Console Output

Skipping 390 KB.. Full Log
           aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  7
     linked to ParamName

   pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
     last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  16
     hist: (null) -> Starting
           aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  16
     value = 34.641525 (null)
   cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
     last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  16
     hist: (null) -> Starting
           aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  16
     value = 7.296560 (null)

   testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes
     last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  18
     hist: (null) -> Starting
           aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  18
     4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
     1 Bodies, 1 Tessellations

     testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  8
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  8
       value = 5.000000 cm
     table has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  8
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  8
       value (1x3) =
        1: Entry1 -> Value1
        2: Entry2 -> Value2
        3: Entry3 -> Value3
     tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  8
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  8
       value (0x0) = NULL with len = 0 ego
     meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  8
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  8
       value (0x0) = NULL with len = 0 writer

     testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  9
 testingAIM/aimCalcOutput instance = 0  index = 1 testingAIMout 0!
 aim_getDiscr 0 on Interface = 0
 aim_getDataSet 0 on Interface = -329
       value = 12.340000 cm
       lazy: aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  18
     tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  18
       hist: (null) -> Child Execute
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  18
       value (0x0) = NULL with len = 0 ego
     meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  9
 testingAIM/aimCalcOutput instance = 0  index = 3 meshFile 0!
       value (0x0) = NULL with len = 0 writer
       lazy: aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  18

     Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  18
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  18
       value = 42 (null)
   testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes
     last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  28
     hist: (null) -> Starting
           aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
     hist: (null) -> Child Execute
           aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  28
     4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
     1 Bodies, 1 Tessellations

     testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  10
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  10
       value = 6.000000 cm
     table has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  12
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  12
       value (1x3) =
        1: Entry1 -> newValue1
        2: Entry2 -> newValue2
        3: Entry3 -> newValue3
     tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  18
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  13
       hist: (null) -> Child Execute
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  23
       linked to tessOut
     meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  10
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  10
       value (0x0) = NULL with len = 0 writer

     testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  11
 testingAIM/aimCalcOutput instance = 1  index = 1 testingAIMout 0!
 aim_getDiscr 1 on Interface = 0
 aim_getDataSet 1 on Interface = -329
       value = 12.340000 cm
       lazy: aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  28
     tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  11
 testingAIM/aimCalcOutput instance = 1  index = 2 tessOut 0!
 tessPtr = 559f8971a1e0
       value = 559f8971a1e0 ego
       lazy: aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  28
     meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  11
 testingAIM/aimCalcOutput instance = 1  index = 3 meshFile 0!
       value (0x0) = NULL with len = 0 writer
       lazy: aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  28

     Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  28
       hist: (null) -> Child Execute
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  28
       value = 42 (null)

   Interface has type BOUND, subtype NONE with 0 attributes
     last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
     hist: (null) -> Starting
           aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  14
     hist: (null) -> Child Execute
           aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
     2 Connecteds, 0 UnConnecteds

     testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
       hist: (null) -> Child Execute
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
       5 DataSets

       xyz has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Child Execute
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
         1113 points, rank=3, units=cm
       xyzd has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         0 points, rank=3, units=(null)
       param has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Child Execute
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
         1113 points, rank=2, units=(null)
       paramd has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         0 points, rank=2, units=(null)
       scalar has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  26
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  15
         hist: (null) -> Child Execute
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:57  26
         1113 points, rank=1, units=(null)
     testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes
       last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
       hist: (null) -> Starting
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
       hist: (null) -> Child Execute
             aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
       6 DataSets

       xyz has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Child Execute
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
         447 points, rank=3, units=cm
       xyzd has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         0 points, rank=3, units=(null)
       param has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Child Execute
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  23
         447 points, rank=2, units=(null)
       paramd has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         0 points, rank=2, units=(null)
       scalar has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  25
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Child Execute
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:41  25
         447 points, rank=1, units=(null)
       vector has type DATASET, subtype NONE with 0 attributes
         last: aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
         hist: (null) -> Starting
               aimTest reynolds:796209 jenkins  2022/11/30  22:21:40  0
 testingAIM/aimTransfer name = vector  instance = 0  npts = 447/3!
         447 points, rank=3, units=(null)

