Console Output

Skipping 347 KB.. Full Log
	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	0m0.224s
user	0m0.148s
sys	0m0.008s
+ set +x

=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/miscUtilsTest passed (as expected)
=============================================

+ expectCSuccess /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest
+ /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest
vlmUtils Tests passed!

real	0m0.234s
user	0m0.155s
sys	0m0.008s
+ set +x

=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest passed (as expected)
=============================================

+ rm -rf aimTest
+ expectCSuccess '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm'
+ /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm
 Root Path = /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/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   = /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/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 = 1962!
 testingAIM/aimDiscr: npts = 1040!
 testingAIM/aimDiscr: tname = Interface, instance = 0!
 testingAIM/aimDiscr: Tessellation set!
 testingAIM/aimDiscr: Body 1/Face 6 matches Interface!
 testingAIM/aimDiscr: ntris = 790!
 testingAIM/aimDiscr: npts = 442!
 testingAIM/aimTransfer name = scalar  instance = 0  npts = 442/1!
 CAPS Info: Bound 'Interface' Normalized Integrated 'scalar'
            Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 3.844036e-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 macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  1
   hist: (null) -> Initial Phase
         aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  1
   2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds

   ParamName has type VALUE, subtype PARAMETER with 0 attributes
     last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  2
     hist: (null) -> Starting
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  2
     value = 0.000000 (null)
   Param has type VALUE, subtype PARAMETER with 0 attributes
     last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  3
     hist: (null) -> Starting
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  3
     value = 99 (null)

   num has type VALUE, subtype GEOMETRYIN with 0 attributes
     last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  6
     hist: (null) -> Initial Phase
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  1
     hist: (null) -> Starting
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  6
     value = 8.000000 (null)
   x has type VALUE, subtype GEOMETRYIN with 0 attributes
     last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  1
     hist: (null) -> Initial Phase
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  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 macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  1
     hist: (null) -> Initial Phase
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  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 macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  1
     hist: (null) -> Initial Phase
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  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 macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  1
     hist: (null) -> Initial Phase
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  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 macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  7
     hist: (null) -> Initial Phase
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  1
     hist: (null) -> Starting
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  7
     linked to ParamName

   pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
     last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  16
     hist: (null) -> Starting
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  16
     value = 34.641525 (null)
   cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
     last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  16
     hist: (null) -> Starting
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  16
     value = 7.296560 (null)

   testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes
     last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  18
     hist: (null) -> Starting
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  18
     4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
     1 Bodies, 1 Tessellations

     testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  8
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  8
       value = 5.000000 cm
     table has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  8
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  8
       value (1x3) =
        1: Entry1 -> Value1
        2: Entry2 -> Value2
        3: Entry3 -> Value3
     tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  8
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  8
       value (0x0) = NULL with len = 0 ego
     meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  8
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  8
       value (0x0) = NULL with len = 0 writer

     testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  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 macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  18
     tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  18
       hist: (null) -> Child Execute
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  18
       value (0x0) = NULL with len = 0 ego
     meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  9
 testingAIM/aimCalcOutput instance = 0  index = 3 meshFile 0!
       value (0x0) = NULL with len = 0 writer
       lazy: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  18

     Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  18
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  18
       value = 42 (null)
   testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes
     last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  28
     hist: (null) -> Starting
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
     hist: (null) -> Child Execute
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  28
     4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
     1 Bodies, 1 Tessellations

     testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  10
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  10
       value = 6.000000 cm
     table has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  12
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  12
       value (1x3) =
        1: Entry1 -> newValue1
        2: Entry2 -> newValue2
        3: Entry3 -> newValue3
     tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  18
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  13
       hist: (null) -> Child Execute
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
       linked to tessOut
     meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  10
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  10
       value (0x0) = NULL with len = 0 writer

     testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  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 macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  28
     tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  11
 testingAIM/aimCalcOutput instance = 1  index = 2 tessOut 0!
 tessPtr = 6000024fc240
       value = 6000024fc240 ego
       lazy: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  28
     meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  11
 testingAIM/aimCalcOutput instance = 1  index = 3 meshFile 0!
       value (0x0) = NULL with len = 0 writer
       lazy: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  28

     Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  28
       hist: (null) -> Child Execute
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  28
       value = 42 (null)

   Interface has type BOUND, subtype NONE with 0 attributes
     last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
     hist: (null) -> Starting
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  14
     hist: (null) -> Child Execute
           aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
     2 Connecteds, 0 UnConnecteds

     testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
       hist: (null) -> Child Execute
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
       5 DataSets

       xyz has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Child Execute
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
         1040 points, rank=3, units=cm
       xyzd has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         0 points, rank=3, units=(null)
       param has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Child Execute
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
         1040 points, rank=2, units=(null)
       paramd has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         0 points, rank=2, units=(null)
       scalar has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  26
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  15
         hist: (null) -> Child Execute
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:41  26
         1040 points, rank=1, units=(null)
     testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes
       last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
       hist: (null) -> Starting
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
       hist: (null) -> Child Execute
             aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
       6 DataSets

