Skipping 414 KB..
Full Logmake[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/skeleton'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/lib/skeletonAIM.so' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/skeleton'
make -C spinnaker
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/spinnaker'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/lib/spinnakerAIM.so' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/spinnaker'
make -C su2
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/su2'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/lib/su2AIM.so' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/su2'
make -C tacs
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/tacs'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/lib/tacsAIM.so' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/tacs'
make -C tetgen
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/tetgen'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/tetgen'
make -C tsfoil
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/tsfoil'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/lib/tsfoilAIM.so' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/tsfoil'
make -C unitTest
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/unitTest'
make[2]: Nothing to be done for 'all'.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/unitTest'
make -C xfoil
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/xfoil'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/lib/xfoilAIM.so' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/xfoil'
make -C zaero
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/zaero'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/zaero'
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim'
(cd Slugs/src; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/Slugs/src'
make[1]: Nothing to be done for 'all'.
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/Slugs/src'
(cd test; make -f aim.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
make[1]: Nothing to be done for 'default'.
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
(cd test; make -f autoExec.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
make[1]: Nothing to be done for 'default'.
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
(cd test; make -f newPhase.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
make[1]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/newPhase' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
(cd test; make -f basic.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
make[1]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/basic' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
(cd test; make -f geomIn.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
make[1]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/geomIn' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
(cd test; make -f utilsTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
make[1]: Nothing to be done for 'default'.
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
(cd test; make -f vVS.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
make[1]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/vVS' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test'
(cd examples; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/avlTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/awaveTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/frictionTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: Nothing to be done for 'fun3d'.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: 'hsm' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/interferenceTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/msesTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/mystranTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/pointwiseTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples'
# CAPS Unit tests
(cd test; ./runUnitTest.sh)
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
aimTransferUtil Tests passed!
real 0m0.057s
user 0m0.053s
sys 0m0.004s
=============================================
CAPS test (using c-executables) case /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/aimTransferUtilTest passed (as expected)
=============================================
+ expectCSuccess /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/miscUtilsTest
+ /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/miscUtilsTest
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 0.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of -2 must be greater than 1 for the input value 9.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 0 must be greater than 1 for the input value 9.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -1.000000E+100 with field with 7!
Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -9.900000E+99 with field with 7!
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 2 must be greater than 2 for the input value -1.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 1.000000E+00
Returning a 'NaN' string.
Error in convert_integerToString: Input 9999999 fails with requested fieldWidth of 6
Returning a 'NaN' string.
Error in convert_integerToString: Input -999999 fails with requested fieldWidth of 6
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth > 15 not verified
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0
Returning a 'NaN' string.
miscUtils Tests passed!
real 0m0.033s
user 0m0.024s
sys 0m0.008s
+ set +x
=============================================
CAPS test (using c-executables) case /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/miscUtilsTest passed (as expected)
=============================================
+ expectCSuccess /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/vlmUtilsTest
+ /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/vlmUtilsTest
vlmUtils Tests passed!
real 0m0.040s
user 0m0.036s
sys 0m0.004s
+ set +x
=============================================
CAPS test (using c-executables) case /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/vlmUtilsTest passed (as expected)
=============================================
+ rm -rf aimTest
+ expectCSuccess '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/aim testingAIM.csm'
+ /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/aim testingAIM.csm
Root Path = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test/aimTest/Scratch
testingAIM/aimInitialize instance = -1 unitSys = (null)!
caps_queryAnalysis = 0 4 3 1
testingAIM/aimInputs instance = -1 index = 1!
in 1: testingAIMin 0
testingAIM/aimInputs instance = -1 index = 2!
in 2: table 0
testingAIM/aimInputs instance = -1 index = 3!
in 3: tessIn 0
testingAIM/aimInputs instance = -1 index = 4!
in 4: meshFile 0
testingAIM/aimOutputs instance = -1 index = 1!
out 1: testingAIMout 0
testingAIM/aimOutputs instance = -1 index = 2!
out 2: tessOut 0
testingAIM/aimOutputs instance = -1 index = 3!
out 3: meshFile 0
testingAIM/aimInitialize instance = 0 unitSys = m!
testingAIM/aimInputs instance = 0 index = 1!
testingAIM/aimInputs instance = 0 index = 2!
testingAIM/aimInputs instance = 0 index = 3!
testingAIM/aimInputs instance = 0 index = 4!
testingAIM/aimOutputs instance = 0 index = 1!
testingAIM/aimOutputs instance = 0 index = 2!
testingAIM/aimOutputs instance = 0 index = 3!
testingAIM/aimBackdoor instance = 0: Input String!
Backdoor return string = aimBackdoor Output
testingAIM/aimInitialize instance = 1 unitSys = (null)!
testingAIM/aimInputs instance = 1 index = 1!
testingAIM/aimInputs instance = 1 index = 2!
testingAIM/aimInputs instance = 1 index = 3!
testingAIM/aimInputs instance = 1 index = 4!
testingAIM/aimOutputs instance = 1 index = 1!
testingAIM/aimOutputs instance = 1 index = 2!
testingAIM/aimOutputs instance = 1 index = 3!
Intent = child
APath = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test/aimTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 1
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
Problem: # Dirty Analyses = 2!
Bound: # Dirty Analyses = 2!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 1!
testingAIM/aimUpdateState instance = 0!
tess is NULL!
testingAIM/aimPreAnalysis instance = 0!
testingAIM/aimPreAnalysis aim_getBounds = 0
Analysis in Bound = Interface
aim_newGeometry = 0!
getDiscr = 0
getDataSet = 0, rank = 1, method = 0
0 scalars!
meshRef = NULL
testingAIM/aimExecute instance = 0!
testingAIM/aimPostAnalysis instance = 0 restart = 0!
testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
After Execute on Parent
Problem: # Dirty Analyses = 1!
Bound: # Dirty Analyses = 1!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 0!
testingAIM/aimCalcOutput instance = 0 index = 2 tessOut 0!
tessPtr = 0
testingAIM/aimUpdateState instance = 1!
tess is NULL!
testingAIM/aimDiscr: tname = Interface, instance = 1!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 3 matches Interface!
testingAIM/aimDiscr: ntris = 2108!
testingAIM/aimDiscr: npts = 1113!
testingAIM/aimDiscr: tname = Interface, instance = 0!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 6 matches Interface!
testingAIM/aimDiscr: ntris = 800!
testingAIM/aimDiscr: npts = 447!
testingAIM/aimTransfer name = scalar instance = 0 npts = 447/1!
CAPS Info: Bound 'Interface' Normalized Integrated 'scalar'
Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 5.564971e-11
testingAIM/aimPreAnalysis instance = 1!
testingAIM/aimPreAnalysis aim_getBounds = 0
Analysis in Bound = Interface
aim_newGeometry = 0!
getDiscr = 0
getDataSet = -303, rank = 0, method = 0
vectors not setup yet!
testingAIM/aimExecute instance = 1!
testingAIM/aimPostAnalysis instance = 1 restart = 0!
