The Jenkins Controller is preparing for shutdown. No new builds can be started.
Skipping 1,626 KB.. Full LogEGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Fuselage, index = 1 Name = Wing, index = 2 Name = Htail, index = 3 Name = Vtail, index = 4 Name = Pod, index = 5 Name = Farfield, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 7 Name = Fuselage, index = 1 Name = riteWing, index = 2 Name = leftWing, index = 3 Name = Htail, index = 4 Name = Vtail, index = 5 Name = Pod, index = 6 Name = Farfield, index = 7 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - Fuselage Mesh sizing name - Htail Mesh sizing name - Pod Mesh sizing name - Vtail Mesh sizing name - leftWing Mesh sizing name - riteWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS CYGWIN_NT-6.1 3.1.7(0.340/5/3) x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS CYGWIN_NT-6.1 3.1.7(0.340/5/3) x86_64 AFLR4 : Compile Date 04/23/24 @ 12:21PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 4 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 100 Faces EGADS : Body 0 has 251 Edges EGADS : Body 0 has 100 Loops EGADS : Body 0 has 149 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 4 Faces EGADS : Body 1 has 8 Edges EGADS : Body 1 has 4 Loops EGADS : Body 1 has 4 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 4 Faces EGADS : Body 2 has 8 Edges EGADS : Body 2 has 4 Loops EGADS : Body 2 has 4 Nodes EGADS : Body 3 is a SolidBody EGADS : Body 3 has 1 Shells EGADS : Body 3 has 6 Faces EGADS : Body 3 has 12 Edges EGADS : Body 3 has 6 Loops EGADS : Body 3 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 6 EGADS : 2 Yes 0 0 1 0 1 1 7 8 9 10 EGADS : 3 Yes 0 0 1 0 1 1 10 11 12 13 14 EGADS : 4 Yes 0 0 1 0 1 1 5 7 12 EGADS : 5 Yes 0 0 1 0 2 1 4 6 15 16 17 EGADS : 18 EGADS : 6 Yes 0 0 1 0 2 1 5 19 20 21 22 EGADS : 7 Yes 0 0 1 0 1 2 4 8 23 EGADS : 8 Yes 0 0 1 0 2 2 7 9 24 25 26 EGADS : 27 EGADS : 9 Yes 0 0 1 0 2 2 8 28 29 30 31 EGADS : 10 Yes 0 0 1 0 1 2 3 11 23 32 33 EGADS : 11 Yes 0 0 1 0 1 3 10 12 23 EGADS : 12 Yes 0 0 1 0 1 3 4 11 13 14 23 EGADS : 34 EGADS : 13 Yes 0 0 1 0 2 3 12 14 35 36 37 EGADS : 38 EGADS : 14 Yes 0 0 1 0 2 3 12 13 38 39 40 EGADS : 41 EGADS : 15 Yes 0 0 1 0 2 5 16 22 42 EGADS : 16 Yes 0 0 1 0 2 5 15 17 42 EGADS : 17 Yes 0 0 1 0 2 5 16 20 42 EGADS : 18 Yes 0 0 1 0 2 5 19 43 44 45 46 EGADS : 47 48 49 EGADS : 19 Yes 0 0 1 0 2 6 18 49 50 51 52 EGADS : 53 54 55 EGADS : 20 Yes 0 0 1 0 2 6 17 21 56 EGADS : 21 Yes 0 0 1 0 2 6 20 22 56 EGADS : 22 Yes 0 0 1 0 2 6 15 21 56 EGADS : 23 Yes 0 0 1 0 1 7 10 11 12 32 33 EGADS : 57 EGADS : 24 Yes 0 0 1 0 2 8 25 31 58 EGADS : 25 Yes 0 0 1 0 2 8 24 26 58 EGADS : 26 Yes 0 0 1 0 2 8 25 29 58 EGADS : 27 Yes 0 0 1 0 2 8 28 59 60 61 62 EGADS : 63 64 65 EGADS : 28 Yes 0 0 1 0 2 9 27 65 66 67 68 EGADS : 69 70 71 EGADS : 29 Yes 0 0 1 0 2 9 26 30 72 EGADS : 30 Yes 0 0 1 0 2 9 29 31 72 EGADS : 31 Yes 0 0 1 0 2 9 24 30 72 EGADS : 32 Yes 0 0 1 0 2 10 23 33 73 74 EGADS : 75 76 EGADS : 33 Yes 0 0 1 0 2 10 23 32 73 77 EGADS : 78 79 EGADS : 34 Yes 0 0 1 0 2 12 57 80 81 82 EGADS : 83 EGADS : 35 Yes 0 0 1 0 2 13 36 41 84 EGADS : 36 Yes 0 0 1 0 2 13 35 37 84 EGADS : 37 Yes 0 0 1 0 2 13 36 39 84 EGADS : 38 Yes 0 0 1 0 2 13 14 EGADS : 39 Yes 0 0 1 0 2 14 37 40 85 EGADS : 40 Yes 0 0 1 0 2 14 39 41 85 EGADS : 41 Yes 0 0 1 0 2 14 35 40 85 EGADS : 42 Yes 0 0 1 0 2 15 16 17 56 EGADS : 43 Yes 0 0 1 0 2 18 44 55 86 EGADS : 44 Yes 0 0 1 0 2 18 43 45 86 EGADS : 45 Yes 0 0 1 0 2 18 44 53 86 EGADS : 46 Yes 0 0 1 0 2 18 47 52 87 EGADS : 47 Yes 0 0 1 0 2 18 46 48 87 EGADS : 48 Yes 0 0 1 0 2 18 47 50 87 EGADS : 49 Yes 0 0 1 0 2 18 19 EGADS : 50 Yes 0 0 1 0 2 19 48 51 88 EGADS : 51 Yes 0 0 1 0 2 19 50 52 88 EGADS : 52 Yes 0 0 1 0 2 19 46 51 88 EGADS : 53 Yes 0 0 1 0 2 19 45 54 89 EGADS : 54 Yes 0 0 1 0 2 19 53 55 89 EGADS : 55 Yes 0 0 1 0 2 19 43 54 89 EGADS : 56 Yes 0 0 1 0 2 20 21 22 42 EGADS : 57 Yes 0 0 1 0 2 23 34 83 90 91 EGADS : 92 EGADS : 58 Yes 0 0 1 0 2 24 25 26 72 EGADS : 59 Yes 0 0 1 0 2 27 60 71 93 EGADS : 60 Yes 0 0 1 0 2 27 59 61 93 EGADS : 61 Yes 0 0 1 0 2 27 60 69 93 EGADS : 62 Yes 0 0 1 0 2 27 63 68 94 EGADS : 63 Yes 0 0 1 0 2 27 62 64 94 EGADS : 64 Yes 0 0 1 0 2 27 63 66 94 EGADS : 65 Yes 0 0 1 0 2 27 28 EGADS : 66 Yes 0 0 1 0 2 28 64 67 95 EGADS : 67 Yes 0 0 1 0 2 28 66 68 95 EGADS : 68 Yes 0 0 1 0 2 28 62 67 95 EGADS : 69 Yes 0 0 1 0 2 28 61 70 96 EGADS : 70 Yes 0 0 1 0 2 28 69 71 96 EGADS : 71 Yes 0 0 1 0 2 28 59 70 96 EGADS : 72 Yes 0 0 1 0 2 29 30 31 58 EGADS : 73 Yes 0 0 1 0 2 32 33 EGADS : 74 Yes 0 0 1 0 2 32 75 79 97 EGADS : 75 Yes 0 0 1 0 2 32 74 76 97 EGADS : 76 Yes 0 0 1 0 2 32 75 77 97 EGADS : 77 Yes 0 0 1 0 2 33 76 78 98 EGADS : 78 Yes 0 0 1 0 2 33 77 79 98 EGADS : 79 Yes 0 0 1 0 2 33 74 78 98 EGADS : 80 Yes 0 0 1 0 2 34 81 92 99 EGADS : 81 Yes 0 0 1 0 2 34 80 82 99 EGADS : 82 Yes 0 0 1 0 2 34 81 90 99 EGADS : 83 Yes 0 0 1 0 2 34 57 EGADS : 84 Yes 0 0 1 0 2 35 36 37 85 EGADS : 85 Yes 0 0 1 0 2 39 40 41 84 EGADS : 86 Yes 0 0 1 0 2 43 44 45 89 EGADS : 87 Yes 0 0 1 0 2 46 47 48 88 EGADS : 88 Yes 0 0 1 0 2 50 51 52 87 EGADS : 89 Yes 0 0 1 0 2 53 54 55 86 EGADS : 90 Yes 0 0 1 0 2 57 82 91 100 EGADS : 91 Yes 0 0 1 0 2 57 90 92 100 EGADS : 92 Yes 0 0 1 0 2 57 80 91 100 EGADS : 93 Yes 0 0 1 0 2 59 60 61 96 EGADS : 94 Yes 0 0 1 0 2 62 63 64 95 EGADS : 95 Yes 0 0 1 0 2 66 67 68 94 EGADS : 96 Yes 0 0 1 0 2 69 70 71 93 EGADS : 97 Yes 0 0 1 0 2 74 75 76 98 EGADS : 98 Yes 0 0 1 0 2 77 78 79 97 EGADS : 99 Yes 0 0 1 0 2 80 81 82 100 EGADS : 100 Yes 0 0 1 0 2 90 91 92 99 EGADS : 101 Yes 1 0 1 0 1 102 103 EGADS : 102 Yes 1 0 1 0 1 101 104 EGADS : 103 Yes 1 0 1 0 1 101 104 EGADS : 104 Yes 1 0 1 0 1 102 103 EGADS : 105 Yes 2 0 1 0 1 106 107 EGADS : 106 Yes 2 0 1 0 1 105 108 EGADS : 107 Yes 2 0 1 0 1 105 108 EGADS : 108 Yes 2 0 1 0 1 106 107 EGADS : 109 Yes 3 0 1 NA NA 111 112 113 114 EGADS : 110 Yes 3 0 1 NA NA 111 112 113 114 EGADS : 111 Yes 3 0 1 NA NA 109 110 113 114 EGADS : 112 Yes 3 0 1 NA NA 109 110 113 114 EGADS : 113 Yes 3 0 1 NA NA 109 110 111 112 EGADS : 114 Yes 3 0 1 NA NA 109 110 111 112 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 8 7 -6 -5 -4 3 -2 EGADS : 2 -9 15 1 -14 -13 12 11 10 EGADS : 3 -16 2 21 -20 -19 18 -17 EGADS : 4 -7 25 24 -23 -3 -22 EGADS : 5 26 -27 28 29 30 31 -32 6 22 4 EGADS : 6 32 33 -30 34 -35 -36 -26 5 EGADS : 7 -24 39 9 38 13 -37 EGADS : 8 -40 -12 -38 -10 46 -45 -44 -43 -42 41 EGADS : 9 -46 -11 40 50 49 -48 44 -47 EGADS : 10 -51 14 16 -55 -54 53 52 EGADS : 11 17 56 57 55 EGADS : 12 -21 23 62 61 60 -56 -18 -59 -58 EGADS : 13 63 -64 65 66 67 68 -69 59 19 EGADS : 14 69 70 -67 71 -72 -73 -63 20 58 EGADS : 15 -74 76 27 -75 EGADS : 16 77 78 -28 -76 EGADS : 17 79 80 -29 -78 EGADS : 18 81 -82 83 84 85 -86 87 88 89 90 -91 -31 EGADS : 19 91 92 -89 93 -94 -95 -85 96 -97 -98 -81 -33 EGADS : 20 99 100 -34 -80 EGADS : 21 -101 102 35 -100 EGADS : 22 -103 75 36 -102 EGADS : 23 -62 37 51 106 105 54 -57 -60 104 EGADS : 24 107 108 -41 -109 EGADS : 25 -110 109 42 -111 EGADS : 26 -112 111 43 -113 EGADS : 27 -114 45 124 -123 -122 -121 -120 119 -118 -117 -116 115 EGADS : 28 -124 47 114 131 130 -129 118 128 127 -126 122 -125 EGADS : 29 -132 113 48 -133 EGADS : 30 134 133 -49 -135 EGADS : 31 136 135 -50 -108 EGADS : 32 -137 -106 -52 143 142 141 -140 139 -138 EGADS : 33 -143 -53 -105 137 -147 -139 -146 -145 144 EGADS : 34 -148 -61 154 -153 -152 -151 -150 149 EGADS : 35 -155 157 64 -156 EGADS : 36 158 159 -65 -157 EGADS : 37 160 161 -66 -159 EGADS : 38 -68 -70 EGADS : 39 162 163 -71 -161 EGADS : 40 -164 165 72 -163 EGADS : 41 -166 156 73 -165 EGADS : 42 167 -79 -77 74 EGADS : 43 -168 170 82 -169 EGADS : 44 171 172 -83 -170 EGADS : 45 173 174 -84 -172 EGADS : 46 -175 177 86 -176 EGADS : 47 178 179 -87 -177 EGADS : 48 180 181 -88 -179 EGADS : 49 -90 -92 EGADS : 50 182 183 -93 -181 EGADS : 51 -184 185 94 -183 EGADS : 52 -186 176 95 -185 EGADS : 53 187 188 -96 -174 EGADS : 54 -189 190 97 -188 EGADS : 55 -191 169 98 -190 EGADS : 56 103 101 -99 -167 EGADS : 57 -154 -104 148 195 194 -193 152 -192 EGADS : 58 -196 -107 110 112 EGADS : 59 197 198 -115 -199 EGADS : 60 -200 199 116 -201 EGADS : 61 -202 201 117 -203 EGADS : 62 204 205 -119 -206 EGADS : 63 -207 206 120 -208 EGADS : 64 -209 208 121 -210 EGADS : 65 123 125 EGADS : 66 -211 210 126 -212 EGADS : 67 213 212 -127 -214 EGADS : 68 215 214 -128 -205 EGADS : 69 -216 203 129 -217 EGADS : 70 218 217 -130 -219 EGADS : 71 220 219 -131 -198 EGADS : 72 -136 196 132 -134 EGADS : 73 147 138 EGADS : 74 -221 223 140 -222 EGADS : 75 224 222 -141 -225 EGADS : 76 226 225 -142 -227 EGADS : 77 228 227 -144 -229 EGADS : 78 -230 229 145 -231 EGADS : 79 -232 231 146 -223 EGADS : 80 233 234 -149 -235 EGADS : 81 -236 235 150 -237 EGADS : 82 -238 237 151 -239 EGADS : 83 153 192 EGADS : 84 240 -160 -158 155 EGADS : 85 166 164 -162 -240 EGADS : 86 241 -173 -171 168 EGADS : 87 -180 -178 175 242 EGADS : 88 -242 186 184 -182 EGADS : 89 191 189 -187 -241 EGADS : 90 -243 239 193 -244 EGADS : 91 245 244 -194 -246 EGADS : 92 247 246 -195 -234 EGADS : 93 -248 -197 200 202 EGADS : 94 -249 -204 207 209 EGADS : 95 -215 249 211 -213 EGADS : 96 -220 248 216 -218 EGADS : 97 -226 250 221 -224 EGADS : 98 -250 -228 230 232 EGADS : 99 -251 -233 236 238 EGADS : 100 -247 251 243 -245 EGADS : 101 -252 254 253 -255 EGADS : 102 -253 256 252 -257 EGADS : 103 258 255 -259 -254 EGADS : 104 259 257 -258 -256 EGADS : 105 260 263 -261 -262 EGADS : 106 261 265 -260 -264 EGADS : 107 -266 262 267 -263 EGADS : 108 -267 264 266 -265 EGADS : 109 268 269 -270 -271 EGADS : 110 -272 275 274 -273 EGADS : 111 276 272 -277 -268 EGADS : 112 -278 270 279 -274 EGADS : 113 271 278 -275 -276 EGADS : 114 -269 277 273 -279 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : 19 19 EGADS : 20 20 EGADS : 21 21 EGADS : 22 22 EGADS : 23 23 EGADS : 24 24 EGADS : 25 25 EGADS : 26 26 EGADS : 27 27 EGADS : 28 28 EGADS : 29 29 EGADS : 30 30 EGADS : 31 31 EGADS : 32 32 EGADS : 33 33 EGADS : 34 34 EGADS : 35 35 EGADS : 36 36 EGADS : 37 37 EGADS : 38 38 EGADS : 39 39 EGADS : 40 40 EGADS : 41 41 EGADS : 42 42 EGADS : 43 43 EGADS : 44 44 EGADS : 45 45 EGADS : 46 46 EGADS : 47 47 EGADS : 48 48 EGADS : 49 49 EGADS : 50 50 EGADS : 51 51 EGADS : 52 52 EGADS : 53 53 EGADS : 54 54 EGADS : 55 55 EGADS : 56 56 EGADS : 57 57 EGADS : 58 58 EGADS : 59 59 EGADS : 60 60 EGADS : 61 61 EGADS : 62 62 EGADS : 63 63 EGADS : 64 64 EGADS : 65 65 EGADS : 66 66 EGADS : 67 67 EGADS : 68 68 EGADS : 69 69 EGADS : 70 70 EGADS : 71 71 EGADS : 72 72 EGADS : 73 73 EGADS : 74 74 EGADS : 75 75 EGADS : 76 76 EGADS : 77 77 EGADS : 78 78 EGADS : 79 79 EGADS : 80 80 EGADS : 81 81 EGADS : 82 82 EGADS : 83 83 EGADS : 84 84 EGADS : 85 85 EGADS : 86 86 EGADS : 87 87 EGADS : 88 88 EGADS : 89 89 EGADS : 90 90 EGADS : 91 91 EGADS : 92 92 EGADS : 93 93 EGADS : 94 94 EGADS : 95 95 EGADS : 96 96 EGADS : 97 97 EGADS : 98 98 EGADS : 99 99 EGADS : 100 100 EGADS : 101 101 EGADS : 102 102 EGADS : 103 103 EGADS : 104 104 EGADS : 105 105 EGADS : 106 106 EGADS : 107 107 EGADS : 108 108 EGADS : 109 109 EGADS : 110 110 EGADS : 111 111 EGADS : 112 112 EGADS : 113 113 EGADS : 114 114 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 8 7 -6 -5 -4 3 -2 EGADS : 2 Yes -9 15 1 -14 -13 12 11 10 EGADS : 3 Yes -16 2 21 -20 -19 18 -17 EGADS : 4 Yes -7 25 24 -23 -3 -22 EGADS : 5 Yes 26 -27 28 29 30 31 -32 6 22 4 EGADS : 6 Yes 32 33 -30 34 -35 -36 -26 5 EGADS : 7 Yes -24 39 9 38 13 -37 EGADS : 8 Yes -40 -12 -38 -10 46 -45 -44 -43 -42 41 EGADS : 9 Yes -46 -11 40 50 49 -48 44 -47 EGADS : 10 Yes -51 14 16 -55 -54 53 52 EGADS : 11 Yes 17 56 57 55 EGADS : 12 Yes -21 23 62 61 60 -56 -18 -59 -58 EGADS : 13 Yes 63 -64 65 66 67 68 -69 59 19 EGADS : 14 Yes 69 70 -67 71 -72 -73 -63 20 58 EGADS : 15 Yes -74 76 27 -75 EGADS : 16 Yes 77 78 -28 -76 EGADS : 17 Yes 79 80 -29 -78 EGADS : 18 Yes 81 -82 83 84 85 -86 87 88 89 90 -91 -31 EGADS : 19 Yes 91 92 -89 93 -94 -95 -85 96 -97 -98 -81 -33 EGADS : 20 Yes 99 100 -34 -80 EGADS : 21 Yes -101 102 35 -100 EGADS : 22 Yes -103 75 36 -102 EGADS : 23 Yes -62 37 51 106 105 54 -57 -60 104 EGADS : 24 Yes 107 108 -41 -109 EGADS : 25 Yes -110 109 42 -111 EGADS : 26 Yes -112 111 43 -113 EGADS : 27 Yes -114 45 124 -123 -122 -121 -120 119 -118 -117 -116 EGADS : 115 EGADS : 28 Yes -124 47 114 131 130 -129 118 128 127 -126 122 -125 EGADS : 29 Yes -132 113 48 -133 EGADS : 30 Yes 134 133 -49 -135 EGADS : 31 Yes 136 135 -50 -108 EGADS : 32 Yes -137 -106 -52 143 142 141 -140 139 -138 EGADS : 33 Yes -143 -53 -105 137 -147 -139 -146 -145 144 EGADS : 34 Yes -148 -61 154 -153 -152 -151 -150 149 EGADS : 35 Yes -155 157 64 -156 EGADS : 36 Yes 158 159 -65 -157 EGADS : 37 Yes 160 161 -66 -159 