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Full LogAFLR2 : Nodes, Trias,Quads= 158 267 0 AFLR4 : Nodes, Trias,Quads= 145 241 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 67 109 0 AFLR4 : Nodes, Trias,Quads= 45 65 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 26 36 0 AFLR4 : Nodes, Trias,Quads= 20 24 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 2793 5566 984 OVERALL : CPU Time = 0.430 seconds Body 1 (of 5) Number of nodes = 1595 Number of elements = 3186 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3186 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 301 Number of elements = 598 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 598 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 298 Number of elements = 592 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 592 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 301 Number of elements = 598 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 598 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 298 Number of elements = 592 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 592 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2793 Total number of elements = 5566 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = tableTopSide, index = 1 Name = leg0Side, index = 2 Name = leg1Side, index = 3 Name = leg2Side, index = 4 Name = leg3Side, index = 5 Getting volume mesh for body 1 (of 5) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR2 : Compile Date 11/21/22 @ 12:54PM 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 11.3.15 AFLR4 : Version Date 12/07/22 @ 10:53AM AFLR4 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR4 : Compile Date 12/11/22 @ 11:55AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 1.772 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1595 3186 462 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.36 AFLR3 : Version Date 11/20/22 @ 09:28PM AFLR3 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR3 : Compile Date 12/11/22 @ 11:52AM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 1595 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid UG3 : 5 Solid UG3 : 6 Solid AFLR3 : CPU Time = 0.006 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 1595 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 320 1689 AFLR3 IG : Nodes, Elements = 640 3362 AFLR3 IG : Nodes, Elements = 960 4997 AFLR3 IG : Nodes, Elements = 1280 6581 AFLR3 IG : Nodes, Elements = 1600 8125 AFLR3 IG : Nodes, Elements = 1602 8136 AFLR3 IG : Nodes, Elements = 1602 8097 AFLR3 IG : Nodes, Elements = 1595 4634 AFLR3 IG : Nodes, Elements = 1595 4673 AFLR3 IG : Nodes, Elements = 1595 4445 AFLR3 IG : Nodes, Elements = 1595 4438 AFLR3 : CPU Time = 0.040 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 1595 4438 AFLR3 GG : Nodes, Elements = 1920 5413 AFLR3 GG : Nodes, Elements = 1920 6730 AFLR3 GG : Nodes, Elements = 1920 6359 AFLR3 GG : Nodes, Elements = 2094 6881 AFLR3 GG : Nodes, Elements = 2094 7705 AFLR3 GG : Nodes, Elements = 2094 7426 AFLR3 GG : Nodes, Elements = 2148 7588 AFLR3 GG : Nodes, Elements = 2148 7831 AFLR3 GG : Nodes, Elements = 2148 7749 AFLR3 GG : Nodes, Elements = 2160 7785 AFLR3 GG : Nodes, Elements = 2160 7829 AFLR3 GG : Nodes, Elements = 2160 7816 AFLR3 GG : Nodes, Elements = 2162 7822 AFLR3 GG : Nodes, Elements = 2162 7826 AFLR3 : CPU Time = 0.043 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 2162 7826 AFLR3 QI : Nodes, Elements = 2161 7821 AFLR3 QI : Nodes, Elements = 2161 7853 AFLR3 QI : Nodes, Elements = 2161 7820 AFLR3 QI : Nodes, Elements = 2161 7795 AFLR3 QI : Nodes, Elements = 2161 7799 AFLR3 QI : Nodes, Elements = 2161 7792 AFLR3 QI : Nodes, Elements = 2161 7791 AFLR3 : CPU Time = 0.034 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 7791 UG3 : Min, Max Ang = 20.17 146.6 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.1 UG3 : No. Tet Elems = 7791 UG3 : Min Vol = 1.27e-06 UG3 : Average Vol = 1.28e-05 UG3 : Total-Tet-Vol = 0.1 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 7791 UG3 : Min, Max Q = 0.508 0.999 UG3 : Average Q = 0.86 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 7791 UG3 : Min, Max Ang = 20.17 146.6 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.1 UG3 : No. Tet Elems = 7791 UG3 : Min Vol = 1.27e-06 UG3 : Average Vol = 1.28e-05 UG3 : Total-Tet-Vol = 0.1 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 7791 UG3 : Min, Max Q = 0.522 1 UG3 : Average Q = 0.86 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 1.526 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6 Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.089 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 301 598 130 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 301 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid AFLR3 : CPU Time = 0.001 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 301 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 62 338 AFLR3 IG : Nodes, Elements = 124 736 AFLR3 IG : Nodes, Elements = 186 1135 AFLR3 IG : Nodes, Elements = 248 1546 AFLR3 IG : Nodes, Elements = 308 1953 AFLR3 IG : Nodes, Elements = 301 1093 AFLR3 IG : Nodes, Elements = 301 941 AFLR3 IG : Nodes, Elements = 301 829 AFLR3 : CPU Time = 0.006 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 301 829 AFLR3 GG : Nodes, Elements = 349 973 AFLR3 GG : Nodes, Elements = 349 1076 AFLR3 GG : Nodes, Elements = 349 1030 AFLR3 GG : Nodes, Elements = 382 1129 AFLR3 GG : Nodes, Elements = 382 1292 AFLR3 GG : Nodes, Elements = 382 1245 AFLR3 GG : Nodes, Elements = 399 1296 AFLR3 GG : Nodes, Elements = 399 1370 AFLR3 GG : Nodes, Elements = 399 1349 AFLR3 GG : Nodes, Elements = 408 1376 AFLR3 GG : Nodes, Elements = 408 1409 AFLR3 GG : Nodes, Elements = 408 1393 AFLR3 GG : Nodes, Elements = 411 1402 AFLR3 GG : Nodes, Elements = 411 1411 AFLR3 GG : Nodes, Elements = 411 1410 AFLR3 : CPU Time = 0.005 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 411 1410 AFLR3 QI : Nodes, Elements = 411 1425 AFLR3 QI : Nodes, Elements = 411 1412 AFLR3 QI : Nodes, Elements = 411 1410 AFLR3 QI : Nodes, Elements = 411 1411 AFLR3 QI : Nodes, Elements = 411 1409 AFLR3 : CPU Time = 0.002 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1409 UG3 : Min, Max Ang = 19.95 147.8 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1409 UG3 : Min Vol = 1.17e-06 UG3 : Average Vol = 1.3e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 1409 UG3 : Min, Max Q = 0.497 0.997 UG3 : Average Q = 0.86 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1409 UG3 : Min, Max Ang = 19.95 147.8 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1409 UG3 : Min Vol = 1.17e-06 UG3 : Average Vol = 1.3e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 1409 UG3 : Min, Max Q = 0.556 1 UG3 : Average Q = 0.87 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.089 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.103 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 298 592 130 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 298 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid AFLR3 : CPU Time = 0.001 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 298 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 62 343 AFLR3 IG : Nodes, Elements = 124 749 AFLR3 IG : Nodes, Elements = 186 1146 AFLR3 IG : Nodes, Elements = 248 1560 AFLR3 IG : Nodes, Elements = 305 1937 AFLR3 IG : Nodes, Elements = 298 1080 AFLR3 IG : Nodes, Elements = 298 937 AFLR3 IG : Nodes, Elements = 298 819 AFLR3 : CPU Time = 0.006 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 298 819 AFLR3 GG : Nodes, Elements = 342 951 AFLR3 GG : Nodes, Elements = 342 1044 AFLR3 GG : Nodes, Elements = 342 983 AFLR3 GG : Nodes, Elements = 376 1085 AFLR3 GG : Nodes, Elements = 376 1256 AFLR3 GG : Nodes, Elements = 376 1209 AFLR3 GG : Nodes, Elements = 395 1266 AFLR3 GG : Nodes, Elements = 395 1349 AFLR3 GG : Nodes, Elements = 395 1321 AFLR3 GG : Nodes, Elements = 401 1339 AFLR3 GG : Nodes, Elements = 401 1364 AFLR3 GG : Nodes, Elements = 401 1352 AFLR3 GG : Nodes, Elements = 403 1358 AFLR3 GG : Nodes, Elements = 403 1368 AFLR3 GG : Nodes, Elements = 403 1363 AFLR3 GG : Nodes, Elements = 405 1369 AFLR3 GG : Nodes, Elements = 405 1377 AFLR3 GG : Nodes, Elements = 405 1374 AFLR3 : CPU Time = 0.005 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 405 1374 AFLR3 QI : Nodes, Elements = 405 1381 AFLR3 QI : Nodes, Elements = 405 1375 AFLR3 QI : Nodes, Elements = 405 1372 AFLR3 QI : Nodes, Elements = 405 1376 AFLR3 QI : Nodes, Elements = 405 1369 AFLR3 : CPU Time = 0.002 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1369 UG3 : Min, Max Ang = 21.02 132.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1369 UG3 : Min Vol = 1.15e-06 UG3 : Average Vol = 1.34e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 1369 UG3 : Min, Max Q = 0.578 0.999 UG3 : Average Q = 0.858 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1369 UG3 : Min, Max Ang = 21.02 132.