Dirty = 0
Problem: # Dirty Analyses = 0!
Bound: # Dirty Analyses = 0!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 0!
Body 1 has length units = cm
Body 2 has length units = cm
aimTest has type PROBLEM, subtype PARAMETRIC with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
hist: (null) -> Initial Phase
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds
ParamName has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 2
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 2
value = 0.000000 (null)
Param has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 3
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 3
value = 99 (null)
num has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 6
hist: (null) -> Initial Phase
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 6
value = 8.000000 (null)
x has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
hist: (null) -> Initial Phase
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
value (8x1) = 7.300000 8.400000 10.400000 11.300000 12.300000 13.800000 14.400000 17.200000 (null)
ymin has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
hist: (null) -> Initial Phase
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
value (8x1) = -1.250000 -1.900000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 (null)
zmin has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
hist: (null) -> Initial Phase
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
value (8x1) = -0.825000 -0.812500 -0.800000 -0.775000 -0.750000 -0.700000 -0.690000 -0.100000 (null)
zmax has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
hist: (null) -> Initial Phase
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
value (8x1) = 0.825000 0.812500 0.800000 0.775000 0.750000 0.700000 0.690000 0.100000 (null)
unused has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 7
hist: (null) -> Initial Phase
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 1
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 7
linked to ParamName
pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 16
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 16
value = 34.641525 (null)
cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 16
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 16
value = 7.296560 (null)
testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 18
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 18
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 8
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 8
value = 5.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 8
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 8
value (1x3) =
1: Entry1 -> Value1
2: Entry2 -> Value2
3: Entry3 -> Value3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 8
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 8
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 8
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 8
value (0x0) = NULL with len = 0 meter
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 9
testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0!
aim_getDiscr 0 on Interface = 0
aim_getDataSet 0 on Interface = -329
value = 12.340000 cm
lazy: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 18
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 18
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 18
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 9
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 18
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 18
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 18
value = 42 (null)
testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 28
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 28
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 10
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 10
value = 6.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 12
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 12
value (1x3) =
1: Entry1 -> newValue1
2: Entry2 -> newValue2
3: Entry3 -> newValue3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 18
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 13
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
linked to tessOut
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 10
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 10
value (0x0) = NULL with len = 0 meter
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 11
testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0!
aim_getDiscr 1 on Interface = 0
aim_getDataSet 1 on Interface = -329
value = 12.340000 cm
lazy: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 28
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 11
testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0!
tessPtr = 5597a95931b0
value = 5597a95931b0 ego
lazy: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 28
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 11
testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 28
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 28
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 28
value = 42 (null)
Interface has type BOUND, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 14
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
2 Connecteds, 0 UnConnecteds
testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
5 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
1113 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
1113 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 26
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 15
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:57 26
1113 points, rank=1, units=(null)
testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
6 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
447 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 23
447 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 25
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Child Execute
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 25
447 points, rank=1, units=(null)
vector has type DATASET, subtype NONE with 0 attributes
last: aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
hist: (null) -> Starting
aimTest reynolds:1605044 jenkins 2024/07/25 22:43:45 0
testingAIM/aimTransfer name = vector instance = 0 npts = 447/3!
447 points, rank=3, units=(null)
1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
8: 14.400000 14.400000 14.400000 14.380647 14.400000 14.381201 14.400000
15: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
22: 14.400000 14.400000 14.390441 14.400000 14.383859 14.400000 14.400000
29: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
36: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
43: 14.385061 14.400000 14.383844 14.400000 14.400000 14.400000 14.400000
50: 14.378338 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
57: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.376665
64: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
78: 14.389247 14.400000 14.400000 14.400000 14.400000 14.382317 14.400000
85: 14.400000 14.400000 14.400000 14.390011 14.400000 14.400000 14.400000
92: 14.400000 14.400000 14.400000 14.400000 14.389865 14.400000 14.389101
99: 14.400000 14.388170 14.400000 14.400000 14.400000 14.400000 14.400000
106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
155: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
162: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
169: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
176: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
183: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
190: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
197: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
204: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
211: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
218: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
225: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
232: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
239: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
246: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
253: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
260: 14.400000 14.400000 14.400000 14.399999 14.400000 14.400000 14.400000
267: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
274: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
281: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
288: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
295: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
302: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
309: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
316: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
323: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
330: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
337: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
344: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
351: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
358: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
