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case with cyclic boundary
2 Attachment(s)
Dear OF-users,
I want to compute the flow around a 5-blades propeller using the MRFSimpleFoam. Pict1 shows the entire flow domain around a single blade. I want to use cyclic boundary conditions. I have used icemcfd hexa to generated the structured mesh. Then I have used the fluent3DMeshToFoam command to convert the mesh. Pict2 shows the outlet boundary. Left and right sides of the flow domain have to be into a unique part or have to be 2 separate parts (icemcfd hexa) ? How to be sure that the mesh was created correctly inside OpenFoam ? Maybe there is a tutorial with cyclic boundary conditions ? Regards, Stephane. |
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