Skipping 1,840 KB..
Full LogEGADS : 88 Yes 111.349293 0 3.80853718
EGADS : 89 Yes 98.7284993 0 0.691329618
EGADS : 90 Yes 98.0587466 0 0
EGADS : 91 Yes 97.6847537 0 0
EGADS : 92 Yes 178.290107 0 12.8669627
EGADS : 93 Yes 186.832635 0 12.8669627
EGADS : 94 Yes 186.332272 0 12.5798928
EGADS : 95 Yes 182.089548 0 12.2721304
EGADS : 96 Yes 166.04434 0 5.74952294
EGADS : 97 Yes 175.677695 0 6.46711426
EGADS : 98 Yes 166.04434 0 7.18470557
EGADS : 99 Yes 182.089548 0 12.8876553
EGADS : 100 Yes 179.185335 0 12.8657508
EGADS : 101 Yes 169.427466 0.726640199 12.8657508
EGADS : 102 Yes 184.850271 0.257175451 37.5422238
EGADS : 103 Yes 188.439012 0 37.5422238
EGADS : 104 Yes 188.681126 0 38.1878596
EGADS : 105 Yes 181.586854 0 38.1878596
EGADS : 106 Yes 166.946942 7.37426242 7.25045332
EGADS : 107 Yes 175.836646 7.55889672 5.90534568
EGADS : 108 Yes 182.40458 35.1488528 12.7578079
EGADS : 109 Yes 186.135993 35.2263522 12.1932049
EGADS : 110 Yes 182.361699 35.1723312 12.1894212
EGADS : 111 Yes 166.844784 7.43019738 5.89633175
EGADS : 112 Yes 99.3800953 41.8796344 2.34192139
EGADS : 113 Yes 104.394138 42.0879216 0.480503378
EGADS : 114 Yes 111.657908 67.3218336 4.77558767
EGADS : 115 Yes 114.968457 67.4483237 3.68923781
EGADS : 116 Yes 112.055908 68.3356022 4.87632098
EGADS : 117 Yes 115.300912 68.4526045 3.81895125
EGADS : 118 Yes 125.330781 95.7095395 7.49106118
EGADS : 119 Yes 126.742253 95.7419985 7.26970731
EGADS : 120 Yes 125.289158 95.7293907 7.22828065
EGADS : 121 Yes 111.907275 68.4064908 3.93793256
EGADS : 122 Yes 111.505559 67.3943173 3.81303994
EGADS : 123 Yes 99.1284577 41.9993571 0.752061491
EGADS : 124 Yes 184.850271 0 37.5422238
EGADS : 125 Yes 169.427466 0 12.8657508
EGADS : 126 Yes 99.3800953 0 2.34192139
EGADS : 127 Yes 104.394138 0 0.480503378
EGADS : 128 Yes 111.657908 0 4.77558767
EGADS : 129 Yes 114.968457 0 3.68923781
EGADS : 130 Yes 111.907885 0 4.87632098
EGADS : 131 Yes 115.321903 0 4.86654259
EGADS : 132 Yes 125.289329 0 7.49106118
EGADS : 133 Yes 126.700876 0 7.71377572
EGADS : 134 Yes 125.33061 0 7.22828065
EGADS : 135 Yes 112.055298 0 3.93793256
EGADS : 136 Yes 111.505559 0 3.81303994
EGADS : 137 Yes 99.1284577 0 0.752061491
EGADS : 138 Yes 186.135993 0 12.1932049
EGADS : 139 Yes 182.361699 0 12.1894212
EGADS : 140 Yes 166.844784 0 5.89633175
EGADS : 141 Yes 175.836646 0 5.90534568
EGADS : 142 Yes 166.946942 0 7.25045332
EGADS : 143 Yes 182.40458 0 12.7578079
EGADS : 144 Yes 170.32959 0.685333031 13.3657508
EGADS : 145 Yes 179.372835 0 13.3657508
EGADS : 146 Yes 185.127395 0.236758105 37.0422238
EGADS : 147 Yes 188.251512 0 37.0422238
EGADS : 148 Yes 185.127395 0 37.0422238
EGADS : 149 Yes 170.32959 0 13.3657508
EGADS : 150 Yes 94.5173952 0 0
EGADS : 151 Yes 94.5173952 0 0
EGADS : 152 Yes 64.5173952 0 0
EGADS : 153 Yes 64.5173952 0 0
EGADS : 154 Yes 94.5173952 29.3018771 0
EGADS : 155 Yes 94.5173952 29.3018771 0
EGADS : 156 Yes 64.5173952 29.3018771 0
EGADS : 157 Yes 64.5173952 29.3018771 0
EGADS : 158 Yes 0 0 1967.5524
EGADS : 159 Yes 0 0 0
EGADS : 160 Yes 0 1953.45847 1967.5524
EGADS : 161 Yes 0 1953.45847 0
EGADS : 162 Yes 2047.79904 0 1967.5524
EGADS : 163 Yes 2047.79904 0 0
EGADS : 164 Yes 2047.79904 1953.45847 1967.5524
EGADS : 165 Yes 2047.79904 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 52.7213
AFLR4 : Reference Length = 43.4102
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.379
AFLR4 : Abs Min Surf Spacing = 0.108525
AFLR4 : Min Surf Spacing = 0.217051
AFLR4 : Max Surf Spacing = 4.34102
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : 23 CAD geometry 0 STD w/BL
AFLR4 : 24 CAD geometry 0 STD w/BL
AFLR4 : 25 CAD geometry 0 STD w/BL
AFLR4 : 26 CAD geometry 0 STD w/BL
AFLR4 : 27 CAD geometry 0 STD w/BL
AFLR4 : 28 CAD geometry 0 STD w/BL
AFLR4 : 29 CAD geometry 0 STD w/BL
AFLR4 : 30 CAD geometry 0 STD w/BL
AFLR4 : 31 CAD geometry 0 STD w/BL
AFLR4 : 32 CAD geometry 0 STD w/BL
AFLR4 : 33 CAD geometry 0 STD w/BL
AFLR4 : 34 CAD geometry 0 STD w/BL
AFLR4 : 35 CAD geometry 0 STD w/BL
AFLR4 : 36 CAD geometry 0 STD w/BL
AFLR4 : 37 CAD geometry 0 STD w/BL
AFLR4 : 38 CAD geometry 0 STD w/BL
AFLR4 : 39 CAD geometry 0 STD w/BL
AFLR4 : 40 CAD geometry 0 STD w/BL
AFLR4 : 41 CAD geometry 0 STD w/BL
AFLR4 : 42 CAD geometry 0 STD w/BL
AFLR4 : 43 CAD geometry 0 STD w/BL
AFLR4 : 44 CAD geometry 0 STD w/BL
AFLR4 : 45 CAD geometry 0 STD w/BL
AFLR4 : 46 CAD geometry 0 STD w/BL
AFLR4 : 47 CAD geometry 0 STD w/BL
AFLR4 : 48 CAD geometry 0 STD w/BL
AFLR4 : 49 CAD geometry 0 STD w/BL
AFLR4 : 50 CAD geometry 0 STD w/BL
AFLR4 : 51 CAD geometry 0 STD w/BL
AFLR4 : 52 CAD geometry 0 STD w/BL
AFLR4 : 53 CAD geometry 0 STD w/BL
AFLR4 : 54 CAD geometry 0 STD w/BL
AFLR4 : 55 CAD geometry 0 STD w/BL
AFLR4 : 56 CAD geometry 0 STD w/BL
AFLR4 : 57 CAD geometry 0 STD w/BL
AFLR4 : 58 CAD geometry 0 STD w/BL
AFLR4 : 59 CAD geometry 0 STD w/BL
AFLR4 : 60 CAD geometry 0 STD w/BL
AFLR4 : 61 CAD geometry 0 STD w/BL
AFLR4 : 62 CAD geometry 0 STD w/BL
AFLR4 : 63 CAD geometry 0 STD w/BL
AFLR4 : 64 CAD geometry 0 STD w/BL
AFLR4 : 65 CAD geometry 0 STD w/BL
AFLR4 : 66 CAD geometry 0 STD w/BL
AFLR4 : 67 CAD geometry 0 STD w/BL
AFLR4 : 68 CAD geometry 0 STD w/BL
AFLR4 : 69 CAD geometry 0 STD w/BL
AFLR4 : 70 CAD geometry 0 STD w/BL
AFLR4 : 71 CAD geometry 0 STD w/BL
AFLR4 : 72 CAD geometry 0 STD w/BL
AFLR4 : 73 CAD geometry 0 STD w/BL
AFLR4 : 74 CAD geometry 0 STD w/BL
AFLR4 : 75 CAD geometry 0 STD w/BL
AFLR4 : 76 CAD geometry 0 STD w/BL
AFLR4 : 77 CAD geometry 0 STD w/BL
AFLR4 : 78 CAD geometry 0 STD w/BL
AFLR4 : 79 CAD geometry 0 STD w/BL
AFLR4 : 80 CAD geometry 0 STD w/BL
AFLR4 : 81 CAD geometry 0 STD w/BL
AFLR4 : 82 CAD geometry 0 STD w/BL
AFLR4 : 83 CAD geometry 0 STD w/BL
AFLR4 : 84 CAD geometry 0 STD w/BL
AFLR4 : 85 CAD geometry 0 STD w/BL
AFLR4 : 86 CAD geometry 0 STD w/BL
AFLR4 : 87 CAD geometry 0 STD w/BL
AFLR4 : 88 CAD geometry 0 STD w/BL
AFLR4 : 89 CAD geometry 0 STD w/BL
AFLR4 : 90 CAD geometry 0 STD w/BL
AFLR4 : 91 CAD geometry 0 STD w/BL
AFLR4 : 92 CAD geometry 0 STD w/BL
AFLR4 : 93 CAD geometry 0 STD w/BL
AFLR4 : 94 CAD geometry 0 STD w/BL
AFLR4 : 95 CAD geometry 0 STD w/BL
AFLR4 : 96 CAD geometry 0 STD w/BL
AFLR4 : 97 CAD geometry 0 STD w/BL
AFLR4 : 98 CAD geometry 0 STD w/BL
AFLR4 : 99 CAD geometry 0 STD w/BL
AFLR4 : 100 CAD geometry 0 STD w/BL
AFLR4 : 101 CAD geometry 0 STD w/BL
AFLR4 : 102 CAD geometry 0 STD w/BL
AFLR4 : 103 CAD geometry 0 STD w/BL
AFLR4 : 104 CAD geometry 0 STD w/BL
AFLR4 : 105 CAD geometry 0 STD w/BL
AFLR4 : 106 CAD geometry 0 STD w/BL
AFLR4 : 107 CAD geometry 0 STD w/BL
AFLR4 : 108 CAD geometry 0 STD w/BL
AFLR4 : 109 CAD geometry 0 FARFIELD
AFLR4 : 110 CAD geometry 0 FARFIELD
AFLR4 : 111 CAD geometry 0 FARFIELD
AFLR4 : 112 CAD geometry 0 FARFIELD
AFLR4 : 113 CAD geometry 0 FARFIELD
AFLR4 : 114 CAD geometry 0 FARFIELD
AFLR4 : Case has 5 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 7 10 11 12 23
AFLR4 : Component 2 includes Definitions 5 6 8 9 15 16 17 18 19 20 21 22 24
AFLR4 : 25 26 27 28 29 30 31 42 43 44 45 46
AFLR4 : 47 48 49 50 51 52 53 54 55 56 58 59
AFLR4 : 60 61 62 63 64 65 66 67 68 69 70 71
AFLR4 : 72 86 87 88 89 93 94 95 96
AFLR4 : Component 3 includes Definitions 13 14 32 33 35 36 37 38 39 40 41 73
AFLR4 : 74 75 76 77 78 79 84 85 97 98
AFLR4 : Component 4 includes Definitions 34 57 80 81 82 83 90 91 92 99 100
AFLR4 : Component 5 includes Definitions 101 102 103 104 105 106 107 108
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
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AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
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AFLR4 : Define CAD surface definition 16