365: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
372: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
379: 14.400000 14.400000 14.400000 14.400000 14.399999 14.400000 14.400000
386: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
393: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
400: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
407: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
414: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
421: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
428: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
435: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
442: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
449: 14.400000 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000
456: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
463: 14.400000 14.400000 14.400000 14.400000 14.399999 14.400000 14.399999
470: 14.400000 14.400000 14.400000 14.400000 14.400000 14.399999 14.400000
477: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
491: 14.399999 14.400000 14.400000 14.400000 14.365872 14.400000 14.400000
498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
505: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
512: 14.400000 14.399999 14.399999 14.400000 14.400000 14.400000 14.400000
519: 14.400000 14.362939 14.399999 14.362723 14.400000 14.400000 14.400000
526: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
533: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
540: 14.400000 14.400000 14.400000 14.399999 14.400000 14.399999 14.400000
547: 14.368368 14.400000 14.400000 14.399999 14.400000 14.369831 14.400000
554: 14.400000 14.400000 14.400000 14.368625 14.399999 14.362939 14.400000
561: 14.400000 14.366035 14.400000 14.400000 14.400000 14.400000 14.400000
568: 14.356726 14.400000 14.369831 14.369176 14.400000 14.399999 14.400000
575: 14.400000 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000
582: 14.399999 14.363748 14.368368 14.400000 14.399999 14.400000 14.400000
589: 14.369831 14.400000 14.359401 14.399999 14.362295 14.400000 14.399999
596: 14.373877 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
603: 14.369218 14.369218 14.400000 14.365682 14.400000 14.369054 14.400000
610: 14.400000 14.400000 14.400000 14.371386 14.368747 14.372230 14.400000
617: 14.375508 14.400000 14.364430 14.374160 14.400000 14.400000 14.400000
624: 14.368709 14.369354 14.400000 14.400000 14.400000 14.399999 14.400000
631: 14.400000 14.400000 14.370155 14.368220 14.400000 14.372237 14.400000
638: 14.400000 14.374425 14.372364 14.400000 14.400000 14.400000 14.400000
645: 14.375987 14.365558 14.368709 14.366781 14.400000 14.369176 14.369354
652: 14.399999 14.373289 14.400000 14.375685 14.374425 14.400000 14.377582
659: 14.399999 14.400000 14.400000 14.366036 14.400000 14.400000 14.400000
666: 14.400000 14.375124 14.400000 14.400000 14.368903 14.368555 14.399999
673: 14.400000 14.371386 14.371386 14.399999 14.400000 14.379372 14.369130
680: 14.374049 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
687: 14.376400 14.399999 14.377760 14.378863 14.374473 14.367810 14.400000
694: 14.400000 14.368784 14.400000 14.371386 14.365916 14.400000 14.373165
701: 14.400000 14.399999 14.372471 14.400000 14.400000 14.400000 14.400000
708: 14.375987 14.379953 14.400000 14.374316 14.377675 14.400000 14.376295
715: 14.400000 14.399999 14.399999 14.368903 14.368784 14.366475 14.400000
722: 14.400000 14.369555 14.400000 14.378687 14.378687 14.378950 14.400000
729: 14.375449 14.376400 14.371321 14.400000 14.400000 14.371351 14.399999
736: 14.400000 14.375126 14.400000 14.400000 14.400000 14.375504 14.368903
743: 14.368514 14.400000 14.400000 14.400000 14.400000 14.379510 14.375124
750: 14.376289 14.374679 14.400000 14.400000 14.399999 14.400000 14.378601
757: 14.399999 14.377088 14.400000 14.375718 14.373640 14.400000 14.400000
764: 14.372001 14.400000 14.400000 14.368903 14.368514 14.400000 14.374569
771: 14.400000 14.375271 14.400000 14.400000 14.400000 14.400000 14.380018
778: 14.399999 14.400000 14.379331 14.400000 14.400000 14.379693 14.400000
785: 14.372552 14.383094 14.375769 14.400000 14.372608 14.378845 14.400000
792: 14.373363 14.368903 14.400000 14.375189 14.378667 14.375797 14.377675
799: 14.400000 14.400000 14.379863 14.373732 14.400000 14.400000 14.400000
806: 14.400000 14.400000 14.375857 14.400000 14.400000 14.400000 14.400000
813: 14.400000 14.400000 14.400000 14.400000 14.376290 14.379510 14.400000
820: 14.400000 14.400000 14.374594 14.400000 14.376305 14.400000 14.373349
827: 14.400000 14.379553 14.379553 14.373363 14.400000 14.377860 14.382472
834: 14.379566 14.400000 14.376493 14.400000 14.400000 14.400000 14.400000
841: 14.378207 14.375251 14.376605 14.400000 14.378626 14.400000 14.400000
848: 14.400000 14.376156 14.377590 14.379497 14.400000 14.375464 14.378358
855: 14.400000 14.380743 14.375541 14.400000 14.373960 14.400000 14.380592
862: 14.379305 14.374687 14.383536 14.400000 14.400000 14.374081 14.400000
869: 14.400000 14.380716 14.379808 14.383716 14.400000 14.383966 14.377272
876: 14.400000 14.379553 14.400000 14.377570 14.400000 14.376445 14.382213
883: 14.400000 14.400000 14.400000 14.400000 14.371272 14.379704 14.400000
890: 14.400000 14.379158 14.400000 14.379112 14.383216 14.380581 14.400000
897: 14.382554 14.400000 14.383382 14.400000 14.381160 14.400000 14.400000
904: 14.385313 14.382398 14.378148 14.381487 14.400000 14.378927 14.380605
911: 14.400000 14.400000 14.382990 14.384339 14.381122 14.380943 14.382554
918: 14.400000 14.375911 14.400000 14.384096 14.379502 14.376270 14.382299
925: 14.400000 14.380606 14.380606 14.383670 14.382868 14.400000 14.380592
932: 14.400000 14.379141 14.400000 14.400000 14.400000 14.400000 14.379453
939: 14.383433 14.382323 14.382931 14.376462 14.385109 14.386913 14.377700
946: 14.384542 14.400000 14.378601 14.387579 14.400000 14.400000 14.400000
953: 14.385467 14.379641 14.381746 14.383298 14.379931 14.400000 14.381446
960: 14.378196 14.400000 14.400000 14.381474 14.400000 14.383687 14.400000
967: 14.400000 14.384788 14.382697 14.379960 14.382187 14.383772 14.400000
974: 14.376286 14.374476 14.383667 14.382627 14.379931 14.384695 14.384795
981: 14.384528 14.385187 14.382443 14.381568 14.384519 14.385991 14.400000
988: 14.381424 14.400000 14.376098 14.383598 14.400000 14.375887 14.382344
995: 14.400000 14.374829 14.400000 14.386850 14.382671 14.380741 14.377878
1002: 14.388595 14.383869 14.385187 14.400000 14.400000 14.386296 14.384522
1009: 14.388515 14.385094 14.381609 14.387264 14.385337 14.386730 14.386730
1016: 14.387884 14.400000 14.376353 14.377969 14.376462 14.384854 14.378940
1023: 14.400000 14.386177 14.385200 14.385211 14.400000 14.400000 14.388399
1030: 14.384905 14.400000 14.400000 14.385855 14.386303 14.386373 14.389777
1037: 14.383001 14.384393 14.387981 14.400000 14.379911 14.378339 14.400000
1044: 14.400000 14.400000 14.380951 14.382823 14.381293 14.400000 14.400000
1051: 14.375959 14.380629 14.382256 14.388550 14.385775 14.389044 14.386740
1058: 14.385318 14.400000 14.380768 14.387137 14.385084 14.386362 14.379022
1065: 14.400000 14.383819 14.400000 14.373221 14.400000 14.387729 14.382944
1072: 14.387356 14.400000 14.390026 14.387727 14.388858 14.400000 14.381248
1079: 14.386362 14.378339 14.400000 14.400000 14.375685 14.381865 14.383342
1086: 14.386099 14.381327 14.386556 14.381954 14.385445 14.383357 14.384113
1093: 14.379911 14.400000 14.383874 14.400000 14.381638 14.391021 14.400000
1100: 14.400000 14.400000 14.400000 14.400000 14.384656 14.400000 14.378251
1107: 14.400000 14.381757 14.383106 14.386337 14.384313 14.383799 14.384686
source getTriangles = 0, nGtris = 2108, nGsegs = 6324, Ds = 0 0
destin getTriangles = 0, nGtris = 800, nGsegs = 2400, Ds = 0 0
In caps_outputObjects:
2 Analyses found
1 Bounds found
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m12.607s
user 0m12.750s
sys 0m2.000s
+ set +x
=============================================
CAPS test (using c-executables) case /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/aim testingAIM.csm passed (as expected)
=============================================
+ rm -rf source.vs destin.vs
+ expectCSuccess '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/autoExec testingAIM.csm'
+ /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/autoExec testingAIM.csm
testingAIM/aimInitialize instance = 0 unitSys = m!
testingAIM/aimInputs instance = 0 index = 1!
testingAIM/aimInputs instance = 0 index = 2!
testingAIM/aimInputs instance = 0 index = 3!
testingAIM/aimInputs instance = 0 index = 4!
testingAIM/aimOutputs instance = 0 index = 1!
testingAIM/aimOutputs instance = 0 index = 2!
testingAIM/aimOutputs instance = 0 index = 3!
testingAIM/aimInitialize instance = 1 unitSys = (null)!
testingAIM/aimInputs instance = 1 index = 1!
testingAIM/aimInputs instance = 1 index = 2!
testingAIM/aimInputs instance = 1 index = 3!
testingAIM/aimInputs instance = 1 index = 4!
testingAIM/aimOutputs instance = 1 index = 1!
testingAIM/aimOutputs instance = 1 index = 2!
testingAIM/aimOutputs instance = 1 index = 3!
