler= 1.0000e-07, nnode= 4, nedge= 4, nface= 1)
executing [ 3] select: body 1
putting Branch Attributes on Body
executing [ 5] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 9] ifthen: 0.00000 EQ 1.00000 and ...
executing [ 16] ifthen: 0.00000 EQ 1.00000 and ...
finalizing:
==> Profile information
Branch type ncall time (sec) pct
box 1 0.001 94.5
select 1 0.000 2.1
ifthen 4 0.000 2.9
endif 4 0.000 0.5
Total 10 0.001
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Didn't find a Surface mesh (Surface_Mesh) from parent - checking for volume mesh
Didn't find a volume mesh (Volume_Mesh) from parent
Creating FEA BEM
Getting quads for BEM!
Mesh for body = 0
Number of nodal coordinates = 400
Number of elements = 361
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 361
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
. EGADS Info: 0 Objects, 0 Reference in Use (of 80) at Close!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
Analysis directory does not currently exist - it will be made automatically
CAPS Info: No symbol for aimExecute in su2AIM
CAPS Info: No symbol for aimCheck in su2AIM
CAPS Info: No symbol for aimData in su2AIM
CAPS Info: No symbol for aimSensitivity in su2AIM
Analysis object with the name, su2AIM, has already been initilized
('An altName of', 'su2AIM_1', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] set: cmean sqrt(area/aspect)
cmean = 2.82843 0.00000
executing [ 2] set: span cmean*aspect
span = 14.14214 0.00000
executing [ 3] set: sspan span/2
sspan = 7.07107 0.00000
executing [ 4] set: croot 2*cmean/(1+taper)
croot = 3.77124 0.00000
executing [ 5] set: ctip croot*taper
ctip = 1.88562 0.00000
executing [ 6] set: xtip sspan*tand(lesweep)
xtip = 4.08248 0.00000
executing [ 7] set: ytip sspan*tand(dihedral)
ytip = 0.12343 0.00000
executing [ 8] set: ybot -0.1*croot
ybot = -0.37712 0.00000
executing [ 9] set: ytop +0.2*croot+ytip
ytop = 0.87767 0.00000
executing [ 10] set: extend 0.02*cmean
extend = 0.05657 0.00000
executing [ 11] mark:
Mark created
executing [ 12] udprim: naca Series 8412.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 13] scale: 3.77124 0.00000 0.00000 0.00000
Body 2 created (toler= 3.7712e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 14] udprim: naca Series 20.00000 (compiled code)
Body 3 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 15] scale: 1.88562 0.00000 0.00000 0.00000
Body 4 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 16] rotatez: -15.00000 0.00000 0.00000
Body 5 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 17] translate: 4.08248 0.12343 -7.07107
Body 6 created (toler= 1.8856e-07, nnode= 3, nedge= 3, nface= 1)
executing [ 18] rule: 0.00000 0.00000
ruling 2 Xsects with 3 Strips each...
Body 7 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 19] store: HalfWing 0.00000 0.00000
Body 7 stored
executing [ 20] restore: HalfWing 0.00000
Body 8 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 21] restore: HalfWing 0.00000
Body 9 restored (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 22] mirror: 0.00000 0.00000 1.00000 0.00000
Body 10 created (toler= 1.0000e-07, nnode= 6, nedge= 9, nface= 5)
executing [ 23] join: 0.00000 0.00000
Body 11 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 24] rotatex: 90.00000 0.00000 0.00000
Body 12 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 25] store: Wing 0.00000 0.00000
Body 12 stored
executing [ 26] restore: Wing 0.00000
Body 13 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 27] restore: Wing 0.00000
Body 14 restored (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 28] scale: 0.40000 0.00000 0.00000 0.00000
Body 15 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 29] translate: 10.00000 0.00000 0.00000
Body 16 created (toler= 1.0000e-07, nnode= 9, nedge= 15, nface= 8)
executing [ 30] sphere: 0.00000 0.00000 0.00000 80.00000
Body 17 created (toler= 1.0000e-05, nnode= 2, nedge= 6, nface= 2)
finalizing:
==> Profile information
Branch type ncall time (sec) pct
sphere 1 0.002 0.6
udprim 2 0.014 3.9
restore 4 0.003 0.8
rule 1 0.064 18.3
join 1 0.074 21.0
translate 2 0.058 16.7
rotatex 1 0.057 16.3
rotatez 1 0.001 0.3
scale 3 0.059 17.0
mirror 1 0.017 5.0
set 10 0.000 0.0
store 2 0.000 0.0
mark 1 0.000 0.0
Total 30 0.350
Linking status during attrMap (Attribute_Map) = -303
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Unrecognized "bcType" specified ("X") for Boundary_Condition tuple Wing1, current options (not all options are valid for this analysis tool - see AIM documentation) are " Inviscid, Viscous, Farfield, Extrapolate, Freestream, BackPressure, Symmetry, SubsonicInflow, SubsonicOutflow, MassflowIn, MassflowOut, MachOutflow, FixedInflow, FixedOutflow"
Premature exit in su2AIM preAnalysis status = -303
.
