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Compressible Flow Around Aerofoil

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Old   July 2, 2008, 02:23
Default Compressible Flow Around Aerofoil
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Vishal
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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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