    1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
    8: 14.400000 14.400000 14.400000 14.380647 14.400000 14.381201 14.400000
   15: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   22: 14.400000 14.400000 14.390441 14.400000 14.383859 14.400000 14.400000
   29: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   36: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   43: 14.385061 14.400000 14.383844 14.400000 14.400000 14.400000 14.400000
   50: 14.378338 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   57: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.376665
   64: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   78: 14.389247 14.400000 14.400000 14.400000 14.400000 14.382317 14.400000
   85: 14.400000 14.400000 14.400000 14.390011 14.400000 14.400000 14.400000
   92: 14.400000 14.400000 14.400000 14.400000 14.389865 14.400000 14.389101
   99: 14.400000 14.388170 14.400000 14.400000 14.400000 14.400000 14.400000
  106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  155: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  162: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  169: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  176: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  183: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  190: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  197: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  204: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  211: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  218: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  225: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  232: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  239: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  246: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  253: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  260: 14.400000 14.400000 14.400000 14.399999 14.400000 14.400000 14.400000
  267: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  274: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  281: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  288: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  295: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  302: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  309: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  316: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  323: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  330: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  337: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  344: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  351: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  358: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  365: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  372: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  379: 14.400000 14.400000 14.400000 14.400000 14.399999 14.400000 14.400000
  386: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  393: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  400: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  407: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  414: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  421: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  428: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  435: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  442: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  449: 14.400000 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000
  456: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  463: 14.400000 14.400000 14.400000 14.400000 14.399999 14.400000 14.399999
  470: 14.400000 14.400000 14.400000 14.400000 14.400000 14.399999 14.400000
  477: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  491: 14.399999 14.400000 14.400000 14.400000 14.365872 14.400000 14.400000
  498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  505: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  512: 14.400000 14.399999 14.399999 14.400000 14.400000 14.400000 14.400000
  519: 14.400000 14.362939 14.399999 14.362723 14.400000 14.400000 14.400000
  526: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  533: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  540: 14.400000 14.400000 14.400000 14.399999 14.400000 14.399999 14.400000
  547: 14.368368 14.400000 14.400000 14.399999 14.400000 14.369831 14.400000
  554: 14.400000 14.400000 14.400000 14.368625 14.399999 14.362939 14.400000
  561: 14.400000 14.366035 14.400000 14.400000 14.400000 14.400000 14.400000
  568: 14.356726 14.400000 14.369831 14.369176 14.400000 14.399999 14.400000
  575: 14.400000 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000
  582: 14.399999 14.363748 14.368368 14.400000 14.399999 14.400000 14.400000
  589: 14.369831 14.400000 14.359401 14.399999 14.362295 14.400000 14.399999
  596: 14.373877 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  603: 14.369218 14.369218 14.400000 14.365682 14.400000 14.369054 14.400000
  610: 14.400000 14.400000 14.400000 14.371386 14.368747 14.372230 14.400000
  617: 14.375508 14.400000 14.364430 14.374160 14.400000 14.400000 14.400000
  624: 14.368709 14.369354 14.400000 14.400000 14.400000 14.399999 14.400000
  631: 14.400000 14.400000 14.370155 14.368220 14.400000 14.372237 14.400000
  638: 14.400000 14.374425 14.372364 14.400000 14.400000 14.400000 14.400000
  645: 14.375987 14.365558 14.368709 14.366781 14.400000 14.369176 14.369354
  652: 14.399999 14.373289 14.400000 14.375685 14.374425 14.400000 14.377582
  659: 14.399999 14.400000 14.400000 14.366036 14.400000 14.400000 14.400000
  666: 14.400000 14.375124 14.400000 14.400000 14.368903 14.368555 14.399999
  673: 14.400000 14.371386 14.371386 14.399999 14.400000 14.379372 14.369130
  680: 14.374049 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  687: 14.376400 14.399999 14.377760 14.378863 14.374473 14.367810 14.400000
  694: 14.400000 14.368784 14.400000 14.371386 14.365916 14.400000 14.373165
  701: 14.400000 14.399999 14.372471 14.400000 14.400000 14.400000 14.400000
  708: 14.375987 14.379953 14.400000 14.374316 14.377675 14.400000 14.376295
  715: 14.400000 14.399999 14.399999 14.368903 14.368784 14.366475 14.400000
  722: 14.400000 14.369555 14.400000 14.378687 14.378687 14.378950 14.400000
  729: 14.375449 14.376400 14.371321 14.400000 14.400000 14.371351 14.399999
  736: 14.400000 14.375126 14.400000 14.400000 14.400000 14.375504 14.368903
  743: 14.368514 14.400000 14.400000 14.400000 14.400000 14.379510 14.375124
  750: 14.376289 14.374679 14.400000 14.400000 14.399999 14.400000 14.378601
  757: 14.399999 14.377088 14.400000 14.375718 14.373640 14.400000 14.400000
  764: 14.372001 14.400000 14.400000 14.368903 14.368514 14.400000 14.374569
  771: 14.400000 14.375271 14.400000 14.400000 14.400000 14.400000 14.380018
  778: 14.399999 14.400000 14.379331 14.400000 14.400000 14.379693 14.400000
  785: 14.372552 14.383094 14.375769 14.400000 14.372608 14.378845 14.400000
  792: 14.373363 14.368903 14.400000 14.375189 14.378667 14.375797 14.377675
  799: 14.400000 14.400000 14.379863 14.373732 14.400000 14.400000 14.400000
  806: 14.400000 14.400000 14.375857 14.400000 14.400000 14.400000 14.400000
  813: 14.400000 14.400000 14.400000 14.400000 14.376290 14.379510 14.400000
  820: 14.400000 14.400000 14.374594 14.400000 14.376305 14.400000 14.373349
  827: 14.400000 14.379553 14.379553 14.373363 14.400000 14.377860 14.382472
  834: 14.379566 14.400000 14.376493 14.400000 14.400000 14.400000 14.400000
  841: 14.378207 14.375251 14.376605 14.400000 14.378626 14.400000 14.400000
  848: 14.400000 14.376156 14.377590 14.379497 14.400000 14.375464 14.378358
  855: 14.400000 14.380743 14.375541 14.400000 14.373960 14.400000 14.380592
  862: 14.379305 14.374687 14.383536 14.400000 14.400000 14.374081 14.400000
  869: 14.400000 14.380716 14.379808 14.383716 14.400000 14.383966 14.377272
  876: 14.400000 14.379553 14.400000 14.377570 14.400000 14.376445 14.382213
  883: 14.400000 14.400000 14.400000 14.400000 14.371272 14.379704 14.400000
  890: 14.400000 14.379158 14.400000 14.379112 14.383216 14.380581 14.400000
  897: 14.382554 14.400000 14.383382 14.400000 14.381160 14.400000 14.400000
  904: 14.385313 14.382398 14.378148 14.381487 14.400000 14.378927 14.380605
  911: 14.400000 14.400000 14.382990 14.384339 14.381122 14.380943 14.382554
  918: 14.400000 14.375911 14.400000 14.384096 14.379502 14.376270 14.382299
  925: 14.400000 14.380606 14.380606 14.383670 14.382868 14.400000 14.380592
  932: 14.400000 14.379141 14.400000 14.400000 14.400000 14.400000 14.379453
  939: 14.383433 14.382323 14.382931 14.376462 14.385109 14.386913 14.377700
  946: 14.384542 14.400000 14.378601 14.387579 14.400000 14.400000 14.400000
  953: 14.385467 14.379641 14.381746 14.383298 14.379931 14.400000 14.381446
  960: 14.378196 14.400000 14.400000 14.381474 14.400000 14.383687 14.400000
  967: 14.400000 14.384788 14.382697 14.379960 14.382187 14.383772 14.400000
  974: 14.376286 14.374476 14.383667 14.382627 14.379931 14.384695 14.384795
  981: 14.384528 14.385187 14.382443 14.381568 14.384519 14.385991 14.400000
  988: 14.381424 14.400000 14.376098 14.383598 14.400000 14.375887 14.382344
  995: 14.400000 14.374829 14.400000 14.386850 14.382671 14.380741 14.377878
 1002: 14.388595 14.383869 14.385187 14.400000 14.400000 14.386296 14.384522
 1009: 14.388515 14.385094 14.381609 14.387264 14.385337 14.386730 14.386730
 1016: 14.387884 14.400000 14.376353 14.377969 14.376462 14.384854 14.378940
 1023: 14.400000 14.386177 14.385200 14.385211 14.400000 14.400000 14.388399
 1030: 14.384905 14.400000 14.400000 14.385855 14.386303 14.386373 14.389777
 1037: 14.383001 14.384393 14.387981 14.400000 14.379911 14.378339 14.400000
 1044: 14.400000 14.400000 14.380951 14.382823 14.381293 14.400000 14.400000
 1051: 14.375959 14.380629 14.382256 14.388550 14.385775 14.389044 14.386740
 1058: 14.385318 14.400000 14.380768 14.387137 14.385084 14.386362 14.379022
 1065: 14.400000 14.383819 14.400000 14.373221 14.400000 14.387729 14.382944
 1072: 14.387356 14.400000 14.390026 14.387727 14.388858 14.400000 14.381248
 1079: 14.386362 14.378339 14.400000 14.400000 14.375685 14.381865 14.383342
 1086: 14.386099 14.381327 14.386556 14.381954 14.385445 14.383357 14.384113
 1093: 14.379911 14.400000 14.383874 14.400000 14.381638 14.391021 14.400000
 1100: 14.400000 14.400000 14.400000 14.400000 14.384656 14.400000 14.378251
 1107: 14.400000 14.381757 14.383106 14.386337 14.384313 14.383799 14.384686
 source getTriangles = 0, nGtris = 2108, nGsegs = 6324, Ds = 0 0
 destin getTriangles = 0, nGtris = 800, nGsegs = 2400, Ds = 0 0
 testingAIM/aimCleanup   instance = 0!
 testingAIM/aimCleanup   instance = 1!

