The Jenkins Controller is preparing for shutdown. No new builds can be started.
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Full Logzmin has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 1 hist: (null) -> Initial Phase aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 1 value (8x1) = -0.825000 -0.812500 -0.800000 -0.775000 -0.750000 -0.700000 -0.690000 -0.100000 (null) zmax has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 1 hist: (null) -> Initial Phase aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 1 value (8x1) = 0.825000 0.812500 0.800000 0.775000 0.750000 0.700000 0.690000 0.100000 (null) unused has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 7 hist: (null) -> Initial Phase aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 1 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 7 linked to ParamName pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 16 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 16 value = 34.641525 (null) cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 16 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 16 value = 7.296560 (null) testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 18 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 18 4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs 1 Bodies, 1 Tessellations testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 8 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 8 value = 5.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 8 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 8 value (1x3) = 1: Entry1 -> Value1 2: Entry2 -> Value2 3: Entry3 -> Value3 tessIn has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 8 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 8 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 8 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 8 value (0x0) = NULL with len = 0 meter testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 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-centOS7:27413 jenkins 2024/04/27 19:18:01 18 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 18 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 18 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 9 testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:18:01 18 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 18 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 18 value = 42 (null) testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:18:01 28 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:18:01 28 4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs 1 Bodies, 1 Tessellations testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 10 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 10 value = 6.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 12 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 12 value (1x3) = 1: Entry1 -> newValue1 2: Entry2 -> newValue2 3: Entry3 -> newValue3 tessIn has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 18 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 13 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 linked to tessOut meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 10 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 10 value (0x0) = NULL with len = 0 meter testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 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-centOS7:27413 jenkins 2024/04/27 19:18:01 28 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 11 testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0! tessPtr = 1a4ea30 value = 1a4ea30 ego lazy: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:18:01 28 meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 11 testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:18:01 28 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:18:01 28 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:18:01 28 value = 42 (null) Interface has type BOUND, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 14 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 2 Connecteds, 0 UnConnecteds testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 5 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 1113 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 1113 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:18:01 26 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 15 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:18:01 26 1113 points, rank=1, units=(null) testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 6 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 447 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 23 447 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 25 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Child Execute aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:43 25 447 points, rank=1, units=(null) vector has type DATASET, subtype NONE with 0 attributes last: aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 hist: (null) -> Starting aimTest reynolds-centOS7:27413 jenkins 2024/04/27 19:17:42 0 testingAIM/aimTransfer name = vector instance = 0 npts = 447/3! 447 points, rank=3, units=(null) 1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 8: 14.400000 14.400000 14.400000 14.380647 14.400000 14.381201 14.400000 15: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 22: 14.400000 14.400000 14.390441 14.400000 14.383859 14.400000 14.400000 29: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 36: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 43: 14.385061 14.400000 14.383844 14.400000 14.400000 14.400000 14.400000 50: 14.378338 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 57: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.376665 64: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 78: 14.389247 14.400000 14.400000 14.400000 14.400000 14.382317 14.400000 85: 14.400000 14.400000 14.400000 14.390011 14.400000 14.400000 14.400000 92: 14.400000 14.400000 14.400000 14.400000 14.389865 14.400000 14.389101 99: 14.400000 14.388170 14.400000 14.400000 14.400000 14.400000 14.400000 106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 155: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 162: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 169: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 176: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 183: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 190: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 197: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 204: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 