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Gmsh reports an OpenCascade exception when opening a .geo file |
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October 21, 2022, 13:09 |
Gmsh reports an OpenCascade exception when opening a .geo file
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#1 |
New Member
Anthony Cummins
Join Date: Sep 2022
Posts: 4
Rep Power: 4 |
Hi all,
I'm trying to open with a .geo file that I know works on the system on which it was created. However, I get a lot of errors when I try to work with it myself. WeDoes anyone know what the problem might be? __________________________________________________ ______________ // Gmsh project created on Fri Oct 21 13:21:18 2022 //SetFactory("Built-in"); SetFactory("OpenCASCADE"); c= 1; h = 3.36; xLe = 0; yLe = 0; xStartDomain = -10*c; xTEConnection = c*3.5+xLe; xLastBoxMiddle = 4*c; xLastBox = 6*c; yMinA = -0.0778244; yMaxA = 0.0619795; t = yMaxA - yMinA; xStartRegion2 = -4*c; xStartRegion2Top = -2*c; yGround = yMinA-h*c; xStartGround = -10*c + xLe + (h*c -yMinA); xEndGround = xLe + 11*c; yOutletBottom = yGround; yOutletTop = h*c - yMinA; xOutlet = xEndGround; nArc = 10; nTop1x = 25; nTop2x = 50; nBot1x = nTop1x; nBot2x = nTop2x; ny = 100; nWake1x = 30; nWake2x = 15; nProgress = 1.1; Point(1) = {1, 0.0604, 0, 1}; Point(2) = {0.999605, 0.0605784, 0, 1}; Point(3) = {0.998419, 0.0610433, 0, 1}; Point(4) = {0.996446, 0.0616005, 0, 1}; Point(5) = {0.993688, 0.0619795, 0, 1}; Point(6) = {0.990149, 0.0619138, 0, 1}; Point(7) = {0.985835, 0.0612488, 0, 1}; Point(8) = {0.980752, 0.0600775, 0, 1}; Point(9) = {0.97491, 0.058799, 0, 1}; Point(10) = {0.968317, 0.0575758, 0, 1}; Point(11) = {0.960983, 0.0563594, 0, 1}; Point(12) = {0.95292, 0.0550487, 0, 1}; Point(13) = {0.944141, 0.0536418, 0, 1}; Point(14) = {0.93466, 0.0522031, 0, 1}; Point(15) = {0.924492, 0.0507849, 0, 1}; Point(16) = {0.913652, 0.0494166, 0, 1}; Point(17) = {0.902158, 0.0481248, 0, 1}; Point(18) = {0.890029, 0.0469341, 0, 1}; Point(19) = {0.877282, 0.0458759, 0, 1}; Point(20) = {0.863939, 0.0449858, 0, 1}; Point(21) = {0.850021, 0.0443008, 0, 1}; Point(22) = {0.835549, 0.043855, 0, 1}; Point(23) = {0.820547, 0.0436621, 0, 1}; Point(24) = {0.805038, 0.0437259, 0, 1}; Point(25) = {0.789046, 0.0440436, 0, 1}; Point(26) = {0.772597, 0.0445904, 0, 1}; Point(27) = {0.755718, 0.0453233, 0, 1}; Point(28) = {0.738434, 0.0461889, 0, 1}; Point(29) = {0.720773, 0.0471253, 0, 1}; Point(30) = {0.702763, 0.0480625, 0, 1}; Point(31) = {0.684432, 0.0489309, 0, 1}; Point(32) = {0.66581, 0.0497114, 0, 1}; Point(33) = {0.646925, 0.0504071, 0, 1}; Point(34) = {0.627808, 0.0510246, 0, 1}; Point(35) = {0.608489, 0.0515775, 0, 1}; Point(36) = {0.588999, 0.0520806, 0, 1}; Point(37) = {0.569368, 0.0525307, 0, 1}; Point(38) = {0.549627, 0.052908, 0, 1}; Point(39) = {0.529808, 0.053199, 0, 1}; Point(40) = {0.509941, 0.0534152, 0, 1}; Point(41) = {0.490059, 0.0535737, 0, 1}; Point(42) = {0.470192, 0.0536746, 0, 1}; Point(43) = {0.450373, 0.0537003, 0, 1}; Point(44) = {0.430632, 0.053639, 0, 1}; Point(45) = {0.411001, 0.0535024, 0, 1}; Point(46) = {0.391511, 