Analysis object with the name, su2AIM, has already been initilized
('An altName of', 'su2AIM_2', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Linking status during attrMap (Attribute_Map) = -303
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Boundary condition name - X
BC name "X" not found in attrMap
Premature exit in su2AIM preAnalysis status = -303
.Linking status during attrMap (Attribute_Map) = -303
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Wing1
Boundary condition name - Wing2
Boundary condition name - Farfield
Done getting CFD boundary conditions
Linking status = -303
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.0.7) "
Getting CFD boundary conditions
Boundary condition name - Wing1
Boundary condition name - Wing2
Boundary condition name - Farfield
Done getting CFD boundary conditions
Linking status = -303
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.0.7) "
. Cleaning up su2Instance - 0
Cleaning up su2Instance - 1
Cleaning up su2Instance - 2
EGADS Info: 0 Objects, 0 Reference in Use (of 2134) at Close!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
Analysis directory does not currently exist - it will be made automatically
CAPS Info: No symbol for aimDiscr in xfoilAIM
CAPS Info: No symbol for aimFreeDiscr in xfoilAIM
CAPS Info: No symbol for aimLocateElement in xfoilAIM
CAPS Info: No symbol for aimUsesDataSet in xfoilAIM
CAPS Info: No symbol for aimExecute in xfoilAIM
CAPS Info: No symbol for aimCheck in xfoilAIM
CAPS Info: No symbol for aimTransfer in xfoilAIM
CAPS Info: No symbol for aimInterpolation in xfoilAIM
CAPS Info: No symbol for aimInterpolateBar in xfoilAIM
CAPS Info: No symbol for aimIntegration in xfoilAIM
CAPS Info: No symbol for aimIntegrateBar in xfoilAIM
CAPS Info: No symbol for aimData in xfoilAIM
CAPS Info: No symbol for aimSensitivity in xfoilAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] dimension: classvar 1.00000 2.00000
executing [ 2] dimension: ztailvar 1.00000 2.00000
executing [ 3] dimension: auppervar 1.00000 4.00000
executing [ 4] dimension: alowervar 1.00000 4.00000
executing [ 5] set: classvar 0.5;1.0;
classvar[1,1] = 0.50000 0.00000
classvar[1,2] = 1.00000 0.00000
executing [ 6] set: ztailvar 0.001;-0.001;
ztailvar[1,1] = 0.00100 0.00000
ztailvar[1,2] = -0.00100 0.00000
executing [ 7] set: al4 0.001
al4 = 0.00100 0.00000
executing [ 8] set: auppervar au1;au2;au3;au4;
auppervar[1,1] = 0.22000 0.00000
auppervar[1,2] = 0.30000 0.00000
auppervar[1,3] = 0.25000 0.00000
auppervar[1,4] = 0.29000 0.00000
executing [ 9] set: alowervar al1;al2;al3;al4;
alowervar[1,1] = -0.12000 0.00000
alowervar[1,2] = -0.02000 0.00000
alowervar[1,3] = -0.03000 0.00000
alowervar[1,4] = 0.00100 0.00000
executing [ 10] udparg: kulfan class 0.50000
Body 1 created (NULL Body)
executing [ 11] udparg: kulfan ztail 0.00100
Body 2 created (NULL Body)
executing [ 12] udparg: kulfan aupper 0.22000
Body 3 created (NULL Body)
executing [ 13] udparg: kulfan alower -0.12000
Body 4 created (NULL Body)
executing [ 14] udprim: kulfan (compiled code)
Body 5 created (toler= 1.0000e-07, nnode= 3, nedge= 3, nface= 1)
finalizing:
==> Profile information
Branch type ncall time (sec) pct
dimension 4 0.000 0.7
udprim 1 0.006 94.9
set 5 0.000 3.1
udparg 4 0.000 1.3
Total 14 0.007
Running xFoil......