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1369 UG3 : Min Vol = 1.15e-06 UG3 : Average Vol = 1.34e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 1369 UG3 : Min, Max Q = 0.661 1 UG3 : Average Q = 0.873 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.110 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.089 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 301 598 130 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 301 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid AFLR3 : CPU Time = 0.001 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 301 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 62 337 AFLR3 IG : Nodes, Elements = 124 738 AFLR3 IG : Nodes, Elements = 186 1163 AFLR3 IG : Nodes, Elements = 248 1543 AFLR3 IG : Nodes, Elements = 308 1980 AFLR3 IG : Nodes, Elements = 301 1112 AFLR3 IG : Nodes, Elements = 301 972 AFLR3 IG : Nodes, Elements = 301 823 AFLR3 : CPU Time = 0.006 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 301 823 AFLR3 GG : Nodes, Elements = 354 982 AFLR3 GG : Nodes, Elements = 354 1132 AFLR3 GG : Nodes, Elements = 354 1056 AFLR3 GG : Nodes, Elements = 382 1140 AFLR3 GG : Nodes, Elements = 382 1293 AFLR3 GG : Nodes, Elements = 382 1237 AFLR3 GG : Nodes, Elements = 399 1288 AFLR3 GG : Nodes, Elements = 399 1362 AFLR3 GG : Nodes, Elements = 399 1336 AFLR3 GG : Nodes, Elements = 405 1354 AFLR3 GG : Nodes, Elements = 405 1386 AFLR3 GG : Nodes, Elements = 405 1370 AFLR3 GG : Nodes, Elements = 410 1385 AFLR3 GG : Nodes, Elements = 410 1399 AFLR3 GG : Nodes, Elements = 410 1398 AFLR3 : CPU Time = 0.005 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 410 1398 AFLR3 QI : Nodes, Elements = 410 1405 AFLR3 QI : Nodes, Elements = 410 1398 AFLR3 QI : Nodes, Elements = 410 1393 AFLR3 QI : Nodes, Elements = 410 1394 AFLR3 QI : Nodes, Elements = 410 1392 AFLR3 : CPU Time = 0.002 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1392 UG3 : Min, Max Ang = 13.52 154.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1392 UG3 : Min Vol = 1.15e-06 UG3 : Average Vol = 1.32e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 1392 UG3 : Min, Max Q = 0.419 0.998 UG3 : Average Q = 0.863 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1392 UG3 : Min, Max Ang = 13.52 154.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1392 UG3 : Min Vol = 1.15e-06 UG3 : Average Vol = 1.32e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 1392 UG3 : Min, Max Q = 0.495 1 UG3 : Average Q = 0.88 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.089 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.118 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 298 592 132 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 298 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid AFLR3 : CPU Time = 0.001 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 298 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 62 334 AFLR3 IG : Nodes, Elements = 124 726 AFLR3 IG : Nodes, Elements = 186 1151 AFLR3 IG : Nodes, Elements = 248 1547 AFLR3 IG : Nodes, Elements = 305 1919 AFLR3 IG : Nodes, Elements = 298 1076 AFLR3 IG : Nodes, Elements = 298 931 AFLR3 IG : Nodes, Elements = 298 822 AFLR3 : CPU Time = 0.006 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 298 822 AFLR3 GG : Nodes, Elements = 349 975 AFLR3 GG : Nodes, Elements = 349 1115 AFLR3 GG : Nodes, Elements = 349 1047 AFLR3 GG : Nodes, Elements = 383 1149 AFLR3 GG : Nodes, Elements = 383 1311 AFLR3 GG : Nodes, Elements = 383 1254 AFLR3 GG : Nodes, Elements = 399 1302 AFLR3 GG : Nodes, Elements = 399 1374 AFLR3 GG : Nodes, Elements = 399 1350 AFLR3 GG : Nodes, Elements = 403 1362 AFLR3 GG : Nodes, Elements = 403 1377 AFLR3 GG : Nodes, Elements = 403 1376 AFLR3 : CPU Time = 0.005 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 403 1376 AFLR3 QI : Nodes, Elements = 402 1370 AFLR3 QI : Nodes, Elements = 402 1376 AFLR3 QI : Nodes, Elements = 402 1371 AFLR3 QI : Nodes, Elements = 402 1365 AFLR3 QI : Nodes, Elements = 402 1368 AFLR3 QI : Nodes, Elements = 402 1364 AFLR3 QI : Nodes, Elements = 402 1363 AFLR3 : CPU Time = 0.002 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1363 UG3 : Min, Max Ang = 21.47 133.3 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1363 UG3 : Min Vol = 1.71e-06 UG3 : Average Vol = 1.35e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 1363 UG3 : Min, Max Q = 0.599 0.999 UG3 : Average Q = 0.859 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1363 UG3 : Min, Max Ang = 21.47 133.3 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1363 UG3 : Min Vol = 1.71e-06 UG3 : Average Vol = 1.35e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 1363 UG3 : Min, Max Q = 0.649 1 UG3 : Average Q = 0.878 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.106 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 Volume mesh: Number of nodes = 3789 Number of elements = 18890 Number of triangles = 5566 Number of quadrilatarals = 0 Number of tetrahedrals = 13324 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing VTK file: volume.vtk.... Finished writing VTK file Writing exodus file .... Block: 'tableTop', blk_id 1, num_entries 7791 Block: 'leg0', blk_id 2, num_entries 1409 Block: 'leg1', blk_id 3, num_entries 1369 Block: 'leg2', blk_id 4, num_entries 1392 Block: 'leg3', blk_id 5, num_entries 1363 Sideset: 'leg0Side', set_id 1, num_entries 598 Sideset: 'leg1Side', set_id 2, num_entries 592 Sideset: 'leg2Side', set_id 3, num_entries 598 Sideset: 'leg3Side', set_id 4, num_entries 592 Sideset: 'tableTopSide', set_id 5, num_entries 3186 Nodeset: 'edge', set_id 1, num_entries 25 Nodeset: 'face1', set_id 2, num_entries 244 Nodeset: 'face2', set_id 3, num_entries 248 Nodeset: 'node', set_id 4, num_entries 1 Finished writing Exodus file real 0m6.034s user 0m5.744s sys 0m0.576s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case plato_aflr_table_PyTest.py passed (as expected) ================================================= ================================================= + echo 'plato_aflr_table_morph_PyTest.py test;' + tee -a /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt plato_aflr_table_morph_PyTest.py test; + python -u plato_aflr_table_morph_PyTest.py -outLevel=0 + tee -a /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = tableTopSide, index = 1 Name = leg0Side, index = 2 Name = leg1Side, index = 3 Name = leg2Side, index = 4 Name = leg3Side, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR2 : Compile Date 11/21/22 @ 12:54PM 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 11.3.15 AFLR4 : Version Date 12/07/22 @ 10:53AM AFLR4 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR4 : Compile Date 12/11/22 @ 11:55AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 5 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 12 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 8 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 4 Faces EGADS : Body 1 has 6 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 6 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 4 Faces EGADS : Body 3 has 6 Edges EGADS : Body 3 has 4 Loops EGADS : Body 3 has 4 Nodes EGADS : Body 4 is a SolidBody EGADS : Body 4 has 1 Shells EGADS : Body 4 has 4 Faces EGADS : Body 4 has 6 Edges EGADS : Body 4 has 4 Loops EGADS : Body 4 has 4 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 3 4 5 6 EGADS : 2 Yes 0 0 1 0 1 3 4 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 5 6 EGADS : 4 Yes 0 0 1 0 1 1 2 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 3 4 EGADS : 6 Yes 0 0 1 0 1 1 2 3 4 EGADS : 7 Yes 1 0 1 0 1 8 9 10 EGADS : 8 Yes 1 0 1 0 1 7 9 10 EGADS : 9 Yes 1 0 1 0 1 7 8 EGADS : 10 Yes 1 0 1 0 1 7 8 EGADS : 11 Yes 2 0 1 0 1 12 13 14 EGADS : 12 Yes 2 0 1 0 1 11 13 14 EGADS : 13 Yes 2 0 1 0 1 11 12 EGADS : 14 Yes 2 0 1 0 1 11 12 EGADS : 15 Yes 3 0 1 0 1 16 17 18 EGADS : 16 Yes 3 0 1 0 1 15 17 18 EGADS : 17 Yes 3 0 1 0 1 15 16 EGADS : 18 Yes 3 0 1 0 1 15 16 EGADS : 19 Yes 4 0 1 0 1 20 21 22 EGADS : 20 Yes 4 0 1 0 1 19 21 22 EGADS : 21 Yes 4 0 1 0 1 19 20 EGADS : 22 Yes 4 0 1 0 1 19 20 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 -5 8 7 -6 EGADS : 3 9 5 -10 -1 EGADS : 4 -11 3 12 -7 EGADS : 5 4 11 -8 -9 EGADS : 6 -2 10 6 -12 EGADS : 7 -13 -14 15 16 EGADS : 8 17 14 -18 -16 EGADS : 9 13 18 EGADS : 10 -15 -17 EGADS : 11 -19 -20 21 22 EGADS : 12 23 20 -24 -22 EGADS : 13 19 24 EGADS : 14 -21 -23 EGADS : 15 -25 -26 27 28 EGADS : 16 29 26 -30 -28 EGADS : 17 25 30 EGADS : 18 -27 -29 EGADS : 19 -31 -32 33 34 EGADS : 20 35 32 -36 -34 EGADS : 21 31 36 EGADS : 22 -33 -35 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 : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 1 2 -3 -4 EGADS : 2 Yes 1 -5 8 7 -6 EGADS : 3 Yes 1 9 5 -10 -1 EGADS : 4 Yes 1 -11 3 12 -7 EGADS : 5 Yes 1 4 11 -8 -9 EGADS : 6 Yes 1 -2 10 6 -12 EGADS : 7 Yes 1 -13 -14 15 16 EGADS : 8 Yes 