|March 26, 2010, 08:46||
case with cyclic boundary
Join Date: Mar 2009
Posts: 300Rep Power: 9
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 ?
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