       xyz has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Child Execute
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
         442 points, rank=3, units=cm
       xyzd has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         0 points, rank=3, units=(null)
       param has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Child Execute
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  23
         442 points, rank=2, units=(null)
       paramd has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         0 points, rank=2, units=(null)
       scalar has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  25
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Child Execute
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  25
         442 points, rank=1, units=(null)
       vector has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
         hist: (null) -> Starting
               aimTest macys.mit.edu:86388 jenkins  2022/11/30  23:06:30  0
 testingAIM/aimTransfer name = vector  instance = 0  npts = 442/3!
         442 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 14.400000 14.400000 14.381076 14.400000
   15: 14.400000 14.385654 14.400000 14.386399 14.400000 14.400000 14.400000
   22: 14.400000 14.400000 14.400000 14.383470 14.400000 14.400000 14.400000
   29: 14.400000 14.390663 14.400000 14.400000 14.400000 14.400000 14.400000
   36: 14.400000 14.400000 14.390526 14.400000 14.400000 14.400000 14.400000
   43: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   50: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   57: 14.400000 14.400000 14.400000 14.400000 14.377038 14.400000 14.377947
   64: 14.400000 14.378370 14.400000 14.380439 14.400000 14.400000 14.400000
   71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   78: 14.390431 14.400000 14.400000 14.400000 14.391064 14.400000 14.384912
   85: 14.400000 14.400000 14.400000 14.400000 14.400000 14.390113 14.400000
   92: 14.400000 14.400000 14.400000 14.400000 14.388870 14.400000 14.400000
   99: 14.400000 14.400000 14.386035 14.400000 14.384898 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 14.400000 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: 14.400000 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: 14.382997 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 14.356448 14.400000 14.400000 14.400000
  386: 14.400000 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: 14.400000 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 14.360432 14.400000 14.400000 14.400000 14.400000 14.400000
  456: 14.400000 14.400000 14.363710 14.400000 14.400000 14.400000 14.400000
  463: 14.400000 14.400000 14.364299 14.400000 14.400000 14.400000 14.400000
  470: 14.400000 14.400000 14.400000 14.363289 14.400000 14.400000 14.362208
  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: 14.400000 14.400000 14.400000 14.365678 14.400000 14.400000 14.400000
  498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.363289 14.400000
  505: 14.400000 14.400000 14.400000 14.361522 14.400000 14.368098 14.400000
  512: 14.400000 14.363976 14.400000 14.400000 14.370432 14.400000 14.400000
  519: 14.400000 14.400000 14.400000 14.400000 14.400000 14.363968 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 14.363289 14.400000 14.400000 14.363979 14.366708
  547: 14.368597 14.400000 14.400000 14.400000 14.400000 14.367920 14.400000
  554: 14.372633 14.400000 14.400000 14.400000 14.400000 14.362154 14.400000
  561: 14.400000 14.400000 14.400000 14.400000 14.400000 14.366708 14.400000
  568: 14.369034 14.400000 14.369841 14.371226 14.400000 14.400000 14.400000
  575: 14.400000 14.400000 14.368408 14.367520 14.400000 14.368432 14.400000
  582: 14.400000 14.400000 14.400000 14.366087 14.400000 14.400000 14.369959
  589: 14.367920 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  596: 14.369369 14.368144 14.400000 14.400000 14.400000 14.400000 14.400000
  603: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  610: 14.367841 14.372775 14.400000 14.400000 14.400000 14.372125 14.378179
  617: 14.400000 14.400000 14.400000 14.400000 14.369095 14.400000 14.400000
  624: 14.400000 14.400000 14.400000 14.400000 14.400000 14.367920 14.371353
  631: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  638: 14.400000 14.400000 14.400000 14.400000 14.377272 14.376093 14.400000
  645: 14.372738 14.400000 14.400000 14.370290 14.400000 14.400000 14.400000
  652: 14.400000 14.365824 14.376750 14.400000 14.371580 14.368734 14.400000
  659: 14.373031 14.400000 14.371453 14.400000 14.376424 14.373411 14.375742
  666: 14.379766 14.400000 14.400000 14.372722 14.400000 14.400000 14.372350
  673: 14.400000 14.369868 14.400000 14.379928 14.400000 14.400000 14.400000
  680: 14.400000 14.400000 14.372894 14.375220 14.400000 14.400000 14.400000
  687: 14.400000 14.400000 14.400000 14.379491 14.373945 14.373477 14.373204
  694: 14.369160 14.400000 14.400000 14.371245 14.400000 14.370144 14.400000
  701: 14.400000 14.367593 14.400000 14.400000 14.400000 14.400000 14.400000
  708: 14.377553 14.400000 14.400000 14.372777 14.400000 14.400000 14.400000
  715: 14.400000 14.374692 14.400000 14.400000 14.400000 14.373031 14.375837
  722: 14.400000 14.400000 14.370074 14.400000 14.380072 14.400000 14.400000
  729: 14.400000 14.400000 14.375022 14.372158 14.400000 14.373856 14.380242
  736: 14.400000 14.377974 14.400000 14.400000 14.380573 14.400000 14.400000
  743: 14.400000 14.400000 14.400000 14.370484 14.372158 14.375910 14.400000
  750: 14.381582 14.375912 14.400000 14.400000 14.379288 14.400000 14.373737
  757: 14.400000 14.400000 14.400000 14.379729 14.382285 14.378584 14.400000
  764: 14.382311 14.400000 14.400000 14.374409 14.371245 14.379232 14.373945
  771: 14.400000 14.376341 14.400000 14.400000 14.377043 14.378486 14.374858
  778: 14.382054 14.400000 14.383869 14.381636 14.377184 14.400000 14.400000
  785: 14.400000 14.372636 14.400000 14.368456 14.383921 14.400000 14.400000
  792: 14.383458 14.400000 14.400000 14.400000 14.400000 14.400000 14.381953
  799: 14.400000 14.374858 14.373072 14.378348 14.379772 14.400000 14.378216
  806: 14.378852 14.400000 14.400000 14.400000 14.380161 14.400000 14.400000
  813: 14.384556 14.381516 14.400000 14.376255 14.400000 14.380120 14.400000
  820: 14.400000 14.380472 14.379996 14.400000 14.373072 14.400000 14.373126
  827: 14.379728 14.388089 14.378410 14.377743 14.383644 14.400000 14.400000
  834: 14.381170 14.377592 14.376925 14.384404 14.383167 14.400000 14.382056
  841: 14.400000 14.383692 14.400000 14.383013 14.384733 14.400000 14.400000
  848: 14.400000 14.380633 14.400000 14.400000 14.400000 14.373808 14.381358
  855: 14.400000 14.400000 14.383124 14.400000 14.400000 14.385360 14.376255
  862: 14.373590 14.400000 14.383049 14.386052 14.382506 14.381131 14.383698
  869: 14.384781 14.379968 14.383657 14.384709 14.377957 14.400000 14.380975
  876: 14.400000 14.375227 14.400000 14.379017 14.378731 14.378357 14.376010
  883: 14.373652 14.383370 14.383357 14.385444 14.385424 14.381819 14.384645
  890: 14.379402 14.389897 14.380433 14.400000 14.383857 14.385410 14.384756
  897: 14.379335 14.385835 14.400000 14.385091 14.374477 14.383079 14.383855
  904: 14.380149 14.374722 14.383296 14.381983 14.376090 14.383810 14.378363
  911: 14.387375 14.383245 14.378412 14.383393 14.382951 14.382465 14.382804
  918: 14.384507 14.385472 14.385336 14.385820 14.384140 14.385028 14.385702
  925: 14.383042 14.388214 14.388256 14.382050 14.381706 14.379795 14.381159
  932: 14.381897 14.378803 14.384372 14.381369 14.386079 14.387357 14.385924
  939: 14.382744 14.381612 14.381032 14.386745 14.385849 14.379042 14.385090
  946: 14.400000 14.381764 14.381240 14.379650 14.385693 14.385693 14.386153
  953: 14.384626 14.387791 14.385449 14.400000 14.385665 14.400000 14.379731
  960: 14.380272 14.385409 14.385781 14.381733 14.382438 14.385533 14.380583
  967: 14.386516 14.384573 14.400000 14.378382 14.384594 14.400000 14.386153
  974: 14.382680 14.389375 14.386802 14.381707 14.379398 14.380377 14.386666
  981: 14.387596 14.388630 14.387987 14.379180 14.386395 14.386595 14.400000
  988: 14.385128 14.382720 14.381637 14.387158 14.381496 14.389287 14.386767
  995: 14.382154 14.388300 14.384113 14.381877 14.390676 14.383198 14.387762
 1002: 14.386642 14.388993 14.383485 14.387635 14.390869 14.381952 14.382376
 1009: 14.381221 14.379752 14.400000 14.382249 14.378060 14.383886 14.382511
 1016: 14.387091 14.386270 14.384482 14.387626 14.381697 14.387252 14.400000
 1023: 14.378331 14.384910 14.381021 14.388566 14.400000 14.388325 14.387032
 1030: 14.378428 14.387252 14.379752 14.400000 14.384558 14.384911 14.381221
 1037: 14.378848 14.384694 14.382523 14.382981
 source getTriangles = 0, nGtris = 1962, nGsegs = 5886, Ds = 0 0
 destin getTriangles = 0, nGtris = 790, nGsegs = 2370, Ds = 0 0
 testingAIM/aimCleanup   instance = 0!
 testingAIM/aimCleanup   instance = 1!