0.0533079, 0, 1}; Point(47) = {0.372192, 0.0530609, 0, 1}; Point(48) = {0.353075, 0.052754, 0, 1}; Point(49) = {0.33419, 0.05238, 0, 1}; Point(50) = {0.315568, 0.0519341, 0, 1}; Point(51) = {0.297237, 0.051413, 0, 1}; Point(52) = {0.279227, 0.0508255, 0, 1}; Point(53) = {0.261566, 0.0502075, 0, 1}; Point(54) = {0.244282, 0.0495947, 0, 1}; Point(55) = {0.227403, 0.0489997, 0, 1}; Point(56) = {0.210954, 0.0484056, 0, 1}; Point(57) = {0.194962, 0.0477958, 0, 1}; Point(58) = {0.179453, 0.0471692, 0, 1}; Point(59) = {0.164451, 0.0465119, 0, 1}; Point(60) = {0.149979, 0.0457238, 0, 1}; Point(61) = {0.136061, 0.0448191, 0, 1}; Point(62) = {0.122718, 0.0438133, 0, 1}; Point(63) = {0.109971, 0.0426546, 0, 1}; Point(64) = {0.0978417, 0.0414712, 0, 1}; Point(65) = {0.086348, 0.0402678, 0, 1}; Point(66) = {0.0755083, 0.0388983, 0, 1}; Point(67) = {0.0653399, 0.0376177, 0, 1}; Point(68) = {0.0558587, 0.0362163, 0, 1}; Point(69) = {0.0470798, 0.0349255, 0, 1}; Point(70) = {0.0390171, 0.0336265, 0, 1}; Point(71) = {0.0316833, 0.0324608, 0, 1}; Point(72) = {0.0250899, 0.0312981, 0, 1}; Point(73) = {0.0192475, 0.0296216, 0, 1}; Point(74) = {0.0141653, 0.026429, 0, 1}; Point(75) = {0.00985132, 0.0229857, 0, 1}; Point(76) = {0.00631233, 0.0191972, 0, 1}; Point(77) = {0.00355396, 0.0142819, 0, 1}; Point(78) = {0.00158058, 0.00992171, 0, 1}; Point(79) = {0.000395301, 0.00402408, 0, 1}; Point(80) = {0, 0, 0, 1}; Point(81) = {0.000395301, -0.00382523, 0, 1}; Point(82) = {0.00158058, -0.00966363, 0, 1}; Point(83) = {0.00355396, -0.0141751, 0, 1}; Point(84) = {0.00631233, -0.0189984, 0, 1}; Point(85) = {0.00985132, -0.0227577, 0, 1}; Point(86) = {0.0141653, -0.0261142, 0, 1}; Point(87) = {0.0192475, -0.0290608, 0, 1}; Point(88) = {0.0250899, -0.0320986, 0, 1}; Point(89) = {0.0316833, -0.0354145, 0, 1}; Point(90) = {0.0390171, -0.0389275, 0, 1}; Point(91) = {0.0470798, -0.0426075, 0, 1}; Point(92) = {0.0558587, -0.0464556, 0, 1}; Point(93) = {0.0653399, -0.0502913, 0, 1}; Point(94) = {0.0755083, -0.0541613, 0, 1}; Point(95) = {0.086348, -0.0579993, 0, 1}; Point(96) = {0.0978417, -0.0616434, 0, 1}; Point(97) = {0.109971, -0.0651169, 0, 1}; Point(98) = {0.122718, -0.0683089, 0, 1}; Point(99) = {0.136061, -0.0711266, 0, 1}; Point(100) = {0.149979, -0.0736086, 0, 1}; Point(101) = {0.164451, -0.0755747, 0, 1}; Point(102) = {0.179453, -0.0768899, 0, 1}; Point(103) = {0.194962, -0.0776846, 0, 1}; Point(104) = {0.210954, -0.0778244, 0, 1}; Point(105) = {0.227403, -0.0773511, 0, 1}; Point(106) = {0.244282, -0.0764985, 0, 1}; Point(107) = {0.261566, -0.0755273, 0, 1}; Point(108) = {0.279227, -0.0745046, 0, 1}; Point(109) = {0.297237, -0.0733613, 0, 1}; Point(110) = {0.315568, -0.072032, 0, 1}; Point(111) = {0.33419, -0.0705279, 0, 1}; Point(112) = {0.353075, -0.0688931, 0, 1}; Point(113) = {0.372192, -0.0671575, 0, 1}; Point(114) = {0.391511, -0.0653079, 0, 1}; Point(115) = {0.411001, -0.0633244, 0, 1}; Point(116) = {0.430632, -0.0611936, 0, 1}; Point(117) = {0.450373, -0.0589077, 0, 1}; Point(118) = {0.470192, -0.0564646, 0, 1}; Point(119) = {0.490059, -0.0538821, 0, 1}; Point(120) = {0.509941, -0.0511821, 0, 