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AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
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AFLR4 : Define CAD surface definition 27
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AFLR4 : Define CAD surface definition 34
AFLR4 : Define CAD surface definition 35
AFLR4 : Define CAD surface definition 36
AFLR4 : Define CAD surface definition 37
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AFLR4 : Define CAD surface definition 39
AFLR4 : Define CAD surface definition 40
AFLR4 : Define CAD surface definition 41
AFLR4 : Define CAD surface definition 42
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AFLR4 : Define CAD surface definition 46
AFLR4 : Define CAD surface definition 47
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AFLR4 : Define CAD surface definition 49
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AFLR4 : Define CAD surface definition 55
AFLR4 : Define CAD surface definition 56
AFLR4 : Define CAD surface definition 57
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AFLR4 : Define CAD surface definition 61
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AFLR4 : Define CAD surface definition 110
AFLR4 : Define CAD surface definition 111
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AFLR4 : Define CAD surface definition 113
AFLR4 : Define CAD surface definition 114
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 539 896 0
AFLR4 : Nodes, Trias,Quads= 595 1008 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 539 896 0
AFLR4 : Nodes, Trias,Quads= 597 1012 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 336 580 0
AFLR4 : Nodes, Trias,Quads= 226 360 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 399 659 0
AFLR4 : Nodes, Trias,Quads= 480 821 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1486 2771 0
AFLR4 : Nodes, Trias,Quads= 1302 2403 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1715 3215 0
AFLR4 : Nodes, Trias,Quads= 1407 2599 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 398 657 0
AFLR4 : Nodes, Trias,Quads= 479 819 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1490 2779 0
AFLR4 : Nodes, Trias,Quads= 1240 2279 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1709 3203 0
AFLR4 : Nodes, Trias,Quads= 1414 2613 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 341 590 0
AFLR4 : Nodes, Trias,Quads= 226 360 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 42 58 0
AFLR4 : Nodes, Trias,Quads= 42 58 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 1171 2161 0
AFLR4 : Nodes, Trias,Quads= 772 1363 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1482 2757 0
AFLR4 : Nodes, Trias,Quads= 949 1691 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1490 2770 0
AFLR4 : Nodes, Trias,Quads= 981 1752 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 37 49 0
AFLR4 : Nodes, Trias,Quads= 39 53 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 97 128 0
AFLR4 : Nodes, Trias,Quads= 85 104 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 37 50 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 3850 7350 0
AFLR4 : Nodes, Trias,Quads= 2376 4402 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 4151 7937 0
AFLR4 : Nodes, Trias,Quads= 2545 4725 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 57 84 0
AFLR4 : Nodes, Trias,Quads= 44 58 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 137 191 0
AFLR4 : Nodes, Trias,Quads= 134 185 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 56 82 0
AFLR4 : Nodes, Trias,Quads= 43 56 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 1252 2323 0
AFLR4 : Nodes, Trias,Quads= 774 1367 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 37 49 0
AFLR4 : Nodes, Trias,Quads= 40 55 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 97 128 0
AFLR4 : Nodes, Trias,Quads= 85 104 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 37 50 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 3833 7312 0
AFLR4 : Nodes, Trias,Quads= 2411 4468 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 3956 7550 0
AFLR4 : Nodes, Trias,Quads= 2508 4654 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 57 84 0
AFLR4 : Nodes, Trias,Quads= 43 56 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 137 191 0
AFLR4 : Nodes, Trias,Quads= 138 193 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 56 82 0
AFLR4 : Nodes, Trias,Quads= 43 56 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 1482 2754 0
AFLR4 : Nodes, Trias,Quads= 972 1734 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 1493 2779 0
AFLR4 : Nodes, Trias,Quads= 953 1699 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 1838 3435 0
AFLR4 : Nodes, Trias,Quads= 1201 2161 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 55 76 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 111 150 0
AFLR4 : Nodes, Trias,Quads= 71 70 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 35 44 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 120 165 0
AFLR4 : Nodes, Trias,Quads= 74 73 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 50 65 0
AFLR4 : Nodes, Trias,Quads= 51 67 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 218 365 0
AFLR4 : Nodes, Trias,Quads= 202 333 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 41 53 0
AFLR4 : Nodes, Trias,Quads= 48 67 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 118 156 0
AFLR4 : Nodes, Trias,Quads= 78 76 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 41 53 0
AFLR4 : Nodes, Trias,Quads= 42 55 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 38 49 0
AFLR4 : Nodes, Trias,Quads= 44 61 0
AFLR4 : Generate optimal mesh on surface definition 47
AFLR2 : Nodes, Trias,Quads= 151 209 0
AFLR4 : Nodes, Trias,Quads= 129 165 0
AFLR4 : Generate optimal mesh on surface definition 48
AFLR2 : Nodes, Trias,Quads= 29 37 0
AFLR4 : Nodes, Trias,Quads= 29 37 0
AFLR4 : Generate optimal mesh on surface definition 49
AFLR2 : Nodes, Trias,Quads= 36 49 0
AFLR4 : Nodes, Trias,Quads= 21 19 0
AFLR4 : Generate optimal mesh on surface definition 50
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 33 43 0
AFLR4 : Generate optimal mesh on surface definition 51
AFLR2 : Nodes, Trias,Quads= 157 216 0
AFLR4 : Nodes, Trias,Quads= 112 126 0
AFLR4 : Generate optimal mesh on surface definition 52
AFLR2 : Nodes, Trias,Quads= 41 53 0
AFLR4 : Nodes, Trias,Quads= 42 55 0
AFLR4 : Generate optimal mesh on surface definition 53
AFLR2 : Nodes, Trias,Quads= 50 67 0
AFLR4 : Nodes, Trias,Quads= 47 61 0
AFLR4 : Generate optimal mesh on surface definition 54
AFLR2 : Nodes, Trias,Quads= 149 204 0
AFLR4 : Nodes, Trias,Quads= 93 92 0
AFLR4 : Generate optimal mesh on surface definition 55
AFLR2 : Nodes, Trias,Quads= 48 64 0
AFLR4 : Nodes, Trias,Quads= 48 64 0
AFLR4 : Generate optimal mesh on surface definition 56
AFLR2 : Nodes, Trias,Quads= 291 497 0
AFLR4 : Nodes, Trias,Quads= 274 463 0
AFLR4 : Generate optimal mesh on surface definition 57
AFLR2 : Nodes, Trias,Quads= 1807 3373 0
AFLR4 : Nodes, Trias,Quads= 1203 2165 0
AFLR4 : Generate optimal mesh on surface definition 58
AFLR2 : Nodes, Trias,Quads= 218 365 0
AFLR4 : Nodes, Trias,Quads= 202 333 0
AFLR4 : Generate optimal mesh on surface definition 59
AFLR2 : Nodes, Trias,Quads= 41 53 0
AFLR4 : Nodes, Trias,Quads= 48 67 0
AFLR4 : Generate optimal mesh on surface definition 60
AFLR2 : Nodes, Trias,Quads= 118 156 0
AFLR4 : Nodes, Trias,Quads= 78 76 0
AFLR4 : Generate optimal mesh on surface definition 61
AFLR2 : Nodes, Trias,Quads= 40 51 0
AFLR4 : Nodes, Trias,Quads= 42 55 0