real	0m12.181s
user	0m11.537s
sys	0m0.294s
+ set +x

=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm passed (as expected)
=============================================

+ rm -rf source.vs destin.vs
+ expectCSuccess '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm'
+ /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm

 testingAIM/aimInitialize  instance = 0  unitSys = m!
 testingAIM/aimInputs instance = 0  index = 1!
 testingAIM/aimInputs instance = 0  index = 2!
 testingAIM/aimInputs instance = 0  index = 3!
 testingAIM/aimInputs instance = 0  index = 4!
 testingAIM/aimOutputs instance = 0  index = 1!
 testingAIM/aimOutputs instance = 0  index = 2!
 testingAIM/aimOutputs instance = 0  index = 3!

 testingAIM/aimInitialize  instance = 1  unitSys = (null)!
 testingAIM/aimInputs instance = 1  index = 1!
 testingAIM/aimInputs instance = 1  index = 2!
 testingAIM/aimInputs instance = 1  index = 3!
 testingAIM/aimInputs instance = 1  index = 4!
 testingAIM/aimOutputs instance = 1  index = 1!
 testingAIM/aimOutputs instance = 1  index = 2!
 testingAIM/aimOutputs instance = 1  index = 3!

 Intent  = child
 APath   = /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/test/autoExecTest/Scratch/testingAIM1
 UnitSys = (null)
 Exec    = 2
 Fields  =  scalar (1 1)  vector (3 1)  scalar (1 0)  vector (3 0)
 Dirty   =  3

 testingAIM/aimUpdateState instance = 0!
   tess is NULL!
 testingAIM/aimPreAnalysis instance = 0!
 testingAIM/aimPreAnalysis aim_getBounds = 0
     aim_newGeometry = 0!
   getDiscr = -303
   meshRef = NULL
 testingAIM/aimExecute instance = 0!
 testingAIM/aimPostAnalysis instance = 0  restart = 0!
 testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
 testingAIM/aimCalcOutput instance = 0  index = 1 testingAIMout 0!
 aim_getDiscr 0 on Interface = -303
 testingAIM/aimCalcOutput instance = 0  index = 3 meshFile 0!
 testingAIM/aimUpdateState instance = 1!
   tess is NULL!
 testingAIM/aimPreAnalysis instance = 1!
 testingAIM/aimPreAnalysis aim_getBounds = 0
     aim_newGeometry = 0!
   mesh file = /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/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	0m0.746s
user	0m0.616s
sys	0m0.153s
+ set +x

=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm passed (as expected)
=============================================

/Library/Developer/CommandLineTools/usr/bin/make -C aim/skeleton test
python -u case.py
Loading file into our Problem
Default num = 8.0
Current num = 16.0
             aim_newGeometry = 0!
   GeometryIn:
       1: num  2  (1,1)
       2: x  2  (8,1)
       3: ymin  2  (8,1)
       4: zmin  2  (8,1)
       5: zmax  2  (8,1)