211: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 218: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 225: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 232: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 239: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 246: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 253: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 260: 14.400000 14.400000 14.400000 14.399999 14.400000 14.400000 14.400000 267: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 274: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 281: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 288: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 295: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 302: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 309: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 316: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 323: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 330: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 337: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 344: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 351: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 358: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 365: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 372: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 379: 14.400000 14.400000 14.400000 14.400000 14.399999 14.400000 14.400000 386: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 393: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 400: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 407: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 414: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 421: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 428: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 435: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 442: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 449: 14.400000 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 456: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 463: 14.400000 14.400000 14.400000 14.400000 14.399999 14.400000 14.399999 470: 14.400000 14.400000 14.400000 14.400000 14.400000 14.399999 14.400000 477: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 491: 14.399999 14.400000 14.400000 14.400000 14.365872 14.400000 14.400000 498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 505: 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 512: 14.400000 14.399999 14.399999 14.400000 14.400000 14.400000 14.400000 519: 14.400000 14.362939 14.399999 14.362723 14.400000 14.400000 14.400000 526: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 533: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 540: 14.400000 14.400000 14.400000 14.399999 14.400000 14.399999 14.400000 547: 14.368368 14.400000 14.400000 14.399999 14.400000 14.369831 14.400000 554: 14.400000 14.400000 14.400000 14.368625 14.399999 14.362939 14.400000 561: 14.400000 14.366035 14.400000 14.400000 14.400000 14.400000 14.400000 568: 14.356726 14.400000 14.369831 14.369176 14.400000 14.399999 14.400000 575: 14.400000 14.399999 14.400000 14.400000 14.400000 14.400000 14.400000 582: 14.399999 14.363748 14.368368 14.400000 14.399999 14.400000 14.400000 589: 14.369831 14.400000 14.359401 14.399999 14.362295 14.400000 14.399999 596: 14.373877 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 603: 14.369218 14.369218 14.400000 14.365682 14.400000 14.369054 14.400000 610: 14.400000 14.400000 14.400000 14.371386 14.368747 14.372230 14.400000 617: 14.375508 14.400000 14.364430 14.374160 14.400000 14.400000 14.400000 624: 14.368709 14.369354 14.400000 14.400000 14.400000 14.399999 14.400000 631: 14.400000 14.400000 14.370155 14.368220 14.400000 14.372237 14.400000 638: 14.400000 14.374425 14.372364 14.400000 14.400000 14.400000 14.400000 645: 14.375987 14.365558 14.368709 14.366781 14.400000 14.369176 14.369354 652: 14.399999 14.373289 14.400000 14.375685 14.374425 14.400000 14.377582 659: 14.399999 14.400000 14.400000 14.366036 14.400000 14.400000 14.400000 666: 14.400000 14.375124 14.400000 14.400000 14.368903 14.368555 14.399999 673: 14.400000 14.371386 14.371386 14.399999 14.400000 14.379372 14.369130 680: 14.374049 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 687: 14.376400 14.399999 14.377760 14.378863 14.374473 14.367810 14.400000 694: 14.400000 14.368784 14.400000 14.371386 14.365916 14.400000 14.373165 701: 14.400000 14.399999 14.372471 14.400000 14.400000 14.400000 14.400000 708: 14.375987 14.379953 14.400000 14.374316 14.377675 14.400000 14.376295 715: 14.400000 14.399999 14.399999 14.368903 14.368784 14.366475 14.400000 722: 14.400000 14.369555 14.400000 14.378687 14.378687 14.378950 14.400000 729: 14.375449 14.376400 14.371321 14.400000 14.400000 14.371351 14.399999 736: 14.400000 14.375126 14.400000 14.400000 14.400000 14.375504 14.368903 743: 14.368514 14.400000 14.400000 14.400000 14.400000 14.379510 14.375124 750: 14.376289 14.374679 14.400000 14.400000 14.399999 14.400000 14.378601 757: 14.399999 14.377088 14.400000 14.375718 14.373640 14.400000 14.400000 764: 14.372001 14.400000 14.400000 14.368903 14.368514 14.400000 14.374569 771: 14.400000 14.375271 14.400000 14.400000 14.400000 14.400000 14.380018 778: 14.399999 14.400000 14.379331 14.400000 14.400000 14.379693 14.400000 785: 14.372552 14.383094 14.375769 14.400000 14.372608 14.378845 14.400000 792: 14.373363 14.368903 14.400000 14.375189 14.378667 14.375797 14.377675 799: 14.400000 14.400000 14.379863 14.373732 14.400000 14.400000 14.400000 806: 14.400000 14.400000 14.375857 14.400000 14.400000 14.400000 14.400000 813: 14.400000 14.400000 14.400000 14.400000 14.376290 14.379510 14.400000 820: 14.400000 14.400000 14.374594 14.400000 14.376305 14.400000 14.373349 827: 14.400000 14.379553 14.379553 14.373363 14.400000 14.377860 14.382472 834: 14.379566 14.400000 14.376493 14.400000 14.400000 14.400000 14.400000 841: 14.378207 14.375251 14.376605 14.400000 14.378626 14.400000 14.400000 848: 14.400000 14.376156 14.377590 14.379497 14.400000 14.375464 14.378358 855: 14.400000 14.380743 14.375541 14.400000 14.373960 14.400000 14.380592 862: 14.379305 14.374687 14.383536 14.400000 14.400000 14.374081 14.400000 869: 14.400000 14.380716 14.379808 14.383716 14.400000 14.383966 14.377272 876: 14.400000 14.379553 14.400000 14.377570 14.400000 14.376445 14.382213 883: 14.400000 14.400000 14.400000 14.400000 14.371272 14.379704 14.400000 890: 14.400000 14.379158 14.400000 14.379112 14.383216 14.380581 14.400000 897: 14.382554 14.400000 14.383382 14.400000 14.381160 14.400000 14.400000 904: 14.385313 14.382398 14.378148 14.381487 