1 17 14 -18 -16 EGADS : 9 Yes 1 13 18 EGADS : 10 Yes 1 -15 -17 EGADS : 11 Yes 1 -19 -20 21 22 EGADS : 12 Yes 1 23 20 -24 -22 EGADS : 13 Yes 1 19 24 EGADS : 14 Yes 1 -21 -23 EGADS : 15 Yes 1 -25 -26 27 28 EGADS : 16 Yes 1 29 26 -30 -28 EGADS : 17 Yes 1 25 30 EGADS : 18 Yes 1 -27 -29 EGADS : 19 Yes 1 -31 -32 33 34 EGADS : 20 Yes 1 35 32 -36 -34 EGADS : 21 Yes 1 31 36 EGADS : 22 Yes 1 -33 -35 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 2 1 1 1 3 EGADS : 2 0 Yes 1 3 1 1 6 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 6 5 1 2 3 EGADS : 6 0 Yes 5 7 1 2 6 EGADS : 7 0 Yes 8 7 1 2 4 EGADS : 8 0 Yes 6 8 1 2 5 EGADS : 9 0 Yes 2 6 1 3 5 EGADS : 10 0 Yes 1 5 1 3 6 EGADS : 11 0 Yes 4 8 1 4 5 EGADS : 12 0 Yes 3 7 1 4 6 EGADS : 13 1 Yes 10 9 1 7 9 EGADS : 14 1 Yes 11 10 1 7 8 EGADS : 15 1 Yes 11 12 1 7 10 EGADS : 16 1 Yes 12 9 1 7 8 EGADS : 17 1 Yes 12 11 1 8 10 EGADS : 18 1 Yes 9 10 1 8 9 EGADS : 19 2 Yes 14 13 1 11 13 EGADS : 20 2 Yes 15 14 1 11 12 EGADS : 21 2 Yes 15 16 1 11 14 EGADS : 22 2 Yes 16 13 1 11 12 EGADS : 23 2 Yes 16 15 1 12 14 EGADS : 24 2 Yes 13 14 1 12 13 EGADS : 25 3 Yes 18 17 1 15 17 EGADS : 26 3 Yes 19 18 1 15 16 EGADS : 27 3 Yes 19 20 1 15 18 EGADS : 28 3 Yes 20 17 1 15 16 EGADS : 29 3 Yes 20 19 1 16 18 EGADS : 30 3 Yes 17 18 1 16 17 EGADS : 31 4 Yes 22 21 1 19 21 EGADS : 32 4 Yes 23 22 1 19 20 EGADS : 33 4 Yes 23 24 1 19 22 EGADS : 34 4 Yes 24 21 1 19 20 EGADS : 35 4 Yes 24 23 1 20 22 EGADS : 36 4 Yes 21 22 1 20 21 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0.5 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 0.1 0.5 EGADS : 4 Yes 0 0.1 0 EGADS : 5 Yes 0.5 0 0.5 EGADS : 6 Yes 0.5 0 0 EGADS : 7 Yes 0.5 0.1 0.5 EGADS : 8 Yes 0.5 0.1 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 0 0 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 0 0.26 EGADS : 14 Yes 0 0 0.46 EGADS : 15 Yes 0 0 0.46 EGADS : 16 Yes 0 0 0.26 EGADS : 17 Yes 0.36 0 0.26 EGADS : 18 Yes 0.36 0 0.46 EGADS : 19 Yes 0.36 0 0.46 EGADS : 20 Yes 0.36 0 0.26 EGADS : 21 Yes 0.36 0 0 EGADS : 22 Yes 0.36 0 0 EGADS : 23 Yes 0.36 0 0 EGADS : 24 Yes 0.36 0 0 AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 1 AFLR4 : Min Bounding Box Length = 0.7 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 0.7 AFLR4 : Reference Length = 10 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.025 AFLR4 : Min Surf Spacing = 0.05 AFLR4 : Max Surf Spacing = 1 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : 15 CAD geometry 0 STD w/BL AFLR4 : 16 CAD geometry 0 STD w/BL AFLR4 : 17 CAD geometry 0 STD w/BL AFLR4 : 18 CAD geometry 0 STD w/BL AFLR4 : 19 CAD geometry 0 STD w/BL AFLR4 : 20 CAD geometry 0 STD w/BL AFLR4 : 21 CAD geometry 0 STD w/BL AFLR4 : 22 CAD geometry 0 STD w/BL AFLR4 : Case has 5 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 AFLR4 : Component 2 includes Definitions 7 8 9 10 AFLR4 : Component 3 includes Definitions 11 12 13 14 AFLR4 : Component 4 includes Definitions 15 16 17 18 AFLR4 : Component 5 includes Definitions 19 20 21 22 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 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 9 10 0 AFLR4 : Nodes, Trias,Quads= 6 4 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 9 10 0 AFLR4 : Nodes, Trias,Quads= 6 4 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 9 10 0 AFLR4 : Nodes, Trias,Quads= 6 4 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 9 10 0 AFLR4 : Nodes, Trias,Quads= 6 4 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 118 194 0 AFLR4 : Nodes, Trias,Quads= 117 192 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 118 194 0 AFLR4 : Nodes, Trias,Quads= 117 192 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 30 42 0 AFLR4 : Nodes, Trias,Quads= 22 26 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 31 44 0 AFLR4 : Nodes, Trias,Quads= 23 28 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 118 194 0 AFLR4 : Nodes, Trias,Quads= 117 192 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 118 194 0 AFLR4 : Nodes, Trias,Quads= 117 192 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 30 42 0 AFLR4 : Nodes, Trias,Quads= 22 26 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 31 44 0 AFLR4 : Nodes, Trias,Quads= 23 28 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 118 194 0 AFLR4 : Nodes, Trias,Quads= 117 192 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 118 194 0 AFLR4 : Nodes, Trias,Quads= 117 192 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 30 42 0 AFLR4 : Nodes, Trias,Quads= 22 26 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 31 44 0 AFLR4 : Nodes, Trias,Quads= 23 28 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 118 194 0 AFLR4 : Nodes, Trias,Quads= 117 192 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 118 194 0 AFLR4 : Nodes, Trias,Quads= 117 192 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 30 42 0 AFLR4 : Nodes, Trias,Quads= 22 26 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 31 44 0 AFLR4 : Nodes, Trias,Quads= 23 28 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 900 1780 488 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Trias = 900 1780 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 7 5 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 7 5 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 15 18 0 AFLR4 : Nodes, Trias,Quads= 11 10 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 15 18 0 AFLR4 : Nodes, Trias,Quads= 11 10 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 7 5 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 7 5 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 126 210 0 AFLR4 : Nodes, Trias,Quads= 120 198 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 126 210 0 AFLR4 : Nodes, Trias,Quads= 120 198 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 25 34 0 AFLR4 : Nodes, Trias,Quads= 21 26 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 25 34 0 AFLR4 : Nodes, Trias,Quads= 21 26 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 126 210 0 AFLR4 : Nodes, Trias,Quads= 120 198 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 126 210 0 AFLR4 : Nodes, Trias,Quads= 120 198 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 25 34 0 AFLR4 : Nodes, Trias,Quads= 21 26 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 25 34 0 AFLR4 : Nodes, Trias,Quads= 21 26 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 126 210 0 AFLR4 : Nodes, Trias,Quads= 120 198 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 126 210 0 AFLR4 : Nodes, Trias,Quads= 120 198 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 25 34 0 AFLR4 : Nodes, Trias,Quads= 21 26 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 25 34 0 AFLR4 : Nodes, Trias,Quads= 21 26 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 126 210 0 AFLR4 : Nodes, Trias,Quads= 120 198 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 126 210 0 AFLR4 : Nodes, Trias,Quads= 120 198 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 25 34 0 AFLR4 : Nodes, Trias,Quads= 21 26 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 25 34 0 AFLR4 : Nodes, Trias,Quads= 21 26 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 926 1832 480 AFLR4 : Proximity BG Surface Grid Generation AFLR4 : Nodes, Trias = 986 1952 AFLR4 : Nodes, Trias = 1206 2392 AFLR4 : Nodes, Trias = 1760 3500 AFLR4 : Nodes, Trias = 2067 4114 AFLR4 : Nodes, Trias = 2106 4192 AFLR4 : Nodes, Trias = 2108 4196 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 110 160 0 AFLR4 : Nodes, Trias,Quads= 120 180 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 119 175 0 AFLR4 : Nodes, Trias,Quads= 126 189 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 992 1859 0 AFLR4 : Nodes, Trias,Quads= 706 1287 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 625 1152 0 AFLR4 : Nodes, Trias,Quads= 618 1138 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 115 167 0 AFLR4 : Nodes, Trias,Quads= 128 193 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 127 189 0 AFLR4 : Nodes, Trias,Quads= 132 199 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 155 262 0 AFLR4 : Nodes, Trias,Quads= 145 242 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 165 280 0 AFLR4 : Nodes, Trias,Quads= 156 262 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 62 100 0 AFLR4 : Nodes, Trias,Quads= 47 70 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 26 36 0 AFLR4 : Nodes, Trias,Quads= 20 24 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 154 260 0 AFLR4 : Nodes, Trias,Quads= 144 240 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 168 286 0 AFLR4 : Nodes, Trias,Quads= 154 258 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 63 102 0 AFLR4 : Nodes, Trias,Quads= 47 70 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 26 36 0 AFLR4 : Nodes, Trias,Quads= 20 24 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 163 276 0 AFLR4 : Nodes, Trias,Quads= 156 262 