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Forum: CFX

February 16, 2016, 16:21

Replies: 12

Transonic rotor convergence problem

Views: 2,957

Posted By turbo

Fine grid is not always better in convergence due...

Fine grid is not always better in convergence due to the relative error magnitudes. Try to reduce the mesh size a little bit and use automatic time scale (that is good enough).

Forum: CFX

February 16, 2016, 16:18

Replies: 12

Transonic rotor convergence problem

Views: 2,957

Posted By turbo

Do not use the mass flow rate at the exit BC in...

Do not use the mass flow rate at the exit BC in compressible flow CFD. Originally the option was not available in any of CFD in turbomachinery area. It was born by many requests from users for...

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