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Reynolds number for compressible flows

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Old   September 21, 2006, 13:03
Default Reynolds number for compressible flows
Compressible flow
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I want to do simulation in fluent for a compressible flow over an airfoil. My reynolds number would shld be 5000 and mach number is 0.3. what conditions should I use and what should be my inlet velocity and all....I am new to plz do help me...

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