Intent = child
APath = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test/autoExecTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 2
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
testingAIM/aimUpdateState instance = 0!
tess is NULL!
testingAIM/aimPreAnalysis instance = 0!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
getDiscr = -303
meshRef = NULL
testingAIM/aimExecute instance = 0!
testingAIM/aimPostAnalysis instance = 0 restart = 0!
testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0!
aim_getDiscr 0 on Interface = -303
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
testingAIM/aimUpdateState instance = 1!
tess is NULL!
testingAIM/aimPreAnalysis instance = 1!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
mesh file = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/test/autoExecTest/Scratch/testingAIM0/meshFile
symLink = 0
getDiscr = -303
testingAIM/aimExecute instance = 1!
testingAIM/aimPostAnalysis instance = 1 restart = 0!
testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0!
aim_getDiscr 1 on Interface = -303
*** testingAIMout (child) = 12.340000 1 1 ***
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m0.601s
user 0m0.676s
sys 0m1.856s
+ set +x
=============================================
CAPS test (using c-executables) case /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/test/autoExec testingAIM.csm passed (as expected)
=============================================
make -C aim/skeleton test
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/skeleton'
python -u case.py
Loading file into our Problem
Default num = 8.0
Current num = 16.0
aim_newGeometry = 0!
GeometryIn:
1: num 2 (1,1)
2: x 2 (8,1)
3: ymin 2 (8,1)
4: zmin 2 (8,1)
5: zmax 2 (8,1)
GeometryOut:
1: pVol 6 (1,1)
2: cVol 6 (1,1)
AnalysisIn:
1: InputVariable 0 (1,1) (null)
2: num 2 (1,1) (null)
3: Mach 2 (1,1) (null)
4: Mesh_Format 3 (1,1) (null)
5: Table 4 (1,3) (null)
Computed sqrtNum = 4.0
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/aim/skeleton'
# pyCAPS Unit tests (and legacy)
make -C pyCAPS/unitTest test
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/pyCAPS/unitTest'
python --version
Python 3.11.9
python -u -m unittest discover
..Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 143
Number of elements = 282
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 282
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 140
Number of elements = 276
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 276
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 283
Combined Number of elements = 558
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 558
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library - d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 209
Number of elements = 414
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 414
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 186
Number of elements = 368
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 368
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 395
Combined Number of elements = 782
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 782
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
..........--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. CAPS Info: Hit last success -- going live!
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
----------------------------------------------------------------------
Ran 100 tests in 13.081s
OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/pyCAPS/unitTest'
make -C legacy/unitTest test
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/legacy/unitTest'
python --version
Python 3.11.9
python -u -m unittest discover
......sAnalysis Info:
Name = UnitTest_fun3dAIM
Intent = None
AnalysisDir = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM
Version = 1.26
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
Analysis Info:
Name = UnitTest_fun3dAIM
Intent = None
AnalysisDir = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM
Version = 1.26
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_1 will be used!
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_2 will be used!
Analysis Info:
Name = UnitTest7_fun3dAIM
Intent = None
AnalysisDir = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest7_fun3dAIM
Version = 1.26
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_3 will be used!
Analysis Info:
Name = UnitTest8_fun3dAIM
Intent = None
AnalysisDir = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest8_fun3dAIM
Version = 1.26
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_4 will be used!
Analysis Info:
Name = UnitTest9_fun3dAIM
Intent = STRUCTURE
AnalysisDir = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest9_fun3dAIM
Version = 1.26
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_5 will be used!
Analysis Info:
Name = UnitTest10_fun3dAIM
Intent = ['CFD', 'STRUCTURE']
AnalysisDir = /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest10_fun3dAIM
Version = 1.26
Execution Flag = 0
Number of Fields = 8
Field name (Rank):
Pressure ( 1 )
P ( 1 )
Cp ( 1 )
CoefficientOfPressure ( 1 )
Temperature ( 1 )
Displacement ( 3 )
EigenVector ( 3 )
EigenVector_# ( 3 )
Dirty state = 3 - Both analysis and geometry inputs are dirty
...Error: Invalid attribute level! Defaulting to 'Face'
..
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_6 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_7 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_8 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_9 will be used!
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_1 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_10 will be used!
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_2 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_11 will be used!
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_3 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_12 will be used!
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_13 will be used!
...No data transfer method (transferMethod) provided - defaulting to "Interpolate"
No data transfer method (transferMethod) provided - defaulting to "Interpolate"
.No data transfer method (transferMethod) provided - defaulting to "Interpolate"
....No data transfer method (transferMethod) provided - defaulting to "Interpolate"
.No data transfer method (transferMethod) provided - defaulting to "Interpolate"
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.s. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
...Error: Invalid attribute level! Defaulting to 'Face'
........ EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
.... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.s... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.Linked Parameter Beta to analysis fun3d input Beta
Linked Parameter Alpha to analysis fun3d input Alpha
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
7FB5979FF640 Odd Degenerate test for side 1: 9!
7FB5AFE3D000 Odd Degenerate test for side 2: 9!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 408
Number of elements = 812
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 812
Elemental Quad4 = 0
7FB5969FD640 Odd Degenerate test for side 1: 9!
7FB5969FD640 Odd Degenerate test for side 2: 9!
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 623
Number of elements = 1242
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1242
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 1031
Combined Number of elements = 2054
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 2054
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
................
----------------------------------------------------------------------
Ran 72 tests in 3.382s
OK (skipped=3)
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.addAttribute' is deprecated. Please use 'Analysis.attr.create'!
WARNING: 'capsAnalysis.getAttribute' is deprecated. Please use 'Analysis.attr["name"].value'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsAnalysis.getAttributeVal' is deprecated. Please use 'Analysis.geometry.attrList'!
WARNING: 'capsAnalysis.getBoundingBox' is deprecated. Please use 'Analysis.bodies'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.saveGeometry' is deprecated. Please use 'Analysis.geometry.save'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.buildGeometry' is deprecated. Please use 'Problem.geometry.build'!
