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Running snappyHexMesh - Rotor Region
Utility snappyHexMesh gradually refines background mesh in direction to the surface model, reading set-up from system/snappyHexMeshDict:
castellatedMesh true; snap true; addLayers true; // Geometry. Definition of all surfaces. All surfaces are of class // searchableSurface. // Surfaces are used // - to specify refinement for any mesh cell intersecting it // - to specify refinement for any mesh cell inside/outside/near // - to 'snap' the mesh boundary to the surface geometry { blade-rot.stl { type triSurfaceMesh; name blade_rot_wall; } hub-rot-tip.stl { type triSurfaceMesh; name hub_rot_tip_wall; } hub-rot-wall.stl { type triSurfaceMesh; name hub_rot_wall; } hub-rot-wheel.stl { type triSurfaceMesh; name hub_rot_wheel_wall; } shroud-rot.stl { type triSurfaceMesh; name shroud_rot_wall; } interface-rot-guide.stl { type triSurfaceMesh; name rotor_spiral_interface; } interface-rot-draft.stl { type triSurfaceMesh; name rotor_drafttube_interface; } }; // Settings for the castellatedMesh generation. castellatedMeshControls { // Refinement parameters // ~~~~~~~~~~~~~~~~~~~~~ // If local number of cells is >= maxLocalCells on any processor // switches from from refinement followed by balancing // (current method) to (weighted) balancing before refinement. maxLocalCells 100000; // Overall cell limit (approximately). Refinement will stop immediately // upon reaching this number so a refinement level might not complete. // Note that this is the number of cells before removing the part which // is not 'visible' from the keepPoint. The final number of cells might // actually be a lot less. maxGlobalCells 2000000; // The surface refinement loop might spend lots of iterations refining just a // few cells. This setting will cause refinement to stop if <= minimumRefine // are selected for refinement. Note: it will at least do one iteration // (unless the number of cells to refine is 0) minRefinementCells 0; // Allow a certain level of imbalance during refining // (since balancing is quite expensive) // Expressed as fraction of perfect balance (= overall number of cells / // nProcs). 0=balance always. maxLoadUnbalance 0.10; // Number of buffer layers between different levels. // 1 means normal 2:1 refinement restriction, larger means slower // refinement. nCellsBetweenLevels 2; // Explicit feature edge refinement // ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ // Specifies a level for any cell intersected by explicitly provided // edges. // This is a featureEdgeMesh, read from constant/triSurface for now. // Specify 'levels' in the same way as the 'distance' mode in the // refinementRegions (see below). The old specification // level 2; // is equivalent to // levels ((0 2)); features ( { file "blade-rot.eMesh"; level 5; } { file "hub-rot-tip.eMesh"; level 5; } { file "hub-rot-wall.eMesh"; level 5; } { file "hub-rot-wheel.eMesh"; level 5; } { file "interface-rot-draft.eMesh"; level 5; } { file "interface-rot-guide.eMesh"; level 5; } { file "shroud-rot.eMesh"; level 5; } ); // Surface based refinement // ~~~~~~~~~~~~~~~~~~~~~~~~ // Specifies two levels for every surface. The first is the minimum level, // every cell intersecting a surface gets refined up to the minimum level. // The second level is the maximum level. Cells that 'see' multiple // intersections where the intersections make an // angle > resolveFeatureAngle get refined up to the maximum level. refinementSurfaces { // patches shroud_rot_wall { level (4 5); patchInfo { type wall; } } hub_rot_wheel_wall { level (4 5); patchInfo { type wall; } } hub_rot_wall { level (4 5); patchInfo { type wall; } } hub_rot_tip_wall { level (4 5); patchInfo { type wall; } } blade_rot_wall { level (5 5); patchInfo { type wall; } } // rotor boundaries rotor_spiral_interface { level (4 4); patchInfo { type patch; } } rotor_drafttube_interface { level (4 4); patchInfo { type patch; } } }
Create the mesh running snappyHexMesh utility:
# snappyHexMesh
When finished, check the mesh running checkMesh and view the mesh in paraview:
# checkMesh -latestTime
# paraFoam
Figure: Francis turbine rotor region mesh view.
Image francis-turbine-cfd-openfoam-rotor-mesh
The final mesh is located in directory with the highest number.