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 155 262 0 AFLR4 : Nodes, Trias,Quads= 145 242 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 63 102 0 AFLR4 : Nodes, Trias,Quads= 47 70 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 26 36 0 AFLR4 : Nodes, Trias,Quads= 20 24 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 166 282 0 AFLR4 : Nodes, Trias,Quads= 156 262 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 158 267 0 AFLR4 : Nodes, Trias,Quads= 145 241 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 67 109 0 AFLR4 : Nodes, Trias,Quads= 45 65 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 26 36 0 AFLR4 : Nodes, Trias,Quads= 20 24 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 2793 5566 984 OVERALL : CPU Time = 0.486 seconds Body 1 (of 5) Number of nodes = 1595 Number of elements = 3186 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3186 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 301 Number of elements = 598 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 598 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 298 Number of elements = 592 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 592 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 301 Number of elements = 598 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 598 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 298 Number of elements = 592 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 592 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2793 Total number of elements = 5566 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = tableTopSide, index = 1 Name = leg0Side, index = 2 Name = leg1Side, index = 3 Name = leg2Side, index = 4 Name = leg3Side, index = 5 Getting volume mesh for body 1 (of 5) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR2 : Compile Date 11/21/22 @ 12:54PM 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 11.3.15 AFLR4 : Version Date 12/07/22 @ 10:53AM AFLR4 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR4 : Compile Date 12/11/22 @ 11:55AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 1.493 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1595 3186 462 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.36 AFLR3 : Version Date 11/20/22 @ 09:28PM AFLR3 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR3 : Compile Date 12/11/22 @ 11:52AM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 1595 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid UG3 : 5 Solid UG3 : 6 Solid AFLR3 : CPU Time = 0.005 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 1595 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 320 1689 AFLR3 IG : Nodes, Elements = 640 3362 AFLR3 IG : Nodes, Elements = 960 4997 AFLR3 IG : Nodes, Elements = 1280 6581 AFLR3 IG : Nodes, Elements = 1600 8125 AFLR3 IG : Nodes, Elements = 1602 8136 AFLR3 IG : Nodes, Elements = 1602 8097 AFLR3 IG : Nodes, Elements = 1595 4634 AFLR3 IG : Nodes, Elements = 1595 4673 AFLR3 IG : Nodes, Elements = 1595 4445 AFLR3 IG : Nodes, Elements = 1595 4438 AFLR3 : CPU Time = 0.102 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 1595 4438 AFLR3 GG : Nodes, Elements = 1920 5413 AFLR3 GG : Nodes, Elements = 1920 6730 AFLR3 GG : Nodes, Elements = 1920 6359 AFLR3 GG : Nodes, Elements = 2094 6881 AFLR3 GG : Nodes, Elements = 2094 7705 AFLR3 GG : Nodes, Elements = 2094 7426 AFLR3 GG : Nodes, Elements = 2148 7588 AFLR3 GG : Nodes, Elements = 2148 7831 AFLR3 GG : Nodes, Elements = 2148 7749 AFLR3 GG : Nodes, Elements = 2160 7785 AFLR3 GG : Nodes, Elements = 2160 7829 AFLR3 GG : Nodes, Elements = 2160 7816 AFLR3 GG : Nodes, Elements = 2162 7822 AFLR3 GG : Nodes, Elements = 2162 7826 AFLR3 : CPU Time = 0.053 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 2162 7826 AFLR3 QI : Nodes, Elements = 2161 7821 AFLR3 QI : Nodes, Elements = 2161 7853 AFLR3 QI : Nodes, Elements = 2161 7820 AFLR3 QI : Nodes, Elements = 2161 7795 AFLR3 QI : Nodes, Elements = 2161 7799 AFLR3 QI : Nodes, Elements = 2161 7792 AFLR3 QI : Nodes, Elements = 2161 7791 AFLR3 : CPU Time = 0.033 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 7791 UG3 : Min, Max Ang = 20.17 146.6 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.1 UG3 : No. Tet Elems = 7791 UG3 : Min Vol = 1.27e-06 UG3 : Average Vol = 1.28e-05 UG3 : Total-Tet-Vol = 0.1 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 7791 UG3 : Min, Max Q = 0.508 0.999 UG3 : Average Q = 0.86 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 7791 UG3 : Min, Max Ang = 20.17 146.6 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.1 UG3 : No. Tet Elems = 7791 UG3 : Min Vol = 1.27e-06 UG3 : Average Vol = 1.28e-05 UG3 : Total-Tet-Vol = 0.1 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 7791 UG3 : Min, Max Q = 0.522 1 UG3 : Average Q = 0.86 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 1.744 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6 Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.139 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 301 598 130 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 301 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid AFLR3 : CPU Time = 0.002 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 301 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 62 338 AFLR3 IG : Nodes, Elements = 124 736 AFLR3 IG : Nodes, Elements = 186 1135 AFLR3 IG : Nodes, Elements = 248 1546 AFLR3 IG : Nodes, Elements = 308 1953 AFLR3 IG : Nodes, Elements = 301 1093 AFLR3 IG : Nodes, Elements = 301 941 AFLR3 IG : Nodes, Elements = 301 829 AFLR3 : CPU Time = 0.009 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 301 829 AFLR3 GG : Nodes, Elements = 349 973 AFLR3 GG : Nodes, Elements = 349 1076 AFLR3 GG : Nodes, Elements = 349 1030 AFLR3 GG : Nodes, Elements = 382 1129 AFLR3 GG : Nodes, Elements = 382 1292 AFLR3 GG : Nodes, Elements = 382 1245 AFLR3 GG : Nodes, Elements = 399 1296 AFLR3 GG : Nodes, Elements = 399 1370 AFLR3 GG : Nodes, Elements = 399 1349 AFLR3 GG : Nodes, Elements = 408 1376 AFLR3 GG : Nodes, Elements = 408 1409 AFLR3 GG : Nodes, Elements = 408 1393 AFLR3 GG : Nodes, Elements = 411 1402 AFLR3 GG : Nodes, Elements = 411 1411 AFLR3 GG : Nodes, Elements = 411 1410 AFLR3 : CPU Time = 0.015 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 411 1410 AFLR3 QI : Nodes, Elements = 411 1425 AFLR3 QI : Nodes, Elements = 411 1412 AFLR3 QI : Nodes, Elements = 411 1410 AFLR3 QI : Nodes, Elements = 411 1411 AFLR3 QI : Nodes, Elements = 411 1409 AFLR3 : CPU Time = 0.004 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1409 UG3 : Min, Max Ang = 19.95 147.8 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1409 UG3 : Min Vol = 1.17e-06 UG3 : Average Vol = 1.3e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 1409 UG3 : Min, Max Q = 0.497 0.997 UG3 : Average Q = 0.86 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1409 UG3 : Min, Max Ang = 19.95 147.8 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1409 UG3 : Min Vol = 1.17e-06 UG3 : Average Vol = 1.3e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 1409 UG3 : Min, Max Q = 0.556 1 UG3 : Average Q = 0.87 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.147 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.114 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 298 592 130 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 298 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid AFLR3 : CPU Time = 0.001 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 298 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 62 343 AFLR3 IG : Nodes, Elements = 124 749 AFLR3 IG : Nodes, Elements = 186 1146 AFLR3 IG : Nodes, Elements = 248 1560 AFLR3 IG : Nodes, Elements = 305 1937 AFLR3 IG : Nodes, Elements = 298 1080 AFLR3 IG : Nodes, Elements = 298 937 AFLR3 IG : Nodes, Elements = 298 819 AFLR3 : CPU Time = 0.007 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 298 819 AFLR3 GG : Nodes, Elements = 342 951 AFLR3 GG : Nodes, Elements = 342 1044 AFLR3 GG : Nodes, Elements = 342 983 AFLR3 GG : Nodes, Elements = 376 1085 AFLR3 GG : Nodes, Elements = 376 1256 AFLR3 GG : Nodes, Elements = 376 1209 AFLR3 GG : Nodes, Elements = 395 1266 AFLR3 GG : Nodes, Elements = 395 1349 AFLR3 GG : Nodes, Elements = 395 1321 AFLR3 GG : Nodes, Elements = 401 1339 AFLR3 GG : Nodes, Elements = 401 1364 AFLR3 GG : Nodes, Elements = 401 1352 AFLR3 GG : Nodes, Elements = 403 1358 AFLR3 GG : Nodes, Elements = 403 1368 AFLR3 GG : Nodes, Elements = 403 1363 AFLR3 GG : Nodes, Elements = 405 1369 AFLR3 GG : Nodes, Elements = 405 1377 AFLR3 GG : Nodes, Elements = 405 1374 AFLR3 : CPU Time = 0.006 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 405 1374 AFLR3 QI : Nodes, Elements = 405 1381 AFLR3 QI : Nodes, Elements = 405 1375 AFLR3 QI : Nodes, Elements = 405 1372 AFLR3 QI : Nodes, Elements = 405 1376 AFLR3 QI : Nodes, Elements = 405 1369 AFLR3 : CPU Time = 0.003 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1369 UG3 : Min, Max Ang = 21.02 132.