EGADS : 38 Yes -68 -70 EGADS : 39 Yes 162 163 -71 -161 EGADS : 40 Yes -164 165 72 -163 EGADS : 41 Yes -166 156 73 -165 EGADS : 42 Yes 167 -79 -77 74 EGADS : 43 Yes -168 170 82 -169 EGADS : 44 Yes 171 172 -83 -170 EGADS : 45 Yes 173 174 -84 -172 EGADS : 46 Yes -175 177 86 -176 EGADS : 47 Yes 178 179 -87 -177 EGADS : 48 Yes 180 181 -88 -179 EGADS : 49 Yes -90 -92 EGADS : 50 Yes 182 183 -93 -181 EGADS : 51 Yes -184 185 94 -183 EGADS : 52 Yes -186 176 95 -185 EGADS : 53 Yes 187 188 -96 -174 EGADS : 54 Yes -189 190 97 -188 EGADS : 55 Yes -191 169 98 -190 EGADS : 56 Yes 103 101 -99 -167 EGADS : 57 Yes -154 -104 148 195 194 -193 152 -192 EGADS : 58 Yes -196 -107 110 112 EGADS : 59 Yes 197 198 -115 -199 EGADS : 60 Yes -200 199 116 -201 EGADS : 61 Yes -202 201 117 -203 EGADS : 62 Yes 204 205 -119 -206 EGADS : 63 Yes -207 206 120 -208 EGADS : 64 Yes -209 208 121 -210 EGADS : 65 Yes 123 125 EGADS : 66 Yes -211 210 126 -212 EGADS : 67 Yes 213 212 -127 -214 EGADS : 68 Yes 215 214 -128 -205 EGADS : 69 Yes -216 203 129 -217 EGADS : 70 Yes 218 217 -130 -219 EGADS : 71 Yes 220 219 -131 -198 EGADS : 72 Yes -136 196 132 -134 EGADS : 73 Yes 147 138 EGADS : 74 Yes -221 223 140 -222 EGADS : 75 Yes 224 222 -141 -225 EGADS : 76 Yes 226 225 -142 -227 EGADS : 77 Yes 228 227 -144 -229 EGADS : 78 Yes -230 229 145 -231 EGADS : 79 Yes -232 231 146 -223 EGADS : 80 Yes 233 234 -149 -235 EGADS : 81 Yes -236 235 150 -237 EGADS : 82 Yes -238 237 151 -239 EGADS : 83 Yes 153 192 EGADS : 84 Yes 240 -160 -158 155 EGADS : 85 Yes 166 164 -162 -240 EGADS : 86 Yes 241 -173 -171 168 EGADS : 87 Yes -180 -178 175 242 EGADS : 88 Yes -242 186 184 -182 EGADS : 89 Yes 191 189 -187 -241 EGADS : 90 Yes -243 239 193 -244 EGADS : 91 Yes 245 244 -194 -246 EGADS : 92 Yes 247 246 -195 -234 EGADS : 93 Yes -248 -197 200 202 EGADS : 94 Yes -249 -204 207 209 EGADS : 95 Yes -215 249 211 -213 EGADS : 96 Yes -220 248 216 -218 EGADS : 97 Yes -226 250 221 -224 EGADS : 98 Yes -250 -228 230 232 EGADS : 99 Yes -251 -233 236 238 EGADS : 100 Yes -247 251 243 -245 EGADS : 101 Yes -252 254 253 -255 EGADS : 102 Yes -253 256 252 -257 EGADS : 103 Yes 258 255 -259 -254 EGADS : 104 Yes 259 257 -258 -256 EGADS : 105 Yes 260 263 -261 -262 EGADS : 106 Yes 261 265 -260 -264 EGADS : 107 Yes -266 262 267 -263 EGADS : 108 Yes -267 264 266 -265 EGADS : 109 Yes 268 269 -270 -271 EGADS : 110 Yes -272 275 274 -273 EGADS : 111 Yes 276 272 -277 -268 EGADS : 112 Yes -278 270 279 -274 EGADS : 113 Yes 271 278 -275 -276 EGADS : 114 Yes -269 277 273 -279 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 2 1 1 2 EGADS : 2 0 Yes 2 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 4 5 1 1 5 EGADS : 5 0 Yes 5 6 1 1 6 EGADS : 6 0 Yes 6 7 1 1 5 EGADS : 7 0 Yes 1 7 1 1 4 EGADS : 8 0 DEGEN 1 1 - 1 EGADS : 9 0 Yes 1 8 1 2 7 EGADS : 10 0 Yes 9 8 1 2 8 EGADS : 11 0 Yes 10 9 1 2 9 EGADS : 12 0 Yes 11 10 1 2 8 EGADS : 13 0 Yes 11 12 1 2 7 EGADS : 14 0 Yes 12 2 1 2 10 EGADS : 15 0 DEGEN 1 1 - 2 EGADS : 16 0 Yes 2 13 1 3 10 EGADS : 17 0 Yes 13 14 1 3 11 EGADS : 18 0 Yes 15 14 1 3 12 EGADS : 19 0 Yes 15 16 1 3 13 EGADS : 20 0 Yes 16 17 1 3 14 EGADS : 21 0 Yes 3 17 1 3 12 EGADS : 22 0 Yes 7 4 1 4 5 EGADS : 23 0 Yes 3 18 1 4 12 EGADS : 24 0 Yes 1 18 1 4 7 EGADS : 25 0 DEGEN 1 1 - 4 EGADS : 26 0 Yes 5 19 1 5 6 EGADS : 27 0 Yes 20 19 1 5 15 EGADS : 28 0 Yes 20 21 1 5 16 EGADS : 29 0 Yes 21 22 1 5 17 EGADS : 30 0 Yes 22 23 1 5 6 EGADS : 31 0 Yes 23 24 1 5 18 EGADS : 32 0 Yes 6 24 1 5 6 EGADS : 33 0 Yes 24 23 1 6 19 EGADS : 34 0 Yes 22 25 1 6 20 EGADS : 35 0 Yes 26 25 1 6 21 EGADS : 36 0 Yes 19 26 1 6 22 EGADS : 37 0 Yes 18 12 1 7 23 EGADS : 38 0 Yes 8 11 1 7 8 EGADS : 39 0 DEGEN 1 1 - 7 EGADS : 40 0 Yes 10 27 1 8 9 EGADS : 41 0 Yes 28 27 1 8 24 EGADS : 42 0 Yes 28 29 1 8 25 EGADS : 43 0 Yes 29 30 1 8 26 EGADS : 44 0 Yes 30 31 1 8 9 EGADS : 45 0 Yes 31 32 1 8 27 EGADS : 46 0 Yes 9 32 1 8 9 EGADS : 47 0 Yes 32 31 1 9 28 EGADS : 48 0 Yes 30 33 1 9 29 EGADS : 49 0 Yes 34 33 1 9 30 EGADS : 50 0 Yes 27 34 1 9 31 EGADS : 51 0 Yes 12 35 1 10 23 EGADS : 52 0 Yes 36 35 1 10 32 EGADS : 53 0 Yes 37 36 1 10 33 EGADS : 54 0 Yes 37 38 1 10 23 EGADS : 55 0 Yes 38 13 1 10 11 EGADS : 56 0 Yes 14 39 1 11 12 EGADS : 57 0 Yes 39 38 1 11 23 EGADS : 58 0 Yes 17 40 1 12 14 EGADS : 59 0 Yes 40 15 1 12 13 EGADS : 60 0 Yes 41 39 1 12 23 EGADS : 61 0 Yes 42 41 1 12 34 EGADS : 62 0 Yes 18 42 1 12 23 EGADS : 63 0 Yes 16 43 1 13 14 EGADS : 64 0 Yes 44 43 1 13 35 EGADS : 65 0 Yes 44 45 1 13 36 EGADS : 66 0 Yes 45 46 1 13 37 EGADS : 67 0 Yes 46 47 1 13 14 EGADS : 68 0 Yes 47 48 1 13 38 EGADS : 69 0 Yes 40 48 1 13 14 EGADS : 70 0 Yes 48 47 1 14 38 EGADS : 71 0 Yes 46 49 1 14 39 EGADS : 72 0 Yes 50 49 1 14 40 EGADS : 73 0 Yes 43 50 1 14 41 EGADS : 74 0 Yes 51 52 1 15 42 EGADS : 75 0 Yes 52 19 1 15 22 EGADS : 76 0 Yes 51 20 1 15 16 EGADS : 77 0 Yes 51 53 1 16 42 EGADS : 78 0 Yes 53 21 1 16 17 EGADS : 79 0 Yes 53 54 1 17 42 EGADS : 80 0 Yes 54 22 1 17 20 EGADS : 81 0 Yes 23 55 1 18 19 EGADS : 82 0 Yes 56 55 1 18 43 EGADS : 83 0 Yes 56 57 1 18 44 EGADS : 84 0 Yes 57 58 1 18 45 EGADS : 85 0 Yes 58 59 1 18 19 EGADS : 86 0 Yes 60 59 1 18 46 EGADS : 87 0 Yes 60 61 1 18 47 EGADS : 88 0 Yes 61 62 1 18 48 EGADS : 89 0 Yes 62 63 1 18 19 EGADS : 90 0 Yes 63 64 1 18 49 EGADS : 91 0 Yes 24 64 1 18 19 EGADS : 92 0 Yes 64 63 1 19 49 EGADS : 93 0 Yes 62 65 1 19 50 EGADS : 94 0 Yes 66 65 1 19 51 EGADS : 95 0 Yes 59 66 1 19 52 EGADS : 96 0 Yes 58 67 1 19 53 EGADS : 97 0 Yes 68 67 1 19 54 EGADS : 98 0 Yes 55 68 1 19 55 EGADS : 99 0 Yes 54 69 1 20 56 EGADS : 100 0 Yes 69 25 1 20 21 EGADS : 101 0 Yes 70 69 1 21 56 EGADS : 102 0 Yes 70 26 1 21 22 EGADS : 103 0 Yes 52 70 1 22 56 EGADS : 104 0 Yes 41 42 1 23 57 EGADS : 105 0 Yes 71 37 1 23 33 EGADS : 106 0 Yes 35 71 1 23 32 EGADS : 107 0 Yes 72 73 1 24 58 EGADS : 108 0 Yes 73 27 1 24 31 EGADS : 109 0 Yes 72 28 1 24 25 EGADS : 110 0 Yes 72 74 1 25 58 EGADS : 111 0 Yes 74 29 1 25 26 EGADS : 112 0 Yes 74 75 1 26 58 EGADS : 113 0 Yes 75 30 1 26 29 EGADS : 114 0 Yes 31 76 1 27 28 EGADS : 115 0 Yes 77 76 1 27 59 EGADS : 116 0 Yes 77 78 1 27 60 EGADS : 117 0 Yes 78 79 1 27 61 EGADS : 118 0 Yes 79 80 1 27 28 EGADS : 119 0 Yes 81 80 1 27 62 EGADS : 120 0 Yes 81 82 1 27 63 EGADS : 121 0 Yes 82 83 1 27 64 EGADS : 122 0 Yes 83 84 1 27 28 EGADS : 123 0 Yes 84 85 1 27 65 EGADS : 124 0 Yes 32 