WARNING: 'capsGeometry.getAttributeMap' is deprecated. Please use 'Problem.geometry.attrMap'!
WARNING: 'capsGeometry.getAttributeVal' is deprecated. Please use 'Problem.geometry.attrList'!
WARNING: 'capsGeometry.getBoundingBox' is deprecated. Please use 'Problem.geometry.bodies'!
WARNING: 'capsGeometry.getGeometryOutVal' is deprecated. Please use 'Problem.geometry.outpmtr["varname"].value'!
WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.saveGeometry' is deprecated. Please use 'Problem.geometry.save'!
WARNING: 'capsGeometry.viewGeometry' is deprecated. Please use 'Problem.geometry.view'!
WARNING: 'capsProblem.addAttribute' is deprecated. Please use 'Problem.attr.create'!
WARNING: 'capsProblem.getAttribute' is deprecated. Please use 'Problem.attr["name"].value'!
WARNING: 'capsProblem.createValue' is deprecated. Please use 'Problem.parameter.create'!
WARNING: '_capsValue.__init__' is deprecated. Please use 'Problem.parameter.create'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
WARNING: 'capsProblem.autoLinkValue' is deprecated. Please use 'Problem.autoLinkParameter'!
Legacy pyCAPS unit testing done!
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/legacy/unitTest'
# CAPS Minimal examples (one per aim)
make -C examples test TYPE=MINIMAL
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/avlTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/awaveTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/frictionTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: Nothing to be done for 'fun3d'.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: 'hsm' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/interferenceTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/msesTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/mystranTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/cCAPS/pointwiseTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples/cCAPS'
(cd /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests
All tests pass!
(cd /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest; ./execute_PyTestRegression.sh MINIMAL)
=================================================
Using python : /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ echo 'abaqus_SingleLoadCase_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
abaqus_SingleLoadCase_PyTest.py test;
+ python -u abaqus_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 49
Number of elements = 36
Number of triangle elements = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes = 49
Total number of elements = 36
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Abaqus grid and connectivity file ....
Finished writing Abaqus grid file
Writing Abaqus instruction file....
Writing properties
Writing materials
Writing constraints
Writing analysis (steps)
Running Abaqus......
Analysis initiated from SIMULIA established products
Abaqus JOB abaqus_CAPS
Abaqus 2023
Abaqus License Manager checked out the following licenses:
Abaqus/Standard checked out 5 tokens from Flexnet server license-4.mit.edu.
<857 out of 1100 licenses remain available>.
Begin Analysis Input File Processor
Thu Jul 25 22:44:18 2024
Run pre
Thu Jul 25 22:44:20 2024
End Analysis Input File Processor
Begin Abaqus/Standard Analysis
Thu Jul 25 22:44:20 2024
Run standard
Thu Jul 25 22:44:22 2024
End Abaqus/Standard Analysis
Begin SIM Wrap-up
Thu Jul 25 22:44:22 2024
Run SMASimUtility
Thu Jul 25 22:44:22 2024
End SIM Wrap-up
Abaqus JOB abaqus_CAPS COMPLETED
Done running Abaqus!
Reading Abaqus DAT file - extracting Mises!
Reading Abaqus DAT file - extracting Displacements!
MISES = [243147500.0, 263053750.0, 305828750.0, 328697500.0, 305828750.0, 263053750.0, 243147500.0, 429271250.0, 735352500.0, 855310000.0, 735352500.0, 429271250.0, 243147500.0, 243147500.0, 328697500.0, 328697500.0, 305828750.0, 263053750.0, 243147500.0, 429271250.0, 735352500.0, 855310000.0, 735352500.0, 429271250.0, 443783125.0, 443783125.0, 443783125.0, 443783125.0, 375120625.0, 502648750.0, 375120625.0, 617621250.0, 502648750.0, 443153750.0, 502648750.0, 443153750.0, 617621250.0, 502648750.0, 375120625.0, 405840833.3333333, 370297500.0, 438917500.0, 370297500.0, 527756250.0, 686105000.0, 527756250.0, 370297500.0, 438917500.0, 399410000.0]
Displacement = [1.3477206e-33, 1.0531118e-33, 6.0715095e-33, 7.4429671e-33, 6.0715062e-33, 1.0531127e-33, 1.3477204e-33, 1.0265013e-32, 1.954589e-32, 2.0157204e-32, 1.9545895e-32, 1.0265011e-32, 1.3477185e-33, 1.0531096e-33, 6.0715071e-33, 7.4429667e-33, 6.0715105e-33, 1.0531132e-33, 1.3477187e-33, 1.0265012e-32, 1.9545896e-32, 2.0157204e-32, 1.9545892e-32, 1.0265015e-32, 0.0093178328, 0.0093178297, 0.0093178328, 0.0093178297, 0.0042233454, 0.0033956155, 0.004223344, 0.011896846, 0.0033956189, 0.010258672, 0.0033956155, 0.010258668, 0.011896846, 0.0033956189, 0.0042233437, 0.0042233424, 0.0015574077, 0.0053518424, 0.0015574093, 0.0036909272, 0.013167546, 0.0036909309, 0.0015574071, 0.0053518403, 0.0015574087]
real 0m6.213s
user 0m3.042s
sys 0m0.945s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case abaqus_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u avl_PyTest.py -outLevel=0
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
CXtot 0.000611907868574681
CYtot -6.289312383470904e-15
CZtot -0.3012861394886091
Cltot -4.782081713039163e-14
Cmtot -0.1945055953450467
Cntot -2.339461801636068e-15
Cl'tot -4.7854363026524e-14
Cn'tot -1.504517153549636e-15
CLtot 0.3012509314150773
CDtot 0.004646353488232845
CDvis 0.0
CLff 0.3009503023520526
CYff -7.719145079534105e-15
CDind 0.004646353488232845
CDff 0.004968969500908293
e 0.9669902146157952
StripForces
Wing cl = [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing cd = [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]
real 0m1.148s
user 0m0.599s
sys 0m0.392s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
Cl = [1.05475230552212, 1.36488869373643, 1.56607214272092, 2.03059709361332, 1.97271083121472, 1.87307153172173, 1.7605047576014]
Cd = [0.0131991208675769, 0.016654024060569, 0.0200551482562873, 0.0458671341846591, 0.07542560093919, 0.0994469174479714, 0.127479430988999]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.496044114214226, 0.461377732041584, 0.442376568201776, 0.361251636069055, 0.276104140854801, 0.214381239320269, 0.132988264746769]
real 0m7.448s
user 0m7.099s
sys 0m0.233s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Cl = 0.37837910855492335
Cd = 0.00777585841721013
Cm = 0.0052626369958117215
real 0m6.699s
user 0m6.290s
sys 0m0.351s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'awave_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
awave_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u awave_PyTest.py -outLevel=0
Writing Awave input file
Body Section, Body ID 1
XCG: 1.571025 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 2
XCG: 2.539271 -3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :RightWingTank
Awave TYPE: 3
Body Section, Body ID 3
XCG: 1.571025 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Body Section, Body ID 4
XCG: 2.539271 3.872983 0.270825
AREA: 0.029452
RAD: 0.096825
ATTRIB:Store
NAME :LeftWingTank
Awave TYPE: 3
Lifting Surface Section, Body ID 5
XLE: 1.571946 -3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 0
Lifting Surface Section, Body ID 6
XLE: 0.000000 0.000000 0.000000
CHORD: 1.614013
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 7
XLE: 1.571946 3.872983 0.249728
CHORD: 0.968408
ATTRIB:Wing
NAME :Wing
Awave TYPE: 1
Lifting Surface Section, Body ID 8
XLE: 5.484123 0.000000 1.468246
CHORD: 0.726185
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 9
XLE: 5.000000 0.000000 0.500000
CHORD: 1.210308
ATTRIB:VTail
NAME :VertTail
Awave TYPE: 4
Lifting Surface Section, Body ID 10
XLE: 5.484123 -0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 0
Lifting Surface Section, Body ID 11
XLE: 5.484123 0.000000 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Lifting Surface Section, Body ID 12
XLE: 5.484123 0.968246 0.500000
CHORD: 0.726185
ATTRIB:HTail
NAME :Stab
Awave TYPE: 5
Body Section, Body ID 13
XCG: -2.000000 0.000000 0.000000
AREA: 0.000000
RAD: 0.000000
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 14
XCG: 0.000000 -0.000000 -0.000000
AREA: 0.818123
RAD: 0.510310
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Warning: capsGroup not found on body 15!