AFLR4 : Generate optimal mesh on surface definition 62
AFLR2 : Nodes, Trias,Quads= 41 53 0
AFLR4 : Nodes, Trias,Quads= 41 53 0
AFLR4 : Generate optimal mesh on surface definition 63
AFLR2 : Nodes, Trias,Quads= 157 216 0
AFLR4 : Nodes, Trias,Quads= 128 158 0
AFLR4 : Generate optimal mesh on surface definition 64
AFLR2 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Generate optimal mesh on surface definition 65
AFLR2 : Nodes, Trias,Quads= 36 49 0
AFLR4 : Nodes, Trias,Quads= 21 19 0
AFLR4 : Generate optimal mesh on surface definition 66
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 32 42 0
AFLR4 : Generate optimal mesh on surface definition 67
AFLR2 : Nodes, Trias,Quads= 151 209 0
AFLR4 : Nodes, Trias,Quads= 100 107 0
AFLR4 : Generate optimal mesh on surface definition 68
AFLR2 : Nodes, Trias,Quads= 38 49 0
AFLR4 : Nodes, Trias,Quads= 41 55 0
AFLR4 : Generate optimal mesh on surface definition 69
AFLR2 : Nodes, Trias,Quads= 51 69 0
AFLR4 : Nodes, Trias,Quads= 48 63 0
AFLR4 : Generate optimal mesh on surface definition 70
AFLR2 : Nodes, Trias,Quads= 149 204 0
AFLR4 : Nodes, Trias,Quads= 93 92 0
AFLR4 : Generate optimal mesh on surface definition 71
AFLR2 : Nodes, Trias,Quads= 48 64 0
AFLR4 : Nodes, Trias,Quads= 48 64 0
AFLR4 : Generate optimal mesh on surface definition 72
AFLR2 : Nodes, Trias,Quads= 292 499 0
AFLR4 : Nodes, Trias,Quads= 272 459 0
AFLR4 : Generate optimal mesh on surface definition 73
AFLR2 : Nodes, Trias,Quads= 35 44 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 74
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Generate optimal mesh on surface definition 75
AFLR2 : Nodes, Trias,Quads= 120 165 0
AFLR4 : Nodes, Trias,Quads= 74 73 0
AFLR4 : Generate optimal mesh on surface definition 76
AFLR2 : Nodes, Trias,Quads= 50 65 0
AFLR4 : Nodes, Trias,Quads= 50 65 0
AFLR4 : Generate optimal mesh on surface definition 77
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 55 76 0
AFLR4 : Generate optimal mesh on surface definition 78
AFLR2 : Nodes, Trias,Quads= 111 150 0
AFLR4 : Nodes, Trias,Quads= 71 70 0
AFLR4 : Generate optimal mesh on surface definition 79
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Generate optimal mesh on surface definition 80
AFLR2 : Nodes, Trias,Quads= 106 156 0
AFLR4 : Nodes, Trias,Quads= 76 96 0
AFLR4 : Generate optimal mesh on surface definition 81
AFLR2 : Nodes, Trias,Quads= 109 149 0
AFLR4 : Nodes, Trias,Quads= 68 67 0
AFLR4 : Generate optimal mesh on surface definition 82
AFLR2 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Generate optimal mesh on surface definition 83
AFLR2 : Nodes, Trias,Quads= 38 48 0
AFLR4 : Nodes, Trias,Quads= 26 24 0
AFLR4 : Generate optimal mesh on surface definition 84
AFLR2 : Nodes, Trias,Quads= 309 534 0
AFLR4 : Nodes, Trias,Quads= 243 402 0
AFLR4 : Generate optimal mesh on surface definition 85
AFLR2 : Nodes, Trias,Quads= 318 550 0
AFLR4 : Nodes, Trias,Quads= 253 420 0
AFLR4 : Generate optimal mesh on surface definition 86
AFLR2 : Nodes, Trias,Quads= 319 545 0
AFLR4 : Nodes, Trias,Quads= 266 439 0
AFLR4 : Generate optimal mesh on surface definition 87
AFLR2 : Nodes, Trias,Quads= 305 507 0
AFLR4 : Nodes, Trias,Quads= 229 355 0
AFLR4 : Generate optimal mesh on surface definition 88
AFLR2 : Nodes, Trias,Quads= 337 566 0
AFLR4 : Nodes, Trias,Quads= 244 380 0
AFLR4 : Generate optimal mesh on surface definition 89
AFLR2 : Nodes, Trias,Quads= 382 660 0
AFLR4 : Nodes, Trias,Quads= 318 532 0
AFLR4 : Generate optimal mesh on surface definition 90
AFLR2 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Nodes, Trias,Quads= 27 34 0
AFLR4 : Generate optimal mesh on surface definition 91
AFLR2 : Nodes, Trias,Quads= 109 149 0
AFLR4 : Nodes, Trias,Quads= 68 67 0
AFLR4 : Generate optimal mesh on surface definition 92
AFLR2 : Nodes, Trias,Quads= 106 156 0
AFLR4 : Nodes, Trias,Quads= 70 84 0
AFLR4 : Generate optimal mesh on surface definition 93
AFLR2 : Nodes, Trias,Quads= 318 543 0
AFLR4 : Nodes, Trias,Quads= 267 441 0
AFLR4 : Generate optimal mesh on surface definition 94
AFLR2 : Nodes, Trias,Quads= 332 556 0
AFLR4 : Nodes, Trias,Quads= 251 394 0
AFLR4 : Generate optimal mesh on surface definition 95
AFLR2 : Nodes, Trias,Quads= 304 505 0
AFLR4 : Nodes, Trias,Quads= 230 357 0
AFLR4 : Generate optimal mesh on surface definition 96
AFLR2 : Nodes, Trias,Quads= 383 662 0
AFLR4 : Nodes, Trias,Quads= 318 532 0
AFLR4 : Generate optimal mesh on surface definition 97
AFLR2 : Nodes, Trias,Quads= 322 558 0
AFLR4 : Nodes, Trias,Quads= 251 416 0
AFLR4 : Generate optimal mesh on surface definition 98
AFLR2 : Nodes, Trias,Quads= 306 528 0
AFLR4 : Nodes, Trias,Quads= 243 402 0
AFLR4 : Generate optimal mesh on surface definition 99
AFLR2 : Nodes, Trias,Quads= 400 707 0
AFLR4 : Nodes, Trias,Quads= 309 525 0
AFLR4 : Generate optimal mesh on surface definition 100
AFLR2 : Nodes, Trias,Quads= 397 701 0
AFLR4 : Nodes, Trias,Quads= 307 521 0
AFLR4 : Generate optimal mesh on surface definition 101
AFLR2 : Nodes, Trias,Quads= 1258 2364 0
AFLR4 : Nodes, Trias,Quads= 1204 2256 0
AFLR4 : Generate optimal mesh on surface definition 102
AFLR2 : Nodes, Trias,Quads= 1440 2712 0
AFLR4 : Nodes, Trias,Quads= 1227 2286 0
AFLR4 : Generate optimal mesh on surface definition 103
AFLR2 : Nodes, Trias,Quads= 1252 2352 0
AFLR4 : Nodes, Trias,Quads= 1235 2318 0
AFLR4 : Generate optimal mesh on surface definition 104
AFLR2 : Nodes, Trias,Quads= 1425 2682 0
AFLR4 : Nodes, Trias,Quads= 1209 2250 0
AFLR4 : Generate optimal mesh on surface definition 105
AFLR2 : Nodes, Trias,Quads= 1252 2352 0
AFLR4 : Nodes, Trias,Quads= 1235 2318 0
AFLR4 : Generate optimal mesh on surface definition 106
AFLR2 : Nodes, Trias,Quads= 1425 2682 0
AFLR4 : Nodes, Trias,Quads= 1209 2250 0
AFLR4 : Generate optimal mesh on surface definition 107
AFLR2 : Nodes, Trias,Quads= 1258 2364 0
AFLR4 : Nodes, Trias,Quads= 1204 2256 0
AFLR4 : Generate optimal mesh on surface definition 108
AFLR2 : Nodes, Trias,Quads= 1440 2712 0
AFLR4 : Nodes, Trias,Quads= 1227 2286 0
AFLR4 : Generate optimal mesh on surface definition 109
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 110
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 111
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 112
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 113
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 114
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 38549 77090 10310
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 38549 77090
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 571 952 0
AFLR4 : Nodes, Trias,Quads= 1069 1948 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 566 943 0
AFLR4 : Nodes, Trias,Quads= 1072 1955 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 378 658 0
AFLR4 : Nodes, Trias,Quads= 404 710 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 441 735 0
AFLR4 : Nodes, Trias,Quads= 714 1281 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1554 2902 0
AFLR4 : Nodes, Trias,Quads= 1546 2886 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1802 3381 0
AFLR4 : Nodes, Trias,Quads= 1819 3415 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 432 718 0
AFLR4 : Nodes, Trias,Quads= 709 1272 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1555 2904 0
AFLR4 : Nodes, Trias,Quads= 1517 2828 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1836 3447 0
AFLR4 : Nodes, Trias,Quads= 1839 3453 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 383 668 0
AFLR4 : Nodes, Trias,Quads= 405 712 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 46 66 0
AFLR4 : Nodes, Trias,Quads= 42 58 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 1202 2219 0
