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Vishal July 2, 2008 02:23

Compressible Flow Around Aerofoil
Dear Fyi,

I am trying to solve density based solver for a flow around aerofoil. My mach no is 0.2. I know it is incompressible flow. Still I want to do it by dens method.

I am getting divergence every time. Can anyone please suggests any solution?

Thanks and Regards, Vishal

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