   GeometryOut:
       1: pVol  6  (1,1)
       2: cVol  6  (1,1)

   AnalysisIn:
       1: InputVariable  0  (1,1) (null)
       2: num  2  (1,1) (null)
       3: Mach  2  (1,1) (null)
       4: Mesh_Format  3  (1,1) (null)
       5: Table  4  (1,3) (null)

Computed sqrtNum = 4.0
# pyCAPS Unit tests (and legacy)
/Library/Developer/CommandLineTools/usr/bin/make -C pyCAPS/unitTest test
python --version
Python 3.9.13
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
Creating FEA BEM
	Mesh for body = 0
	Number of nodal coordinates = 265
	Number of elements = 526
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 526
	Elemental Quad4 = 0
Creating FEA BEM
	Mesh for body = 1
	Number of nodal coordinates = 265
	Number of elements = 526
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 526
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 530
	Combined Number of elements = 1052
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 1052
	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
Creating FEA BEM
	Mesh for body = 0
	Number of nodal coordinates = 533
	Number of elements = 1062
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1062
	Elemental Quad4 = 0
Creating FEA BEM
	Mesh for body = 1
	Number of nodal coordinates = 533
	Number of elements = 1062
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1062
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1066
	Combined Number of elements = 2124
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 2124
	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 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 -> __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 18.318s

OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
/Library/Developer/CommandLineTools/usr/bin/make -C legacy/unitTest test
python --version
Python 3.9.13
python -u -m unittest discover
......sAnalysis Info:
	Name           =  UnitTest_fun3dAIM
	Intent         =  None
	AnalysisDir    =  /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM
	Version        =  1.22
	Execution Flag =  0
	Number of Fields =  7
	Field name (Rank):
	  Pressure ( 1 )
	  P ( 1 )
	  Cp ( 1 )
	  CoefficientOfPressure ( 1 )
	  Displacement ( 3 )
	  EigenVector ( 3 )
	  EigenVector_# ( 3 )
	Dirty state    =  3  -  Both analysis and geometry inputs are dirty
Analysis Info:
	Name           =  UnitTest_fun3dAIM
	Intent         =  None
	AnalysisDir    =  /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM
	Version        =  1.22
	Execution Flag =  0
	Number of Fields =  7
	Field name (Rank):
	  Pressure ( 1 )
	  P ( 1 )
	  Cp ( 1 )
	  CoefficientOfPressure ( 1 )
	  Displacement ( 3 )
	  EigenVector ( 3 )
	  EigenVector_# ( 3 )
	Dirty state    =  3  -  Both analysis and geometry inputs are dirty
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_1 will be used!

Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_2 will be used!
Analysis Info:
	Name           =  UnitTest7_fun3dAIM
	Intent         =  None
	AnalysisDir    =  /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest7_fun3dAIM
	Version        =  1.22
	Execution Flag =  0
	Number of Fields =  7
	Field name (Rank):
	  Pressure ( 1 )
	  P ( 1 )
	  Cp ( 1 )
	  CoefficientOfPressure ( 1 )
	  Displacement ( 3 )
	  EigenVector ( 3 )
	  EigenVector_# ( 3 )
	Dirty state    =  3  -  Both analysis and geometry inputs are dirty

Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_3 will be used!
Analysis Info:
	Name           =  UnitTest8_fun3dAIM
	Intent         =  None
	AnalysisDir    =  /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest8_fun3dAIM
	Version        =  1.22
	Execution Flag =  0
	Number of Fields =  7
	Field name (Rank):
	  Pressure ( 1 )
	  P ( 1 )
	  Cp ( 1 )
	  CoefficientOfPressure ( 1 )
	  Displacement ( 3 )
	  EigenVector ( 3 )
	  EigenVector_# ( 3 )
	Dirty state    =  3  -  Both analysis and geometry inputs are dirty

Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_4 will be used!
Analysis Info:
	Name           =  UnitTest9_fun3dAIM
	Intent         =  STRUCTURE
	AnalysisDir    =  /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest9_fun3dAIM
	Version        =  1.22
	Execution Flag =  0
	Number of Fields =  7
	Field name (Rank):
	  Pressure ( 1 )
	  P ( 1 )
	  Cp ( 1 )
	  CoefficientOfPressure ( 1 )
	  Displacement ( 3 )
	  EigenVector ( 3 )
	  EigenVector_# ( 3 )
	Dirty state    =  3  -  Both analysis and geometry inputs are dirty

Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_5 will be used!
Analysis Info:
	Name           =  UnitTest10_fun3dAIM
	Intent         =  ['CFD', 'STRUCTURE']
	AnalysisDir    =  /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest10_fun3dAIM
	Version        =  1.22
	Execution Flag =  0
	Number of Fields =  7
	Field name (Rank):
	  Pressure ( 1 )
	  P ( 1 )
	  Cp ( 1 )
	  CoefficientOfPressure ( 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 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
Creating FEA BEM
 700007CD3000 Odd Degenerate test for side 1: 9!
 7FF84C7314C0 Odd Degenerate test for side 2: 9!
	Mesh for body = 0
	Number of nodal coordinates = 1114
	Number of elements = 2224
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 2224
	Elemental Quad4 = 0
Creating FEA BEM
 700007CD3000 Odd Degenerate test for side 1: 9!
 7FF84C7314C0 Odd Degenerate test for side 2: 9!
	Mesh for body = 1
	Number of nodal coordinates = 1114
	Number of elements = 2224
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 2224
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2228
	Combined Number of elements = 4448
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 4448
	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 8.390s