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1369 UG3 : Min Vol = 1.15e-06 UG3 : Average Vol = 1.34e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 1369 UG3 : Min, Max Q = 0.578 0.999 UG3 : Average Q = 0.858 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1369 UG3 : Min, Max Ang = 21.02 132.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1369 UG3 : Min Vol = 1.15e-06 UG3 : Average Vol = 1.34e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 1369 UG3 : Min, Max Q = 0.661 1 UG3 : Average Q = 0.873 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.112 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.113 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 301 598 130 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 301 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid AFLR3 : CPU Time = 0.001 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 301 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 62 337 AFLR3 IG : Nodes, Elements = 124 738 AFLR3 IG : Nodes, Elements = 186 1163 AFLR3 IG : Nodes, Elements = 248 1543 AFLR3 IG : Nodes, Elements = 308 1980 AFLR3 IG : Nodes, Elements = 301 1112 AFLR3 IG : Nodes, Elements = 301 972 AFLR3 IG : Nodes, Elements = 301 823 AFLR3 : CPU Time = 0.007 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 301 823 AFLR3 GG : Nodes, Elements = 354 982 AFLR3 GG : Nodes, Elements = 354 1132 AFLR3 GG : Nodes, Elements = 354 1056 AFLR3 GG : Nodes, Elements = 382 1140 AFLR3 GG : Nodes, Elements = 382 1293 AFLR3 GG : Nodes, Elements = 382 1237 AFLR3 GG : Nodes, Elements = 399 1288 AFLR3 GG : Nodes, Elements = 399 1362 AFLR3 GG : Nodes, Elements = 399 1336 AFLR3 GG : Nodes, Elements = 405 1354 AFLR3 GG : Nodes, Elements = 405 1386 AFLR3 GG : Nodes, Elements = 405 1370 AFLR3 GG : Nodes, Elements = 410 1385 AFLR3 GG : Nodes, Elements = 410 1399 AFLR3 GG : Nodes, Elements = 410 1398 AFLR3 : CPU Time = 0.007 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 410 1398 AFLR3 QI : Nodes, Elements = 410 1405 AFLR3 QI : Nodes, Elements = 410 1398 AFLR3 QI : Nodes, Elements = 410 1393 AFLR3 QI : Nodes, Elements = 410 1394 AFLR3 QI : Nodes, Elements = 410 1392 AFLR3 : CPU Time = 0.002 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1392 UG3 : Min, Max Ang = 13.52 154.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1392 UG3 : Min Vol = 1.15e-06 UG3 : Average Vol = 1.32e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 1392 UG3 : Min, Max Q = 0.419 0.998 UG3 : Average Q = 0.863 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1392 UG3 : Min, Max Ang = 13.52 154.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1392 UG3 : Min Vol = 1.15e-06 UG3 : Average Vol = 1.32e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 1392 UG3 : Min, Max Q = 0.495 1 UG3 : Average Q = 0.88 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.124 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.101 seconds DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 298 592 132 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 298 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid AFLR3 : CPU Time = 0.002 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 298 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 62 334 AFLR3 IG : Nodes, Elements = 124 726 AFLR3 IG : Nodes, Elements = 186 1151 AFLR3 IG : Nodes, Elements = 248 1547 AFLR3 IG : Nodes, Elements = 305 1919 AFLR3 IG : Nodes, Elements = 298 1076 AFLR3 IG : Nodes, Elements = 298 931 AFLR3 IG : Nodes, Elements = 298 822 AFLR3 : CPU Time = 0.007 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 298 822 AFLR3 GG : Nodes, Elements = 349 975 AFLR3 GG : Nodes, Elements = 349 1115 AFLR3 GG : Nodes, Elements = 349 1047 AFLR3 GG : Nodes, Elements = 383 1149 AFLR3 GG : Nodes, Elements = 383 1311 AFLR3 GG : Nodes, Elements = 383 1254 AFLR3 GG : Nodes, Elements = 399 1302 AFLR3 GG : Nodes, Elements = 399 1374 AFLR3 GG : Nodes, Elements = 399 1350 AFLR3 GG : Nodes, Elements = 403 1362 AFLR3 GG : Nodes, Elements = 403 1377 AFLR3 GG : Nodes, Elements = 403 1376 AFLR3 : CPU Time = 0.008 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 403 1376 AFLR3 QI : Nodes, Elements = 402 1370 AFLR3 QI : Nodes, Elements = 402 1376 AFLR3 QI : Nodes, Elements = 402 1371 AFLR3 QI : Nodes, Elements = 402 1365 AFLR3 QI : Nodes, Elements = 402 1368 AFLR3 QI : Nodes, Elements = 402 1364 AFLR3 QI : Nodes, Elements = 402 1363 AFLR3 : CPU Time = 0.003 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1363 UG3 : Min, Max Ang = 21.47 133.3 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1363 UG3 : Min Vol = 1.71e-06 UG3 : Average Vol = 1.35e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 1363 UG3 : Min, Max Q = 0.599 0.999 UG3 : Average Q = 0.859 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 1363 UG3 : Min, Max Ang = 21.47 133.3 UG3 : Average Angle = 70.1 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 0.0184 UG3 : No. Tet Elems = 1363 UG3 : Min Vol = 1.71e-06 UG3 : Average Vol = 1.35e-05 UG3 : Total-Tet-Vol = 0.0184 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 1363 UG3 : Min, Max Q = 0.649 1 UG3 : Average Q = 0.878 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- OVERALL : CPU Time = 0.149 seconds EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 Volume mesh: Number of nodes = 3789 Number of elements = 18890 Number of triangles = 5566 Number of quadrilatarals = 0 Number of tetrahedrals = 13324 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Writing exodus file .... Block: 'tableTop', blk_id 1, num_entries 7791 Block: 'leg0', blk_id 2, num_entries 1409 Block: 'leg1', blk_id 3, num_entries 1369 Block: 'leg2', blk_id 4, num_entries 1392 Block: 'leg3', blk_id 5, num_entries 1363 Sideset: 'leg0Side', set_id 1, num_entries 598 Sideset: 'leg1Side', set_id 2, num_entries 592 Sideset: 'leg2Side', set_id 3, num_entries 598 Sideset: 'leg3Side', set_id 4, num_entries 592 Sideset: 'tableTopSide', set_id 5, num_entries 3186 Nodeset: 'edge', set_id 1, num_entries 25 Nodeset: 'face1', set_id 2, num_entries 244 Nodeset: 'face2', set_id 3, num_entries 248 Nodeset: 'node', set_id 4, num_entries 1 Finished writing Exodus file Projecting tessellation 1 (of 5) on to new body Projecting tessellation 2 (of 5) on to new body Projecting tessellation 3 (of 5) on to new body Projecting tessellation 4 (of 5) on to new body Projecting tessellation 5 (of 5) on to new body real 0m6.756s user 0m6.130s sys 0m0.461s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case plato_aflr_table_morph_PyTest.py passed (as expected) ================================================= ================================================= + echo 'plato_tetgen_table_PyTest.py test;' + tee -a /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt plato_tetgen_table_PyTest.py test; + python -u plato_tetgen_table_PyTest.py -outLevel=0 + tee -a /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = tableTopSide, index = 1 Name = leg0Side, index = 2 Name = leg1Side, index = 3 Name = leg2Side, index = 4 Name = leg3Side, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 5) Getting surface mesh for body 2 (of 5) Getting surface mesh for body 3 (of 5) Getting surface mesh for body 4 (of 5) Getting surface mesh for body 5 (of 5) Body 1 (of 5) Number of nodes = 642 Number of elements = 1280 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1280 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 1070 Number of elements = 2136 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2136 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 1070 Number of elements = 2136 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2136 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 1070 Number of elements = 2136 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2136 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 1070 Number of elements = 2136 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2136 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4922 Total number of elements = 9824 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = tableTopSide, index = 1 Name = leg0Side, index = 2 Name = leg1Side, index = 3 Name = leg2Side, index = 4 Name = leg3Side, index = 5 Body 1 number of surface: nodes - 642, elements - 1280 Body 2 number of surface: nodes - 1070, elements - 2136 Body 3 number of surface: nodes - 1070, elements - 2136 Body 4 number of surface: nodes - 1070, elements - 2136 Body 5 number of surface: nodes - 1070, elements - 2136 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.04272 Creating surface mesh ... Surface mesh seconds: 0.003388 Recovering boundaries... Boundary recovery seconds: 0.012194 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.001194 Recovering Delaunayness... Delaunay recovery seconds: 0.012405 Refining mesh... Refinement seconds: 