real	0m17.259s
user	0m17.179s
sys	0m4.257s
+ set +x

=============================================
CAPS test (using c-executables) case /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/test/aim testingAIM.csm passed (as expected)
=============================================

+ rm -rf source.vs destin.vs
+ expectCSuccess '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/test/autoExec testingAIM.csm'
+ /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/test/autoExec testingAIM.csm

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

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

 Intent  = child
 APath   = /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/test/autoExecTest/Scratch/testingAIM1
 UnitSys = (null)
 Exec    = 2
 Fields  =  scalar (1 1)  vector (3 1)  scalar (1 0)  vector (3 0)
 Dirty   =  3

 testingAIM/aimUpdateState instance = 0!
   tess is NULL!
 testingAIM/aimPreAnalysis instance = 0!
 testingAIM/aimPreAnalysis aim_getBounds = 0
     aim_newGeometry = 0!
   getDiscr = -303
   meshRef = NULL
 testingAIM/aimExecute instance = 0!
 testingAIM/aimPostAnalysis instance = 0  restart = 0!
 testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
 testingAIM/aimCalcOutput instance = 0  index = 1 testingAIMout 0!
 aim_getDiscr 0 on Interface = -303
 testingAIM/aimCalcOutput instance = 0  index = 3 meshFile 0!
 testingAIM/aimUpdateState instance = 1!
   tess is NULL!
 testingAIM/aimPreAnalysis instance = 1!
 testingAIM/aimPreAnalysis aim_getBounds = 0
     aim_newGeometry = 0!
   mesh file = /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/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	0m0.552s
user	0m0.725s
sys	0m3.387s
+ set +x