OK (skipped=3)
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.addAttribute' is deprecated. Please use 'Analysis.attr.create'!
WARNING: 'capsAnalysis.getAttribute' is deprecated. Please use 'Analysis.attr["name"].value'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsAnalysis.getAttributeVal' is deprecated. Please use 'Analysis.geometry.attrList'!
WARNING: 'capsAnalysis.getBoundingBox' is deprecated. Please use 'Analysis.bodies'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.saveGeometry' is deprecated. Please use 'Analysis.geometry.save'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.buildGeometry' is deprecated. Please use 'Problem.geometry.build'!
WARNING: 'capsGeometry.getAttributeMap' is deprecated. Please use 'Problem.geometry.attrMap'!
WARNING: 'capsGeometry.getAttributeVal' is deprecated. Please use 'Problem.geometry.attrList'!
WARNING: 'capsGeometry.getBoundingBox' is deprecated. Please use 'Problem.geometry.bodies'!
WARNING: 'capsGeometry.getGeometryOutVal' is deprecated. Please use 'Problem.geometry.outpmtr["varname"].value'!
WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.saveGeometry' is deprecated. Please use 'Problem.geometry.save'!
WARNING: 'capsGeometry.viewGeometry' is deprecated. Please use 'Problem.geometry.view'!
WARNING: 'capsProblem.addAttribute' is deprecated. Please use 'Problem.attr.create'!
WARNING: 'capsProblem.getAttribute' is deprecated. Please use 'Problem.attr["name"].value'!
WARNING: 'capsProblem.createValue' is deprecated. Please use 'Problem.parameter.create'!
WARNING: '_capsValue.__init__' is deprecated. Please use 'Problem.parameter.create'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
WARNING: 'capsProblem.autoLinkValue' is deprecated. Please use 'Problem.autoLinkParameter'!
Legacy pyCAPS unit testing done!
# CAPS Minimal examples (one per aim)
/Library/Developer/CommandLineTools/usr/bin/make -C examples test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
(make -C cCAPS -f avlTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/cCAPS/avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/cCAPS/awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/cCAPS/frictionTest' is up to date.
(make -C cCAPS -f fun3d.make)
make[2]: Nothing to be done for `fun3d'.
(make -C cCAPS -f hsm.make)
make[2]: `hsm' is up to date.
(make -C cCAPS -f interferenceTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/cCAPS/interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/cCAPS/msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/cCAPS/mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[2]: `/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/cCAPS/pointwiseTest' is up to date.
(cd /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests

All tests pass!


=================================================
=================================================
(cd /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest; ./execute_PyTestRegression.sh MINIMAL)

=================================================
Using python : /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/venv/bin/python
=================================================

Running.... MINIMAL PyTests

=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
CXtot   0.0006119078685748102
CYtot   -6.295467348382128e-15
CZtot   -0.3012861394885953
Cltot   -4.784258926526785e-14
Cmtot   -0.1945055953450382
Cntot   -2.338191252215186e-15
Cl'tot  -4.787610967125373e-14
Cn'tot  -1.502866821492718e-15
CLtot   0.3012509314150635
CDtot   0.004646353488232475
CDvis   0.0
CLff    0.3009503023520388
CYff    -7.723329422293541e-15
CDind   0.004646353488232475
CDff    0.004968969500907922
e       0.9669902146157789
StripForces 
Wing  cl =  [0.02994790451347, 0.08555545178933, 0.1329003532587, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.3101221284189, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805664, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996427, 0.2453427152623, 0.2100182422921, 0.17330251928, 0.1329003532723, 0.08555545180787, 0.0299479045408]
Wing  cd =  [-0.004234137763162, -0.004494543653192, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946409, 0.000511459807839, 0.0021191472861, 0.004145189908974, 0.006609094404181, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.006609094404439, 0.00414518990926, 0.002119147286384, 0.0005114598080993, -0.0007386538944077, -0.001762021024096, -0.002739626801367, -0.003752887372445, -0.004494543653162, -0.004234137764545]

real	0m0.922s
user	0m0.566s
sys	0m0.407s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Cl =  [0.986723182710886, 1.2799652419791, 1.4683981236607, 1.65936133274719, 1.80584451281702, 1.89831579818148, 1.84790962938869, 1.7599548720172, 1.6551743532269]
Cd =  [0.0125901672123978, 0.0157267711976652, 0.0189519330659563, 0.0231513145535944, 0.0306140208948482, 0.0433620548565242, 0.0708699896705891, 0.0928530378324824, 0.118977178460167]
Alpha =  [0.0, 3.0, 5.0, 7.0, 9.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.499360558881994, 0.463997145318173, 0.444733833301506, 0.424150787096401, 0.400117472035192, 0.364373550846399, 0.280961990144754, 0.220047241766122, 0.139581369732674]

real	0m1.145s
user	0m1.084s
sys	0m0.199s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Cl =  0.3909761266249304
Cd =  0.007985935765448251
Cm =  0.002385293228416037

real	0m2.591s
user	0m2.214s
sys	0m0.249s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'awave_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
awave_PyTest.py test;
+ python -u awave_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Writing Awave input file
Body Section, Body ID 1
	XCG:   1.571025 -3.872983 0.270825
	AREA:  0.029452
	RAD:   0.096825
	ATTRIB:Store
	NAME  :RightWingTank
	Awave TYPE: 3

Body Section, Body ID 2
	XCG:   2.539271 -3.872983 0.270825
	AREA:  0.029452
	RAD:   0.096825
	ATTRIB:Store
	NAME  :RightWingTank
	Awave TYPE: 3

Body Section, Body ID 3
	XCG:   1.571025 3.872983 0.270825
	AREA:  0.029452
	RAD:   0.096825
	ATTRIB:Store
	NAME  :LeftWingTank
	Awave TYPE: 3

Body Section, Body ID 4
	XCG:   2.539271 3.872983 0.270825
	AREA:  0.029452
	RAD:   0.096825
	ATTRIB:Store
	NAME  :LeftWingTank
	Awave TYPE: 3

Lifting Surface Section, Body ID 5
	XLE:   1.571946 -3.872983 0.249728
	CHORD: 0.968408
	ATTRIB:Wing
	NAME  :Wing
	Awave TYPE: 0

