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test case for 2D Euler Code

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Old   May 26, 2005, 09:01
Default test case for 2D Euler Code
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Can I get resources for NACA 0012 aerofoil Cd, Cl values for different mach numbers (sub sonic, transonic and super sonic cases) experimental as well as as computational? I am happy if I get Inviscid as well as viscous flow cases. Thanking you.
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