1}; Point(121) = {0.529808, -0.048365, 0, 1}; Point(122) = {0.549627, -0.0454112, 0, 1}; Point(123) = {0.569368, -0.0423111, 0, 1}; Point(124) = {0.588999, -0.039096, 0, 1}; Point(125) = {0.608489, -0.035806, 0, 1}; Point(126) = {0.627808, -0.0324515, 0, 1}; Point(127) = {0.646925, -0.0290112, 0, 1}; Point(128) = {0.66581, -0.0254699, 0, 1}; Point(129) = {0.684432, -0.0218487, 0, 1}; Point(130) = {0.702763, -0.018181, 0, 1}; Point(131) = {0.720773, -0.0144874, 0, 1}; Point(132) = {0.738434, -0.0107618, 0, 1}; Point(133) = {0.755718, -0.00699652, 0, 1}; Point(134) = {0.772597, -0.00320282, 0, 1}; Point(135) = {0.789046, 0.000585036, 0, 1}; Point(136) = {0.805038, 0.00433399, 0, 1}; Point(137) = {0.820547, 0.00802701, 0, 1}; Point(138) = {0.835549, 0.011667, 0, 1}; Point(139) = {0.850021, 0.0152554, 0, 1}; Point(140) = {0.863939, 0.0187866, 0, 1}; Point(141) = {0.877282, 0.0222372, 0, 1}; Point(142) = {0.890029, 0.0255826, 0, 1}; Point(143) = {0.902158, 0.0288016, 0, 1}; Point(144) = {0.913652, 0.0318906, 0, 1}; Point(145) = {0.924492, 0.034874, 0, 1}; Point(146) = {0.93466, 0.0377273, 0, 1}; Point(147) = {0.944141, 0.0403881, 0, 1}; Point(148) = {0.95292, 0.0428671, 0, 1}; Point(149) = {0.960983, 0.0452231, 0, 1}; Point(150) = {0.968317, 0.0474328, 0, 1}; Point(151) = {0.97491, 0.0493574, 0, 1}; Point(152) = {0.980752, 0.0509158, 0, 1}; Point(153) = {0.985835, 0.0522553, 0, 1}; Point(154) = {0.990149, 0.0537617, 0, 1}; Point(155) = {0.993688, 0.0555086, 0, 1}; Point(156) = {0.996446, 0.0573218, 0, 1}; Point(157) = {0.998419, 0.0589173, 0, 1}; Point(158) = {0.999605, 0.060011, 0, 1}; //Line(1) = {1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47, 48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62, 63, 64, 65, 66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77, 78, 79, 80, 81, 82, 83, 84, 85, 86, 87, 88, 89, 90, 91, 92, 93, 94, 95, 96, 97, 98, 99, 100, 101, 102, 103, 104, 105, 106, 107, 108, 109, 110, 111, 112, 113, 114, 115, 116, 117, 118, 119, 120, 121, 122, 123, 124, 125, 126, 127, 128, 129, 130, 131, 132, 133, 134, 135, 136, 137, 138, 139, 140, 141, 142, 143, 144, 145, 146, 147, 148, 149, 150, 151, 152, 153, 154, 155, 156, 157, 158,1}; Point(160) = {xStartGround,yGround,0, 1}; //startGround Point(161) = {xEndGround,yGround,0,1}; //endGround Point(162) = {xOutlet, yOutletBottom, 0, 1}; //outletBottom Point(163) = {xOutlet, yOutletTop, 0, 1}; //outletTop Point(164) = {xLe,yGround,0,1}; //LE Projected on the ground Point(165) = {xStartGround,yOutletTop,0,1}; //LE Projected to top of domain Point(166) = {xLe,yLe,0,1}; //LE Point(167) = {xStartDomain,yLe,0,1}; //Left side of the domain Point(168) = {xStartGround,yLe,0,1}; //Middle of front circle Point(169) = {xStartDomain,yOutletTop,0,1}; Point(170) = {xStartDomain,yOutletBottom,0,1}; Point(171) = {xStartRegion2Top,yOutletTop,0,1}; Point(172) = {xStartRegion2,yOutletBottom,0,1}; //lines between domain points Line(2) = {160,161}; Line(3) = {162,163}; //+ //+ //+ Circle(4) = {160,168,165}; //+ Line(5) = {165, 163}; //+ //+ Line(6) = {168, 170}; //+ Line(7) = {168, 169}; //+ //+ BooleanUnion{ Line{7}; Delete; }{ Line{4}; Delete; } //+ Recursive Delete { Line{7}; Line{8}; } //+ BooleanUnion{ Line{6}; Delete; }{ Line{9}; Delete; } //+ Recursive Delete { Line{11}; } //+ Recursive Delete { Line{12}; } Point(187) = {xStartDomain,yOutletBottom,0,1}; Line(8) = {75, 173}; //+ Line(9) = {85, 187}; Line(38) = {173,187}; //+ Line(11) = {51, 171}; //+ Line(12) = {109, 172}; Point(176) = {xTEConnection,yOutletTop,0,1}; Point(177) = {xTEConnection,yOutletBottom,0,1}; //+ Line(15) = {1, 176}; //+ Line(16) = {1, 177}; Point(178) = {xLastBox,yOutletBottom,0,1}; Point(179) = {xLastBox,yOutletTop,0,1}; Point(180) = {xLastBox,yLe,0,1}; Point(181) = {xOutlet,yLe,0,1}; Point(186) = {xLastBoxMiddle,yLe,0,1}; //+ Line(17) = {1, 186}; //+ Line(18) = {186, 181}; //+ Line(19) = {186, 179}; //+ Line(20) = {186, 178}; //+ airfoil splines Spline(21) = {75, 74, 73, 72, 71, 70, 69, 68, 67, 66, 65, 64, 63, 62, 61, 60, 59, 58, 57, 56, 55, 54, 53, 52, 51}; //top part 1 //+ Spline(22) = {75, 76, 77, 78, 79, 80, 81, 82, 83, 84, 85}; //arc //+ Spline(23) = {85, 86, 87, 88, 89, 90, 91, 92, 93, 94, 95, 96, 97, 98, 99, 100, 101, 102, 103, 104, 105, 106, 107, 108, 109}; //bottom part 1 //+ Spline(24) = {51, 50, 49, 48, 47, 46, 45, 44, 43, 42, 41, 40, 39, 38, 37, 36, 35, 34, 33, 32, 31, 30, 29, 28, 27, 26, 25, 24, 23, 22, 21, 20, 19, 18, 17, 16, 15, 14, 13, 12, 11, 10, 9, 8, 7, 6, 5, 4, 3, 2, 1}; //top part 2 //+ Spline(25) = {109, 110, 111, 111, 112, 113, 114, 115, 116, 117, 118, 119, 120, 121, 122, 123, 124, 125, 126, 127, 128, 129, 130, 131, 132, 133, 134, 135, 136, 137, 138, 139, 140, 141, 142, 143, 144, 145, 146, 147, 148, 149, 150, 151, 152, 153, 154, 155, 156, 157, 158, 1}; //bottom part 2 //+ //+ Recursive Delete { Line{5}; Line{2}; } //+ Line(26) = {165, 171}; //+ Line(27) = {171, 176}; //+ Line(28) = {176, 179}; //+ Line(29) = {179, 163}; //+ Line(30) = {160, 172}; //+ Line(31) = {172, 177}; //+ Line(32) = {177, 178}; //+ Line(33) = {178, 162}; //+ //+ Point(182) = {xStartGround-1.5*c,yOutletTop,0,1}; Point(183) = {xStartGround+2*c,yOutletTop,0,1}; Point(184) = {xStartGround-1.5*c,yOutletBottom,0,1}; Point(185) = {xStartGround-2*c,yOutletBottom,0,1}; // //+ Bezier(34) = {173, 182, 183, 171}; //+ Bezier(35) = {175, 184, 185, 172}; //+ Recursive Delete { Line{10}; Line{26}; Line{13}; Line{30}; } //+ Recursive Delete { Line{3}; } //+ Line(36) = {181, 163}; //+ Line(37) = {181, 162}; //+ Recursive Delete { Line{14}; Line{35}; } //+ Line(39) = {187, 172}; //+ Point(188) = {-8, 1.6, 0, 1.0}; //+ Spline(40) = {187, 188, 171}; //+ BooleanUnion{ Line{8}; Delete; }{ Line{40}; Delete; } //+ //+ Recursive Delete { Line{41}; Line{34}; Line{38}; } //Line(44) = {75, 189}; Transfinite Line {42} = nArc Using Bump 0.3; //arcDomain Transfinite Line {43} = nTop1x Using Progression 1; //BezierTop Transfinite Line {27} = nTop2x Using Progression 1; //TopAirfoilDomain Transfinite Line {28} = nWake1x Using Progression 1; //TopWake1Domain Transfinite Line {29} = nWake2x Using Progression 1; //TopWake2Domain Transfinite Line {36} = ny Using Progression nProgress; //OutletUpperDomain Transfinite Line {37} = ny Using Progression