Lifting Surface Section, Body ID 6
	XLE:   0.000000 0.000000 0.000000
	CHORD: 1.614013
	ATTRIB:Wing
	NAME  :Wing
	Awave TYPE: 1

Lifting Surface Section, Body ID 7
	XLE:   1.571946 3.872983 0.249728
	CHORD: 0.968408
	ATTRIB:Wing
	NAME  :Wing
	Awave TYPE: 1

Lifting Surface Section, Body ID 8
	XLE:   5.484123 0.000000 1.468246
	CHORD: 0.726185
	ATTRIB:VTail
	NAME  :VertTail
	Awave TYPE: 4

Lifting Surface Section, Body ID 9
	XLE:   5.000000 0.000000 0.500000
	CHORD: 1.210308
	ATTRIB:VTail
	NAME  :VertTail
	Awave TYPE: 4

Lifting Surface Section, Body ID 10
	XLE:   5.484123 -0.968246 0.500000
	CHORD: 0.726185
	ATTRIB:HTail
	NAME  :Stab
	Awave TYPE: 0

Lifting Surface Section, Body ID 11
	XLE:   5.484123 0.000000 0.500000
	CHORD: 0.726185
	ATTRIB:HTail
	NAME  :Stab
	Awave TYPE: 5

Lifting Surface Section, Body ID 12
	XLE:   5.484123 0.968246 0.500000
	CHORD: 0.726185
	ATTRIB:HTail
	NAME  :Stab
	Awave TYPE: 5

Body Section, Body ID 13
	XCG:   -2.000000 0.000000 0.000000
	AREA:  0.000000
	RAD:   0.000000
	ATTRIB:Fuse
	NAME  :Fuselage
	Awave TYPE: 2

Body Section, Body ID 14
	XCG:   0.000000 -0.000000 -0.000000
	AREA:  0.818123
	RAD:   0.510310
	ATTRIB:Fuse
	NAME  :Fuselage
	Awave TYPE: 2

Warning: capsGroup not found on body 15!
Body Section, Body ID 15
	XCG:   1.613743 -0.000000 0.000000
	AREA:  0.327249
	RAD:   0.322749
	ATTRIB:Fuse
	NAME  :(null)
	Awave TYPE: 2

Body Section, Body ID 16
	XCG:   5.000000 -0.000000 0.500000
	AREA:  0.081812
	RAD:   0.161374
	ATTRIB:Fuse
	NAME  :Fuselage
	Awave TYPE: 2

Body Section, Body ID 17
	XCG:   6.210307 -0.000000 0.500000
	AREA:  0.000818
	RAD:   0.016137
	ATTRIB:Fuse
	NAME  :Fuselage
	Awave TYPE: 2

AwaveTypes: 2 5 4 2 2
Points for all four fuselage sections :: 5 0 0 0
Number of Mach-Alpha cases = 2
dyld[86719]: Library not loaded: @rpath/libquadmath.0.dylib
  Referenced from: <9408E7F0-C471-3836-8093-ED7A4EF9985F> /usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libgfortran.5.dylib
  Reason: tried: '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS@rpath/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/usr/local/lib/libquadmath.0.dylib' (no such file), '/usr/lib/libquadmath.0.dylib' (no such file, not in dyld cache)
sh: line 1: 86719 Abort trap: 6           awave awaveInput.txt > awaveOutput.txt
Traceback (most recent call last):
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/pyCAPS/awave_PyTest.py", line 49, in <module>
    CdWave = myAnalysis.output.CDwave
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 1968, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


real	0m0.699s
user	0m0.550s
sys	0m0.187s
+ status=1
+ set +x

=================================================
CAPS verification (using pyCAPS) case awave_PyTest.py failed (as NOT expected)
=================================================


=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
dyld[86742]: Library not loaded: @rpath/libquadmath.0.dylib
  Referenced from: <9408E7F0-C471-3836-8093-ED7A4EF9985F> /usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libgfortran.5.dylib
  Reason: tried: '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS@rpath/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/test/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/usr/local/lib/libquadmath.0.dylib' (no such file), '/usr/lib/libquadmath.0.dylib' (no such file, not in dyld cache)
sh: line 1: 86742 Abort trap: 6           friction frictionInput.txt frictionOutput.txt > Info.out
Traceback (most recent call last):
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/pyCAPS/friction_PyTest.py", line 62, in <module>
    Cdtotal = myAnalysis.output.CDtotal
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1950, in __getattr__
    return self._capsItems[name].value
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1880, in value
    return self._valObj.getValue()
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 1968, in getValue
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================


real	0m0.625s
user	0m0.461s
sys	0m0.189s
+ status=1
+ set +x

=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py failed (as NOT expected)
=================================================


=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go.  Other input will terminate the job.
Cl =  0.933417
Cd =  0.000284
Cd Wave =  0.0
Cm =  -0.203436
Cp _Critcal =  -1.303869

real	0m0.737s
user	0m0.483s
sys	0m0.186s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6

Getting mesh sizing parameters
	Mesh sizing name - Airfoil
	Mesh sizing name - AirfoilTE
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes be 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 - delaundoMesh.mesh
	Swapping y and z coordinates!