=============================================
CAPS test (using c-executables) case /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/test/autoExec testingAIM.csm passed (as expected)
=============================================

make -C aim/skeleton test
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/aim/skeleton'
python -u case.py
Loading file into our Problem
Default num = 8.0
Current num = 16.0
             aim_newGeometry = 0!
   GeometryIn:
       1: num  2  (1,1)
       2: x  2  (8,1)
       3: ymin  2  (8,1)
       4: zmin  2  (8,1)
       5: zmax  2  (8,1)

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

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

Computed sqrtNum = 4.0
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/aim/skeleton'
# pyCAPS Unit tests (and legacy)
make -C pyCAPS/unitTest test
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/pyCAPS/unitTest'
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 12.289s

OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/pyCAPS/unitTest'
make -C legacy/unitTest test
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/unitTest'
python --version
Python 3.9.13
python -u -m unittest discover
......sAnalysis Info:
	Name           =  UnitTest_fun3dAIM
	Intent         =  None
	AnalysisDir    =  /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/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    =  /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/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    =  /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/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    =  /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/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    =  /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/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    =  /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/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
 7F846B3FD640 Odd Degenerate test for side 1: 9!
 7F846BBFE640 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
 7F846BBFE640 Odd Degenerate test for side 1: 9!
 7F846C3FF640 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 3.435s

OK (skipped=3)
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.addAttribute' is deprecated. Please use 'Analysis.attr.create'!
WARNING: 'capsAnalysis.getAttribute' is deprecated. Please use 'Analysis.attr["name"].value'!
WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsAnalysis.getAttributeVal' is deprecated. Please use 'Analysis.geometry.attrList'!
WARNING: 'capsAnalysis.getBoundingBox' is deprecated. Please use 'Analysis.bodies'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.saveGeometry' is deprecated. Please use 'Analysis.geometry.save'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.buildGeometry' is deprecated. Please use 'Problem.geometry.build'!
WARNING: 'capsGeometry.getAttributeMap' is deprecated. Please use 'Problem.geometry.attrMap'!
WARNING: 'capsGeometry.getAttributeVal' is deprecated. Please use 'Problem.geometry.attrList'!
WARNING: 'capsGeometry.getBoundingBox' is deprecated. Please use 'Problem.geometry.bodies'!
WARNING: 'capsGeometry.getGeometryOutVal' is deprecated. Please use 'Problem.geometry.outpmtr["varname"].value'!
WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.saveGeometry' is deprecated. Please use 'Problem.geometry.save'!
WARNING: 'capsGeometry.viewGeometry' is deprecated. Please use 'Problem.geometry.view'!
WARNING: 'capsProblem.addAttribute' is deprecated. Please use 'Problem.attr.create'!
WARNING: 'capsProblem.getAttribute' is deprecated. Please use 'Problem.attr["name"].value'!
WARNING: 'capsProblem.createValue' is deprecated. Please use 'Problem.parameter.create'!
WARNING: '_capsValue.__init__' is deprecated. Please use 'Problem.parameter.create'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
WARNING: 'capsProblem.autoLinkValue' is deprecated. Please use 'Problem.autoLinkParameter'!
Legacy pyCAPS unit testing done!
make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/unitTest'
# CAPS Minimal examples (one per aim)
make -C examples test TYPE=MINIMAL
make[1]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/cCAPS/avlTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/cCAPS/awaveTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/cCAPS/frictionTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: Nothing to be done for 'fun3d'.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: 'hsm' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/cCAPS/interferenceTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/cCAPS/msesTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/cCAPS/mystranTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
make[2]: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/cCAPS/pointwiseTest' is up to date.
make[2]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples/cCAPS'
(cd /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests

All tests pass!

(cd /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest; ./execute_PyTestRegression.sh MINIMAL)

=================================================
Using python : /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/venv/bin/python
=================================================

Running.... MINIMAL PyTests

=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/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   0.000611907868574681
CYtot   -6.289312383470904e-15
CZtot   -0.3012861394886091
Cltot   -4.782081713039163e-14
Cmtot   -0.1945055953450467
Cntot   -2.339461801636068e-15
Cl'tot  -4.7854363026524e-14
Cn'tot  -1.504517153549636e-15
CLtot   0.3012509314150773
CDtot   0.004646353488232845
CDvis   0.0
CLff    0.3009503023520526
CYff    -7.719145079534105e-15
CDind   0.004646353488232845
CDff    0.004968969500908293
e       0.9669902146157952
StripForces 
Wing  cl =  [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing  cd =  [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]