AFLR4 : Nodes, Trias,Quads= 1064 1943 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1620 3027 0
AFLR4 : Nodes, Trias,Quads= 1129 2045 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1598 2980 0
AFLR4 : Nodes, Trias,Quads= 1140 2064 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 48 68 0
AFLR4 : Nodes, Trias,Quads= 43 58 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 110 149 0
AFLR4 : Nodes, Trias,Quads= 111 151 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 41 56 0
AFLR4 : Nodes, Trias,Quads= 40 54 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 4338 8304 0
AFLR4 : Nodes, Trias,Quads= 2672 4972 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 4716 9046 0
AFLR4 : Nodes, Trias,Quads= 2861 5336 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 64 96 0
AFLR4 : Nodes, Trias,Quads= 45 58 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 152 207 0
AFLR4 : Nodes, Trias,Quads= 151 205 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 57 84 0
AFLR4 : Nodes, Trias,Quads= 44 58 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 1295 2404 0
AFLR4 : Nodes, Trias,Quads= 1047 1908 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 50 71 0
AFLR4 : Nodes, Trias,Quads= 46 63 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 105 139 0
AFLR4 : Nodes, Trias,Quads= 112 153 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 41 56 0
AFLR4 : Nodes, Trias,Quads= 41 56 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 4337 8300 0
AFLR4 : Nodes, Trias,Quads= 2720 5066 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 4465 8550 0
AFLR4 : Nodes, Trias,Quads= 2798 5216 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 62 93 0
AFLR4 : Nodes, Trias,Quads= 43 55 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 155 212 0
AFLR4 : Nodes, Trias,Quads= 150 202 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 61 90 0
AFLR4 : Nodes, Trias,Quads= 45 58 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 1620 3023 0
AFLR4 : Nodes, Trias,Quads= 1131 2045 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 1611 3009 0
AFLR4 : Nodes, Trias,Quads= 1124 2035 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 1949 3650 0
AFLR4 : Nodes, Trias,Quads= 1320 2392 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 54 70 0
AFLR4 : Nodes, Trias,Quads= 62 86 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 120 163 0
AFLR4 : Nodes, Trias,Quads= 76 75 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 39 50 0
AFLR4 : Nodes, Trias,Quads= 26 24 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 127 173 0
AFLR4 : Nodes, Trias,Quads= 80 79 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 54 71 0
AFLR4 : Nodes, Trias,Quads= 53 69 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 267 455 0
AFLR4 : Nodes, Trias,Quads= 240 401 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 47 61 0
AFLR4 : Nodes, Trias,Quads= 54 75 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 133 182 0
AFLR4 : Nodes, Trias,Quads= 82 80 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 43 55 0
AFLR4 : Nodes, Trias,Quads= 45 59 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 48 64 0
AFLR4 : Nodes, Trias,Quads= 50 68 0
AFLR4 : Generate optimal mesh on surface definition 47
AFLR2 : Nodes, Trias,Quads= 174 240 0
AFLR4 : Nodes, Trias,Quads= 159 210 0
AFLR4 : Generate optimal mesh on surface definition 48
AFLR2 : Nodes, Trias,Quads= 29 37 0
AFLR4 : Nodes, Trias,Quads= 29 37 0
AFLR4 : Generate optimal mesh on surface definition 49
AFLR2 : Nodes, Trias,Quads= 37 48 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 50
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Generate optimal mesh on surface definition 51
AFLR2 : Nodes, Trias,Quads= 189 267 0
AFLR4 : Nodes, Trias,Quads= 130 149 0
AFLR4 : Generate optimal mesh on surface definition 52
AFLR2 : Nodes, Trias,Quads= 43 55 0
AFLR4 : Nodes, Trias,Quads= 44 57 0
AFLR4 : Generate optimal mesh on surface definition 53
AFLR2 : Nodes, Trias,Quads= 52 71 0
AFLR4 : Nodes, Trias,Quads= 47 61 0
AFLR4 : Generate optimal mesh on surface definition 54
AFLR2 : Nodes, Trias,Quads= 167 232 0
AFLR4 : Nodes, Trias,Quads= 101 100 0
AFLR4 : Generate optimal mesh on surface definition 55
AFLR2 : Nodes, Trias,Quads= 57 79 0
AFLR4 : Nodes, Trias,Quads= 51 67 0
AFLR4 : Generate optimal mesh on surface definition 56
AFLR2 : Nodes, Trias,Quads= 358 621 0
AFLR4 : Nodes, Trias,Quads= 346 597 0
AFLR4 : Generate optimal mesh on surface definition 57
AFLR2 : Nodes, Trias,Quads= 1868 3489 0
AFLR4 : Nodes, Trias,Quads= 1322 2397 0
AFLR4 : Generate optimal mesh on surface definition 58
AFLR2 : Nodes, Trias,Quads= 266 453 0
AFLR4 : Nodes, Trias,Quads= 240 401 0
AFLR4 : Generate optimal mesh on surface definition 59
AFLR2 : Nodes, Trias,Quads= 47 61 0
AFLR4 : Nodes, Trias,Quads= 54 75 0
AFLR4 : Generate optimal mesh on surface definition 60
AFLR2 : Nodes, Trias,Quads= 134 184 0
AFLR4 : Nodes, Trias,Quads= 82 80 0
AFLR4 : Generate optimal mesh on surface definition 61
AFLR2 : Nodes, Trias,Quads= 43 55 0
AFLR4 : Nodes, Trias,Quads= 46 61 0
AFLR4 : Generate optimal mesh on surface definition 62
AFLR2 : Nodes, Trias,Quads= 43 55 0
AFLR4 : Nodes, Trias,Quads= 45 59 0
AFLR4 : Generate optimal mesh on surface definition 63
AFLR2 : Nodes, Trias,Quads= 195 275 0
AFLR4 : Nodes, Trias,Quads= 177 239 0
AFLR4 : Generate optimal mesh on surface definition 64
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Generate optimal mesh on surface definition 65
AFLR2 : Nodes, Trias,Quads= 37 48 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 66
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 29 36 0
AFLR4 : Generate optimal mesh on surface definition 67
AFLR2 : Nodes, Trias,Quads= 169 235 0
AFLR4 : Nodes, Trias,Quads= 132 161 0
AFLR4 : Generate optimal mesh on surface definition 68
AFLR2 : Nodes, Trias,Quads= 42 54 0
AFLR4 : Nodes, Trias,Quads= 46 62 0
AFLR4 : Generate optimal mesh on surface definition 69
AFLR2 : Nodes, Trias,Quads= 54 74 0
AFLR4 : Nodes, Trias,Quads= 48 62 0
AFLR4 : Generate optimal mesh on surface definition 70
AFLR2 : Nodes, Trias,Quads= 167 232 0
AFLR4 : Nodes, Trias,Quads= 101 100 0
AFLR4 : Generate optimal mesh on surface definition 71
AFLR2 : Nodes, Trias,Quads= 57 79 0
AFLR4 : Nodes, Trias,Quads= 51 67 0
AFLR4 : Generate optimal mesh on surface definition 72
AFLR2 : Nodes, Trias,Quads= 345 596 0
AFLR4 : Nodes, Trias,Quads= 345 596 0
AFLR4 : Generate optimal mesh on surface definition 73
AFLR2 : Nodes, Trias,Quads= 39 50 0
AFLR4 : Nodes, Trias,Quads= 26 24 0
AFLR4 : Generate optimal mesh on surface definition 74
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Generate optimal mesh on surface definition 75
AFLR2 : Nodes, Trias,Quads= 124 168 0
AFLR4 : Nodes, Trias,Quads= 79 78 0
AFLR4 : Generate optimal mesh on surface definition 76
AFLR2 : Nodes, Trias,Quads= 54 71 0
AFLR4 : Nodes, Trias,Quads= 54 71 0
AFLR4 : Generate optimal mesh on surface definition 77
AFLR2 : Nodes, Trias,Quads= 54 70 0
AFLR4 : Nodes, Trias,Quads= 62 86 0
AFLR4 : Generate optimal mesh on surface definition 78
AFLR2 : Nodes, Trias,Quads= 121 165 0
AFLR4 : Nodes, Trias,Quads= 76 75 0
AFLR4 : Generate optimal mesh on surface definition 79
AFLR2 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Generate optimal mesh on surface definition 80
AFLR2 : Nodes, Trias,Quads= 110 163 0
AFLR4 : Nodes, Trias,Quads= 78 99 0
AFLR4 : Generate optimal mesh on surface definition 81
AFLR2 : Nodes, Trias,Quads= 112 150 0
AFLR4 : Nodes, Trias,Quads= 73 72 0
AFLR4 : Generate optimal mesh on surface definition 82