Writing TECPLOT file: delaundoMesh.dat ....
Finished writing TECPLOT file


real	0m0.810s
user	0m0.778s
sys	0m0.519s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Getting mesh sizing parameters
	Mesh sizing name - LeadingEdge
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 1749
Number of elements = 1889
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 1889
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 1
Number of node elements          = 1
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 3 (of 4)
Number of nodes    = 53
Number of elements = 34
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 34
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 4 (of 4)
Number of nodes    = 53
Number of elements = 34
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 34
----------------------------
Total number of nodes    = 1856
Total number of elements = 1958

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_3.dat ....
Finished writing TECPLOT file


real	0m5.664s
user	0m16.885s
sys	0m5.386s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/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 = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.3
AFLR2    : Version Date   06/09/22 @ 05:16PM
AFLR2    : Compile OS     Darwin 19.6.0 x86_64
AFLR2    : Compile Date   07/02/22 @ 03:34PM
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          =     0.013   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       484
AFLR2 QI : Nodes, Faces      =      6032      5618
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       530
AFLR2 QI : Nodes, Faces      =      6032      5595
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       812
AFLR2 QI : Nodes, Faces      =      6032      5454
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       552
AFLR2 QI : Nodes, Faces      =      6032      5584
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       542
AFLR2 QI : Nodes, Faces      =      6032      5589
AFLR2 QI : Nodes, Faces      =      6032       542
AFLR2 QI : Nodes, Faces      =      6032      5589
 
AFLR2    : CPU Time          =     0.008   seconds
 
AFLR2    : DONE
Number of nodes = 6032
Number of elements = 6475
Number of tris = 542
Number of quad = 5589

Writing TECPLOT file: pyCAPS_AFLR2_Test.dat ....
Finished writing TECPLOT file


real	0m0.815s
user	0m0.781s
sys	0m0.361s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/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
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

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_Surf_2.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_Surf_3.dat ....
Finished writing TECPLOT 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
Number of surface nodes - 7304
Number of surface elements - 14572
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.3
AFLR2    : Version Date   06/09/22 @ 05:16PM
AFLR2    : Compile OS     Darwin 19.6.0 x86_64
AFLR2    : Compile Date   07/02/22 @ 03:34PM
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 10.22.23
AFLR4    : Version Date   07/14/22 @ 02:23PM
AFLR4    : Compile OS     Darwin 19.6.0 x86_64
AFLR4    : Compile Date   07/18/22 @ 06:42PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.22
EGADS    : OpenCASCADE Version 7.6.0
EGADS    : ---------------------------------------

OVERALL  : CPU Time          =     0.153   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.22
EGADS    : OpenCASCADE Version 7.6.0
EGADS    : ---------------------------------------

OVERALL  : CPU Time          =     0.116   seconds
Volume mesh:
	Number of nodes = 158715
	Number of elements = 475708
	Number of triangles = 14572
	Number of quadrilatarals = 0
	Number of tetrahedrals = 227432
	Number of pyramids= 470
	Number of prisms= 233234
	Number of hexahedrals= 0

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file


real	0m12.244s
user	0m11.555s
sys	0m0.566s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 267
Number of elements = 530
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3139
Total number of elements = 6266

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
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:  0.02814
Creating surface mesh ...
Surface mesh seconds:  0.007577
Recovering boundaries...
Boundary recovery seconds:  0.072665
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.007792
Suppressing Steiner points ...
Steiner suppression seconds:  1.3e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.010622
Refining mesh...
  4188 insertions, added 2137 points, 127272 tetrahedra in queue.
  1394 insertions, added 414 points, 131442 tetrahedra in queue.
  1858 insertions, added 464 points, 129858 tetrahedra in queue.
  2477 insertions, added 450 points, 111812 tetrahedra in queue.
  3302 insertions, added 490 points, 67833 tetrahedra in queue.
  4401 insertions, added 401 points, 112 tetrahedra in queue.
Refinement seconds:  0.696483
Smoothing vertices...
Mesh smoothing seconds:  0.443593
Improving mesh...
Mesh improvement seconds:  0.015642
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.003124
Total running seconds:  1.28597

Statistics:

  Input points: 3139
  Input facets: 6266
  Input segments: 9399
  Input holes: 2
  Input regions: 0

  Mesh points: 7895
  Mesh tetrahedra: 38676
  Mesh faces: 80485
  Mesh faces on exterior boundary: 6266
  Mesh faces on input facets: 6266
  Mesh edges on input segments: 9399
  Steiner points inside domain: 4756

Done meshing using TetGen!

Writing TECPLOT file: pyCAPS_Tetgen_Test.dat ....
	Binary output is not currently supported for Tecplot output
	..... switching to ASCII!
Finished writing TECPLOT file


real	0m6.245s
user	0m6.192s
sys	0m0.346s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/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 = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.3
AFLR2    : Version Date   06/09/22 @ 05:16PM
AFLR2    : Compile OS     Darwin 19.6.0 x86_64
AFLR2    : Compile Date   07/02/22 @ 03:34PM
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          =     0.038   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       863
AFLR2 QI : Nodes, Faces      =     11154     10450
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154      1031
AFLR2 QI : Nodes, Faces      =     11154     10366
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154      1637
AFLR2 QI : Nodes, Faces      =     11154     10063
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154      1025
AFLR2 QI : Nodes, Faces      =     11154     10369
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11153      1013
AFLR2 QI : Nodes, Faces      =     11153     10374
AFLR2 QI : Nodes, Faces      =     11153      1013
AFLR2 QI : Nodes, Faces      =     11153     10374
 
AFLR2    : CPU Time          =     0.018   seconds
 
AFLR2    : DONE
Number of nodes = 11153
Number of elements = 11932
Number of tris = 1013
Number of quad = 10374