real	0m0.523s
user	0m0.434s
sys	0m0.427s
+ status=0
+ set +x

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


=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Cl =  [0.986723182710393, 1.27996524197906, 1.4683981236604, 1.65936133274566, 1.80584451282044, 1.89831579818228, 1.8479096293896, 1.75995487201918, 1.65517435322733]
Cd =  [0.0125901672123701, 0.0157267711976542, 0.0189519330659632, 0.0231513145536885, 0.0306140208946916, 0.0433620548565217, 0.0708699896705503, 0.0928530378323145, 0.118977178460154]
Alpha =  [0.0, 3.0, 5.0, 7.0, 9.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.49936055887155, 0.463997145318054, 0.444733833301408, 0.424150787095459, 0.400117472036691, 0.364373550846682, 0.280961990145327, 0.2200472417656, 0.139581369732118]

real	0m2.571s
user	0m2.513s
sys	0m0.343s
+ status=0
+ set +x

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


=================================================
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'mses_PyTest.py test;'
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Cl =  0.39097622077641775
Cd =  0.00798593605836464
Cm =  0.0023852664481895467

real	0m7.307s
user	0m6.836s
sys	0m0.433s
+ status=0
+ set +x

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


=================================================
+ echo 'awave_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
awave_PyTest.py test;
+ python -u awave_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Writing Awave input file
Body Section, Body ID 1
	XCG:   1.571025 -3.872983 0.270825
	AREA:  0.029452
	RAD:   0.096825
	ATTRIB:Store
	NAME  :RightWingTank
	Awave TYPE: 3

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

AwaveTypes: 2 5 4 2 2
Points for all four fuselage sections :: 5 0 0 0
Number of Mach-Alpha cases = 2
CdWave =  [1.13332772, 0.216380954]

real	0m0.637s
user	0m0.574s
sys	0m0.305s
+ status=0
+ set +x

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


=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u friction_PyTest.py -outLevel=0
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]

real	0m0.475s
user	0m0.449s
sys	0m0.319s
+ status=0
+ set +x

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


=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go.  Other input will terminate the job.
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Cl =  0.933329
Cd =  0.000283
Cd Wave =  0.0
Cm =  -0.203433
Cp _Critcal =  -1.303869

real	0m0.521s
user	0m0.470s
sys	0m0.282s
+ status=0
+ set +x

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


=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/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	0m0.705s
user	0m0.831s
sys	0m1.567s
+ status=0
+ set +x

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


=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/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	0m8.281s
user	0m22.145s
sys	0m42.626s
+ status=0
+ set +x

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


=================================================
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'aflr2_PyTest.py test;'
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 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     Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR2    : Compile Date   06/13/22 @ 12:42PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.017   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6034     11724
AFLR2 QI : Nodes, Faces      =      6033       454
AFLR2 QI : Nodes, Faces      =      6033      5634
AFLR2 QI : Nodes, Faces      =      6033     11722
AFLR2 QI : Nodes, Faces      =      6032       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          =     0.011   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	0m0.758s
user	0m0.897s
sys	0m2.729s
+ status=0
+ set +x

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


=================================================
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'aflr4_and_aflr3_PyTest.py test;'
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
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     Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR2    : Compile Date   06/13/22 @ 12:42PM
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     Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR4    : Compile Date   07/19/22 @ 12:23AM
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          =     0.248   seconds

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

OVERALL  : CPU Time          =     0.125   seconds
Volume mesh:
	Number of nodes = 156847
	Number of elements = 464284
	Number of triangles = 14572
	Number of quadrilatarals = 0
	Number of tetrahedrals = 216008
	Number of pyramids= 469
	Number of prisms= 233235
	Number of hexahedrals= 0

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


real	0m16.144s
user	0m15.556s
sys	0m0.530s
+ status=0
+ set +x

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


=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u tetgen_PyTest.py -outLevel=0
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:  0.034501
Creating surface mesh ...
Surface mesh seconds:  0.009888
Recovering boundaries...
Boundary recovery seconds:  0.095404
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.016991
Suppressing Steiner points ...
Steiner suppression seconds:  2.1e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.018256
Refining mesh...
  4190 insertions, added 2180 points, 134280 tetrahedra in queue.
  1395 insertions, added 459 points, 138994 tetrahedra in queue.
  1859 insertions, added 487 points, 137112 tetrahedra in queue.
  2478 insertions, added 498 points, 120303 tetrahedra in queue.
  3304 insertions, added 499 points, 74342 tetrahedra in queue.
  4404 insertions, added 474 points, 460 tetrahedra in queue.
Refinement seconds:  1.08104
Smoothing vertices...
Mesh smoothing seconds:  0.783584
Improving mesh...
Mesh improvement seconds:  0.021508
Jettisoning redundant points.

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

Output seconds:  0.004684
Total running seconds:  2.06611

Statistics:

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

  Mesh points: 8309
  Mesh tetrahedra: 41161
  Mesh faces: 85455
  Mesh faces on exterior boundary: 6266
  Mesh faces on input facets: 6266
  Mesh edges on input segments: 9399
  Steiner points inside domain: 5170

Done meshing using TetGen!