85 1 27 28 EGADS : 125 0 Yes 85 84 1 28 65 EGADS : 126 0 Yes 83 86 1 28 66 EGADS : 127 0 Yes 87 86 1 28 67 EGADS : 128 0 Yes 80 87 1 28 68 EGADS : 129 0 Yes 79 88 1 28 69 EGADS : 130 0 Yes 89 88 1 28 70 EGADS : 131 0 Yes 76 89 1 28 71 EGADS : 132 0 Yes 75 90 1 29 72 EGADS : 133 0 Yes 90 33 1 29 30 EGADS : 134 0 Yes 91 90 1 30 72 EGADS : 135 0 Yes 91 34 1 30 31 EGADS : 136 0 Yes 73 91 1 31 72 EGADS : 137 0 Yes 71 92 1 32 33 EGADS : 138 0 Yes 92 93 1 32 73 EGADS : 139 0 Yes 94 93 1 32 33 EGADS : 140 0 Yes 94 95 1 32 74 EGADS : 141 0 Yes 96 95 1 32 75 EGADS : 142 0 Yes 97 96 1 32 76 EGADS : 143 0 Yes 36 97 1 32 33 EGADS : 144 0 Yes 98 97 1 33 77 EGADS : 145 0 Yes 98 99 1 33 78 EGADS : 146 0 Yes 99 94 1 33 79 EGADS : 147 0 Yes 93 92 1 33 73 EGADS : 148 0 Yes 41 100 1 34 57 EGADS : 149 0 Yes 101 100 1 34 80 EGADS : 150 0 Yes 101 102 1 34 81 EGADS : 151 0 Yes 102 103 1 34 82 EGADS : 152 0 Yes 103 104 1 34 57 EGADS : 153 0 Yes 104 105 1 34 83 EGADS : 154 0 Yes 42 105 1 34 57 EGADS : 155 0 Yes 106 107 1 35 84 EGADS : 156 0 Yes 107 43 1 35 41 EGADS : 157 0 Yes 106 44 1 35 36 EGADS : 158 0 Yes 106 108 1 36 84 EGADS : 159 0 Yes 108 45 1 36 37 EGADS : 160 0 Yes 108 109 1 37 84 EGADS : 161 0 Yes 109 46 1 37 39 EGADS : 162 0 Yes 109 110 1 39 85 EGADS : 163 0 Yes 110 49 1 39 40 EGADS : 164 0 Yes 111 110 1 40 85 EGADS : 165 0 Yes 111 50 1 40 41 EGADS : 166 0 Yes 107 111 1 41 85 EGADS : 167 0 Yes 52 54 1 42 56 EGADS : 168 0 Yes 112 113 1 43 86 EGADS : 169 0 Yes 113 55 1 43 55 EGADS : 170 0 Yes 112 56 1 43 44 EGADS : 171 0 Yes 112 114 1 44 86 EGADS : 172 0 Yes 114 57 1 44 45 EGADS : 173 0 Yes 114 115 1 45 86 EGADS : 174 0 Yes 115 58 1 45 53 EGADS : 175 0 Yes 116 117 1 46 87 EGADS : 176 0 Yes 117 59 1 46 52 EGADS : 177 0 Yes 116 60 1 46 47 EGADS : 178 0 Yes 116 118 1 47 87 EGADS : 179 0 Yes 118 61 1 47 48 EGADS : 180 0 Yes 118 119 1 48 87 EGADS : 181 0 Yes 119 62 1 48 50 EGADS : 182 0 Yes 119 120 1 50 88 EGADS : 183 0 Yes 120 65 1 50 51 EGADS : 184 0 Yes 121 120 1 51 88 EGADS : 185 0 Yes 121 66 1 51 52 EGADS : 186 0 Yes 117 121 1 52 88 EGADS : 187 0 Yes 115 122 1 53 89 EGADS : 188 0 Yes 122 67 1 53 54 EGADS : 189 0 Yes 123 122 1 54 89 EGADS : 190 0 Yes 123 68 1 54 55 EGADS : 191 0 Yes 113 123 1 55 89 EGADS : 192 0 Yes 105 104 1 57 83 EGADS : 193 0 Yes 103 124 1 57 90 EGADS : 194 0 Yes 125 124 1 57 91 EGADS : 195 0 Yes 100 125 1 57 92 EGADS : 196 0 Yes 73 75 1 58 72 EGADS : 197 0 Yes 126 127 1 59 93 EGADS : 198 0 Yes 127 76 1 59 71 EGADS : 199 0 Yes 126 77 1 59 60 EGADS : 200 0 Yes 126 128 1 60 93 EGADS : 201 0 Yes 128 78 1 60 61 EGADS : 202 0 Yes 128 129 1 61 93 EGADS : 203 0 Yes 129 79 1 61 69 EGADS : 204 0 Yes 130 131 1 62 94 EGADS : 205 0 Yes 131 80 1 62 68 EGADS : 206 0 Yes 130 81 1 62 63 EGADS : 207 0 Yes 130 132 1 63 94 EGADS : 208 0 Yes 132 82 1 63 64 EGADS : 209 0 Yes 132 133 1 64 94 EGADS : 210 0 Yes 133 83 1 64 66 EGADS : 211 0 Yes 133 134 1 66 95 EGADS : 212 0 Yes 134 86 1 66 67 EGADS : 213 0 Yes 135 134 1 67 95 EGADS : 214 0 Yes 135 87 1 67 68 EGADS : 215 0 Yes 131 135 1 68 95 EGADS : 216 0 Yes 129 136 1 69 96 EGADS : 217 0 Yes 136 88 1 69 70 EGADS : 218 0 Yes 137 136 1 70 96 EGADS : 219 0 Yes 137 89 1 70 71 EGADS : 220 0 Yes 127 137 1 71 96 EGADS : 221 0 Yes 138 139 1 74 97 EGADS : 222 0 Yes 139 95 1 74 75 EGADS : 223 0 Yes 138 94 1 74 79 EGADS : 224 0 Yes 140 139 1 75 97 EGADS : 225 0 Yes 140 96 1 75 76 EGADS : 226 0 Yes 141 140 1 76 97 EGADS : 227 0 Yes 141 97 1 76 77 EGADS : 228 0 Yes 142 141 1 77 98 EGADS : 229 0 Yes 142 98 1 77 78 EGADS : 230 0 Yes 142 143 1 78 98 EGADS : 231 0 Yes 143 99 1 78 79 EGADS : 232 0 Yes 143 138 1 79 98 EGADS : 233 0 Yes 144 145 1 80 99 EGADS : 234 0 Yes 145 100 1 80 92 EGADS : 235 0 Yes 144 101 1 80 81 EGADS : 236 0 Yes 144 146 1 81 99 EGADS : 237 0 Yes 146 102 1 81 82 EGADS : 238 0 Yes 146 147 1 82 99 EGADS : 239 0 Yes 147 103 1 82 90 EGADS : 240 0 Yes 107 109 1 84 85 EGADS : 241 0 Yes 113 115 1 86 89 EGADS : 242 0 Yes 117 119 1 87 88 EGADS : 243 0 Yes 147 148 1 90 100 EGADS : 244 0 Yes 148 124 1 90 91 EGADS : 245 0 Yes 149 148 1 91 100 EGADS : 246 0 Yes 149 125 1 91 92 EGADS : 247 0 Yes 145 149 1 92 100 EGADS : 248 0 Yes 127 129 1 93 96 EGADS : 249 0 Yes 131 133 1 94 95 EGADS : 250 0 Yes 141 138 1 97 98 EGADS : 251 0 Yes 145 147 1 99 100 EGADS : 252 1 Yes 150 151 1 101 102 EGADS : 253 1 Yes 152 153 1 101 102 EGADS : 254 1 Yes 150 152 1 101 103 EGADS : 255 1 Yes 151 153 1 101 103 EGADS : 256 1 Yes 152 150 1 102 104 EGADS : 257 1 Yes 153 151 1 102 104 EGADS : 258 1 Yes 150 151 1 103 104 EGADS : 259 1 Yes 152 153 1 103 104 EGADS : 260 2 Yes 154 155 1 105 106 EGADS : 261 2 Yes 156 157 1 105 106 EGADS : 262 2 Yes 154 156 1 105 107 EGADS : 263 2 Yes 155 157 1 105 107 EGADS : 264 2 Yes 156 154 1 106 108 EGADS : 265 2 Yes 157 155 1 106 108 EGADS : 266 2 Yes 154 155 1 107 108 EGADS : 267 2 Yes 156 157 1 107 108 EGADS : 268 3 Yes 159 158 NA 109 111 EGADS : 269 3 Yes 158 160 NA 109 114 EGADS : 270 3 Yes 161 160 NA 109 112 EGADS : 271 3 Yes 159 161 NA 109 113 EGADS : 272 3 Yes 163 162 NA 110 111 EGADS : 273 3 Yes 162 164 NA 110 114 EGADS : 274 3 Yes 165 164 NA 110 112 EGADS : 275 3 Yes 163 165 NA 110 113 EGADS : 276 3 Yes 159 163 NA 111 113 EGADS : 277 3 Yes 158 162 NA 111 114 EGADS : 278 3 Yes 161 165 NA 112 113 EGADS : 279 3 Yes 160 164 NA 112 114 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 138.735679 0 0 EGADS : 3 Yes 138.735679 10 0 EGADS : 4 Yes 91.4431034 10 0 EGADS : 5 Yes 101.394838 9.57026016 0 EGADS : 6 Yes 60.4564096 9.22070855 0 EGADS : 7 Yes 66.3702786 10 0 EGADS : 8 Yes 66.3702786 0 0 EGADS : 9 Yes 60.4564096 0 0 EGADS : 10 Yes 101.394838 0 0 EGADS : 11 Yes 91.4431034 0 0 EGADS : 12 Yes 138.735679 0 0 EGADS : 13 Yes 182.735679 0 7 EGADS : 14 Yes 182.735679 0.5 8.5 EGADS : 15 Yes 170.082709 3.23189118 6.05567631 EGADS : 16 Yes 173.917386 2.15088318 5.45718433 EGADS : 17 Yes 165.632409 4.19275142 5.19595925 EGADS : 18 Yes 138.735679 0 10 EGADS : 19 Yes 101.472983 13.4242093 0 EGADS : 20 Yes 97.4296648 13.4242093 0 EGADS : 21 Yes 97.813734 32.4820648 1.13332088 EGADS : 22 Yes 101.859411 32.4820648 0.137585788 EGADS : 23 Yes 101.933561 36.1389817 0.623232781 EGADS : 24 Yes 79.3047874 36.1389817 0 EGADS : 25 Yes 97.813734 32.4820648 0 EGADS : 26 Yes 97.4296648 13.4242093 0 EGADS : 27 Yes 101.472983 0 0 EGADS : 28 Yes 97.4296648 0 