AFLR2 : Nodes, Trias,Quads= 30 39 0
AFLR4 : Nodes, Trias,Quads= 29 37 0
AFLR4 : Generate optimal mesh on surface definition 83
AFLR2 : Nodes, Trias,Quads= 48 65 0
AFLR4 : Nodes, Trias,Quads= 29 27 0
AFLR4 : Generate optimal mesh on surface definition 84
AFLR2 : Nodes, Trias,Quads= 346 603 0
AFLR4 : Nodes, Trias,Quads= 282 475 0
AFLR4 : Generate optimal mesh on surface definition 85
AFLR2 : Nodes, Trias,Quads= 358 625 0
AFLR4 : Nodes, Trias,Quads= 295 499 0
AFLR4 : Generate optimal mesh on surface definition 86
AFLR2 : Nodes, Trias,Quads= 349 600 0
AFLR4 : Nodes, Trias,Quads= 295 492 0
AFLR4 : Generate optimal mesh on surface definition 87
AFLR2 : Nodes, Trias,Quads= 348 584 0
AFLR4 : Nodes, Trias,Quads= 261 410 0
AFLR4 : Generate optimal mesh on surface definition 88
AFLR2 : Nodes, Trias,Quads= 368 621 0
AFLR4 : Nodes, Trias,Quads= 277 439 0
AFLR4 : Generate optimal mesh on surface definition 89
AFLR2 : Nodes, Trias,Quads= 411 714 0
AFLR4 : Nodes, Trias,Quads= 358 608 0
AFLR4 : Generate optimal mesh on surface definition 90
AFLR2 : Nodes, Trias,Quads= 30 39 0
AFLR4 : Nodes, Trias,Quads= 28 35 0
AFLR4 : Generate optimal mesh on surface definition 91
AFLR2 : Nodes, Trias,Quads= 111 148 0
AFLR4 : Nodes, Trias,Quads= 73 72 0
AFLR4 : Generate optimal mesh on surface definition 92
AFLR2 : Nodes, Trias,Quads= 102 150 0
AFLR4 : Nodes, Trias,Quads= 79 104 0
AFLR4 : Generate optimal mesh on surface definition 93
AFLR2 : Nodes, Trias,Quads= 349 600 0
AFLR4 : Nodes, Trias,Quads= 295 492 0
AFLR4 : Generate optimal mesh on surface definition 94
AFLR2 : Nodes, Trias,Quads= 379 641 0
AFLR4 : Nodes, Trias,Quads= 290 463 0
AFLR4 : Generate optimal mesh on surface definition 95
AFLR2 : Nodes, Trias,Quads= 330 551 0
AFLR4 : Nodes, Trias,Quads= 250 391 0
AFLR4 : Generate optimal mesh on surface definition 96
AFLR2 : Nodes, Trias,Quads= 419 729 0
AFLR4 : Nodes, Trias,Quads= 364 619 0
AFLR4 : Generate optimal mesh on surface definition 97
AFLR2 : Nodes, Trias,Quads= 351 612 0
AFLR4 : Nodes, Trias,Quads= 292 494 0
AFLR4 : Generate optimal mesh on surface definition 98
AFLR2 : Nodes, Trias,Quads= 351 612 0
AFLR4 : Nodes, Trias,Quads= 285 480 0
AFLR4 : Generate optimal mesh on surface definition 99
AFLR2 : Nodes, Trias,Quads= 428 759 0
AFLR4 : Nodes, Trias,Quads= 365 633 0
AFLR4 : Generate optimal mesh on surface definition 100
AFLR2 : Nodes, Trias,Quads= 421 746 0
AFLR4 : Nodes, Trias,Quads= 358 620 0
AFLR4 : Generate optimal mesh on surface definition 101
AFLR2 : Nodes, Trias,Quads= 1261 2368 0
AFLR4 : Nodes, Trias,Quads= 1271 2388 0
AFLR4 : Generate optimal mesh on surface definition 102
AFLR2 : Nodes, Trias,Quads= 1462 2754 0
AFLR4 : Nodes, Trias,Quads= 1283 2396 0
AFLR4 : Generate optimal mesh on surface definition 103
AFLR2 : Nodes, Trias,Quads= 1251 2348 0
AFLR4 : Nodes, Trias,Quads= 1307 2460 0
AFLR4 : Generate optimal mesh on surface definition 104
AFLR2 : Nodes, Trias,Quads= 1444 2718 0
AFLR4 : Nodes, Trias,Quads= 1284 2398 0
AFLR4 : Generate optimal mesh on surface definition 105
AFLR2 : Nodes, Trias,Quads= 1251 2348 0
AFLR4 : Nodes, Trias,Quads= 1307 2460 0
AFLR4 : Generate optimal mesh on surface definition 106
AFLR2 : Nodes, Trias,Quads= 1444 2718 0
AFLR4 : Nodes, Trias,Quads= 1284 2398 0
AFLR4 : Generate optimal mesh on surface definition 107
AFLR2 : Nodes, Trias,Quads= 1261 2368 0
AFLR4 : Nodes, Trias,Quads= 1271 2388 0
AFLR4 : Generate optimal mesh on surface definition 108
AFLR2 : Nodes, Trias,Quads= 1462 2754 0
AFLR4 : Nodes, Trias,Quads= 1283 2396 0
AFLR4 : Generate optimal mesh on surface definition 109
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 110
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 111
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 112
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 113
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 114
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 45757 91506 10862
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 46599 93190
AFLR4 : Nodes, Trias = 46796 93584
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1125 1953 0
AFLR4 : Nodes, Trias,Quads= 1721 3145 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1144 1991 0
AFLR4 : Nodes, Trias,Quads= 1721 3145 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 840 1529 0
AFLR4 : Nodes, Trias,Quads= 623 1095 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 978 1745 0
AFLR4 : Nodes, Trias,Quads= 1213 2215 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 2585 4899 0
AFLR4 : Nodes, Trias,Quads= 2072 3873 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 2387 4519 0
AFLR4 : Nodes, Trias,Quads= 2079 3903 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 969 1728 0
AFLR4 : Nodes, Trias,Quads= 1202 2194 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 2599 4926 0
AFLR4 : Nodes, Trias,Quads= 2075 3878 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 2370 4482 0
AFLR4 : Nodes, Trias,Quads= 2124 3990 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 896 1638 0
AFLR4 : Nodes, Trias,Quads= 653 1152 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 47 68 0
AFLR4 : Nodes, Trias,Quads= 42 58 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 1882 3501 0
AFLR4 : Nodes, Trias,Quads= 1684 3105 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1996 3734 0
AFLR4 : Nodes, Trias,Quads= 1475 2692 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 2072 3880 0
AFLR4 : Nodes, Trias,Quads= 1500 2736 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 54 78 0
AFLR4 : Nodes, Trias,Quads= 44 58 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 118 157 0
AFLR4 : Nodes, Trias,Quads= 111 143 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 51 73 0
AFLR4 : Nodes, Trias,Quads= 44 59 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 4837 9280 0
AFLR4 : Nodes, Trias,Quads= 2870 5346 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 5272 10138 0
AFLR4 : Nodes, Trias,Quads= 3059 5712 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 68 103 0
AFLR4 : Nodes, Trias,Quads= 47 61 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 167 224 0
AFLR4 : Nodes, Trias,Quads= 167 224 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 63 94 0
AFLR4 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 2230 4197 0
AFLR4 : Nodes, Trias,Quads= 1675 3087 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 58 85 0
AFLR4 : Nodes, Trias,Quads= 49 67 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 118 157 0
AFLR4 : Nodes, Trias,Quads= 111 143 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 50 71 0
AFLR4 : Nodes, Trias,Quads= 45 61 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 4951 9503 0
AFLR4 : Nodes, Trias,Quads= 2949 5499 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 5002 9604 0
AFLR4 : Nodes, Trias,Quads= 2993 5586 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 63 94 0
AFLR4 : Nodes, Trias,Quads= 44 56 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 169 228 0
AFLR4 : Nodes, Trias,Quads= 173 236 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 72 110 0
AFLR4 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 2100 3936 0
AFLR4 : Nodes, Trias,Quads= 1487 2710 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 2030 3802 0
AFLR4 : Nodes, Trias,Quads= 1465 2672 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 2162 4053 0
AFLR4 : Nodes, Trias,Quads= 1460 2649 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 60 78 0
AFLR4 : Nodes, Trias,Quads= 61 80 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 123 163 0