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


real	0m3.953s
user	0m3.924s
sys	0m0.363s
+ status=0
+ set +x

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


=================================================
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'su2_and_AFLR2_PyTest.py test;'
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 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     Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR2    : Compile Date   06/13/22 @ 12:42PM
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          =     0.055   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          =     0.029   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|  1.2456e-01|    0.070615|    2.738611|    1.108464|    5.599347|    0.058184|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.1684e-01|   -0.454267|    2.190680|    1.555679|    5.064740|    0.060630|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.1332e-01|   -0.565341|    2.070468|    1.485403|    4.949698|    0.060586|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.1230e-01|   -0.726390|    1.920921|    1.383781|    4.787685|    0.072845|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.1130e-01|   -0.883308|    1.823260|    1.266042|    4.630445|    0.126180|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.1084e-01|   -1.042499|    1.755083|    1.151079|    4.468758|    0.301945|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.1036e-01|   -1.231529|    1.700482|    1.105648|    4.268760|    0.849538|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.0987e-01|   -1.327203|    1.639352|    1.129519|    4.117576|    2.769795|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.0994e-01|   -1.267223|    1.565550|    1.141885|    4.144438|   46.482609|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.0981e-01|   -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	0m2.340s
user	0m2.320s
sys	0m2.639s
+ status=0
+ set +x

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


=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.796888
 Tessellating body 1 with  MaxEdge = 0.094922  Sag = 0.003797  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9  > autoInputs.out
 Executing: ./aero.csh > aero.out
C_A  0.053141419
C_Y  -0.0016408234
C_N  0.0010818265
C_D  0.053146802
C_S  -0.0016408234
C_L  -0.0007734413
C_l  0.000390969
C_m  -0.00073233
C_n  -0.0427853
C_M_x  -0.00110246
C_M_y  -0.00073233
C_M_z  -0.0427729

real	0m30.658s
user	0m54.941s
sys	0m11.259s
+ status=0
+ set +x

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


=================================================
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'masstran_PyTest.py test;'
masstran_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u masstran_PyTest.py -outLevel=0

Getting results mass properties.....

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 1159
Number of elements = 798
Number of 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, -4.234557619726e-11]
CG        [1.222256036874, 0.1634981473778, -4.234646255666e-11]
Ixx       22133.97306033
Iyy       23448.30046709
Izz       1389.213122582
Ixy       164.2055275657
Ixz       -7.454848862776e-06
Iyz       1.707686870183e-06
I         [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454848862776e-06, 1.707686870183e-06]
II        [[22133.97306033, -164.2055275657, 7.454848862776e-06], [-164.2055275657, 23448.30046709, -1.707686870183e-06], [7.454848862776e-06, -1.707686870183e-06, 1389.213122582]]

real	0m9.599s
user	0m14.834s
sys	1m14.660s
+ status=0
+ set +x

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


=================================================
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
hsm_SingleLoadCase_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 81
	Number of elements = 96
	Elemental Tria3 = 0
	Elemental Quad4 = 64

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
 Matrix Non-zero Entries = 5741

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.130E-01  0.165E+00  0.153E-04    1.000  ddy @ (   0.25   0.06   0.00)
   1*   0.260E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   1*   0.240E-05  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.09   0.00)
   2    0.379E-02  0.505E-01  0.750E-04    1.000  ddy @ (   0.25   0.19   0.00)
   2*   0.420E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   3    0.168E-02  0.225E-01  0.208E-04    1.000  ddy @ (   0.25   0.06   0.00)
   4    0.325E-03  0.427E-02  0.250E-05    1.000  ddy @ (   0.25   0.19   0.00)
   5    0.794E-05  0.112E-03  0.170E-06    1.000  ddy @ (   0.25   0.19   0.00)
   6    0.387E-08  0.598E-07  0.197E-09    1.000  ddy @ (   0.25   0.06   0.00)
   7    0.848E-15  0.147E-13  0.924E-15    1.000  ddy @ (   0.25   0.19   0.00)

 Converging n vectors ...
 it =  1    dn =  0.788E-01   rlx = 1.000  (  59 )
 it =  2    dn =  0.566E-16   rlx = 1.000  (  35 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.691E-03   rlx = 1.000  (  45 )
 it =  2    de =  0.404E-04   rlx = 1.000  (   9 )
 it =  3    de =  0.142E-07   rlx = 1.000  (  46 )
 it =  4    de =  0.521E-11   rlx = 1.000  (  62 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat

real	0m1.146s
user	0m0.881s
sys	0m0.233s
+ status=0
+ set +x

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


=================================================
+ echo 'mystran_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
mystran_PyTest.py test;
+ python -u mystran_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 293
Number of elements = 217
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes    = 293
Total number of elements = 217
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 293
	Number of elements = 217
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 217

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties

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

Load tuple is NULL - No loads applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file