0 EGADS : 29 Yes 97.813734 0 1.13332088 EGADS : 30 Yes 101.859411 0 0.137585788 EGADS : 31 Yes 101.933561 0 0.623232781 EGADS : 32 Yes 79.3047874 0 0 EGADS : 33 Yes 97.813734 0 0 EGADS : 34 Yes 97.4296648 0 0 EGADS : 35 Yes 165.632409 0 5.19595925 EGADS : 36 Yes 173.917386 0 5.45718433 EGADS : 37 Yes 170.082709 0 6.05567631 EGADS : 38 Yes 182.735679 0 8.5 EGADS : 39 Yes 182.735679 0 10 EGADS : 40 Yes 152.352929 6.10042442 6.29668524 EGADS : 41 Yes 178.110679 0 10 EGADS : 42 Yes 153.398995 0 10 EGADS : 43 Yes 175.677695 6.9022299 6.46711426 EGADS : 44 Yes 166.04434 6.9022299 7.18470557 EGADS : 45 Yes 182.089548 35.660592 12.8876553 EGADS : 46 Yes 186.332272 35.660592 12.5798928 EGADS : 47 Yes 186.832635 37.0111495 12.8669627 EGADS : 48 Yes 178.290107 37.0111495 12.8669627 EGADS : 49 Yes 182.089548 35.660592 12.2721304 EGADS : 50 Yes 166.04434 6.9022299 5.74952294 EGADS : 51 Yes 97.9345512 13.6726922 0 EGADS : 52 Yes 101.285733 13.7821489 0 EGADS : 53 Yes 98.3601422 32.2302343 1.01304299 EGADS : 54 Yes 101.782457 32.3393376 0 EGADS : 55 Yes 104.269362 41.7493571 1.27010611 EGADS : 56 Yes 98.7284993 41.7493571 2.38400378 EGADS : 57 Yes 111.349293 67.6443173 4.84589548 EGADS : 58 Yes 115.050367 67.6443173 4.25578139 EGADS : 59 Yes 115.248847 68.1210465 4.31074802 EGADS : 60 Yes 111.581644 68.1210465 4.89111513 EGADS : 61 Yes 125.153699 95.9694651 7.50848923 EGADS : 62 Yes 126.843146 95.9694651 7.52165604 EGADS : 63 Yes 127.552357 97.6729236 7.7180639 EGADS : 64 Yes 122.391317 97.6729236 6.99272703 EGADS : 65 Yes 125.153699 95.9694651 7.20550678 EGADS : 66 Yes 111.581644 68.1210465 3.86588195 EGADS : 67 Yes 111.349293 67.6443173 3.80853718 EGADS : 68 Yes 98.7284993 41.7493571 0.691329618 EGADS : 69 Yes 98.0587466 32.2320648 0 EGADS : 70 Yes 97.6847537 13.6742093 0 EGADS : 71 Yes 152.352929 0 6.29668524 EGADS : 72 Yes 97.9345512 0 0 EGADS : 73 Yes 101.285733 0 0 EGADS : 74 Yes 98.3601422 0 1.01304299 EGADS : 75 Yes 101.782457 0 0 EGADS : 76 Yes 104.269362 0 1.27010611 EGADS : 77 Yes 98.7284993 0 2.38400378 EGADS : 78 Yes 111.349293 0 4.84589548 EGADS : 79 Yes 115.050367 0 4.25578139 EGADS : 80 Yes 115.248847 0 4.31074802 EGADS : 81 Yes 111.581644 0 4.89111513 EGADS : 82 Yes 125.153699 0 7.50848923 EGADS : 83 Yes 126.843146 0 7.52165604 EGADS : 84 Yes 127.552357 0 7.7180639 EGADS : 85 Yes 122.391317 0 6.99272703 EGADS : 86 Yes 125.153699 0 7.20550678 EGADS : 87 Yes 111.581644 0 3.86588195 EGADS : 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 = 21.7051 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 1060.6 AFLR4 : Abs Min Surf Spacing = 0.0542627 AFLR4 : Min Surf Spacing = 0.108525 AFLR4 : Max Surf Spacing = 2.17051 AFLR4 : Global Scale Factor = 2 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 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR4 : Define CAD surface definition 19 AFLR4 : Define CAD surface definition 20 AFLR4 : Define CAD surface definition 21 AFLR4 : Define CAD surface definition 22 AFLR4 : Define CAD surface definition 23 AFLR4 : Define CAD surface definition 24 AFLR4 : Define CAD surface definition 25 AFLR4 : Define CAD surface definition 26 AFLR4 : Define CAD surface definition 27 AFLR4 : Define CAD surface definition 28 AFLR4 : Define CAD surface definition 29 AFLR4 : Define CAD surface definition 30 AFLR4 : Define CAD surface definition 31 AFLR4 : Define CAD surface definition 32 AFLR4 : Define CAD surface definition 33 AFLR4 : Define CAD surface definition 34 AFLR4 : Define CAD surface definition 35 AFLR4 : Define CAD surface definition 36 AFLR4 : Define CAD surface definition 37 AFLR4 : Define CAD surface definition 38 AFLR4 : Define CAD surface definition 39 AFLR4 : Define CAD surface definition 40 AFLR4 : Define CAD surface definition 41 AFLR4 : Define CAD surface definition 42 AFLR4 : Define CAD surface definition 43 AFLR4 : Define CAD surface definition 44 AFLR4 : Define CAD surface definition 45 AFLR4 : Define CAD surface definition 46 AFLR4 : Define CAD surface definition 47 AFLR4 : Define CAD surface definition 48 AFLR4 : Define CAD surface definition 49 AFLR4 : Define CAD surface definition 50 AFLR4 : Define CAD surface definition 51 AFLR4 : Define CAD surface definition 52 AFLR4 : Define CAD surface definition 53 AFLR4 : Define CAD surface definition 54 AFLR4 : Define CAD surface definition 55 AFLR4 : Define CAD surface definition 56 AFLR4 : Define CAD surface definition 57 AFLR4 : Define CAD surface definition 58 AFLR4 : Define CAD surface definition 59 AFLR4 : Define CAD surface definition 60 AFLR4 : Define CAD surface definition 61 AFLR4 : Define CAD surface definition 62 AFLR4 : Define CAD surface definition 63 AFLR4 : Define CAD surface definition 64 AFLR4 : Define CAD surface definition 65 AFLR4 : Define CAD surface definition 66 AFLR4 : Define CAD surface definition 67 AFLR4 : Define CAD surface definition 68 AFLR4 : Define CAD surface definition 69 AFLR4 : Define CAD surface definition 70 AFLR4 : Define CAD surface definition 71 AFLR4 : Define CAD surface definition 72 AFLR4 : Define CAD surface definition 73 AFLR4 : Define CAD surface definition 74 AFLR4 : Define CAD surface definition 75 AFLR4 : Define CAD surface definition 76 AFLR4 : Define CAD surface definition 77 AFLR4 : Define CAD surface definition 78 AFLR4 : Define CAD surface definition 79 AFLR4 : Define CAD surface definition 80 AFLR4 : Define CAD surface definition 81 AFLR4 : Define CAD surface definition 82 AFLR4 : Define CAD surface definition 83 AFLR4 : Define CAD surface definition 84 AFLR4 : Define CAD surface definition 85 AFLR4 : Define CAD surface definition 86 AFLR4 : Define CAD surface definition 87 AFLR4 : Define CAD surface definition 88 AFLR4 : Define CAD surface definition 89 AFLR4 : Define CAD surface definition 90 AFLR4 : Define CAD surface definition 91 AFLR4 : Define CAD surface definition 92 AFLR4 : Define CAD surface definition 93 AFLR4 : Define CAD surface definition 94 AFLR4 : Define CAD surface definition 95 AFLR4 : Define CAD surface definition 96 AFLR4 : Define CAD surface definition 97 AFLR4 : Define CAD surface definition 98 AFLR4 : Define CAD surface definition 99 AFLR4 : Define CAD surface definition 100 AFLR4 : Define CAD surface definition 101 AFLR4 : Define CAD surface definition 102 AFLR4 : Define CAD surface