0.00202 Improving mesh... Mesh improvement seconds: 0.003263 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000687 Total running seconds: 0.078037 Statistics: Input points: 642 Input facets: 1280 Input segments: 1920 Input holes: 0 Input regions: 1 Mesh points: 642 Mesh tetrahedra: 1722 Mesh faces: 4084 Mesh faces on exterior boundary: 1280 Mesh faces on input facets: 1280 Mesh edges on input segments: 1920 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.239919 Creating surface mesh ... Surface mesh seconds: 0.006376 Recovering boundaries... Boundary recovery seconds: 0.029917 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.006656 Recovering Delaunayness... Delaunay recovery seconds: 0.073066 Refining mesh... Refinement seconds: 0.233487 Smoothing vertices... Mesh smoothing seconds: 0.199325 Improving mesh... Mesh improvement seconds: 0.01338 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.00185 Total running seconds: 0.804306 Statistics: Input points: 1070 Input facets: 2136 Input segments: 3204 Input holes: 0 Input regions: 2 Mesh points: 1315 Mesh tetrahedra: 4460 Mesh faces: 9988 Mesh faces on exterior boundary: 2136 Mesh faces on input facets: 2136 Mesh edges on input segments: 3204 Steiner points inside domain: 245 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.24897 Creating surface mesh ... Surface mesh seconds: 0.007629 Recovering boundaries... Boundary recovery seconds: 0.017855 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.00591 Recovering Delaunayness... Delaunay recovery seconds: 0.075559 Refining mesh... Refinement seconds: 0.247117 Smoothing vertices... Mesh smoothing seconds: 0.212406 Improving mesh... Mesh improvement seconds: 0.012969 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001749 Total running seconds: 0.830442 Statistics: Input points: 1070 Input facets: 2136 Input segments: 3204 Input holes: 0 Input regions: 3 Mesh points: 1314 Mesh tetrahedra: 4436 Mesh faces: 9940 Mesh faces on exterior boundary: 2136 Mesh faces on input facets: 2136 Mesh edges on input segments: 3204 Steiner points inside domain: 244 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.246873 Creating surface mesh ... Surface mesh seconds: 0.00666 Recovering boundaries... Boundary recovery seconds: 0.0173 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.005495 Recovering Delaunayness... Delaunay recovery seconds: 0.073357 Refining mesh... Refinement seconds: 0.14415 Smoothing vertices... Mesh smoothing seconds: 0.128111 Improving mesh... Mesh improvement seconds: 0.006759 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001041 Total running seconds: 0.630029 Statistics: Input points: 1070 Input facets: 2136 Input segments: 3204 Input holes: 0 Input regions: 4 Mesh points: 1317 Mesh tetrahedra: 4459 Mesh faces: 9986 Mesh faces on exterior boundary: 2136 Mesh faces on input facets: 2136 Mesh edges on input segments: 3204 Steiner points inside domain: 247 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.161269 Creating surface mesh ... Surface mesh seconds: 0.003427 Recovering boundaries... Boundary recovery seconds: 0.010684 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.004816 Recovering Delaunayness... Delaunay recovery seconds: 0.049566 Refining mesh... Refinement seconds: 0.181715 Smoothing vertices... Mesh smoothing seconds: 0.158441 Improving mesh... Mesh improvement seconds: 0.008591 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001306 Total running seconds: 0.58002 Statistics: Input points: 1070 Input facets: 2136 Input segments: 3204 Input holes: 0 Input regions: 5 Mesh points: 1312 Mesh tetrahedra: 4414 Mesh faces: 9896 Mesh faces on exterior boundary: 2136 Mesh faces on input facets: 2136 Mesh edges on input segments: 3204 Steiner points inside domain: 242 Done meshing using TetGen! Writing VTK file: volume.vtk.... Finished writing VTK file Writing exodus file .... Block: 'tableTop', blk_id 1, num_entries 1722 Block: 'leg0', blk_id 2, num_entries 4460 Block: 'leg1', blk_id 3, num_entries 4436 Block: 'leg2', blk_id 4, num_entries 4459 Block: 'leg3', blk_id 5, num_entries 4414 Sideset: 'leg0Side', set_id 1, num_entries 2136 Sideset: 'leg1Side', set_id 2, num_entries 2136 Sideset: 'leg2Side', set_id 3, num_entries 2136 Sideset: 'leg3Side', set_id 4, num_entries 2136 Sideset: 'tableTopSide', set_id 5, num_entries 1280 Nodeset: 'edge', set_id 1, num_entries 17 Nodeset: 'face1', set_id 2, num_entries 99 Nodeset: 'face2', set_id 3, num_entries 99 Nodeset: 'node', set_id 4, num_entries 1 Finished writing Exodus file real 0m5.769s user 0m5.743s sys 0m0.552s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case plato_tetgen_table_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt + echo 'plato_tetgen_cyli_box_PyTest.py test;' plato_tetgen_cyli_box_PyTest.py test; + tee -a /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt + python -u plato_tetgen_cyli_box_PyTest.py -outLevel=0 EGADS Warning: Loop 2 marked with -1 EGADS Warning: Loop 2 marked with -1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = box, index = 1 Name = cyl2, index = 2 Name = box;cyl2, index = 3 Name = cyl1, index = 4 Name = cyl1;box;cyl2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 3603 Number of elements = 7330 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 7330 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3603 Total number of elements = 7330 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = box, index = 1 Name = cyl2, index = 2 Name = box;cyl2, index = 3 Name = cyl1, index = 4 Name = cyl1;box;cyl2, index = 5 Number of surface: nodes - 3603, elements - 7330 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.510129 Creating surface mesh ... Surface mesh seconds: 0.020022 Recovering boundaries... Boundary recovery seconds: 0.073045 Removing exterior tetrahedra ... Warning: The 3-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.005342 Recovering Delaunayness... Delaunay recovery seconds: 0.336914 Refining mesh... Refinement seconds: 0.87503 Smoothing vertices... Mesh smoothing seconds: 1.06317 Improving mesh... Mesh improvement seconds: 0.07021 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.007553 Total running seconds: 2.96205 Statistics: Input points: 3603 Input facets: 7330 Input segments: 10931 Input holes: 0 Input regions: 3 Mesh points: 5634 Mesh tetrahedra: 29520 Mesh faces: 60657 Mesh faces on exterior boundary: 3234 Mesh faces on input facets: 7330 Mesh edges on input segments: 10931 Steiner points inside domain: 2031 Done meshing using TetGen! Writing VTK file: volume.vtk.... Finished writing VTK file Writing exodus file .... Block: 'c', blk_id 3, num_entries 12838 Block: 'b', blk_id 2, num_entries 11116 Block: 'a', blk_id 1, num_entries 5566 Sideset: 'box', set_id 1, num_entries 3234 Sideset: 'cyl1', set_id 2, num_entries 2120 Sideset: 'cyl2', set_id 3, num_entries 2314 Finished writing Exodus file real 0m8.025s user 0m7.453s sys 0m0.407s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case plato_tetgen_cyli_box_PyTest.py passed (as expected) ================================================= ================================================= + echo 'plato_aflr_tetgen_table_PyTest.py test;' + tee -a /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt plato_aflr_tetgen_table_PyTest.py test; + python -u plato_aflr_tetgen_table_PyTest.py -outLevel=0 + tee -a /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = tableTopSide, index = 1 Name = leg0Side, index = 2 Name = leg1Side, index = 3 Name = leg2Side, index = 4 Name = leg3Side, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR2 : Compile Date 11/21/22 @ 12:54PM 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 11.3.15 AFLR4 : Version Date 12/07/22 @ 10:53AM AFLR4 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64 AFLR4 : Compile Date 12/11/22 @ 11:55AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.6.