14.400000 14.378927 14.380605 911: 14.400000 14.400000 14.382990 14.384339 14.381122 14.380943 14.382554 918: 14.400000 14.375911 14.400000 14.384096 14.379502 14.376270 14.382299 925: 14.400000 14.380606 14.380606 14.383670 14.382868 14.400000 14.380592 932: 14.400000 14.379141 14.400000 14.400000 14.400000 14.400000 14.379453 939: 14.383433 14.382323 14.382931 14.376462 14.385109 14.386913 14.377700 946: 14.384542 14.400000 14.378601 14.387579 14.400000 14.400000 14.400000 953: 14.385467 14.379641 14.381746 14.383298 14.379931 14.400000 14.381446 960: 14.378196 14.400000 14.400000 14.381474 14.400000 14.383687 14.400000 967: 14.400000 14.384788 14.382697 14.379960 14.382187 14.383772 14.400000 974: 14.376286 14.374476 14.383667 14.382627 14.379931 14.384695 14.384795 981: 14.384528 14.385187 14.382443 14.381568 14.384519 14.385991 14.400000 988: 14.381424 14.400000 14.376098 14.383598 14.400000 14.375887 14.382344 995: 14.400000 14.374829 14.400000 14.386850 14.382671 14.380741 14.377878 1002: 14.388595 14.383869 14.385187 14.400000 14.400000 14.386296 14.384522 1009: 14.388515 14.385094 14.381609 14.387264 14.385337 14.386730 14.386730 1016: 14.387884 14.400000 14.376353 14.377969 14.376462 14.384854 14.378940 1023: 14.400000 14.386177 14.385200 14.385211 14.400000 14.400000 14.388399 1030: 14.384905 14.400000 14.400000 14.385855 14.386303 14.386373 14.389777 1037: 14.383001 14.384393 14.387981 14.400000 14.379911 14.378339 14.400000 1044: 14.400000 14.400000 14.380951 14.382823 14.381293 14.400000 14.400000 1051: 14.375959 14.380629 14.382256 14.388550 14.385775 14.389044 14.386740 1058: 14.385318 14.400000 14.380768 14.387137 14.385084 14.386362 14.379022 1065: 14.400000 14.383819 14.400000 14.373221 14.400000 14.387729 14.382944 1072: 14.387356 14.400000 14.390026 14.387727 14.388858 14.400000 14.381248 1079: 14.386362 14.378339 14.400000 14.400000 14.375685 14.381865 14.383342 1086: 14.386099 14.381327 14.386556 14.381954 14.385445 14.383357 14.384113 1093: 14.379911 14.400000 14.383874 14.400000 14.381638 14.391021 14.400000 1100: 14.400000 14.400000 14.400000 14.400000 14.384656 14.400000 14.378251 1107: 14.400000 14.381757 14.383106 14.386337 14.384313 14.383799 14.384686 source getTriangles = 0, nGtris = 2108, nGsegs = 6324, Ds = 0 0 destin getTriangles = 0, nGtris = 800, nGsegs = 2400, Ds = 0 0 In caps_outputObjects: 2 Analyses found 1 Bounds found testingAIM/aimCleanup instance = 0! testingAIM/aimCleanup instance = 1! real 0m18.888s user 0m18.875s sys 0m0.112s + set +x ============================================= CAPS test (using c-executables) case /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/test/aim testingAIM.csm passed (as expected) ============================================= + rm -rf source.vs destin.vs + expectCSuccess '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/test/autoExec testingAIM.csm' + /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 = /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 = /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 0m0.632s user 0m0.626s sys 0m0.123s + set +x ============================================= CAPS test (using c-executables) case /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/test/autoExec testingAIM.csm passed (as expected) ============================================= make -C aim/skeleton test make[1]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/aim/skeleton' # pyCAPS Unit tests (and legacy) make -C pyCAPS/unitTest test make[1]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/pyCAPS/unitTest' python --version Python 3.11.9 python -u -m unittest discover ..Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 143 Number of elements = 282 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 282 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 140 Number of elements = 276 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 276 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 283 Combined Number of elements = 558 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 558 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ..Writing D3 Javascript library - d3.v3.min.js ........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .No analysis directory provided - defaulting to altName Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 209 Number of elements = 414 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 414 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 186 Number of elements = 368 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 368 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 395 Combined Number of elements = 782 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 782 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input ..........--> Opening DESPMTR file "unitGeom.param" updating CFGPMTR series [ 1, 1] = 8412.000000 updating CFGPMTR series2 [ 1, 1] = 20.000000 updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000 updating CFGPMTR nrow [ 1, 1] = 3.000000 updating CFGPMTR ncol [ 1, 1] = 2.000000 updating DESPMTR area [ 1, 1] = 40.000000 updating DESPMTR aspect [ 1, 1] = 5.000000 updating DESPMTR taper [ 1, 1] = 0.500000 updating DESPMTR twist [ 1, 1] = 15.000000 updating DESPMTR wing:lesweep [ 1, 1] = 30.000000 updating DESPMTR wing:dihedral [ 1, 1] = 1.000000 updating DESPMTR wing:chord:root [ 1, 1] = 1.560000 updating DESPMTR htail [ 1, 1] = 1.000000 updating DESPMTR htail:chord [ 1, 1] = 2.000000 updating DESPMTR vtail:chord [ 1, 1] = 3.000000 updating DESPMTR vtail [ 1, 1] = 4.000000 updating DESPMTR sphereR [ 1, 1] = 80.000000 updating DESPMTR v@1:d_name [ 1, 1] = 1.000000 updating DESPMTR despMat [ 1, 1] = 11.000000 updating DESPMTR despMat [ 1, 2] = 12.000000 updating DESPMTR despMat [ 2, 1] = 13.000000 updating DESPMTR despMat [ 2, 2] = 14.000000 updating DESPMTR despMat [ 3, 1] = 15.000000 updating DESPMTR despMat [ 3, 2] = 16.000000 updating DESPMTR despCol [ 1, 1] = 11.000000 updating DESPMTR despCol [ 2, 1] = 13.000000 updating DESPMTR despCol [ 3, 1] = 15.000000 updating DESPMTR despRow [ 1, 1] = 11.000000 updating DESPMTR despRow [ 1, 2] = 12.000000 updating DESPMTR despRow [ 1, 3] = 13.000000 ERROR:: DESPMTR file "unitGeom.param" not found CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! ..Linked Parameter Beta to analysis su2 input Beta Linked Parameter Alpha to analysis su2 input Alpha No linkable data found for Altitude No linkable data found for Strings No linkable data found for Strings2 Linked Parameter Beta to analysis su2 input Beta Linked Parameter Alpha to analysis su2 input Alpha ............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . CAPS Info: Hit last success -- going live! ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .--> Opening DESPMTR file "unitGeom.param" updating CFGPMTR series [ 1, 1] = 8412.000000 updating CFGPMTR series2 [ 1, 1] = 20.000000 updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000 updating CFGPMTR nrow [ 1, 1] = 3.000000 updating CFGPMTR ncol [ 1, 1] = 2.000000 updating DESPMTR area [ 1, 1] = 40.000000 updating DESPMTR aspect [ 1, 1] = 5.000000 updating DESPMTR taper [ 1, 1] = 0.500000 updating DESPMTR twist [ 1, 1] = 15.000000 updating DESPMTR wing:lesweep [ 1, 1] = 30.000000 updating DESPMTR wing:dihedral [ 1, 1] = 1.000000 updating DESPMTR wing:chord:root [ 1, 1] = 1.560000 updating DESPMTR htail [ 1, 1] = 1.000000 updating DESPMTR htail:chord [ 1, 1] = 2.000000 updating DESPMTR vtail:chord [ 1, 1] = 3.000000 updating DESPMTR vtail [ 1, 1] = 4.000000 updating DESPMTR sphereR [ 1, 1] = 80.000000 updating DESPMTR v@1:d_name [ 1, 1] = 1.000000 updating DESPMTR despMat [ 1, 1] = 11.000000 updating DESPMTR despMat [ 1, 2] = 12.000000 updating DESPMTR despMat [ 2, 1] = 13.000000 updating DESPMTR despMat [ 2, 2] = 14.000000 updating DESPMTR despMat [ 3, 1] = 15.000000 updating DESPMTR despMat [ 3, 2] = 16.000000 updating DESPMTR despCol [ 1, 1] = 11.000000 updating DESPMTR despCol [ 2, 1] = 13.000000 updating DESPMTR despCol [ 3, 1] = 15.000000 updating DESPMTR despRow [ 1, 1] = 11.000000 updating DESPMTR despRow [ 1, 2] = 12.000000 updating DESPMTR despRow [ 1, 3] = 13.000000 ERROR:: DESPMTR file "unitGeom.param" not found CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ---------------------------------------------------------------------- Ran 100 tests in 15.119s 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 `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/pyCAPS/unitTest' make -C legacy/unitTest test make[1]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/unitTest' python --version Python 3.11.9 python -u -m unittest discover ......sAnalysis Info: Name = UnitTest_fun3dAIM Intent = None AnalysisDir = /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty Analysis Info: Name = UnitTest_fun3dAIM Intent = None AnalysisDir = /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_1 will be used! Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_2 will be used! Analysis Info: Name = UnitTest7_fun3dAIM Intent = None AnalysisDir = /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest7_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_3 will be used! Analysis Info: Name = UnitTest8_fun3dAIM Intent = None AnalysisDir = /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest8_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_4 will be used! Analysis Info: Name = UnitTest9_fun3dAIM Intent = STRUCTURE AnalysisDir = /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest9_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_5 will be used! Analysis Info: Name = UnitTest10_fun3dAIM Intent = ['CFD', 'STRUCTURE'] AnalysisDir = /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest10_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty ...Error: Invalid attribute level! Defaulting to 'Face' .. Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_6 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_7 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_8 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_9 will be used! Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_1 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_10 will be used! Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_2 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_11 will be used! Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_3 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_12 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_13 will be used! ...No data transfer method (transferMethod) provided - defaulting to "Interpolate" No data transfer method (transferMethod) provided - defaulting to "Interpolate" .No data transfer method (transferMethod) provided - defaulting to "Interpolate" ....No data transfer method (transferMethod) provided - defaulting to "Interpolate" .No data transfer method (transferMethod) provided - defaulting to "Interpolate" . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .s. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ...Error: Invalid attribute level! Defaulting to 'Face' ........ EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! .... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .s... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .Linked Parameter Beta to analysis fun3d input Beta Linked Parameter Alpha to analysis fun3d input Alpha Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 7F47E1CF1700 Odd Degenerate test for side 1: 9! 7F480030C740 Odd Degenerate test for side 2: 9! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 408 Number of elements = 812 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 812 Elemental Quad4 = 0 7F47E1CF1700 Odd Degenerate test for side 1: 9! 7F47E1CF1700 Odd Degenerate test for side 2: 9! Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 623 Number of elements = 1242 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1242 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 1031 Combined Number of elements = 2054 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 2054 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input ................ ---------------------------------------------------------------------- Ran 72 tests in 4.500s 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 `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/unitTest' # CAPS Minimal examples (one per aim) make -C examples test TYPE=MINIMAL make[1]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples' (make -C cCAPS -f aeroelastic_SU2.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f avlTest.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/cCAPS/avlTest' is up to date. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f awaveTest.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/cCAPS/awaveTest' is up to date. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f frictionTest.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/cCAPS/frictionTest' is up to date. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f fun3d.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: Nothing to be done for `fun3d'. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f hsm.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: `hsm' is up to date. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f interferenceTest.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/cCAPS/interferenceTest' is up to date. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f msesTest.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/cCAPS/msesTest' is up to date. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f mystran.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/cCAPS/mystranTest' is up to date. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (make -C cCAPS -f pointwiseTest.make) make[2]: Entering directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' make[2]: `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/cCAPS/pointwiseTest' is up to date. make[2]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples/cCAPS' (cd /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest; ./execute_CTestRegression.sh MINIMAL) Running.... MINIMAL c-Tests All tests pass! (cd /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest; ./execute_PyTestRegression.sh MINIMAL) ================================================= Using python : /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/venv/bin/python ================================================= Running.... MINIMAL PyTests ================================================= + echo 'avl_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 0.0006119078685746836 CYtot -6.288067668554914e-15 CZtot -0.3012861394886091 Cltot -4.782099331324466e-14 Cmtot -0.1945055953450467 Cntot -2.339543963831951e-15 Cl'tot -4.785454061647156e-14 Cn'tot -1.504596228417061e-15 CLtot 0.3012509314150772 CDtot 0.004646353488232841 CDvis 0.0 CLff 0.3009503023520527 CYff -7.718708857566269e-15 CDind 0.004646353488232841 CDff 0.004968969500908292 e 0.9669902146157957 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 0m0.694s user 0m0.538s sys 0m0.408s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt + echo 'xfoil_PyTest.py test;' xfoil_PyTest.py test; + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt + python -u xfoil_PyTest.py -outLevel=0 -noPlotData Cl = [1.05475230552567, 1.36488869373635, 1.56607214272105, 2.03059709344862, 1.97271083121169, 1.87307153172386, 1.76050475760117] Cd = [0.0131991208675727, 0.0166540240605751, 0.0200551482562831, 0.0458671341969345, 0.0754256009394856, 0.0994469174477522, 0.127479430989037] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.4960441144043, 0.461377732041502, 0.44237656820185, 0.361251636355465, 0.276104140853559, 0.214381239321467, 0.132988264746661] real 0m4.964s user 0m4.882s sys 0m0.293s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected) ================================================= ================================================= + echo 'mses_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt mses_PyTest.py test; + python -u mses_PyTest.py -outLevel=0 -noPlotData + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Cl = 0.37837910855492407 Cd = 0.007775858417210143 Cm = 0.005262636995811319 real 0m5.257s user 0m5.144s sys 0m0.410s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected) ================================================= ================================================= + echo 'awave_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt awave_PyTest.py test; + python -u awave_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 = [1.13334703, 0.216387704] real 0m0.789s user 0m0.760s sys 0m0.343s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected) ================================================= ================================================= + echo 'friction_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Loading AIM Setting Mach & Altitude Values Lifting Surface: Body = 1, units m XLE: 1.571946 -3.872983 0.249728 XTE: 2.536563 -3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 2, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.614012 0.000000 0.002015 Chord: 1.614013 Arc: 3.308635 T/C: 0.127839 Type: Wing Lifting Surface: Body = 3, units m XLE: 1.571946 3.872983 0.249728 XTE: 2.536563 3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 4, units m XLE: 5.484123 0.000000 1.468246 XTE: 6.210307 0.000915 1.468246 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: VTail Lifting Surface: Body = 5, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.210307 0.001525 0.500000 Chord: 1.210308 Arc: 2.471195 T/C: 0.120035 Type: VTail Lifting Surface: Body = 6, units m XLE: 5.484123 -0.968246 0.500000 XTE: 6.210307 -0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Lifting Surface: Body = 7, units m XLE: 5.484123 0.968246 0.500000 XTE: 6.210307 0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Body of Revolution: Body = 8, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 9, units m Arc: 3.714180 Diameter: 1.020621 Type: Fuse Body of Revolution: Body = 10, units m Arc: 2.771209 Diameter: 0.645497 Type: Fuse Body of Revolution: Body = 11, units m Arc: 1.013945 Diameter: 0.322749 Type: Fuse Body of Revolution: Body = 12, units m Arc: 0.101394 Diameter: 0.032275 Type: Fuse Number of sections 4, number of revolution sections 1 Number of Mach-Altitude cases = 2 Total drag = [0.0132, 0.01226] Form drag = [0.0033, 0.00307] Friction drag = [0.0099, 0.00919] real 0m0.575s user 0m0.420s sys 0m0.290s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tsfoil_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt tsfoil_PyTest.py test; + python -u tsfoil_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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. Cl = 0.933329 Cd = 0.000283 Cd Wave = 0.0 Cm = -0.203433 Cp _Critcal = -1.303869 real 0m0.556s user 0m0.496s sys 0m0.326s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected) ================================================= ================================================= + echo 'delaundo_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt delaundo_PyTest.py test; + python -u delaundo_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 in the x-y plane... attempting to rotate mesh through node swapping! Swapping z and y coordinates! Writing delaundo control file - delaundo.ctr Writing out *.pts file Reading delaundo mesh file - delaundo_CAPS.mesh Swapping y and z coordinates! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file real 0m0.785s user 0m0.737s sys 0m0.422s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt + echo 'egadsTess_PyTest.py test;' egadsTess_PyTest.py test; + python -u egadsTess_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 = 3793 Number of elements = 4001 Number of triangle elements = 0 Number of quadrilateral elements = 4001 Body 2 (of 4) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 3 (of 4) Number of nodes = 76 Number of elements = 55 Number of triangle elements = 0 Number of quadrilateral elements = 55 Body 4 (of 4) Number of nodes = 100 Number of elements = 73 Number of triangle elements = 0 Number of quadrilateral elements = 73 ---------------------------- Total number of nodes = 3970 Total number of elements = 4129 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file real 0m6.244s user 0m13.278s sys 0m1.326s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt + echo 'aflr2_PyTest.py test;' aflr2_PyTest.py test; + python -u aflr2_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM 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 = 0.018 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 6034 11724 AFLR2 QI : Nodes, Faces = 6033 454 AFLR2 QI : Nodes, Faces = 6033 5634 AFLR2 QI : Nodes, Faces = 6033 11722 AFLR2 QI : Nodes, Faces = 6032 462 AFLR2 QI : Nodes, Faces = 6032 5629 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 456 AFLR2 QI : Nodes, Faces = 6032 5632 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 474 AFLR2 QI : Nodes, Faces = 6032 5623 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6031 486 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 QI : Nodes, Faces = 6031 488 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 : CPU Time = 0.009 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file real 0m0.692s user 0m0.655s sys 0m0.325s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr4_and_aflr3_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt aflr4_and_aflr3_PyTest.py test; + python -u aflr4_and_aflr3_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wing1 Mesh sizing name - Wing2 Done getting mesh sizing parameters Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR4 : Compile Date 04/23/24 @ 12:17PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 151604 Number of elements = 458324 Number of triangles = 14380 Number of quadrilatarals = 0 Number of tetrahedrals = 222892 Number of pyramids = 425 Number of prisms = 220627 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file real 0m15.837s user 0m15.254s sys 0m0.444s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tetgen_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt tetgen_PyTest.py test; + python -u tetgen_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 2236 Number of elements = 4468 Number of triangle elements = 4468 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 636 Number of elements = 1268 Number of triangle elements = 1268 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 267 Number of elements = 530 Number of triangle elements = 530 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3139 Total number of elements = 6266 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 3139, elements - 6266 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.03 Creating surface mesh ... Surface mesh seconds: 0.01 Recovering boundaries... Boundary recovery seconds: 0.06 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0 Suppressing Steiner points ... Steiner suppression seconds: 0 Recovering Delaunayness... Delaunay recovery seconds: 0.01 Refining mesh... 4190 insertions, added 2180 points, 134280 tetrahedra in queue. 1395 insertions, added 459 points, 138994 tetrahedra in queue. 1859 insertions, added 487 points, 137112 tetrahedra in queue. 2478 insertions, added 498 points, 120303 tetrahedra in queue. 3304 insertions, added 499 points, 74342 tetrahedra in queue. 4404 insertions, added 474 points, 460 tetrahedra in queue. Refinement seconds: 0.85 Smoothing vertices... Mesh smoothing seconds: 0.69 Improving mesh... Mesh improvement seconds: 0.02 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0 Total running seconds: 1.67 Statistics: Input points: 3139 Input facets: 6266 Input segments: 9399 Input holes: 2 Input regions: 0 Mesh points: 8309 Mesh tetrahedra: 41161 Mesh faces: 85455 Mesh faces on exterior boundary: 6266 Mesh faces on input facets: 6266 Mesh edges on input segments: 9399 Steiner points inside domain: 5170 Done meshing using TetGen! Writing Tecplot file .... Finished writing Tecplot file real 0m3.208s user 0m3.465s sys 0m0.379s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_AFLR2_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt su2_and_AFLR2_PyTest.py test; + python -u su2_and_AFLR2_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Saving geometry Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM 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 = 0.006 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 = 0.086 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 11156 21767 AFLR2 QI : Nodes, Faces = 11155 819 AFLR2 QI : Nodes, Faces = 11155 10473 AFLR2 QI : Nodes, Faces = 11155 21765 AFLR2 QI : Nodes, Faces = 11154 811 AFLR2 QI : Nodes, Faces = 11154 10476 AFLR2 QI : Nodes, Faces = 11154 21763 AFLR2 QI : Nodes, Faces = 11154 805 AFLR2 QI : Nodes, Faces = 11154 10479 AFLR2 QI : Nodes, Faces = 11154 21763 AFLR2 QI : Nodes, Faces = 11154 911 AFLR2 QI : Nodes, Faces = 11154 10426 AFLR2 QI : Nodes, Faces = 11154 21763 AFLR2 QI : Nodes, Faces = 11153 915 AFLR2 QI : Nodes, Faces = 11153 10423 AFLR2 QI : Nodes, Faces = 11153 917 AFLR2 QI : Nodes, Faces = 11153 10423 AFLR2 : CPU Time = 0.018 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 11153 Number of elements = 11885 Number of tris = 917 Number of quad = 10423 EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Airfoil Boundary condition name - InFlow Boundary condition name - OutFlow Boundary condition name - TunnelWall Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.4. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 1 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 1 m. Reference origin for moment evaluation is (0, 0, 0). Surface(s) where the force coefficients are evaluated: BC_5. Surface(s) plotted in the output file: BC_5, BC_2. Input mesh file name: ../aflr2/aflr2_CAPS.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 10. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat. Surface file name: surface_flow_pyCAPS_su2_aflr2. Volume file name: flow_pyCAPS_su2_aflr2. Restart file name: restart_flow_pyCAPS_su2_aflr2.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_5| | | BC_2| +-----------------------------------------------------------------------+ | Inlet boundary| BC_4| +-----------------------------------------------------------------------+ | Outlet boundary| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Two dimensional problem. 11153 grid points. 11340 volume elements. 4 surface markers. 98 boundary elements in index 0 (Marker = BC_2). 24 boundary elements in index 1 (Marker = BC_3). 24 boundary elements in index 2 (Marker = BC_4). 399 boundary elements in index 3 (Marker = BC_5). 