Body Section, Body ID 15
XCG: 1.613743 -0.000000 0.000000
AREA: 0.327249
RAD: 0.322749
ATTRIB:Fuse
NAME :(null)
Awave TYPE: 2
Body Section, Body ID 16
XCG: 5.000000 -0.000000 0.500000
AREA: 0.081812
RAD: 0.161374
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
Body Section, Body ID 17
XCG: 6.210307 -0.000000 0.500000
AREA: 0.000818
RAD: 0.016137
ATTRIB:Fuse
NAME :Fuselage
Awave TYPE: 2
AwaveTypes: 2 5 4 2 2
Points for all four fuselage sections :: 5 0 0 0
Number of Mach-Alpha cases = 2
CdWave = [1.13332772, 0.216380954]
real 0m0.648s
user 0m0.623s
sys 0m0.318s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u friction_PyTest.py -outLevel=0
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
real 0m0.480s
user 0m0.483s
sys 0m0.316s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go. Other input will terminate the job.
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Cl = 0.933329
Cd = 0.000283
Cd Wave = 0.0
Cm = -0.203433
Cp _Critcal = -1.303869
real 0m0.547s
user 0m0.454s
sys 0m0.253s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u delaundo_PyTest.py -outLevel=0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Getting mesh sizing parameters
Mesh sizing name - Airfoil
Mesh sizing name - AirfoilTE
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m0.861s
user 0m0.897s
sys 0m2.016s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'egadsTess_PyTest.py test;'
egadsTess_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u egadsTess_PyTest.py -outLevel=0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting mesh sizing parameters
Mesh sizing name - LeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes = 3793
Number of elements = 4001
Number of triangle elements = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 76
Number of elements = 55
Number of triangle elements = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes = 100
Number of elements = 73
Number of triangle elements = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes = 3970
Total number of elements = 4129
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m7.745s
user 0m23.401s
sys 0m28.142s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:33PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 316 634
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 681 1018
AFLR2 GGp: Nodes, Faces = 1013 1682
AFLR2 GGp: Nodes, Faces = 1339 2334
AFLR2 GGp: Nodes, Faces = 1652 2960
AFLR2 GGp: Nodes, Faces = 1957 3570
AFLR2 GGp: Nodes, Faces = 2252 4160
AFLR2 GGp: Nodes, Faces = 2526 4708
AFLR2 GGp: Nodes, Faces = 2809 5274
AFLR2 GGp: Nodes, Faces = 3083 5822
AFLR2 GGp: Nodes, Faces = 3327 6310
AFLR2 GGp: Nodes, Faces = 3564 6784
AFLR2 GGp: Nodes, Faces = 3788 7232
AFLR2 GGp: Nodes, Faces = 3995 7646
AFLR2 GGp: Nodes, Faces = 4194 8044
AFLR2 GGp: Nodes, Faces = 4394 8444
AFLR2 GGp: Nodes, Faces = 4585 8826
AFLR2 GGp: Nodes, Faces = 4772 9200
AFLR2 GGp: Nodes, Faces = 4943 9542
AFLR2 GGp: Nodes, Faces = 5129 9914
AFLR2 GGp: Nodes, Faces = 5293 10242
AFLR2 GGp: Nodes, Faces = 5447 10550
AFLR2 GGp: Nodes, Faces = 5594 10844
AFLR2 GGp: Nodes, Faces = 5716 11088
AFLR2 GGp: Nodes, Faces = 5830 11316
AFLR2 GGp: Nodes, Faces = 5909 11474
AFLR2 GGp: Nodes, Faces = 5964 11584
AFLR2 GGp: Nodes, Faces = 6006 11668
AFLR2 GGp: Nodes, Faces = 6025 11706
AFLR2 GGp: Nodes, Faces = 6034 11724
AFLR2 : CPU Time = 0.017 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 6034 11724
AFLR2 QI : Nodes, Faces = 6033 454
AFLR2 QI : Nodes, Faces = 6033 5634
AFLR2 QI : Nodes, Faces = 6033 11722
AFLR2 QI : Nodes, Faces = 6032 462
AFLR2 QI : Nodes, Faces = 6032 5629
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 456
AFLR2 QI : Nodes, Faces = 6032 5632
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 474
AFLR2 QI : Nodes, Faces = 6032 5623
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6031 486
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 QI : Nodes, Faces = 6031 488
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 : CPU Time = 0.009 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
real 0m0.785s
user 0m0.948s
sys 0m3.751s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:33PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:42PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 150512
Number of elements = 451696
Number of triangles = 14380
Number of quadrilatarals = 0
Number of tetrahedrals = 216264
Number of pyramids = 427
Number of prisms = 220625
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m18.596s
user 0m17.765s
sys 0m0.588s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 2236
Number of elements = 4468
Number of triangle elements = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 636
Number of elements = 1268
Number of triangle elements = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 267
Number of elements = 530
Number of triangle elements = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3139
Total number of elements = 6266
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 3139, elements - 6266
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.029781
Creating surface mesh ...
