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[mesh manipulation] How to fix NASA grid for NACA 0012 |
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November 17, 2024, 21:24 |
How to fix NASA grid for NACA 0012
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#1 |
New Member
Join Date: Oct 2024
Posts: 3
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Hello, everyone.
I am trying to use NACA 0012 meshs provided by NASA (https://turbmodels.larc.nasa.gov/naca0012_grids.html). These are the steps I've made so far:
plot3dToFoam -noBlank n0012_897-257.p3dfmt Code:
/*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2406 | | \\ / A nd | Website: www.openfoam.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ Build : _be01ca78-20240625 OPENFOAM=2406 version=2406 Arch : "LSB;label=32;scalar=64" Exec : plot3dToFoam -noBlank ../../../meshs/n0012_897-257.p3dfmt Date : Nov 17 2024 Time : 22:15:05 Host : nitro PID : 18342 I/O : uncollated Case : /home/gabriel/Documents/cfd-models-comparison/simulations/3D/simpleFoam/kOmegaSST nProcs : 1 trapFpe: Floating point exception trapping enabled (FOAM_SIGFPE). fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 5, maxFileModificationPolls 20) allowSystemOperations : Allowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Reading 1 blocks block 0 nx:2 ny:897 nz:257 Reading block points block 0: Reading 461058 x coordinates... Reading 461058 y coordinates... Reading 461058 z coordinates... Looking at cell 0 0 0 to determine orientation. Right-handed block. Merged points within 1e-15 distance. Merged from 461058 down to 460672 points. Creating cells Creating boundary patches --> FOAM Warning : From Foam::polyMesh::polyMesh(const Foam::IOobject&, Foam::pointField&&, const Foam::cellShapeList&, const Foam::faceListList&, const Foam::wordList&, const Foam::wordList&, const Foam::word&, const Foam::word&, const Foam::wordList&, bool) in file meshes/polyMesh/polyMeshFromShapeMesh.C at line 640 Found 460672 undefined faces in mesh; adding to default patch defaultFaces Writing polyMesh End Code:
/*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2406 | | \\ / A nd | Website: www.openfoam.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ Build : _be01ca78-20240625 OPENFOAM=2406 version=2406 Arch : "LSB;label=32;scalar=64" Exec : autoPatch -overwrite 45 Date : Nov 17 2024 Time : 22:15:10 Host : nitro PID : 18388 I/O : uncollated Case : /home/gabriel/Documents/cfd-models-comparison/simulations/3D/simpleFoam/kOmegaSST nProcs : 1 trapFpe: Floating point exception trapping enabled (FOAM_SIGFPE). fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 5, maxFileModificationPolls 20) allowSystemOperations : Allowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create polyMesh for time = 0 Mesh read in = 1.01 s Feature:45 minCos :0.707107 Assigned 512 faces to patch auto0 Assigned 229376 faces to patch auto1 Assigned 229376 faces to patch auto2 Assigned 512 faces to patch auto3 Assigned 896 faces to patch auto4 End Code:
/*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2406 | | \\ / A nd | Website: www.openfoam.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ Build : _be01ca78-20240625 OPENFOAM=2406 version=2406 Arch : "LSB;label=32;scalar=64" Exec : checkMesh Date : Nov 17 2024 Time : 22:15:19 Host : nitro PID : 18474 I/O : uncollated Case : /home/gabriel/Documents/cfd-models-comparison/simulations/3D/simpleFoam/kOmegaSST nProcs : 1 trapFpe: Floating point exception trapping enabled (FOAM_SIGFPE). fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 5, maxFileModificationPolls 20) allowSystemOperations : Allowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create mesh for time = 0 Check mesh... Time = 0 Mesh stats points: 460672 internal points: 0 faces: 918464 internal faces: 457792 cells: 229376 faces per cell: 6 boundary patches: 6 point zones: 0 face zones: 0 cell zones: 0 Overall number of cells of each type: hexahedra: 229376 prisms: 0 wedges: 0 pyramids: 0 tet wedges: 0 tetrahedra: 0 polyhedra: 0 Checking topology... Boundary definition OK. Cell to face addressing OK. Point usage OK. Upper triangular ordering OK. Face vertices OK. Number of regions: 1 (OK). Checking patch topology for multiply connected surfaces... Patch Faces Points Surface topology defaultFaces 0 0 ok (empty) auto0 512 1026 ok (non-closed singly connected) auto1 229376 230336 ok (non-closed singly connected) auto2 229376 230336 ok (non-closed singly connected) auto3 512 1024 ok (non-closed singly connected) auto4 896 1794 ok (non-closed singly connected) ".*" 460672 460672 ok (closed singly connected) Checking faceZone topology for multiply connected surfaces... No faceZones found. Checking basic cellZone addressing... No cellZones found. Checking basic pointZone addressing... No pointZones found. Checking geometry... Overall domain bounding box (-484.457 -1 -507.807) (501 0 507.807) Mesh has 3 geometric (non-empty/wedge) directions (1 1 1) Mesh has 3 solution (non-empty) directions (1 1 1) Boundary openness (-7.45106e-19 7.70971e-15 2.26771e-19) OK. ***High aspect ratio cells found, Max aspect ratio: 3.17847e+07, number of cells 87404 <<Writing 87404 cells with high aspect ratio to set highAspectRatioCells Minimum face area = 9.5796e-11. Maximum face area = 843.777. Face area magnitudes OK. Min volume = 9.5796e-11. Max volume = 843.777. Total volume = 875558. Cell volumes OK. Mesh non-orthogonality Max: 19.8306 average: 1.63523 Non-orthogonality check OK. Face pyramids OK. Max skewness = 0.201756 OK. Coupled point location match (average 0) OK. Failed 1 mesh checks. End How can I improve this mesh or identify the high aspect ratio cells? And what should I do if I identify them? Thank you, guys! |
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Tags |
airfoil 3d, aspect ratio, nasa |
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