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 5 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 12 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 8 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 4 Faces EGADS : Body 1 has 6 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 6 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 4 Faces EGADS : Body 3 has 6 Edges EGADS : Body 3 has 4 Loops EGADS : Body 3 has 4 Nodes EGADS : Body 4 is a SolidBody EGADS : Body 4 has 1 Shells EGADS : Body 4 has 4 Faces EGADS : Body 4 has 6 Edges EGADS : Body 4 has 4 Loops EGADS : Body 4 has 4 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 3 4 5 6 EGADS : 2 Yes 0 0 1 0 1 3 4 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 5 6 EGADS : 4 Yes 0 0 1 0 1 1 2 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 3 4 EGADS : 6 Yes 0 0 1 0 1 1 2 3 4 EGADS : 7 Yes 1 0 1 0 1 8 9 10 EGADS : 8 Yes 1 0 1 0 1 7 9 10 EGADS : 9 Yes 1 0 1 0 1 7 8 EGADS : 10 Yes 1 0 1 0 1 7 8 EGADS : 11 Yes 2 0 1 0 1 12 13 14 EGADS : 12 Yes 2 0 1 0 1 11 13 14 EGADS : 13 Yes 2 0 1 0 1 11 12 EGADS : 14 Yes 2 0 1 0 1 11 12 EGADS : 15 Yes 3 0 1 0 1 16 17 18 EGADS : 16 Yes 3 0 1 0 1 15 17 18 EGADS : 17 Yes 3 0 1 0 1 15 16 EGADS : 18 Yes 3 0 1 0 1 15 16 EGADS : 19 Yes 4 0 1 0 1 20 21 22 EGADS : 20 Yes 4 0 1 0 1 19 21 22 EGADS : 21 Yes 4 0 1 0 1 19 20 EGADS : 22 Yes 4 0 1 0 1 19 20 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 -5 8 7 -6 EGADS : 3 9 5 -10 -1 EGADS : 4 -11 3 12 -7 EGADS : 5 4 11 -8 -9 EGADS : 6 -2 10 6 -12 EGADS : 7 -13 -14 15 16 EGADS : 8 17 14 -18 -16 EGADS : 9 13 18 EGADS : 10 -15 -17 EGADS : 11 -19 -20 21 22 EGADS : 12 23 20 -24 -22 EGADS : 13 19 24 EGADS : 14 -21 -23 EGADS : 15 -25 -26 27 28 EGADS : 16 29 26 -30 -28 EGADS : 17 25 30 EGADS : 18 -27 -29 EGADS : 19 -31 -32 33 34 EGADS : 20 35 32 -36 -34 EGADS : 21 31 36 EGADS : 22 -33 -35 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 : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 1 2 -3 -4 EGADS : 2 Yes 1 -5 8 7 -6 EGADS : 3 Yes 1 9 5 -10 -1 EGADS : 4 Yes 1 -11 3 12 -7 EGADS : 5 Yes 1 4 11 -8 -9 EGADS : 6 Yes 1 -2 10 6 -12 EGADS : 7 Yes 1 -13 -14 15 16 EGADS : 8 Yes 1 17 14 -18 -16 EGADS : 9 Yes 1 13 18 EGADS : 10 Yes 1 -15 -17 EGADS : 11 Yes 1 -19 -20 21 22 EGADS : 12 Yes 1 23 20 -24 -22 EGADS : 13 Yes 1 19 24 EGADS : 14 Yes 1 -21 -23 EGADS : 15 Yes 1 -25 -26 27 28 EGADS : 16 Yes 1 29 26 -30 -28 EGADS : 17 Yes 1 25 30 EGADS : 18 Yes 1 -27 -29 EGADS : 19 Yes 1 -31 -32 33 34 EGADS : 20 Yes 1 35 32 -36 -34 EGADS : 21 Yes 1 31 36 EGADS : 22 Yes 1 -33 -35 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 2 1 1 1 3 EGADS : 2 0 Yes 1 3 1 1 6 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 6 5 1 2 3 EGADS : 6 0 Yes 5 7 1 2 6 EGADS : 7 0 Yes 8 7 1 2 4 EGADS : 8 0 Yes 6 8 1 2 5 EGADS : 9 0 Yes 2 6 1 3 5 EGADS : 10 0 Yes 1 5 1 3 6 EGADS : 11 0 Yes 4 8 1 4 5 EGADS : 12 0 Yes 3 7 1 4 6 EGADS : 13 1 Yes 10 9 1 7 9 EGADS : 14 1 Yes 11 10 1 7 8 EGADS : 15 1 Yes 11 12 1 7 10 EGADS : 16 1 Yes 12 9 1 7 8 EGADS : 17 1 Yes 12 11 1 8 10 EGADS : 18 1 Yes 9 10 1 8 9 EGADS : 19 2 Yes 14 13 1 11 13 EGADS : 20 2 Yes 15 14 1 11 12 EGADS : 21 2 Yes 15 16 1 11 14 EGADS : 22 2 Yes 16 13 1 11 12 EGADS : 23 2 Yes 16 15 1 12 14 EGADS : 24 2 Yes 13 14 1 12 13 EGADS : 25 3 Yes 18 17 1 15 17 EGADS : 26 3 Yes 19 18 1 15 16 EGADS : 27 3 Yes 19 20 1 15 18 EGADS : 28 3 Yes 20 17 1 15 16 EGADS : 29 3 Yes 20 19 1 16 18 EGADS : 30 3 Yes 17 18 1 16 17 EGADS : 31 4 Yes 22 21 1 19 21 EGADS : 32 4 Yes 23 22 1 19 20 EGADS : 33 4 Yes 23 24 1 19 22 EGADS : 34 4 Yes 24 21 1 19 20 EGADS : 35 4 Yes 24 23 1 20 22 EGADS : 36 4 Yes 21 22 1 20 21 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0.5 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 0.1 0.5 EGADS : 4 Yes 0 0.1 0 EGADS : 5 Yes 0.5 0 0.5 EGADS : 6 Yes 0.5 0 0 EGADS : 7 Yes 0.5 0.1 0.5 EGADS : 8 Yes 0.5 0.1 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 0 0 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 0 0.26 EGADS : 14 Yes 0 0 0.46 EGADS : 15 Yes 0 0 0.46 EGADS : 16 Yes 0 0 0.26 EGADS : 17 Yes 0.36 0 0.26 EGADS : 18 Yes 0.36 0 0.46 EGADS : 19 Yes 0.36 0 0.46 EGADS : 20 Yes 0.36 0 0.26 EGADS : 21 Yes 0.36 0 0 EGADS : 22 Yes 0.36 0 0 EGADS : 23 Yes 0.36 0 0 EGADS : 24 Yes 0.36 0 0 AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 1 AFLR4 : Min Bounding Box Length = 0.7 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 0.7 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.005 AFLR4 : Max Surf Spacing = 0.1 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : 15 CAD geometry 0 STD w/BL AFLR4 : 16 CAD geometry 0 STD w/BL AFLR4 : 17 CAD geometry 0 STD w/BL AFLR4 : 18 CAD geometry 0 STD w/BL AFLR4 : 19 CAD geometry 0 STD w/BL AFLR4 : 20 CAD geometry 0 STD w/BL AFLR4 : 21 CAD geometry 0 STD w/BL AFLR4 : 22 CAD geometry 0 STD w/BL AFLR4 : Case has 5 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 AFLR4 : Component 2 includes Definitions 7 8 9 10 AFLR4 : Component 3 includes Definitions 11 12 13 14 AFLR4 : Component 4 includes Definitions 15 16 17 18 AFLR4 : Component 5 includes Definitions 19 20 21 22 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 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 49 64 0 AFLR4 : Nodes, Trias,Quads= 34 34 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 49 64 0 AFLR4 : Nodes, Trias,Quads= 34 34 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 229 400 0 AFLR4 : Nodes, Trias,Quads= 212 366 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 230 402 0 AFLR4 : Nodes, Trias,Quads= 212 366 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 49 64 0 AFLR4 : Nodes, Trias,Quads= 34 34 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 49 64 0 AFLR4 : Nodes, Trias,Quads= 34 34 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2258 4330 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2259 4332 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 515 964 0 AFLR4 : Nodes, Trias,Quads= 413 760 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 402 738 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2258 4330 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2259 4332 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 515 964 0 AFLR4 : Nodes, Trias,Quads= 413 760 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 402 738 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2258 4330 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2259 4332 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 515 964 0 AFLR4 : Nodes, Trias,Quads= 413 760 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 402 738 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2258 4330 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2259 4332 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 515 964 0 AFLR4 : Nodes, Trias,Quads= 413 760 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 402 738 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 20764 41508 2224 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Trias = 20764 41508 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Nodes, Trias,Quads= 30 28 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Nodes, Trias,Quads= 30 28 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 201 348 0 AFLR4 : Nodes, Trias,Quads= 193 332 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 204 354 0 AFLR4 : Nodes, Trias,Quads= 193 332 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Nodes, Trias,Quads= 30 28 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Nodes, Trias,Quads= 30 28 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Nodes, Trias,Quads= 2244 4302 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 496 926 0 AFLR4 : Nodes, Trias,Quads= 416 766 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 502 938 0 AFLR4 : Nodes, Trias,Quads= 408 750 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Nodes, Trias,Quads= 2243 4300 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Nodes, Trias,Quads= 2249 4312 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 496 926 0 AFLR4 : Nodes, Trias,Quads= 416 766 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 502 938 0 AFLR4 : Nodes, Trias,Quads= 408 750 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Nodes, Trias,Quads= 2244 4302 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Nodes, Trias,Quads= 2249 4312 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 496 926 0 AFLR4 : Nodes, Trias,Quads= 416 766 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 502 938 0 AFLR4 : Nodes, Trias,Quads= 408 750 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Nodes, Trias,Quads= 2244 4302 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Nodes, Trias,Quads= 2246 4306 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 496 926 0 AFLR4 : Nodes, Trias,Quads= 416 766 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 502 938 0 AFLR4 : Nodes, Trias,Quads= 408 750 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 20653 41286 2208 AFLR4 : Proximity BG Surface Grid Generation AFLR4 : Nodes, Trias = 21566 43112 AFLR4 : Nodes, Trias = 22450 44880 AFLR4 : Nodes, Trias = 22542 45064 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 311 517 0 AFLR4 : Nodes, Trias,Quads= 309 513 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 313 521 0 AFLR4 : Nodes, Trias,Quads= 309 513 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3277 6339 0 AFLR4 : Nodes, Trias,Quads= 1431 2647 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1864 3566 0 AFLR4 : Nodes, Trias,Quads= 1736 3310 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 315 525 0 AFLR4 : Nodes, Trias,Quads= 307 509 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 318 530 0 AFLR4 : Nodes, Trias,Quads= 314 522 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 2301 4412 0 AFLR4 : Nodes, Trias,Quads= 2272 4354 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 2302 