Writing MYSTRAN instruction file....
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Natural freq ( Mode 0 ) =  0.5358645269893247 (Hz)
Natural freq ( Mode 1 ) =  0.5358645288538302 (Hz)
Natural freq ( Mode 2 ) =  2.6579076333721185 (Hz)
Natural freq ( Mode 3 ) =  2.6579076479978427 (Hz)
Natural freq ( Mode 4 ) =  3.2133127087466975 (Hz)
Natural freq ( Mode 5 ) =  3.2133127114362425 (Hz)
Natural freq ( Mode 6 ) =  3.712843116135463 (Hz)
Natural freq ( Mode 7 ) =  3.712843117326941 (Hz)
Natural freq ( Mode 8 ) =  6.903423804859605 (Hz)
Natural freq ( Mode 9 ) =  6.903423839338914 (Hz)
Natural freq ( Mode 10 ) =  8.827207024344524 (Hz)
Natural freq ( Mode 11 ) =  8.827207031330142 (Hz)
Natural freq ( Mode 12 ) =  9.03449773731031 (Hz)
Natural freq ( Mode 13 ) =  9.034497746173443 (Hz)
Natural freq ( Mode 14 ) =  12.8109559408829 (Hz)
Natural freq ( Mode 15 ) =  12.810955955402907 (Hz)
Natural freq ( Mode 16 ) =  14.595903948824276 (Hz)
Natural freq ( Mode 17 ) =  14.59590396022714 (Hz)
Natural freq ( Mode 18 ) =  17.253138349030806 (Hz)
Natural freq ( Mode 19 ) =  17.253138376649513 (Hz)
Natural freq ( Mode 20 ) =  19.538997520944356 (Hz)
Natural freq ( Mode 21 ) =  19.538997554170034 (Hz)
Natural freq ( Mode 22 ) =  20.568307328701618 (Hz)
Natural freq ( Mode 23 ) =  20.56830734866142 (Hz)
Natural freq ( Mode 24 ) =  21.24686865493497 (Hz)
Natural freq ( Mode 25 ) =  21.24686866016843 (Hz)
Natural freq ( Mode 26 ) =  26.056089983769358 (Hz)
Natural freq ( Mode 27 ) =  26.056090002586494 (Hz)
Natural freq ( Mode 28 ) =  28.34916233172509 (Hz)
Natural freq ( Mode 29 ) =  28.34916240000593 (Hz)
Natural freq ( Mode 30 ) =  30.373999861912047 (Hz)
Natural freq ( Mode 31 ) =  30.374000056369606 (Hz)
Natural freq ( Mode 32 ) =  33.67251107899125 (Hz)
Natural freq ( Mode 33 ) =  33.672511087763944 (Hz)
Natural freq ( Mode 34 ) =  36.20316316640763 (Hz)
Natural freq ( Mode 35 ) =  36.20316318691549 (Hz)
Natural freq ( Mode 36 ) =  37.222792092183724 (Hz)
Natural freq ( Mode 37 ) =  37.22279210235211 (Hz)
Natural freq ( Mode 38 ) =  39.818094936465606 (Hz)
Natural freq ( Mode 39 ) =  39.818095134840526 (Hz)
Natural freq ( Mode 40 ) =  41.667071059937285 (Hz)
Natural freq ( Mode 41 ) =  41.66707106302638 (Hz)
Natural freq ( Mode 42 ) =  44.898935272842216 (Hz)
Natural freq ( Mode 43 ) =  44.89893529507135 (Hz)
Natural freq ( Mode 44 ) =  47.604563839454244 (Hz)
Natural freq ( Mode 45 ) =  47.6045640014132 (Hz)
Natural freq ( Mode 46 ) =  49.15118222210395 (Hz)
Natural freq ( Mode 47 ) =  49.15118223332836 (Hz)

real	0m12.935s
user	0m18.704s
sys	1m55.092s
+ status=0
+ set +x

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


=================================================
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo '../corsairlite/qp.py test;'
../corsairlite/qp.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u ../corsairlite/qp.py -outLevel=0

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	0m2.188s
user	0m2.288s
sys	0m0.880s
+ status=0
+ set +x

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


*************************************************
*************************************************

=================================================
Did not run examples for:

Astros
=================================================

All tests pass!

make[1]: Leaving directory '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/examples'
(cd legacy/examples/regressionTest; ./execute_PyTestRegression.sh MINIMAL)

=================================================
Legacy Using python : /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/ESP/venv/bin/python
=================================================

Running.... MINIMAL PyTests

=================================================
+ rm -rf avl_PyTest
+ echo 'avl_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/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)
Running AVL
CXtot   0.000611907868574681
CYtot   -6.289312383470904e-15
CZtot   -0.3012861394886091
Cltot   -4.782081713039163e-14
Cmtot   -0.1945055953450467
Cntot   -2.339461801636068e-15
Cl'tot  -4.7854363026524e-14
Cn'tot  -1.504517153549636e-15
CLtot   0.3012509314150773
CDtot   0.004646353488232845
CDvis   0.0
CLff    0.3009503023520526
CYff    -7.719145079534105e-15
CDind   0.004646353488232845
CDff    0.004968969500908293
e       0.9669902146157952
StripForces 
Wing  cl =  [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing  cd =  [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m0.491s
user	0m0.468s
sys	0m0.361s
+ status=0
+ set +x

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


=================================================
+ rm -rf xfoil_PyTest
+ echo 'xfoil_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt


Running xFoil......
Cl =  [0.986723182710393, 1.27996524197906, 1.4683981236604, 1.65936133274566, 1.80584451282044, 1.89831579818228, 1.8479096293896, 1.75995487201918, 1.65517435322733]
Cd =  [0.0125901672123701, 0.0157267711976542, 0.0189519330659632, 0.0231513145536885, 0.0306140208946916, 0.0433620548565217, 0.0708699896705503, 0.0928530378323145, 0.118977178460154]
Alpha =  [0.0, 3.0, 5.0, 7.0, 9.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.49936055887155, 0.463997145318054, 0.444733833301408, 0.424150787095459, 0.400117472036691, 0.364373550846682, 0.280961990145327, 0.2200472417656, 0.139581369732118]
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m2.206s
user	0m2.225s
sys	0m0.305s
+ status=0
+ set +x

