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July 2, 2008, 03:23 |
Compressible Flow Around Aerofoil
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#1 |
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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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