definition 103 AFLR4 : Define CAD surface definition 104 AFLR4 : Define CAD surface definition 105 AFLR4 : Define CAD surface definition 106 AFLR4 : Define CAD surface definition 107 AFLR4 : Define CAD surface definition 108 AFLR4 : Define CAD surface definition 109 AFLR4 : Define CAD surface definition 110 AFLR4 : Define CAD surface definition 111 AFLR4 : Define CAD surface definition 112 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= 372 602 0 AFLR4 : Nodes, Trias,Quads= 377 612 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 374 606 0 AFLR4 : Nodes, Trias,Quads= 379 616 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 222 372 0 AFLR4 : Nodes, Trias,Quads= 154 236 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 269 430 0 AFLR4 : Nodes, Trias,Quads= 297 486 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1027 1883 0 AFLR4 : Nodes, Trias,Quads= 811 1451 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1253 2321 0 AFLR4 : Nodes, Trias,Quads= 1024 1863 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 269 430 0 AFLR4 : Nodes, Trias,Quads= 297 486 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 1036 1901 0 AFLR4 : Nodes, Trias,Quads= 831 1491 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 1253 2321 0 AFLR4 : Nodes, Trias,Quads= 1024 1863 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 227 382 0 AFLR4 : Nodes, Trias,Quads= 156 240 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 34 46 0 AFLR4 : Nodes, Trias,Quads= 32 42 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 862 1577 0 AFLR4 : Nodes, Trias,Quads= 586 1025 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 1470 2736 0 AFLR4 : Nodes, Trias,Quads= 925 1646 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 1449 2692 0 AFLR4 : Nodes, Trias,Quads= 956 1706 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 38 51 0 AFLR4 : Nodes, Trias,Quads= 40 55 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 94 124 0 AFLR4 : Nodes, Trias,Quads= 83 102 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= 3345 6360 0 AFLR4 : Nodes, Trias,Quads= 2083 3836 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 4005 7651 0 AFLR4 : Nodes, Trias,Quads= 2471 4583 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= 133 185 0 AFLR4 : Nodes, Trias,Quads= 130 179 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= 886 1625 0 AFLR4 : Nodes, Trias,Quads= 579 1011 0 AFLR4 : Generate optimal mesh on surface definition 24 AFLR2 : Nodes, Trias,Quads= 38 51 0 AFLR4 : Nodes, Trias,Quads= 40 55 0 AFLR4 : Generate optimal mesh on surface definition 25 AFLR2 : Nodes, Trias,Quads= 94 124 0 AFLR4 : Nodes, Trias,Quads= 83 102 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= 3394 6451 0 AFLR4 : Nodes, Trias,Quads= 2160 3983 0 AFLR4 : Generate optimal mesh on surface definition 28 AFLR2 : Nodes, Trias,Quads= 3803 7251 0 AFLR4 : Nodes, Trias,Quads= 2427 4499 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= 133 185 0 AFLR4 : Nodes, Trias,Quads= 134 187 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= 1450 2694 0 AFLR4 : Nodes, Trias,Quads= 944 1682 0 AFLR4 : Generate optimal mesh on surface definition 33 AFLR2 : Nodes, Trias,Quads= 1483 2762 0 AFLR4 : Nodes, Trias,Quads= 928 1652 0 AFLR4 : Generate optimal mesh on surface definition 34 AFLR2 : Nodes, Trias,Quads= 1540 2866 0 AFLR4 : Nodes, Trias,Quads= 939 1664 0 AFLR4 : Generate optimal mesh on surface definition 35 AFLR2 : Nodes, Trias,Quads= 50 65 0 AFLR4 : Nodes, Trias,Quads= 57 79 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= 30 38 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= 213 356 0 AFLR4 : Nodes, Trias,Quads= 197 324 0 AFLR4 : Generate optimal mesh on surface definition 43 AFLR2 : Nodes, Trias,Quads= 41 53 0 AFLR4 : Nodes, Trias,Quads= 49 69 0 AFLR4 : Generate optimal mesh on surface definition 44 AFLR2 : Nodes, Trias,Quads= 103 144 0 AFLR4 : Nodes, Trias,Quads= 60 58 0 AFLR4 : Generate optimal mesh on surface definition 45 AFLR2 : Nodes, Trias,Quads= 26 34 0 AFLR4 : Nodes, Trias,Quads= 27 36 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= 143 194 0 AFLR4 : Nodes, Trias,Quads= 130 168 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= 51 69 0 AFLR4 : Nodes, Trias,Quads= 48 63 0 AFLR4 : Generate optimal mesh on surface definition 54 AFLR2 : Nodes, Trias,Quads= 152 211 0 AFLR4 : Nodes, Trias,Quads= 92 91 0 AFLR4 : Generate optimal mesh on surface definition 55 AFLR2 : Nodes, Trias,Quads= 50 67 0 AFLR4 : Nodes, Trias,Quads= 50 67 0 AFLR4 : Generate optimal mesh on surface definition 56 AFLR2 : Nodes, Trias,Quads= 285 486 0 AFLR4 : Nodes, Trias,Quads= 266 448 0 AFLR4 : Generate optimal mesh on surface definition 57 AFLR2 : Nodes, Trias,Quads= 1531 2848 0 AFLR4 : Nodes, Trias,Quads= 935 1656 0 AFLR4 : Generate optimal mesh on surface definition 58 AFLR2 : Nodes, Trias,Quads= 213 356 0 AFLR4 : Nodes, Trias,Quads= 197 324 0 AFLR4 : Generate optimal mesh on surface definition 59 AFLR2 : Nodes, Trias,Quads= 41 53 0 AFLR4 : Nodes, Trias,Quads= 49 69 0 AFLR4 : Generate optimal mesh on surface definition 60 AFLR2 : Nodes, Trias,Quads= 103 144 0 AFLR4 : Nodes, Trias,Quads= 60 58 0 AFLR4 : Generate optimal mesh on surface definition 61 AFLR2 : Nodes, Trias,Quads= 26 34 0 AFLR4 : Nodes, Trias,Quads= 28 38 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= 33 41 0 AFLR4 : Nodes, Trias,Quads= 34 43 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= 143 194 0 AFLR4 : Nodes, Trias,Quads= 101 110 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= 50 67 0 AFLR4 : Nodes, Trias,Quads= 47 61 0 AFLR4 : Generate optimal mesh on surface definition 70 AFLR2 : Nodes, Trias,Quads= 152 211 0 AFLR4 : Nodes, Trias,Quads= 92 91 0 AFLR4 : Generate optimal mesh on surface definition 71 AFLR2 : Nodes, Trias,Quads= 50 67 0 AFLR4 : Nodes, Trias,Quads= 50 67 0 AFLR4 : Generate optimal mesh on surface definition 72 AFLR2 : Nodes, Trias,Quads= 285 486 0 AFLR4 : Nodes, Trias,Quads= 264 444 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= 50 65 0 AFLR4 : Nodes, Trias,Quads= 57 79 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= 30 38 0 AFLR4 : Nodes, Trias,Quads= 31 40 0 AFLR4 : Generate optimal mesh on surface definition 80 AFLR2 : Nodes, Trias,Quads= 64 87 0 AFLR4 : Nodes, Trias,Quads= 