4414 0 AFLR4 : Nodes, Trias,Quads= 2275 4360 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 548 1028 0 AFLR4 : Nodes, Trias,Quads= 423 778 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 549 1030 0 AFLR4 : Nodes, Trias,Quads= 418 768 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 2301 4412 0 AFLR4 : Nodes, Trias,Quads= 2272 4354 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 2302 4414 0 AFLR4 : Nodes, Trias,Quads= 2276 4362 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 548 1028 0 AFLR4 : Nodes, Trias,Quads= 423 778 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 549 1030 0 AFLR4 : Nodes, Trias,Quads= 418 768 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 2301 4412 0 AFLR4 : Nodes, Trias,Quads= 2272 4354 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 2302 4414 0 AFLR4 : Nodes, Trias,Quads= 2275 4360 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 548 1028 0 AFLR4 : Nodes, Trias,Quads= 423 778 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 549 1030 0 AFLR4 : Nodes, Trias,Quads= 418 768 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 2301 4412 0 AFLR4 : Nodes, Trias,Quads= 2271 4352 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 2302 4414 0 AFLR4 : Nodes, Trias,Quads= 2274 4358 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 548 1028 0 AFLR4 : Nodes, Trias,Quads= 423 778 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 549 1030 0 AFLR4 : Nodes, Trias,Quads= 418 768 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 24536 49052 2818 OVERALL : CPU Time = 2.149 seconds Body 1 (of 5) Number of nodes = 4009 Number of elements = 8014 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 8014 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 5132 Number of elements = 10260 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 10260 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 5133 Number of elements = 10262 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 10262 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 5132 Number of elements = 10260 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 10260 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 5130 Number of elements = 10256 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 10256 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 24536 Total number of elements = 49052 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = tableTopSide, index = 1 Name = leg0Side, index = 2 Name = leg1Side, index = 3 Name = leg2Side, index = 4 Name = leg3Side, index = 5 Body 1 number of surface: nodes - 4009, elements - 8014 Body 2 number of surface: nodes - 5132, elements - 10260 Body 3 number of surface: nodes - 5133, elements - 10262 Body 4 number of surface: nodes - 5132, elements - 10260 Body 5 number of surface: nodes - 5130, elements - 10256 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.065549 Creating surface mesh ... Surface mesh seconds: 0.015381 Recovering boundaries... Boundary recovery seconds: 0.0304 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.005412 Recovering Delaunayness... Delaunay recovery seconds: 0.009387 Refining mesh... Refinement seconds: 0.109613 Smoothing vertices... Mesh smoothing seconds: 0.244784 Improving mesh... Mesh improvement seconds: 0.03288 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.004412 Total running seconds: 0.51822 Statistics: Input points: 4009 Input facets: 8014 Input segments: 12021 Input holes: 0 Input regions: 1 Mesh points: 4773 Mesh tetrahedra: 15871 Mesh faces: 35749 Mesh faces on exterior boundary: 8014 Mesh faces on input facets: 8014 Mesh edges on input segments: 12021 Steiner points inside domain: 764 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.179335 Creating surface mesh ... Surface mesh seconds: 0.029439 Recovering boundaries... Boundary recovery seconds: 0.089577 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.047345 Recovering Delaunayness... Delaunay recovery seconds: 0.03582 Refining mesh... Refinement seconds: 0.412773 Smoothing vertices... Mesh smoothing seconds: 0.343275 Improving mesh... Mesh improvement seconds: 0.038633 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.007763 Total running seconds: 1.18448 Statistics: Input points: 5132 Input facets: 10260 Input segments: 15390 Input holes: 0 Input regions: 2 Mesh points: 6601 Mesh tetrahedra: 23352 Mesh faces: 51834 Mesh faces on exterior boundary: 10260 Mesh faces on input facets: 10260 Mesh edges on input segments: 15390 Steiner points inside domain: 1469 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.177886 Creating surface mesh ... Surface mesh seconds: 0.029305 Recovering boundaries... Boundary recovery seconds: 0.112203 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.060554 Recovering Delaunayness... Delaunay recovery seconds: 0.035118 Refining mesh... Refinement seconds: 0.478576 Smoothing vertices... Mesh smoothing seconds: 0.377952 Improving mesh... Mesh improvement seconds: 0.03741 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.008904 Total running seconds: 1.31861 Statistics: Input points: 5133 Input facets: 10262 Input segments: 15393 Input holes: 0 Input regions: 3 Mesh points: 6578 Mesh tetrahedra: 23237 Mesh faces: 51605 Mesh faces on exterior boundary: 10262 Mesh faces on input facets: 10262 Mesh edges on input segments: 15393 Steiner points inside domain: 1445 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.182144 Creating surface mesh ... Surface mesh seconds: 0.024858 Recovering boundaries... Boundary recovery seconds: 0.086701 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.066579 Recovering Delaunayness... Delaunay recovery seconds: 0.047014 Refining mesh... Refinement seconds: 0.345285 Smoothing vertices... Mesh smoothing seconds: 0.337912 Improving mesh... Mesh improvement seconds: 0.030218 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.008585 Total running seconds: 1.13007 Statistics: Input points: 5132 Input facets: 10260 Input segments: 15390 Input holes: 0 Input regions: 4 Mesh points: 6591 Mesh tetrahedra: 23307 Mesh faces: 51744 Mesh faces on exterior boundary: 10260 Mesh faces on input facets: 10260 Mesh edges on input segments: 15390 Steiner points inside domain: 1459 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.249411 Creating surface mesh ... Surface mesh seconds: 0.032075 Recovering boundaries... Boundary recovery seconds: 0.135108 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.08013 Recovering Delaunayness... Delaunay recovery seconds: 0.06351 Refining mesh... Refinement seconds: 0.639931 Smoothing vertices... Mesh smoothing seconds: 0.538815 Improving mesh... Mesh improvement seconds: 0.055283 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.011788 Total running seconds: 1.80698 Statistics: Input points: 5130 Input facets: 10256 Input segments: 15384 Input holes: 0 Input regions: 5 Mesh points: 6609 Mesh tetrahedra: 23392 Mesh faces: 51912 Mesh faces on exterior boundary: 10256 Mesh faces on input facets: 10256 Mesh edges on input segments: 15384 Steiner points inside domain: 1479 Done meshing using TetGen! Writing VTK file: volume.vtk.... Finished writing VTK file Writing exodus file .... Block: 'tableTop', blk_id 1, num_entries 15871 Block: 'leg0', blk_id 2, num_entries 23352 Block: 'leg1', blk_id 3, num_entries 23237 Block: 'leg2', blk_id 4, num_entries 23307 Block: 'leg3', blk_id 5, num_entries 23392 Sideset: 'leg0Side', set_id 1, num_entries 10260 Sideset: 'leg1Side', set_id 2, num_entries 10262 Sideset: 'leg2Side', set_id 3, num_entries 10260 Sideset: 'leg3Side', set_id 4, num_entries 10256 Sideset: 'tableTopSide', set_id 5, num_entries 8014 Nodeset: 'edge', set_id 1, num_entries 41 Nodeset: 'face1', set_id 2, num_entries 610 Nodeset: 'face2', set_id 3, num_entries 617 Nodeset: 'node', set_id 4, num_entries 1 Finished writing Exodus file real 0m16.135s user 0m15.348s sys 0m0.632s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case plato_aflr_tetgen_table_PyTest.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: Astros Nastran ================================================= All tests pass! [GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/STRUCTURE/LINUX64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] Obtaining reference build from same job (7.6,CAPS/STRUCTURE,LINUX64,reynolds) [Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=LINUX64,buildnode=reynolds #174' to compute new, fixed, and outstanding issues [Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0 [Static Analysis] Evaluating quality gates [Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1 [Static Analysis] -> All quality gates have been passed [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=LINUX64,buildnode=reynolds #176'. [Checks API] No suitable checks publisher found. [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] done Finished: SUCCESS