917 triangles. 10423 quadrilaterals. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 917 TRIANGLE volume elements. There has been a re-orientation of 10423 QUADRILATERAL volume elements. There has been a re-orientation of 73 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 999.878. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 49.3184| 90| | CV Face Area Aspect Ratio| 1.00035| 33.4982| | CV Sub-Volume Ratio| 1.00001| 7.89914| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11153| 1/1.00| 10| | 1| 2702| 1/4.13| 7.38309| | 2| 549| 1/4.92| 4.99198| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.06265 m. Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m. Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_5 is NOT a single straight. Boundary marker BC_2 is NOT a single straight. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 216054| 1| m^2/s^2| 216054| | Velocity-X| 136.119| 1| m/s| 136.119| | Velocity-Y| 0| 1| m/s| 0| | Velocity Magnitude| 136.119| 1| m/s| 136.119| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.4| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.0139e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 9.9263e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 9.8792e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 9.8384e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 9.7849e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 9.8132e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.7893e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 9.9534e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 9.9375e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 9.8741e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.22124| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |CSV file |surface_flow_pyCAPS_su2_aflr2.csv | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary |flow_pyCAPS_su2_aflr2.szplt | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt| Error in tecFileWriterClose: Not all node map values for zone 1 have been written. Currently need 994 more values.0: Error finishing Tecplot file output. Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). +-----------------------------------------------------------------------+ --------------------------- Finalizing Solver --------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.072253 Cd = -0.01151 Cmz = 0.070975 Cx = -0.01151 Cy = 0.072253 Pressure Contribution Cl_p = 0.072253 Cd_p = -0.01151 Cmz_p = 0.070975 Cx_p = -0.01151 Cy_p = 0.072253 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m2.470s user 0m2.320s sys 0m0.603s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'masstran_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Getting results mass properties..... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 1159 Number of elements = 798 Number of triangle elements = 0 Number of quadrilateral elements = 798 ---------------------------- Total number of nodes = 1159 Total number of elements = 798 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Constraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1159 Number of elements = 798 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 798 Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - Ribs_and_Spars No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Area 3.428666259747 Mass 5383.006027803 Centroid [1.222256036874, 0.1634981473778, -4.234505810751e-11] CG [1.222256036874, 0.1634981473778, -4.234637807833e-11] Ixx 22133.97306033 Iyy 23448.30046709 Izz 1389.213122582 Ixy 164.2055275657 Ixz -7.45484669011e-06 Iyz 1.707686795832e-06 I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.45484669011e-06, 1.707686795832e-06] II [[22133.97306033, -164.2055275657, 7.45484669011e-06], [-164.2055275657, 23448.30046709, -1.707686795832e-06], [7.45484669011e-06, -1.707686795832e-06, 1389.213122582]] real 0m4.392s user 0m6.925s sys 0m1.664s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected) ================================================= ================================================= + echo 'hsm_SingleLoadCase_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt hsm_SingleLoadCase_PyTest.py test; + python -u hsm_SingleLoadCase_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Creating HSM BEM Getting quads for BEM! Number of nodal coordinates = 81 Number of elements = 96 Elemental Tria3 = 0 Elemental Quad4 = 64 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 9 MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 32 ->HSMSOL Matrix Non-zero Entries = 5741 Converging HSM equation system ... iter dr dd dp rlx max 1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00) 1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00) 2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00) 2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00) 4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00) 5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00) 6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00) 7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00) Converging n vectors ... it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 ) it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 ) Converging e1,e2 vectors ... it = 1 de = 0.691E-03 rlx = 1.000 ( 45 ) it = 2 de = 0.404E-04 rlx = 1.000 ( 9 ) it = 3 de = 0.142E-07 rlx = 1.000 ( 46 ) it = 4 de = 0.521E-11 rlx = 1.000 ( 62 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat real 0m1.317s user 0m1.258s sys 0m0.284s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo '../corsairlite/qp.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt ../corsairlite/qp.py test; + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 0m2.224s user 0m2.347s sys 0m0.526s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: abaqus Cart3D Astros Mystran ================================================= All tests pass! make[1]: Leaving directory `/home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/examples' (cd legacy/examples/regressionTest; ./execute_PyTestRegression.sh MINIMAL) ================================================= Legacy Using python : /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/ESP/venv/bin/python ================================================= Running.... MINIMAL PyTests ================================================= + rm -rf avl_PyTest + echo 'avl_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 0.0006119078685746836 CYtot -6.288067668554914e-15 CZtot -0.3012861394886091 Cltot -4.782099331324466e-14 Cmtot -0.1945055953450467 Cntot -2.339543963831951e-15 Cl'tot -4.785454061647156e-14 Cn'tot -1.504596228417061e-15 CLtot 0.3012509314150772 CDtot 0.004646353488232841 CDvis 0.0 CLff 0.3009503023520527 CYff -7.718708857566269e-15 CDind 0.004646353488232841 CDff 0.004968969500908292 e 0.9669902146157957 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: '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: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! 