AFLR4 : Nodes, Trias,Quads= 81 79 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 43 56 0
AFLR4 : Nodes, Trias,Quads= 28 26 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 35 45 0
AFLR4 : Nodes, Trias,Quads= 35 45 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 130 173 0
AFLR4 : Nodes, Trias,Quads= 85 83 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 56 73 0
AFLR4 : Nodes, Trias,Quads= 56 73 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 319 551 0
AFLR4 : Nodes, Trias,Quads= 285 483 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 60 83 0
AFLR4 : Nodes, Trias,Quads= 61 85 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 142 196 0
AFLR4 : Nodes, Trias,Quads= 86 84 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Nodes, Trias,Quads= 45 58 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 56 77 0
AFLR4 : Nodes, Trias,Quads= 50 65 0
AFLR4 : Generate optimal mesh on surface definition 47
AFLR2 : Nodes, Trias,Quads= 196 267 0
AFLR4 : Nodes, Trias,Quads= 193 261 0
AFLR4 : Generate optimal mesh on surface definition 48
AFLR2 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Generate optimal mesh on surface definition 49
AFLR2 : Nodes, Trias,Quads= 44 59 0
AFLR4 : Nodes, Trias,Quads= 27 25 0
AFLR4 : Generate optimal mesh on surface definition 50
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Generate optimal mesh on surface definition 51
AFLR2 : Nodes, Trias,Quads= 206 287 0
AFLR4 : Nodes, Trias,Quads= 147 169 0
AFLR4 : Generate optimal mesh on surface definition 52
AFLR2 : Nodes, Trias,Quads= 51 69 0
AFLR4 : Nodes, Trias,Quads= 47 61 0
AFLR4 : Generate optimal mesh on surface definition 53
AFLR2 : Nodes, Trias,Quads= 57 79 0
AFLR4 : Nodes, Trias,Quads= 50 65 0
AFLR4 : Generate optimal mesh on surface definition 54
AFLR2 : Nodes, Trias,Quads= 171 233 0
AFLR4 : Nodes, Trias,Quads= 107 105 0
AFLR4 : Generate optimal mesh on surface definition 55
AFLR2 : Nodes, Trias,Quads= 63 89 0
AFLR4 : Nodes, Trias,Quads= 53 69 0
AFLR4 : Generate optimal mesh on surface definition 56
AFLR2 : Nodes, Trias,Quads= 429 754 0
AFLR4 : Nodes, Trias,Quads= 409 714 0
AFLR4 : Generate optimal mesh on surface definition 57
AFLR2 : Nodes, Trias,Quads= 2122 3973 0
AFLR4 : Nodes, Trias,Quads= 1457 2643 0
AFLR4 : Generate optimal mesh on surface definition 58
AFLR2 : Nodes, Trias,Quads= 321 555 0
AFLR4 : Nodes, Trias,Quads= 287 487 0
AFLR4 : Generate optimal mesh on surface definition 59
AFLR2 : Nodes, Trias,Quads= 60 83 0
AFLR4 : Nodes, Trias,Quads= 61 85 0
AFLR4 : Generate optimal mesh on surface definition 60
AFLR2 : Nodes, Trias,Quads= 141 194 0
AFLR4 : Nodes, Trias,Quads= 86 84 0
AFLR4 : Generate optimal mesh on surface definition 61
AFLR2 : Nodes, Trias,Quads= 51 69 0
AFLR4 : Nodes, Trias,Quads= 47 61 0
AFLR4 : Generate optimal mesh on surface definition 62
AFLR2 : Nodes, Trias,Quads= 47 61 0
AFLR4 : Nodes, Trias,Quads= 50 67 0
AFLR4 : Generate optimal mesh on surface definition 63
AFLR2 : Nodes, Trias,Quads= 221 306 0
AFLR4 : Nodes, Trias,Quads= 235 334 0
AFLR4 : Generate optimal mesh on surface definition 64
AFLR2 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Generate optimal mesh on surface definition 65
AFLR2 : Nodes, Trias,Quads= 44 59 0
AFLR4 : Nodes, Trias,Quads= 27 25 0
AFLR4 : Generate optimal mesh on surface definition 66
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 29 36 0
AFLR4 : Generate optimal mesh on surface definition 67
AFLR2 : Nodes, Trias,Quads= 183 249 0
AFLR4 : Nodes, Trias,Quads= 148 179 0
AFLR4 : Generate optimal mesh on surface definition 68
AFLR2 : Nodes, Trias,Quads= 48 64 0
AFLR4 : Nodes, Trias,Quads= 45 58 0
AFLR4 : Generate optimal mesh on surface definition 69
AFLR2 : Nodes, Trias,Quads= 52 70 0
AFLR4 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Generate optimal mesh on surface definition 70
AFLR2 : Nodes, Trias,Quads= 170 231 0
AFLR4 : Nodes, Trias,Quads= 107 105 0
AFLR4 : Generate optimal mesh on surface definition 71
AFLR2 : Nodes, Trias,Quads= 63 89 0
AFLR4 : Nodes, Trias,Quads= 53 69 0
AFLR4 : Generate optimal mesh on surface definition 72
AFLR2 : Nodes, Trias,Quads= 415 727 0
AFLR4 : Nodes, Trias,Quads= 397 691 0
AFLR4 : Generate optimal mesh on surface definition 73
AFLR2 : Nodes, Trias,Quads= 42 54 0
AFLR4 : Nodes, Trias,Quads= 28 26 0
AFLR4 : Generate optimal mesh on surface definition 74
AFLR2 : Nodes, Trias,Quads= 35 45 0
AFLR4 : Nodes, Trias,Quads= 35 45 0
AFLR4 : Generate optimal mesh on surface definition 75
AFLR2 : Nodes, Trias,Quads= 130 173 0
AFLR4 : Nodes, Trias,Quads= 85 83 0
AFLR4 : Generate optimal mesh on surface definition 76
AFLR2 : Nodes, Trias,Quads= 57 75 0
AFLR4 : Nodes, Trias,Quads= 56 73 0
AFLR4 : Generate optimal mesh on surface definition 77
AFLR2 : Nodes, Trias,Quads= 60 78 0
AFLR4 : Nodes, Trias,Quads= 61 80 0
AFLR4 : Generate optimal mesh on surface definition 78
AFLR2 : Nodes, Trias,Quads= 123 163 0
AFLR4 : Nodes, Trias,Quads= 81 79 0
AFLR4 : Generate optimal mesh on surface definition 79
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 33 43 0
AFLR4 : Generate optimal mesh on surface definition 80
AFLR2 : Nodes, Trias,Quads= 108 159 0
AFLR4 : Nodes, Trias,Quads= 84 111 0
AFLR4 : Generate optimal mesh on surface definition 81
AFLR2 : Nodes, Trias,Quads= 118 157 0
AFLR4 : Nodes, Trias,Quads= 77 75 0
AFLR4 : Generate optimal mesh on surface definition 82
AFLR2 : Nodes, Trias,Quads= 34 45 0
AFLR4 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Generate optimal mesh on surface definition 83
AFLR2 : Nodes, Trias,Quads= 50 66 0
AFLR4 : Nodes, Trias,Quads= 32 30 0
AFLR4 : Generate optimal mesh on surface definition 84
AFLR2 : Nodes, Trias,Quads= 407 718 0
AFLR4 : Nodes, Trias,Quads= 317 538 0
AFLR4 : Generate optimal mesh on surface definition 85
AFLR2 : Nodes, Trias,Quads= 414 731 0
AFLR4 : Nodes, Trias,Quads= 322 547 0
AFLR4 : Generate optimal mesh on surface definition 86
AFLR2 : Nodes, Trias,Quads= 381 659 0
AFLR4 : Nodes, Trias,Quads= 322 541 0
AFLR4 : Generate optimal mesh on surface definition 87
AFLR2 : Nodes, Trias,Quads= 414 706 0
AFLR4 : Nodes, Trias,Quads= 301 480 0
AFLR4 : Generate optimal mesh on surface definition 88
AFLR2 : Nodes, Trias,Quads= 423 723 0
AFLR4 : Nodes, Trias,Quads= 311 499 0
AFLR4 : Generate optimal mesh on surface definition 89
AFLR2 : Nodes, Trias,Quads= 464 814 0
AFLR4 : Nodes, Trias,Quads= 390 666 0
AFLR4 : Generate optimal mesh on surface definition 90
AFLR2 : Nodes, Trias,Quads= 33 43 0
AFLR4 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Generate optimal mesh on surface definition 91
AFLR2 : Nodes, Trias,Quads= 119 159 0
AFLR4 : Nodes, Trias,Quads= 77 75 0
AFLR4 : Generate optimal mesh on surface definition 92
AFLR2 : Nodes, Trias,Quads= 108 159 0
AFLR4 : Nodes, Trias,Quads= 77 97 0
AFLR4 : Generate optimal mesh on surface definition 93
AFLR2 : Nodes, Trias,Quads= 390 676 0
AFLR4 : Nodes, Trias,Quads= 329 554 0
AFLR4 : Generate optimal mesh on surface definition 94
AFLR2 : Nodes, Trias,Quads= 455 782 0
AFLR4 : Nodes, Trias,Quads= 337 546 0
AFLR4 : Generate optimal mesh on surface definition 95
AFLR2 : Nodes, Trias,Quads= 371 625 0
AFLR4 : Nodes, Trias,Quads= 274 431 0
AFLR4 : Generate optimal mesh on surface definition 96
AFLR2 : Nodes, Trias,Quads= 464 814 0
AFLR4 : Nodes, Trias,Quads= 391 668 0
AFLR4 : Generate optimal mesh on surface definition 97
AFLR2 : Nodes, Trias,Quads= 409 721 0
AFLR4 : Nodes, Trias,Quads= 320 543 0
AFLR4 : Generate optimal mesh on surface definition 98
AFLR2 : Nodes, Trias,Quads= 401 706 0
AFLR4 : Nodes, Trias,Quads= 316 536 0
AFLR4 : Generate optimal mesh on surface definition 99
AFLR2 : Nodes, Trias,Quads= 470 839 0
