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Compressible Flow Around Aerofoil

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July 2, 2008, 02:23	Compressible Flow Around Aerofoil	#1
Vishal Guest Posts: n/a	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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