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 0m0.683s user 0m0.467s sys 0m0.312s + 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 /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt xfoil_PyTest.py test; + python -u xfoil_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Running xFoil...... Cl = [1.05475230552567, 1.36488869373635, 1.56607214272105, 2.03059709344862, 1.97271083121169, 1.87307153172386, 1.76050475760117] Cd = [0.0131991208675727, 0.0166540240605751, 0.0200551482562831, 0.0458671341969345, 0.0754256009394856, 0.0994469174477522, 0.127479430989037] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.4960441144043, 0.461377732041502, 0.44237656820185, 0.361251636355465, 0.276104140853559, 0.214381239321467, 0.132988264746661] WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__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 0m4.712s user 0m4.496s sys 0m0.219s + 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 /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt awave_PyTest.py test; + python -u awave_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 = [1.13334703, 0.216387704] WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__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 0m0.770s user 0m0.669s sys 0m0.255s + 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 /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt aflr2_PyTest.py test; + python -u aflr2_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM 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 = 0.026 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 6034 11724 AFLR2 QI : Nodes, Faces = 6033 454 AFLR2 QI : Nodes, Faces = 6033 5634 AFLR2 QI : Nodes, Faces = 6033 11722 AFLR2 QI : Nodes, Faces = 6032 462 AFLR2 QI : Nodes, Faces = 6032 5629 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 456 AFLR2 QI : Nodes, Faces = 6032 5632 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 474 AFLR2 QI : Nodes, Faces = 6032 5623 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6031 486 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 QI : Nodes, Faces = 6031 488 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 : CPU Time = 0.012 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! 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: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.827s user 0m0.839s sys 0m0.429s + 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 /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt delaundo_PyTest.py test; + python -u delaundo_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/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 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 .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__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 0m0.691s user 0m0.650s sys 0m0.412s + 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 /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt 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 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, -4.234505810751e-11] CG [1.222256036874, 0.1634981473778, -4.234637807833e-11] Ixx 22133.97306033 Iyy 23448.30046709 Izz 1389.213122582 Ixy 164.2055275657 Ixz -7.45484669011e-06 Iyz 1.707686795832e-06 I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.45484669011e-06, 1.707686795832e-06] II [[22133.97306033, -164.2055275657, 7.45484669011e-06], [-164.2055275657, 23448.30046709, -1.707686795832e-06], [7.45484669011e-06, -1.707686795832e-06, 1389.213122582]] WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m4.100s user 0m6.929s sys 0m1.694s + 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 /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt hsm_SingleLoadCase_PyTest.py test; + python -u hsm_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /home/jenkins/workspace/ESP_Commit/7.7/LINUX64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Creating HSM BEM Getting quads for BEM! Number of nodal coordinates = 81 Number of elements = 96 Elemental Tria3 = 0 Elemental Quad4 = 64 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 9 MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 32 ->HSMSOL Matrix Non-zero Entries = 5741 Converging HSM equation system ... iter dr dd dp rlx max 1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00) 1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00) 2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00) 2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00) 4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00) 5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00) 6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00) 7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00) Converging n vectors ... it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 ) it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 ) Converging e1,e2 vectors ... it = 1 de = 0.691E-03 rlx = 1.000 ( 45 ) it = 2 de = 0.404E-04 rlx = 1.000 ( 9 ) it = 3 de = 0.142E-07 rlx = 1.000 ( 46 ) it = 4 de = 0.521E-11 rlx = 1.000 ( 62 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! 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: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.360s user 0m1.293s sys 0m0.295s + 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-centOS7] is in [[windows10x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [GNU C Compiler (gcc)] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [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: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [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: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [MSBuild] -> found 0 issues (skipped 0 duplicates) [MSBuild] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [MSBuild] -> found 0 issues (skipped 0 duplicates) [MSBuild] Successfully parsed console log [MSBuild] -> found 0 issues (skipped 0 duplicates) [MSBuild] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [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] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Commit/7.7/LINUX64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [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=7.7,ESP_ARCH=LINUX64,buildnode=reynolds-centOS7 #7570'. [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