nProgress; //OutletLowerDomain Transfinite Line {33} = nWake2x Using Progression 1; //BottomWake2Domain Transfinite Line {32} = nWake1x Using Progression 1; //BottomWake1Domain Transfinite Line {31} = nBot2x Using Progression 1; //BottomAirfoilDomain Transfinite Line {39} = nBot1x Using Progression 1; //BezierBottom Transfinite Line {9} = ny Using Progression nProgress; //ArcLower Transfinite Line {40} = ny Using Progression nProgress; //ArcUpper Transfinite Line {11} = ny Using Progression nProgress; //AirfoilUp Transfinite Line {15} = ny Using Progression nProgress; //TeUp Transfinite Line {19} = ny Using Progression nProgress; //Wake1Up Transfinite Line {20} = ny Using Progression nProgress; //Wake1Down Transfinite Line {16} = ny Using Progression nProgress; //TeDown Transfinite Line {12} = ny Using Progression nProgress; //airfoilDown Transfinite Line {22} = nArc Using Progression 1; //AirofilArc Transfinite Line {21} = nTop1x Using Progression 1; //AirfoilTop1 Transfinite Line {24} = nTop2x Using Progression 1; //AirfoilTop2 Transfinite Line {23} = nBot1x Using Progression 1; //AirfoilBottom1 Transfinite Line {25} = nBot2x Using Progression 1; //AirfoilBottom2 Transfinite Line {17} = nWake1x Using Progression nProgress; //wake1X Transfinite Line {18} = nWake2x Using Progression nProgress; //wake2X //+ Line Loop(1) = {22, 9, -42, -40}; //+ Plane Surface(1) = {1}; //+ Line Loop(2) = {21, 11, -40, -43}; //+ Plane Surface(2) = {2}; //+ Line Loop(10) = {24, 15, -27, -11}; //+ Plane Surface(3) = {10}; //+ Line Loop(4) = {17, 19, -28, -15}; //+ Plane Surface(4) = {4}; //+ Line Loop(5) = {18, 36, -29, -19}; //+ Plane Surface(5) = {5}; //+ Line Loop(6) = {18, 37, -33, -20}; //+ Plane Surface(6) = {6}; //+ Line Loop(7) = {17, 20, -32, -16}; //+ Plane Surface(7) = {7}; //+ Line Loop(8) = {25, 16, -31, -12}; //+ Plane Surface(8) = {8}; //+ Line Loop(9) = {23, 12, -39, -9}; //+ Plane Surface(9) = {9}; //+ Transfinite Surface {1}; //+ Transfinite Surface {2}; //+ Transfinite Surface {3}; //+ Transfinite Surface {4}; //+ Transfinite Surface {5}; //+ Transfinite Surface {6}; //+ Transfinite Surface {7}; //+ Transfinite Surface {8}; //+ Transfinite Surface {9}; //+ Recombine Surface {1, 2, 3, 4, 5, 6, 7, 8, 9}; //+ //+ //+ //+ Extrude {0, 0, 1} { Surface{2}; Surface{1}; Surface{9}; Line{42}; Line{43}; Surface{3}; Line{27}; Line{11}; Line{40}; Line{15}; Line{28}; Surface{5}; Line{19}; Line{29}; Line{36}; Line{37}; Surface{6}; Line{18}; Line{33}; Line{20}; Surface{7}; Line{16}; Line{32}; Line{31}; Line{12}; Line{9}; Line{39}; Surface{4}; Surface{8}; Layers{1}; Recombine; } //+ Physical Volume("Fluid") = {3, 2, 1, 4, 9, 7, 8, 5, 6}; //+ Physical Surface("Inlet") = {21, 43, 37, 33, 17, 12, 25, 40, 29}; //+ Physical Surface("Outlet") = {28, 32}; //+ Physical Surface("Side") = {14, 26, 41, 31, 35, 39, 44, 22, 18, 1, 9, 2, 3, 8, 4, 7, 6, 5}; //+ Physical Surface("Airfoil") = {42, 19, 23, 10, 15}; //+ __________________________________________________ _________________ |
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October 23, 2022, 16:32 |
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#2 |