.
Running xFoil......
. EGADS Info: 0 Objects, 0 Reference in Use (of 91) at Close!
Definition of "kt" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/ESP/udunits/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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/unit/DARWIN64/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
Analysis directory does not currently exist - it will be made automatically
CAPS Info: No symbol for aimDiscr in xfoilAIM
CAPS Info: No symbol for aimFreeDiscr in xfoilAIM
CAPS Info: No symbol for aimLocateElement in xfoilAIM
CAPS Info: No symbol for aimUsesDataSet in xfoilAIM
CAPS Info: No symbol for aimExecute in xfoilAIM
CAPS Info: No symbol for aimCheck in xfoilAIM
CAPS Info: No symbol for aimTransfer in xfoilAIM
CAPS Info: No symbol for aimInterpolation in xfoilAIM
CAPS Info: No symbol for aimInterpolateBar in xfoilAIM
CAPS Info: No symbol for aimIntegration in xfoilAIM
CAPS Info: No symbol for aimIntegrateBar in xfoilAIM
CAPS Info: No symbol for aimData in xfoilAIM
CAPS Info: No symbol for aimSensitivity in xfoilAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed
Interim EGADS version 1.19 (with OpenCASCADE 7.4.1)
executing [ 1] udprim: naca Thickness 0.12000 Camber 0.02000 sharpte 1.00000 (compiled code)
Body 1 created (toler= 1.0000e-07, nnode= 2, nedge= 2, nface= 1)
finalizing:
==> Profile information
Branch type ncall time (sec) pct
udprim 1 0.006 100.0
Total 1 0.006
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
Running xFoil......
. EGADS Info: 0 Objects, 0 Reference in Use (of 67) at Close!
----------------------------------------------------------------------
Ran 67 tests in 43.862s
OK (skipped=10)
Cleaning up egadsInstance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Cleaning up egadsInstance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 2185) at Close!
Cleaning up egadsInstance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 2185) at Close!
Cleaning up egadsInstance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 2185) at Close!
Cleaning up egadsInstance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 2143) at Close!
Cleaning up egadsInstance - 0
Cleaning up astrosInstance - 0
EGADS Info: 18 Objects, 23 Reference in Use (of 59) at Close!
--> temporary directory "tmp_OpenCSM_00" removed
Cleaning up egadsInstance - 0
Cleaning up astrosInstance - 0
EGADS Info: 59 Objects, 80 Reference in Use (of 1825) at Close!
EGADS Info: 2 unattached Objects (24 References) removed!
Cleaning up aflr4Instance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Cleaning up aflr4Instance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 2189) at Close!
Cleaning up aflr4Instance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 2185) at Close!
Cleaning up aflr4Instance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 2189) at Close!
Cleaning up aflr4Instance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 2659) at Close!
Cleaning up aflr2Instance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 1050) at Close!
Cleaning up aflr2Instance - 0
EGADS Info: 0 Objects, 0 Reference in Use (of 1050) at Close!
+++ set +x
[Execution node] check if [macys_VM] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Sleeping for 5 seconds due to JENKINS-32191...
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping mining
[Clang (LLVM based)] Sleeping for 5 seconds due to JENKINS-32191...
[Clang (LLVM based)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_QuickTestCaps/7.4/CAPS/unit/DARWIN64')
[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,DARWIN64,macys_VM)
[Static Analysis] Using reference build 'ESP_QuickTestCaps/CASREV=7.4,ESP_ARCH=DARWIN64,buildnode=macys_VM #24' 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=DARWIN64,buildnode=macys_VM #26'.
[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