Surface mesh seconds: 0.00696
Recovering boundaries...
Boundary recovery seconds: 0.067459
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.009958
Suppressing Steiner points ...
Steiner suppression seconds: 1.7e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.012877
Refining mesh...
4190 insertions, added 2180 points, 134280 tetrahedra in queue.
1395 insertions, added 459 points, 138994 tetrahedra in queue.
1859 insertions, added 487 points, 137112 tetrahedra in queue.
2478 insertions, added 498 points, 120303 tetrahedra in queue.
3304 insertions, added 499 points, 74342 tetrahedra in queue.
4404 insertions, added 474 points, 460 tetrahedra in queue.
Refinement seconds: 0.893695
Smoothing vertices...
Mesh smoothing seconds: 0.524066
Improving mesh...
Mesh improvement seconds: 0.013611
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.002624
Total running seconds: 1.56125
Statistics:
Input points: 3139
Input facets: 6266
Input segments: 9399
Input holes: 2
Input regions: 0
Mesh points: 8309
Mesh tetrahedra: 41161
Mesh faces: 85455
Mesh faces on exterior boundary: 6266
Mesh faces on input facets: 6266
Mesh edges on input segments: 9399
Steiner points inside domain: 5170
Done meshing using TetGen!
Writing Tecplot file ....
Finished writing Tecplot file
real 0m2.968s
user 0m3.264s
sys 0m0.347s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:33PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 545 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 545 545
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 110 222
AFLR2 IG : Nodes, Faces = 220 442
AFLR2 IG : Nodes, Faces = 330 662
AFLR2 IG : Nodes, Faces = 440 882
AFLR2 IG : Nodes, Faces = 517 1036
AFLR2 IG : Nodes, Faces = 545 1092
AFLR2 IG : Nodes, Faces = 549 1092
AFLR2 IG : Nodes, Faces = 545 545
AFLR2 : CPU Time = 0.002 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 545 545
AFLR2 GGp: Nodes, Faces = 1083 1621
AFLR2 GGp: Nodes, Faces = 1616 2687
AFLR2 GGp: Nodes, Faces = 2144 3743
AFLR2 GGp: Nodes, Faces = 2661 4777
AFLR2 GGp: Nodes, Faces = 3171 5797
AFLR2 GGp: Nodes, Faces = 3672 6799
AFLR2 GGp: Nodes, Faces = 4158 7771
AFLR2 GGp: Nodes, Faces = 4653 8761
AFLR2 GGp: Nodes, Faces = 5142 9739
AFLR2 GGp: Nodes, Faces = 5608 10671
AFLR2 GGp: Nodes, Faces = 6055 11565
AFLR2 GGp: Nodes, Faces = 6482 12419
AFLR2 GGp: Nodes, Faces = 6880 13215
AFLR2 GGp: Nodes, Faces = 7257 13969
AFLR2 GGp: Nodes, Faces = 7614 14683
AFLR2 GGp: Nodes, Faces = 7947 15349
AFLR2 GGp: Nodes, Faces = 8276 16007
AFLR2 GGp: Nodes, Faces = 8575 16605
AFLR2 GGp: Nodes, Faces = 8869 17193
AFLR2 GGp: Nodes, Faces = 9140 17735
AFLR2 GGp: Nodes, Faces = 9401 18257
AFLR2 GGp: Nodes, Faces = 9654 18763
AFLR2 GGp: Nodes, Faces = 9887 19229
AFLR2 GGp: Nodes, Faces = 10110 19675
AFLR2 GGp: Nodes, Faces = 10315 20085
AFLR2 GGp: Nodes, Faces = 10497 20449
AFLR2 GGp: Nodes, Faces = 10656 20767
AFLR2 GGp: Nodes, Faces = 10791 21037
AFLR2 GGp: Nodes, Faces = 10919 21293
AFLR2 GGp: Nodes, Faces = 11022 21499
AFLR2 GGp: Nodes, Faces = 11092 21639
AFLR2 GGp: Nodes, Faces = 11145 21745
AFLR2 GGp: Nodes, Faces = 11156 21767
AFLR2 : CPU Time = 0.046 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 11156 21767
AFLR2 QI : Nodes, Faces = 11155 819
AFLR2 QI : Nodes, Faces = 11155 10473
AFLR2 QI : Nodes, Faces = 11155 21765
AFLR2 QI : Nodes, Faces = 11154 811
AFLR2 QI : Nodes, Faces = 11154 10476
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11154 805
AFLR2 QI : Nodes, Faces = 11154 10479
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11154 911
AFLR2 QI : Nodes, Faces = 11154 10426
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11153 915
AFLR2 QI : Nodes, Faces = 11153 10423
AFLR2 QI : Nodes, Faces = 11153 917
AFLR2 QI : Nodes, Faces = 11153 10423
AFLR2 : CPU Time = 0.017 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 49.3184| 90|
| CV Face Area Aspect Ratio| 1.00035| 33.4982|
| CV Sub-Volume Ratio| 1.00001| 7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11153| 1/1.00| 10|
| 1| 2702| 1/4.13| 7.38309|
| 2| 549| 1/4.92| 4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 9.3726e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 9.1606e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 9.1598e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 9.1223e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 9.1530e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 9.1460e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.1216e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 9.1357e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 9.1608e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 9.1723e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.22124| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file |surface_flow_pyCAPS_su2_aflr2.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary |flow_pyCAPS_su2_aflr2.szplt |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.072253 Cd = -0.01151
Cmz = 0.070975
Cx = -0.01151 Cy = 0.072253
Pressure Contribution
Cl_p = 0.072253 Cd_p = -0.01151
Cmz_p = 0.070975
Cx_p = -0.01151 Cy_p = 0.072253
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m2.280s
user 0m2.241s
sys 0m5.745s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 3.796888
Tessellating body 1 with MaxEdge = 0.094922 Sag = 0.003797 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9 > autoInputs.out
Executing: ./aero.csh > aero.out
C_A 0.029869406
C_Y -0.0013620922
C_N 0.060708385
C_D 0.031969903
C_S -0.0013620922
C_L 0.059628976
C_l 0.0472604
C_m -0.000208726
C_n -0.022715
C_M_x 0.0464388
C_M_y -0.000208726
C_M_z -0.0243505
real 0m21.715s
user 0m43.747s
sys 0m6.977s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Getting results mass properties.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Area 3.428666259747
Mass 5383.006027803
Centroid [1.222256036874, 0.1634981473778, -4.234505810751e-11]
CG [1.222256036874, 0.1634981473778, -4.234637807833e-11]
Ixx 22133.97306033
Iyy 23448.30046709
Izz 1389.213122582
Ixy 164.2055275657
Ixz -7.45484669011e-06
Iyz 1.707686795832e-06
I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.45484669011e-06, 1.707686795832e-06]
II [[22133.97306033, -164.2055275657, 7.45484669011e-06], [-164.2055275657, 23448.30046709, -1.707686795832e-06], [7.45484669011e-06, -1.707686795832e-06, 1389.213122582]]
real 0m8.605s
user 0m14.466s
sys 0m54.328s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
real 0m0.878s
user 0m0.758s
sys 0m0.152s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'mystran_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
mystran_PyTest.py test;
+ python -u mystran_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Getting results for natural frequencies.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 293
Number of elements = 217
Number of triangle elements = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes = 293
Total number of elements = 217
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 293
Number of elements = 217
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 217
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Load tuple is NULL - No loads applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing MYSTRAN instruction file....