64 87 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= 308 532 0 AFLR4 : Nodes, Trias,Quads= 242 400 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= 195 322 0 AFLR4 : Nodes, Trias,Quads= 162 256 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= 307 521 0 AFLR4 : Nodes, Trias,Quads= 238 383 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= 64 87 0 AFLR4 : Nodes, Trias,Quads= 60 79 0 AFLR4 : Generate optimal mesh on surface definition 93 AFLR2 : Nodes, Trias,Quads= 195 322 0 AFLR4 : Nodes, Trias,Quads= 162 256 0 AFLR4 : Generate optimal mesh on surface definition 94 AFLR2 : Nodes, Trias,Quads= 330 552 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= 306 519 0 AFLR4 : Nodes, Trias,Quads= 237 381 0 AFLR4 : Generate optimal mesh on surface definition 97 AFLR2 : Nodes, Trias,Quads= 320 554 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= 246 408 0 AFLR4 : Generate optimal mesh on surface definition 99 AFLR2 : Nodes, Trias,Quads= 342 598 0 AFLR4 : Nodes, Trias,Quads= 273 460 0 AFLR4 : Generate optimal mesh on surface definition 100 AFLR2 : Nodes, Trias,Quads= 339 592 0 AFLR4 : Nodes, Trias,Quads= 269 452 0 AFLR4 : Generate optimal mesh on surface definition 101 AFLR2 : Nodes, Trias,Quads= 553 1009 0 AFLR4 : Nodes, Trias,Quads= 573 1049 0 AFLR4 : Generate optimal mesh on surface definition 102 AFLR2 : Nodes, Trias,Quads= 549 997 0 AFLR4 : Nodes, Trias,Quads= 465 829 0 AFLR4 : Generate optimal mesh on surface definition 103 AFLR2 : Nodes, Trias,Quads= 550 1003 0 AFLR4 : Nodes, Trias,Quads= 572 1047 0 AFLR4 : Generate optimal mesh on surface definition 104 AFLR2 : Nodes, Trias,Quads= 539 977 0 AFLR4 : Nodes, Trias,Quads= 461 821 0 AFLR4 : Generate optimal mesh on surface definition 105 AFLR2 : Nodes, Trias,Quads= 550 1003 0 AFLR4 : Nodes, Trias,Quads= 572 1047 0 AFLR4 : Generate optimal mesh on surface definition 106 AFLR2 : Nodes, Trias,Quads= 539 977 0 AFLR4 : Nodes, Trias,Quads= 461 821 0 AFLR4 : Generate optimal mesh on surface definition 107 AFLR2 : Nodes, Trias,Quads= 553 1009 0 AFLR4 : Nodes, Trias,Quads= 573 1049 0 AFLR4 : Generate optimal mesh on surface definition 108 AFLR2 : Nodes, Trias,Quads= 549 997 0 AFLR4 : Nodes, Trias,Quads= 465 829 0 AFLR4 : Generate optimal mesh on surface definition 109 AFLR2 : Nodes, Trias,Quads= 20 26 0 AFLR4 : Nodes, Trias,Quads= 16 18 0 AFLR4 : Generate optimal mesh on surface definition 110 AFLR2 : Nodes, Trias,Quads= 20 26 0 AFLR4 : Nodes, Trias,Quads= 16 18 0 AFLR4 : Generate optimal mesh on surface definition 111 AFLR2 : Nodes, Trias,Quads= 20 26 0 AFLR4 : Nodes, Trias,Quads= 16 18 0 AFLR4 : Generate optimal mesh on surface definition 112 AFLR2 : Nodes, Trias,Quads= 20 26 0 AFLR4 : Nodes, Trias,Quads= 16 18 0 AFLR4 : Generate optimal mesh on surface definition 113 AFLR2 : Nodes, Trias,Quads= 20 26 0 AFLR4 : Nodes, Trias,Quads= 16 18 0 AFLR4 : Generate optimal mesh on surface definition 114 AFLR2 : Nodes, Trias,Quads= 20 26 0 AFLR4 : Nodes, Trias,Quads= 16 18 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 28367 56726 9050 AFLR4 : Auto Mode Turned OFF OVERALL : CPU Time = 2.993 seconds Body 1 (of 4) Number of nodes = 24565 Number of elements = 49126 Number of triangle elements = 49126 Number of quadrilateral elements = 0 Body 2 (of 4) Number of nodes = 1873 Number of elements = 3746 Number of triangle elements = 3746 Number of quadrilateral elements = 0 Body 3 (of 4) Number of nodes = 1873 Number of elements = 3746 Number of triangle elements = 3746 Number of quadrilateral elements = 0 Body 4 (of 4) Number of nodes = 56 Number of elements = 108 Number of triangle elements = 108 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 28367 Total number of elements = 56726 1 file(s) copied. --> Toal Elements 56726 real 0m12.757s user 0m0.000s sys 0m0.062s + 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/7.8/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 1 file(s) copied. 1 file(s) copied. real 0m13.443s user 0m0.000s sys 0m0.077s + 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/7.8/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 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 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 triangle elements = 24443 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 11910 Total number of elements = 24443 1 file(s) copied. real 0m15.810s user 0m0.030s sys 0m0.077s + 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/7.8/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 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 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 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 triangle elements = 7671 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3546 Total number of elements = 7671 1 file(s) copied. real 0m14.769s user 0m0.015s sys 0m0.123s + 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/7.8/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 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 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 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 triangle elements = 13725 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 6580 Total number of elements = 13725 1 file(s) copied. real 0m15.621s user 0m0.015s sys 0m0.061s + 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/7.8/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 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 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 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 triangle elements = 91025 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 45179 Total number of elements = 91025 1 file(s) copied. real 0m19.976s user 0m0.046s sys 0m0.031s + 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/7.8/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 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 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 triangle elements = 0 Number of quadrilateral elements = 74322 ---------------------------- Total number of nodes = 72029 Total number of elements = 74322 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 = 1655 Number of elements = 3225 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 triangle elements = 0 Number of quadrilateral elements = 2928 ---------------------------- Total number of nodes = 3009 Total number of elements = 2928 1 file(s) copied. real 0m24.616s user 0m0.030s sys 0m0.092s + 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/7.8/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 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 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 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 triangle elements = 0 Number of quadrilateral elements = 6607 ---------------------------- Total number of nodes = 6181 Total number of elements = 6607 1 file(s) copied. real 0m15.088s user 0m0.015s sys 0m0.093s + 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/7.8/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 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 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 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 triangle elements = 0 Number of quadrilateral elements = 22191 ---------------------------- Total number of nodes = 22190 Total number of elements = 22191 1 file(s) copied. real 0m15.672s user 0m0.015s sys 0m0.061s + 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/7.8/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 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 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 0m12.432s user 0m0.031s sys 0m0.062s + 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/7.8/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 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 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 0m11.811s user 0m0.000s sys 0m0.077s + 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/7.8/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... 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 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 = 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 : 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 10: 0.466966 real 0m18.496s user 0m0.000s sys 0m0.061s + 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/7.8/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... 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 triangle elements = 0 Number of quadrilateral elements = 227 Body 2 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 236 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 = 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 : 0.0357647 2 : 0.0365801 3 : 0.102451 4 : 0.102453 5 : 0.159637 6 : 0.1611 7 : 0.215446 8 : 0.215462 9 : 0.350115 10: 0.351196 real 0m20.510s user 0m0.000s sys 0m0.186s + 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/7.8/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... 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 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 0m16.429s user 0m0.015s sys 0m0.061s + 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/7.8/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... 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 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 0m16.107s user 0m0.015s sys 0m0.092s + 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/7.8/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) Body 1 (of 4) Number of nodes = 11 Number of elements = 6 Number of triangle elements = 0 Number of quadrilateral elements = 6 Body 2 (of 4) Number of nodes = 11 Number of elements = 6 Number of triangle elements = 0 Number of quadrilateral elements = 6 Body 3 (of 4) Number of nodes = 11 Number of elements = 6 Number of triangle elements = 0 Number of quadrilateral elements = 6 Body 4 (of 4) Number of nodes = 939 Number of elements = 1094 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 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 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 Mass_Increment tuple is NULL - No mass increments 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 mass increment set Writing Nastran instruction file.... Warning: No loads specified for case Flutter!!!! Writing mass increment cards Writing aero card Writing analysis cards, 0 Writing constraint ADD cards Writing constraint cards Writing material cards Writing property cards Writing coordinate system cards Writing aeroelastic cards Done writing aeroelastic cards Done writing files ==> Running Nastran... 'nastran' is not recognized as an internal or external command, operable program or batch file. Traceback (most recent call last): File "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\training\WIN64.2019\CAPS\training\data\session10\nastran_5_Flutter.py", line 138, in <module> nastran.postAnalysis() File "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\training\WIN64.2019\CAPS\pyCAPS\pyCAPS\problem.py", line 2159, in postAnalysis self._analysisObj.postAnalysis() File "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\training\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\training\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 2914, in postAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\training\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_IOERR: ================================================================================ nastranAIM.c:3037 in aimPostAnalysis(): Error: Unable to open file: nastran_modal.f06 ================================================================================ real 0m15.350s user 0m0.015s sys 0m0.124s + status=1 + set +x ================================================= data/session10/nastran_5_Flutter.py failed (as NOT expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: session07 pointwise session08 su2 session08 fun3d session11 fun3d+astros session11 su2+astros ================================================= ================================================= Summary of examples NOT finished as expected data/session10/nastran_5_Flutter.py See training.log for more details. ================================================= Build step 'Conditional step (single)' marked build as failure [GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE' [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Skipped based on build state FAILURE Finished: FAILURE