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February 27, 2010, 10:56 |
Import problem
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#1 |
New Member
Andrew Carmichael
Join Date: Feb 2010
Posts: 4
Rep Power: 16 |
Hi there,
I'm currently trying to import a model I created in Gmsh into OpenFoam using the gmshToFoam function. The models seems to work perfectly in Gsmh, meaning I dont get any errors. However, when I import it to Open Foam, I get the following error: (my gmsh code is just after it) /*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 1.6 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ Build : 1.6-53b7f692aa41 Exec : gmshToFoam Batmodel.msh Date : Feb 27 2010 Time : 15:53:40 Host : aeflight12 PID : 8996 Case : /projects/arc06/simplemodel nProcs : 1 SigFpe : Enabling floating point exception trapping (FOAM_SIGFPE). // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Found $MeshFormat tag; assuming version 2 file format. Starting to read physical names at line 5 Physical names:9 1 WingSurface 2 Symmetryplane 3 UpperBound 4 Outlet 5 Inlet 6 Floor 7 Wall 8 Wing 9 ControlVolumeBox Starting to read points at line 17 Vertices to be read:40 Vertices read:40 Starting to read cells at line 60 Cells to be read:223 Mapping region 1 to Foam patch 0 Mapping region 2 to Foam patch 1 Mapping region 3 to Foam patch 2 Mapping region 4 to Foam patch 3 Mapping region 5 to Foam patch 4 Mapping region 6 to Foam patch 5 Mapping region 7 to Foam patch 6 Mapping region 8 to Foam cellZone 0 Mapping region 9 to Foam cellZone 1 Cells: total:179 hex :0 prism:0 pyr :0 tet :179 CellZones: Zone Size 0 21 1 158 Skipping tag at line 286 Patch 0 gets name WingSurface Patch 1 gets name Symmetryplane Patch 2 gets name UpperBound Patch 3 gets name Outlet Patch 4 gets name Inlet Patch 5 gets name Floor Patch 6 gets name Wall --> FOAM Warning : From function polyMesh:olyMesh(... construct from shapes...) in file meshes/polyMesh/polyMeshFromShapeMesh.C at line 577 Found 12 undefined faces in mesh; adding to default patch. Finding faces of patch 0 --> FOAM Warning : Not using gmsh face 3(0 1 3) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(1 2 3) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(2 4 3) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(5 3 4) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(6 5 4) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(7 5 6) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(5 7 8) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(18 3 0) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(17 3 18) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(1 18 0) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(19 18 1) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(17 18 19) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(19 1 20) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(1 2 20) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(19 20 17) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(4 20 2) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(21 20 4) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(20 21 17) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(22 3 17) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(22 5 3) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(22 17 21) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(21 4 23) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(4 6 23) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(23 22 21) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(6 7 23) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(23 7 24) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(24 22 23) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(24 7 25) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(7 8 25) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(5 25 8) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(22 25 5) since zero vertex is not on boundary of polyMesh --> FOAM Warning : Not using gmsh face 3(22 24 25) since zero vertex is not on boundary of polyMesh Finding faces of patch 1 Finding faces of patch 2 Finding faces of patch 3 Finding faces of patch 4 Finding faces of patch 5 Finding faces of patch 6 FaceZones: Zone Size 0 32 Writing zone 0 to cellZone Wing and cellSet Writing zone 1 to cellZone ControlVolumeBox and cellSet Writing zone 0 to faceZone Wing and faceSet End ----------------------------------------------------------- /*Wing points*/ Point(1) = { 0, 0, 0, 0.05} ; Point(2) = { 0, 0, 0.09, 0.05} ; Point(3) = { 0.0151, -0.00294, 0.125, 0.05} ; Point(4) = { 0.037, 0.00576, 0.0089, 0.05} ; Point(5) = { 0.0956, 0.00248, 0.0796, 0.05} ; Point(6) = { 0.159, -0.0138, -0.0217, 0.05} ; Point(7) = { 0.174, 0.00236, 0.0817, 0.05} ; Point(8) = { 0.232, 0.01840, 0.05490, 0.05} ; Point(9) = { 0.271, -0.0347, 0.011, 0.05} ; size = 0.5; /*Coordinates of the box around the wing*/ Point (10) = {-0.01, 0.3, -0.25, size} ; Point (11) = {-0.01, 0.3, 0.4, size} ; Point (12) = {-0.01, -0.3, 0.4, size} ; Point (13) = {-0.01, -0.3, -0.25, size} ; Point (14) = {0.5, 0.3, -0.25, size} ; Point (15) = {0.5, 0.3, 0.4, size} ; Point (16) = {0.5, -0.3, 0.4, size} ; Point (17) = {0.5, -0.3, -0.25, size} ; /*Wing Lines*/ Line(1) = {1, 2} ; Line(2) = {2, 3} ; Line(3) = {3, 4} ; Line(4) = {4, 1} ; Line(5) = {2, 4} ; Line(6) = {3, 5} ; Line(7) = {5, 4} ; Line(8) = {6, 4} ; Line(9) = {5, 6} ; Line(10) = {5, 7} ; Line(11) = {7, 6} ; Line(12) = {7, 8} ; Line(13) = {8, 6} ; Line(14) = {8, 9} ; Line(15) = {9, 6} ; /*Box Lines*/ Line(40) = {10, 11} ; Line(41) = {11, 12} ; Line(42) = {12, 13} ; Line(43) = {13, 10} ; Line(44) = {10, 14} ; Line(45) = {13, 17} ; Line(46) = {12, 16} ; Line(47) = {11, 15} ; Line(48) = {14, 15} ; Line(49) = {15, 16} ; Line(50) = {16, 17} ; Line(51) = {17, 14} ; /*Wing Surfaces*/ Line Loop(16) = {4, 1, 5} ; Plane Surface(17) = {16} ; Line Loop(18) = {-5, 2, 3} ; Plane Surface(19) = {18} ; Line Loop(20) = {-3, 6, 7} ; Plane Surface(21) = {20} ; Line Loop(22) = {-7, 9, 8} ; Plane Surface(23) = {22} ; Line Loop(24) = {-9, 10, 11} ; Plane Surface(25) = {24} ; Line Loop(26) = {-11, 12, 13} ; Plane Surface(27) = {26} ; Line Loop(28) = {-13, 14, 15} ; Plane Surface(29) = {28} ; Extrude {0,0.001,0} { Surface{17,19,21,23,25,27,29}; } /*Box surfaces*/ Line Loop(352) = {40, 41, 42, 43} ; Plane Surface(353) = {352} ; Line Loop(354) = {40, 47, -48, -44} ; Plane Surface(355) = {354} ; Line Loop(356) = {41, 46, -49, -47} ; Plane Surface(357) = {356} ; Line Loop(358) = {-43, 45, 51, -44} ; Plane Surface(359) = {358} ; Line Loop(360) = {-42, 46, 50, -45} ; Plane Surface(361) = {360} ; Line Loop(362) = {48, 49, 50, 51} ; Plane Surface(363) = {362} ; /*Box Volume*/ Surface Loop(100) = {355, 357, 363, 359, 353, 361} ; /*Wing Volume*/ Surface Loop(222) = {17, 19, 21, 23, 25, 27, 29, 169, 118, 59, 63, 80, 97, 131, 148, 165, 170, 153, 136, 119, 102, 85, 68} ; Physical Surface("WingSurface") = {17, 19, 21, 23, 25, 27, 29, 169, 118, 59, 63, 80, 97, 131, 148, 165, 170, 153, 136, 119, 102, 85, 68} ; /*Physical Surface ("Upper wing surface") = {17, 19, 21, 23, 25, 27, 29} ;*/ /*Physical Surface ("Lower Wing Surface") = {170, 153, 136, 119, 102, 85, 68} ;*/ /*Physical Surface ("Wing edge") = {169, 118, 59, 63, 80, 97, 131, 148, 165} ;*/ Physical Surface ("Symmetry plane") = {353} ; Physical Surface ("Upper Bound") = {355} ; Physical Surface ("Outlet") = {357} ; Physical Surface ("Inlet") = {359} ; Physical Surface ("Floor") = {361} ; Physical Surface ("Wall") = {363} ; Physical Volume("Wing") = {1, 2, 3, 4, 5, 6, 7} ; Volume(10) = {100, 222} ; Physical Volume("Control Volume Box") = {10} ; does anyone have any ideas?? thanks! |
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