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Compressible flow September 21, 2006 13:03

Reynolds number for compressible flows
 
Hi,

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 fluent...so plz do help me...

Raj


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