AFLR4 : Nodes, Trias,Quads= 392 683 0
AFLR4 : Generate optimal mesh on surface definition 100
AFLR2 : Nodes, Trias,Quads= 471 841 0
AFLR4 : Nodes, Trias,Quads= 388 675 0
AFLR4 : Generate optimal mesh on surface definition 101
AFLR2 : Nodes, Trias,Quads= 1611 3054 0
AFLR4 : Nodes, Trias,Quads= 1405 2642 0
AFLR4 : Generate optimal mesh on surface definition 102
AFLR2 : Nodes, Trias,Quads= 1501 2830 0
AFLR4 : Nodes, Trias,Quads= 1330 2488 0
AFLR4 : Generate optimal mesh on surface definition 103
AFLR2 : Nodes, Trias,Quads= 1614 3060 0
AFLR4 : Nodes, Trias,Quads= 1487 2806 0
AFLR4 : Generate optimal mesh on surface definition 104
AFLR2 : Nodes, Trias,Quads= 1475 2778 0
AFLR4 : Nodes, Trias,Quads= 1329 2486 0
AFLR4 : Generate optimal mesh on surface definition 105
AFLR2 : Nodes, Trias,Quads= 1609 3050 0
AFLR4 : Nodes, Trias,Quads= 1438 2708 0
AFLR4 : Generate optimal mesh on surface definition 106
AFLR2 : Nodes, Trias,Quads= 1475 2778 0
AFLR4 : Nodes, Trias,Quads= 1329 2486 0
AFLR4 : Generate optimal mesh on surface definition 107
AFLR2 : Nodes, Trias,Quads= 1601 3034 0
AFLR4 : Nodes, Trias,Quads= 1454 2740 0
AFLR4 : Generate optimal mesh on surface definition 108
AFLR2 : Nodes, Trias,Quads= 1501 2830 0
AFLR4 : Nodes, Trias,Quads= 1330 2488 0
AFLR4 : Generate optimal mesh on surface definition 109
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 110
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 111
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 112
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 113
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 114
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 54873 109738 12420
OVERALL : CPU Time = 8.948 seconds
Body 1 (of 4)
Number of nodes = 44131
Number of elements = 88258
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 88258
Number of quadrilateral elements = 0
Body 2 (of 4)
Number of nodes = 5211
Number of elements = 10422
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 10422
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 5211
Number of elements = 10422
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 10422
Number of quadrilateral elements = 0
Body 4 (of 4)
Number of nodes = 320
Number of elements = 636
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 54873
Total number of elements = 109738
1 file(s) copied.
--> Toal Elements 109738
real 0m20.722s
user 0m0.000s
sys 0m0.139s
+ status=0
+ set +x
=================================================
solutions/session06/aflr4_InviscidTransport_150k.py passed (as expected)
=================================================
=================================================
tess_1_Geom.py test;
+ python tess_1_Geom.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
1 file(s) copied.
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
1 file(s) copied.
real 0m15.544s
user 0m0.046s
sys 0m0.076s
+ status=0
+ set +x
=================================================
data/session09/tess_1_Geom.py passed (as expected)
=================================================
=================================================
tess_2_TFI_Templates.py test;
+ python tess_2_TFI_Templates.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 11081
Number of elements = 22785
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 22785
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 11081
Total number of elements = 22785
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 11910
Number of elements = 24443
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 24443
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 11910
Total number of elements = 24443
1 file(s) copied.
real 0m14.900s
user 0m0.046s
sys 0m0.109s
+ status=0
+ set +x
=================================================
data/session09/tess_2_TFI_Templates.py passed (as expected)
=================================================
=================================================
tess_3_Params.py test;
+ python tess_3_Params.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 732
Number of elements = 1781
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1781
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 732
Total number of elements = 1781
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 936
Number of elements = 2232
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2232
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 936
Total number of elements = 2232
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 3546
Number of elements = 7671
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 7671
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3546
Total number of elements = 7671
1 file(s) copied.
real 0m16.285s
user 0m0.046s
sys 0m0.093s
+ status=0
+ set +x
=================================================
data/session09/tess_3_Params.py passed (as expected)
=================================================
=================================================
tess_4_Params.py test;
+ python tess_4_Params.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1402
Number of elements = 3129
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3129
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1402
Total number of elements = 3129
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 2095
Number of elements = 4566
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4566
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2095
Total number of elements = 4566
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 6580
Number of elements = 13725
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 13725
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 6580
Total number of elements = 13725
1 file(s) copied.
real 0m15.397s
user 0m0.015s
sys 0m0.077s
+ status=0
+ set +x
=================================================
data/session09/tess_4_Params.py passed (as expected)
=================================================
=================================================
tess_5_Params.py test;
+ python tess_5_Params.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 3861
Number of elements = 8063
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 8063
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3861
Total number of elements = 8063
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 12390
Number of elements = 25248
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 25248
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 12390
Total number of elements = 25248
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 45179
Number of elements = 91025
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 91025
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 45179
Total number of elements = 91025
1 file(s) copied.
real 0m21.480s
user 0m0.061s
sys 0m0.124s
+ status=0
+ set +x
=================================================
data/session09/tess_5_Params.py passed (as expected)
=================================================
=================================================
tess_6_TriQuad.py test;
+ python tess_6_TriQuad.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 8294
Number of elements = 17175
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 17175
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 8294
Total number of elements = 17175
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 72029
Number of elements = 74322
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 74322
----------------------------
Total number of nodes = 72029
Total number of elements = 74322
1 file(s) copied.