Senior Member
Join Date: Oct 2011
Posts: 242
Rep Power: 17 |
Hello,
GMSH indicates you the line where the first problem occurs. This is line 296, in the definition of Spline(25). Point 111 is listed twice, which is why spline creation fails. At least I would expect it to fail, maybe a different GMSH version handles that differently, ignore or else. Removing this point results in no error on my pc with linux binaries 4.10.4. That being said there are still weird things in the script as multiply defined points, for example points 195 and 207 are superimposed. Maybe that's ok, maybe not... |
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October 24, 2022, 06:59 |
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#3 |
New Member
Anthony Cummins
Join Date: Sep 2022
Posts: 4
Rep Power: 4 |
Hi, thanks for your time in replying to this post. Unfortunately, your solution does not work for me. I'm using gmsh 3.0.6 (and the file was created using the same version), but I get a whole host of errors when I load the file. Removing the point does not change anything for me. Here's the error log from gmsh:
__________________________________________________ _______________ Error : OpenCASCADE exception Error : 'AirfoilMesh.geo', line 224 : Could not add circle Error : Unknown OpenCASCADE entity of dimension 1 with tag 4 Error : 'AirfoilMesh.geo', line 238 : Could not apply boolean operator Error : Unknown OpenCASCADE entity of dimension 1 with tag 8 Error : Unknown OpenCASCADE entity of dimension 1 with tag 9 Error : 'AirfoilMesh.geo', line 244 : Could not apply boolean operator Error : Unknown OpenCASCADE entity of dimension 1 with tag 11 Error : Unknown OpenCASCADE entity of dimension 1 with tag 12 Error : Unknown OpenCASCADE vertex with tag 173 Error : 'AirfoilMesh.geo', line 255 : Could not add line Error : Unknown OpenCASCADE vertex with tag 173 Error : 'AirfoilMesh.geo', line 258 : Could not add line Error : Unknown OpenCASCADE vertex with tag 165 Error : 'AirfoilMesh.geo', line 304 : Could not add line Error : Unknown OpenCASCADE vertex with tag 160 Error : 'AirfoilMesh.geo', line 312 : Could not add line Error : Unknown OpenCASCADE vertex with tag 173 Error : 'AirfoilMesh.geo', line 329 : Could not add Bezier Error : Unknown OpenCASCADE vertex with tag 175 Error : 'AirfoilMesh.geo', line 331 : Could not add Bezier Error : Unknown OpenCASCADE entity of dimension 1 with tag 10 Error : Unknown OpenCASCADE entity of dimension 1 with tag 26 Error : Unknown OpenCASCADE entity of dimension 1 with tag 13 Error : Unknown OpenCASCADE entity of dimension 1 with tag 30 Error : Unknown OpenCASCADE entity of dimension 1 with tag 14 Error : Unknown OpenCASCADE entity of dimension 1 with tag 35 Error : Unknown OpenCASCADE entity of dimension 1 with tag 8 Error : 'AirfoilMesh.geo', line 357 : Could not apply boolean operator Error : Unknown OpenCASCADE entity of dimension 1 with tag 41 Error : Unknown OpenCASCADE entity of dimension 1 with tag 34 Error : Unknown OpenCASCADE entity of dimension 1 with tag 38 Error : Unknown OpenCASCADE edge with tag 42 Error : 'AirfoilMesh.geo', line 