Writing TECPLOT file: pyCAPS_su2_aflr2.dat ....
Finished writing TECPLOT file


Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Warning: No boundary condition specified for capsGroup 2DSlice!
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.4.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.4.0 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   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 2012-2022, 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.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.
11387 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).
1013 triangles.
10374 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 1013 TRIANGLE volume elements.
There has been a re-orientation of 10374 QUADRILATERAL volume elements.
There has been a re-orientation of 545 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.877.
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.)|        49.1197|             90|
|     CV Face Area Aspect Ratio|        1.00061|         32.974|
|           CV Sub-Volume Ratio|        1.00002|        6.32859|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11153|    1/1.00|        10|
|         1|      2707|    1/4.12|   7.38992|
|         2|       555|    1/4.88|   5.01918|
+-------------------------------------------+
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
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.0425e-01|    0.070615|    2.738611|    1.108464|    5.599347|    0.058184|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.8741e-02|   -0.454267|    2.190680|    1.555679|    5.064740|    0.060630|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.3345e-02|   -0.565341|    2.070468|    1.485403|    4.949698|    0.060586|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.9534e-02|   -0.726390|    1.920921|    1.383781|    4.787685|    0.072845|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.6675e-02|   -0.883308|    1.823260|    1.266042|    4.630445|    0.126180|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.4765e-02|   -1.042499|    1.755083|    1.151079|    4.468758|    0.301945|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.4672e-02|   -1.231529|    1.700482|    1.105648|    4.268760|    0.849538|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.5222e-02|   -1.327203|    1.639352|    1.129519|    4.117576|    2.769795|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.4569e-02|   -1.267223|    1.565550|    1.141885|    4.144438|   46.482609|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.3874e-02|   -1.220125|    1.493905|    1.121919|    4.191590|   -5.798185|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.22013|         < -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).
+-----------------------------------------------------------------------+

------------------------- Solver Postprocessing -------------------------
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 =  0.083415 Cd =  -0.014386
Cmz =  0.080305
Cx =  -0.014386 Cy =  0.083415
Pressure Contribution
Cl_p =  0.083415 Cd_p =  -0.014386
Cmz_p =  0.080305
Cx_p =  -0.014386 Cy_p =  0.083415
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m2.807s
user	0m2.159s
sys	0m0.938s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================

./execute_PyTestRegression.sh: line 191: ulimit: stack size: cannot modify limit: Operation not permitted

=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/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  0.050108722
C_Y  -0.0015626888
C_N  0.0065057682
C_D  0.050305245
C_S  -0.0015626888
C_L  0.0047530359
C_l  0.00381162
C_m  -0.00346146
C_n  -0.0401149
C_M_x  0.00240931
C_M_y  -0.00346146
C_M_z  -0.0402235

real	0m16.615s
user	0m29.842s
sys	0m0.812s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Creating FEA BEM
	capsIgnore attribute found for edge - 3!!
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m1.264s
user	0m0.611s
sys	0m0.306s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 80
	Number of elements = 63
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 63
Creating FEA BEM
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 81
	Combined Number of elements = 64
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 63
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 80
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Body
	Property name - Edge
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	8 automatic connections were made for capsConnect Root (node id 81)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Flutter
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aero card
	Writing analysis cards
	Writing constraint cards--each subcase individually
	Writing material cards
	Writing property cards
	Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

real	0m1.046s
user	0m0.757s
sys	0m0.361s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/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 node elements          = 0
Number of line elements          = 0
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, -4.234473120249e-11]
CG        [1.222256036874, 0.1634981473778, -4.23458286392e-11]
Ixx       22133.97306033
Iyy       23448.30046709
Izz       1389.213122582
Ixy       164.2055275657
Ixz       -7.454850184304e-06
Iyz       1.707683171333e-06
I         [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454850184304e-06, 1.707683171333e-06]
II        [[22133.97306033, -164.2055275657, 7.454850184304e-06], [-164.2055275657, 23448.30046709, -1.707683171333e-06], [7.454850184304e-06, -1.707683171333e-06, 1389.213122582]]

real	0m4.891s
user	0m10.551s
sys	0m7.758s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
 Information: Dynamic Loader Error for hsmAIM.so
              dlopen(hsmAIM.so, 0x0082): Library not loaded: @rpath/libquadmath.0.dylib
  Referenced from: <9408E7F0-C471-3836-8093-ED7A4EF9985F> /usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libgfortran.5.dylib
  Reason: tried: '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS@rpath/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/x86_64-apple-darwin21/12/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/gcc/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/tbb/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/mkl/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/opt/intel/oneapi/ipp/2021.3.0/lib/libquadmath.0.dylib' (no such file), '/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/usr/local/Cellar/gcc/12.2.0/lib/gcc/current/libquadmath.0.dylib' (no such file), '/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/lib/libquadmath.0.dylib' (no such file), '/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib/libquadmath.0.dylib' (no such file), '/usr/local/lib/libquadmath.0.dylib' (no such file), '/usr/lib/libquadmath.0.dylib' (no such file, not in dyld cache)
Traceback (most recent call last):
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/pyCAPS/hsm_SingleLoadCase_PyTest.py", line 31, in <module>
    myAnalysis = myProblem.analysis.create(aim = "hsmAIM")
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 3134, in create
    analysisObj = self._problemObj.makeAnalysis(aim,
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 1914, in makeAnalysis
    _raiseStatus(stat, msg=msg, errors=capsErrs(nErr, errs))
  File "/Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: EGADS_NULLOBJ: Failed to make AIM 'hsmAIM':
================================================================================
================================================================================

 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m0.436s
user	0m0.386s
sys	0m0.105s
+ status=1
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py failed (as NOT expected)
=================================================


=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Commit/7.6/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt

Objective
---------
   -21.56250 dimensionless

Variables
---------
   x  :  1.62500   [-]   The X variable
   y  :  1.37500   [-]   The Y variable

Constants
---------
   c   :  3         [-]   A constant
   c2  :  2         [-]   A constant

Sensitivities
-------------
   c   :  + 0.46957   A constant
   c2  :  - 0.22338   A constant

Solve Report
------------
   Solve Method           :  Quadratic Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m11.983s
user	0m1.883s
sys	0m0.272s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================


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Did not run examples for:

Mystran
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Summary of examples NOT finished as expected

awave_PyTest.py
friction_PyTest.py
hsm_SingleLoadCase_PyTest.py

See pyCAPSlog.txt for more details.
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make[1]: *** [pyCAPStest] Error 1
make: *** [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