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1655
Number of elements = 3225
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3225
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1655
Total number of elements = 3225
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 3009
Number of elements = 2928
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 2928
----------------------------
Total number of nodes = 3009
Total number of elements = 2928
1 file(s) copied.
real 0m27.205s
user 0m0.030s
sys 0m0.186s
+ status=0
+ set +x
=================================================
data/session09/tess_6_TriQuad.py passed (as expected)
=================================================
=================================================
tess_7_MeshSizing.py test;
+ python tess_7_MeshSizing.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 8294
Number of elements = 17175
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 17175
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 8294
Total number of elements = 17175
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - leadingEdge
Mesh sizing name - rootLeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 3890
Number of elements = 8352
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 8352
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3890
Total number of elements = 8352
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - leadingEdge
Mesh sizing name - rootLeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 6181
Number of elements = 6607
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 6607
----------------------------
Total number of nodes = 6181
Total number of elements = 6607
1 file(s) copied.
real 0m14.774s
user 0m0.000s
sys 0m0.077s
+ status=0
+ set +x
=================================================
data/session09/tess_7_MeshSizing.py passed (as expected)
=================================================
=================================================
tess_8_MeshSizing.py test;
+ python tess_8_MeshSizing.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1655
Number of elements = 3225
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3225
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1655
Total number of elements = 3225
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - rootLeadingEdge
Mesh sizing name - wingSpar1
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 6585
Number of elements = 13196
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 13196
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 6585
Total number of elements = 13196
1 file(s) copied.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - rootLeadingEdge
Mesh sizing name - wingSpar1
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 22190
Number of elements = 22191
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 22191
----------------------------
Total number of nodes = 22190
Total number of elements = 22191
1 file(s) copied.
real 0m17.371s
user 0m0.077s
sys 0m0.123s
+ status=0
+ set +x
=================================================
data/session09/tess_8_MeshSizing.py passed (as expected)
=================================================
=================================================
tess_MinQuad.py test;
+ python tess_MinQuad.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\..\data\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = leftWingSkin, index = 5
Name = wingTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 299
Number of elements = 387
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 387
----------------------------
Total number of nodes = 299
Total number of elements = 387
1 file(s) copied.
--> Total Elements 387
real 0m12.230s
user 0m0.015s
sys 0m0.123s
+ status=0
+ set +x
=================================================
solutions/session09/tess_MinQuad.py passed (as expected)
=================================================
=================================================
tess_2k.py test;
+ python tess_2k.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\..\data\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - rootLeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1289
Number of elements = 1189
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 1189
----------------------------
Total number of nodes = 1289
Total number of elements = 1189
1 file(s) copied.
--> Total Elements 1189
real 0m14.552s
user 0m0.000s
sys 0m0.155s
+ status=0
+ set +x
=================================================
solutions/session09/tess_2k.py passed (as expected)
=================================================
=================================================
astros_1_ModalClamped.py test;
+ python astros_1_ModalClamped.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
==> Running ASTROS pre-analysis...
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 235
Number of elements = 227
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 227
----------------------------
Total number of nodes = 235
Total number of elements = 227
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
Aero_Reference value is NULL - No aero reference parameters set
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 - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_DENORMAL
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 9
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
--> Eigen-frequencies:
1 : 0.0357647
2 : 0.102451
3 : 0.102451
4 : 0.159637
5 : 0.159637
6 : 0.215446
7 : 0.215446
8 : 0.350115
9 : 0.350115
real 0m20.266s
user 0m0.000s
sys 0m0.107s
+ status=0
+ set +x
=================================================
data/session10/astros_1_ModalClamped.py passed (as expected)
=================================================
=================================================
astros_2_ModalSupport.py test;
+ python astros_2_ModalSupport.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
==> Running ASTROS pre-analysis...
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Name = ribSupport, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 235
Number of elements = 227
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 227
Body 2 (of 2)
Number of nodes = 1
Number of elements = 1
Number of node elements = 1
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 236
Total number of elements = 228
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 = 1
Name = ribRootPoint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = ribRoot, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Name = ribSupport, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 236
Combined Number of elements = 228
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 227
Aero_Reference value is NULL - No aero reference parameters set
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 - 6
Property name - leftWingSkin
Property name - ribSupport
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribRootPoint
No "constraintType" specified for Constraint tuple ribRootPoint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple ribRootPoint, going to use constraint name
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribRootPoint
No "groupName" specified for Support tuple ribRootPoint, going to use support name
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - ribRoot
No "groupName" specified for Connection tuple ribRoot!
Looking for automatic connections from the use of capsConnectLink for ribRoot
19 automatic connections were made for capsConnect ribRoot (node id 236)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing support cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_DENORMAL
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
--> Eigen-frequencies:
1 : 2.87907e-08
2 : 0.0357647
3 : 0.0365801
4 : 0.102451
5 : 0.102453
6 : 0.159637
7 : 0.1611
8 : 0.215446
9 : 0.215462
10: 0.350115
real 0m26.644s
user 0m0.092s
sys 0m0.326s
+ status=0
+ set +x
=================================================
data/session10/astros_2_ModalSupport.py passed (as expected)
=================================================
=================================================
astros_3_StaticClamped.py test;
+ python astros_3_StaticClamped.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
==> Running ASTROS pre-analysis...
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 235
Number of elements = 227
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 227
----------------------------
Total number of nodes = 235
Total number of elements = 227
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
Aero_Reference value is NULL - No aero reference parameters set
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 - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftPointLoad
No "groupName" specified for Load tuple leftPointLoad, going to use load name
Load name - ritePointLoad
No "groupName" specified for Load tuple ritePointLoad, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
--> Maximum displacements:
--> Tmax 43461.879162311016
--> T1max 738.595
--> T2max 3686.25
--> T3max 43363.8
real 0m18.272s
user 0m0.031s
sys 0m0.155s
+ status=0
+ set +x
=================================================
data/session10/astros_3_StaticClamped.py passed (as expected)
=================================================
=================================================
astros_4_Composite.py test;
+ python astros_4_Composite.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
==> Running ASTROS pre-analysis...
ERROR:: (edge_not_found) in Branch Brch_000207 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training\data\ESP\wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 235
Number of elements = 227
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 227
----------------------------
Total number of nodes = 235
Total number of elements = 227
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftPointLoad
No "groupName" specified for Load tuple leftPointLoad, going to use load name
Load name - ritePointLoad
No "groupName" specified for Load tuple ritePointLoad, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
--> Maximum displacements:
--> Tmax 12131.654370141774
--> T1max 275.241
--> T2max 1005.74
--> T3max 12103.5
real 0m17.614s
user 0m0.061s
sys 0m0.046s
+ status=0
+ set +x
=================================================
data/session10/astros_4_Composite.py passed (as expected)
=================================================
=================================================
nastran_5_Flutter.py test;
+ python nastran_5_Flutter.py
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/training/WIN64.2019/CAPS/training/training.log
==> Loading geometry from file "..\ESP\wing3.csm"...
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
Information: Dynamic Loader for scribeWake.DLL not found
==> Running Nastran pre-analysis...
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Wing, index = 1
Name = wingSpar2, index = 2
Name = wingRib, index = 3
Name = riteWingSkin, index = 4
Name = wingSpar1, index = 5
Name = leftWingSkin, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = leadingEdge, index = 3
Name = rootLeadingEdge, index = 4
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)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 (of 4)
Number of nodes = 11
Number of elements = 6
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 6
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 2 (of 4)
Number of nodes = 11
Number of elements = 6
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 6
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 3 (of 4)
Number of nodes = 11
Number of elements = 6
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 6
Body 4 (of 4)
Number of nodes = 939
Number of elements = 1094
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 1094
----------------------------
Total number of nodes = 972
Total number of elements = 1112
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Wing, index = 1
Name = wingSpar2, index = 2
Name = wingRib, index = 3
Name = riteWingSkin, index = 4
Name = wingSpar1, index = 5
Name = leftWingSkin, index = 6
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 11
Number of elements = 6
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 6
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 11
Number of elements = 6
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 6
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 11
Number of elements = 6
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 6
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 939
Number of elements = 1094
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 1094
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 972
Combined Number of elements = 1112
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 1112
Getting vortex lattice surface data
VLM surface name - upperWing
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 108
Surface 2: Number of points found for aero-spline = 108
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 - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing Nastran instruction file....
Warning: No loads specified for case Flutter!!!!
Writing aero card
Writing analysis cards
Writing constraint ADD cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
Writing aeroelastic cards
==> Running Nastran...
'nastran' is not recognized as an internal or external command,
operable program or batch file.
real 0m18.259s
user 0m0.061s
sys 0m0.124s
+ status=0
+ set +x
=================================================
data/session10/nastran_5_Flutter.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
session07 pointwise
session08 su2
session08 fun3d
session11 fun3d+astros
session11 su2+astros
=================================================
All tests pass!
(venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training>set /a "err=0+0+0+0"
(venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\training>exit /b 0
(venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019\CAPS\aim\skeleton>exit 0
[GNU C Compiler (gcc)] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019')
[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: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019')
[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: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\training\WIN64.2019')
[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_RegCaps/CASREV=7.6,ESPTEST=CAPS/training,ESP_ARCH=WIN64.2019,buildnode=windows10x64 #619'.
[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
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