392 : Could not add line loop Error : Unknown OpenCASCADE line loop with tag 1 Error : 'AirfoilMesh.geo', line 394 : Could not add plane surface Error : Unknown OpenCASCADE edge with tag 43 Error : 'AirfoilMesh.geo', line 396 : Could not add line loop Error : Unknown OpenCASCADE line loop with tag 2 Error : 'AirfoilMesh.geo', line 398 : Could not add plane surface Error : Unknown OpenCASCADE entity of dimension 2 with tag 2 Error : 'AirfoilMesh.geo', line 457 : Could not extrude shapes Info : Done reading 'AirfoilMesh.geo' Info : Reading 'AirfoilMesh.geo'... Error : OpenCASCADE exception Error : 'AirfoilMesh.geo', line 224 : Could not add circle Error : Unknown OpenCASCADE entity of dimension 1 with tag 4 Error : 'AirfoilMesh.geo', line 238 : Could not apply boolean operator Error : Unknown OpenCASCADE entity of dimension 1 with tag 8 Error : Unknown OpenCASCADE entity of dimension 1 with tag 9 Error : 'AirfoilMesh.geo', line 244 : Could not apply boolean operator Error : Unknown OpenCASCADE entity of dimension 1 with tag 11 Error : Unknown OpenCASCADE entity of dimension 1 with tag 12 Error : Unknown OpenCASCADE vertex with tag 173 Error : 'AirfoilMesh.geo', line 255 : Could not add line Error : Unknown OpenCASCADE vertex with tag 173 Error : 'AirfoilMesh.geo', line 258 : Could not add line Error : Unknown OpenCASCADE vertex with tag 165 Error : 'AirfoilMesh.geo', line 304 : Could not add line Error : Unknown OpenCASCADE vertex with tag 160 Error : 'AirfoilMesh.geo', line 312 : Could not add line Error : Unknown OpenCASCADE vertex with tag 173 Error : 'AirfoilMesh.geo', line 329 : Could not add Bezier Error : Unknown OpenCASCADE vertex with tag 175 Error : 'AirfoilMesh.geo', line 331 : Could not add Bezier Error : Unknown OpenCASCADE entity of dimension 1 with tag 10 Error : Unknown OpenCASCADE entity of dimension 1 with tag 26 Error : Unknown OpenCASCADE entity of dimension 1 with tag 13 Error : Unknown OpenCASCADE entity of dimension 1 with tag 30 Error : Unknown OpenCASCADE entity of dimension 1 with tag 14 Error : Unknown OpenCASCADE entity of dimension 1 with tag 35 Error : Unknown OpenCASCADE entity of dimension 1 with tag 8 Error : 'AirfoilMesh.geo', line 357 : Could not apply boolean operator Error : Unknown OpenCASCADE entity of dimension 1 with tag 41 Error : Unknown OpenCASCADE entity of dimension 1 with tag 34 Error : Unknown OpenCASCADE entity of dimension 1 with tag 38 Error : Unknown OpenCASCADE edge with tag 42 Error : 'AirfoilMesh.geo', line 392 : Could not add line loop Error : Unknown OpenCASCADE line loop with tag 1 Error : 'AirfoilMesh.geo', line 394 : Could not add plane surface Error : Unknown OpenCASCADE edge with tag 43 Error : 'AirfoilMesh.geo', line 396 : Could not add line loop Error : Unknown OpenCASCADE line loop with tag 2 Error : 'AirfoilMesh.geo', line 398 : Could not add plane surface Error : Unknown OpenCASCADE entity of dimension 2 with tag 2 Error : 'AirfoilMesh.geo', line 457 : Could not extrude shapes Info : Done reading 'AirfoilMesh.geo' Info : Calling 'gedit AirfoilMesh.geo &' |
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