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September 21, 2006, 14:03 |
Reynolds number for compressible flows
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#1 |
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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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