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Natural freq ( Mode 0 ) = 0.5358645270129999 (Hz)
Natural freq ( Mode 1 ) = 0.5358645288000637 (Hz)
Natural freq ( Mode 2 ) = 2.6579076333816722 (Hz)
Natural freq ( Mode 3 ) = 2.6579076480186012 (Hz)
Natural freq ( Mode 4 ) = 3.2133127087218645 (Hz)
Natural freq ( Mode 5 ) = 3.213312711432576 (Hz)
Natural freq ( Mode 6 ) = 3.7128431161841053 (Hz)
Natural freq ( Mode 7 ) = 3.7128431173689016 (Hz)
Natural freq ( Mode 8 ) = 6.903423804863681 (Hz)
Natural freq ( Mode 9 ) = 6.903423839346651 (Hz)
Natural freq ( Mode 10 ) = 8.82720702524307 (Hz)
Natural freq ( Mode 11 ) = 8.82720703135989 (Hz)
Natural freq ( Mode 12 ) = 9.03449773735593 (Hz)
Natural freq ( Mode 13 ) = 9.034497746243224 (Hz)
Natural freq ( Mode 14 ) = 12.810955940857177 (Hz)
Natural freq ( Mode 15 ) = 12.810955955283573 (Hz)
Natural freq ( Mode 16 ) = 14.595903948633964 (Hz)
Natural freq ( Mode 17 ) = 14.595903960059545 (Hz)
Natural freq ( Mode 18 ) = 17.253138348969568 (Hz)
Natural freq ( Mode 19 ) = 17.253138376627454 (Hz)
Natural freq ( Mode 20 ) = 19.538997521006213 (Hz)
Natural freq ( Mode 21 ) = 19.538997554215 (Hz)
Natural freq ( Mode 22 ) = 20.56830732889029 (Hz)
Natural freq ( Mode 23 ) = 20.568307348661286 (Hz)
Natural freq ( Mode 24 ) = 21.246868655916405 (Hz)
Natural freq ( Mode 25 ) = 21.246868660548955 (Hz)
Natural freq ( Mode 26 ) = 26.05608998380775 (Hz)
Natural freq ( Mode 27 ) = 26.05609000311102 (Hz)
Natural freq ( Mode 28 ) = 28.34916233211744 (Hz)
Natural freq ( Mode 29 ) = 28.349162400361656 (Hz)
Natural freq ( Mode 30 ) = 30.373999863572596 (Hz)
Natural freq ( Mode 31 ) = 30.3740000570112 (Hz)
Natural freq ( Mode 32 ) = 33.67251107901609 (Hz)
Natural freq ( Mode 33 ) = 33.672511087829136 (Hz)
Natural freq ( Mode 34 ) = 36.20316316648002 (Hz)
Natural freq ( Mode 35 ) = 36.20316318963648 (Hz)
Natural freq ( Mode 36 ) = 37.22279209381622 (Hz)
Natural freq ( Mode 37 ) = 37.22279210262193 (Hz)
Natural freq ( Mode 38 ) = 39.81809493912653 (Hz)
Natural freq ( Mode 39 ) = 39.81809513541885 (Hz)
Natural freq ( Mode 40 ) = 41.66707106123649 (Hz)
Natural freq ( Mode 41 ) = 41.66707106540778 (Hz)
Natural freq ( Mode 42 ) = 44.898935274249375 (Hz)
Natural freq ( Mode 43 ) = 44.89893529616552 (Hz)
Natural freq ( Mode 44 ) = 47.60456384135717 (Hz)
Natural freq ( Mode 45 ) = 47.604564003760714 (Hz)
Natural freq ( Mode 46 ) = 49.15118222293705 (Hz)
Natural freq ( Mode 47 ) = 49.15118223337741 (Hz)
real 0m12.668s
user 0m18.947s
sys 2m10.597s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mystran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Traceback (most recent call last):
File "/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/pyCAPS/corsairlite/core/pint_custom/registry.py", line 526, in load_definitions
ref = importlib_resources.files(__name__).joinpath(file)
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/importlib/resources/_common.py", line 22, in files
return from_package(get_package(package))
^^^^^^^^^^^^^^^^^^^^
File "/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/importlib/resources/_common.py", line 55, in get_package
raise TypeError(f'{package!r} is not a package')
TypeError: 'corsairlite.core.pint_custom.registry' is not a package
During handling of the above exception, another exception occurred:
Traceback (most recent call last):
File "/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/ESP/LINUX64/examples/pyCAPS/../corsairlite/qp.py", line 1, in <module>
from corsairlite import units
File "/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/pyCAPS/corsairlite/__init__.py", line 5, in <module>
units = UnitRegistry()
^^^^^^^^^^^^^^
File "/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/pyCAPS/corsairlite/core/pint_custom/registry.py", line 112, in __call__
obj._after_init()
File "/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/pyCAPS/corsairlite/core/pint_custom/registry.py", line 1858, in _after_init
super()._after_init()
File "/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/pyCAPS/corsairlite/core/pint_custom/registry.py", line 262, in _after_init
self.load_definitions("default_en.txt", True)
File "/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/pyCAPS/corsairlite/core/pint_custom/registry.py", line 541, in load_definitions
raise ValueError("While opening {}\n{}".format(file, msg))
ValueError: While opening default_en.txt
'corsairlite.core.pint_custom.registry' is not a package
real 0m0.241s
user 0m0.284s
sys 0m0.295s
+ status=1
+ set +x
=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py failed (as NOT expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
Astros
=================================================
=================================================
Summary of examples NOT finished as expected
../corsairlite/qp.py
See pyCAPSlog.txt for more details.
=================================================
make[1]: *** [Makefile:56: pyCAPStest] Error 1
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.7/LINUX64.gnu12/CAPS/examples'
make: *** [Makefile:60: testcommit] Error 2
Build step 'Conditional step (single)' marked build as failure
[GNU C Compiler (gcc)ClangMSBuild] Skipping execution of recorder since overall result is 'FAILURE'
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: FAILURE