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Forum: FLUENT

October 10, 2012, 16:08

Replies: 8

Supersonic Inlet for a Compressible Flow in a Nozzle

Views: 6,558

Posted By NormalVector

Sure. It may take more a more aggressive...

Sure. It may take more a more aggressive relaxation effort than a 0.1 change so you can try that as well.

Forum: FLUENT

October 10, 2012, 15:14

Replies: 8

Supersonic Inlet for a Compressible Flow in a Nozzle

Views: 6,558

Posted By NormalVector

Which solver diverges first? That may be a hint....

Which solver diverges first? That may be a hint. I've had divergence problems before and if I under-relax the solver that diverges first a little bit (~0.05 to ~0.1 change) it helps.

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