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Forum: FLUENT February 4, 2015, 11:21

Replies: 19 Continuity convergence issue on a 3d wing Views: 11,754 Posted By sajad Hi all, I'm modelling a a 3d rotor blade using... Hi all, I'm modelling a a 3d rotor blade using density based transient solver in Ansys Fluent. I am using pressure far field BC and Spalart-Allmaras turbulence model. I have problem with residuals....

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