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


=================================================
+ rm -rf awave_PyTest
+ echo 'awave_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
awave_PyTest.py test;
+ python -u awave_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/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
 Running AWAVE 
 Running Post Analysis
CdWave =  [1.13332772, 0.216380954]
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m0.562s
user	0m0.607s
sys	0m0.349s
+ status=0
+ set +x

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


=================================================
+ rm -rf aflr2_PyTest
+ echo 'aflr2_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 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     Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR2    : Compile Date   06/13/22 @ 12:42PM
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          =     0.019   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          =     0.014   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

WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m0.667s
user	0m0.801s
sys	0m2.164s
+ status=0
+ set +x

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


=================================================
+ rm -rf delaundo_PyTest
+ echo 'delaundo_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5

Getting mesh sizing parameters
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes 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


Running Delaundo......
Reading delaundo mesh file - delaundoMesh.mesh
	Swapping y and z coordinates!

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

WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m0.728s
user	0m0.854s
sys	0m6.403s
+ status=0
+ set +x

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


=================================================
+ rm -rf masstran_PyTest
+ echo 'masstran_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u masstran_PyTest.py -verbosity=0 -workDir=runDirectory
No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 1159
Number of elements = 798
Number of 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
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1159
	Number of elements = 798
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 798

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

Getting results mass properties.....

Area      3.428666259747
Mass      5383.006027803
Centroid  [1.222256036874, 0.1634981473778, -4.234557619726e-11]
CG        [1.222256036874, 0.1634981473778, -4.234646255666e-11]
Ixx       22133.97306033
Iyy       23448.30046709
Izz       1389.213122582
Ixy       164.2055275657
Ixz       -7.454848862776e-06
Iyz       1.707686870183e-06
I         [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454848862776e-06, 1.707686870183e-06]
II        [[22133.97306033, -164.2055275657, 7.454848862776e-06], [-164.2055275657, 23448.30046709, -1.707686870183e-06], [7.454848862776e-06, -1.707686870183e-06, 1389.213122582]]
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m8.771s
user	0m15.460s
sys	2m19.868s
+ status=0
+ set +x

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


=================================================
+ rm -rf hsm_SingleLoadCase_PyTest
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
+ python -u hsm_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 81
	Number of elements = 96
	Elemental Tria3 = 0
	Elemental Quad4 = 64

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
 Matrix Non-zero Entries = 5741

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.130E-01  0.165E+00  0.153E-04    1.000  ddy @ (   0.25   0.06   0.00)
   1*   0.260E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   1*   0.240E-05  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.09   0.00)
   2    0.379E-02  0.505E-01  0.750E-04    1.000  ddy @ (   0.25   0.19   0.00)
   2*   0.420E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   3    0.168E-02  0.225E-01  0.208E-04    1.000  ddy @ (   0.25   0.06   0.00)
   4    0.325E-03  0.427E-02  0.250E-05    1.000  ddy @ (   0.25   0.19   0.00)
   5    0.794E-05  0.112E-03  0.170E-06    1.000  ddy @ (   0.25   0.19   0.00)
   6    0.387E-08  0.598E-07  0.197E-09    1.000  ddy @ (   0.25   0.06   0.00)
   7    0.848E-15  0.147E-13  0.924E-15    1.000  ddy @ (   0.25   0.19   0.00)

 Converging n vectors ...
 it =  1    dn =  0.788E-01   rlx = 1.000  (  59 )
 it =  2    dn =  0.566E-16   rlx = 1.000  (  35 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.691E-03   rlx = 1.000  (  45 )
 it =  2    de =  0.404E-04   rlx = 1.000  (   9 )
 it =  3    de =  0.142E-07   rlx = 1.000  (  46 )
 it =  4    de =  0.521E-11   rlx = 1.000  (  62 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m0.783s
user	0m0.810s
sys	0m0.303s
+ status=0
+ set +x

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


*************************************************
*************************************************

=================================================
Legacy Did not run examples for:

Astros
=================================================

All tests pass!

[Execution node] check if [reynolds] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[MSBuild] Parsing console log (workspace: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10')
[MSBuild] -> found 0 issues (skipped 0 duplicates)
[MSBuild] Parsing console log (workspace: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10')
[MSBuild] -> found 0 issues (skipped 0 duplicates)
[MSBuild] Successfully parsed console log
[MSBuild] -> found 0 issues (skipped 0 duplicates)
[MSBuild] Parsing console log (workspace: '/jenkins/workspace/ESP_Commit/7.6/LINUX64.gnu10')
[MSBuild] Skipping post processing
[MSBuild] No filter has been set, publishing all 0 issues
[MSBuild] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.6,LINUX64.gnu10,reynolds)
[Static Analysis] Using reference build 'ESP_Commit/CASREV=7.6,ESP_ARCH=LINUX64.gnu10,buildnode=reynolds #6922' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Commit/CASREV=7.6,ESP_ARCH=LINUX64.gnu10,buildnode=reynolds #6923'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS