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anybody matched NACA0012 data using Fluent?

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Old   February 1, 2008, 12:56
Default anybody matched NACA0012 data using Fluent?
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Hi, i'm running an airfoil simulation on fluent for NACA 0012. I cant seem to get the lift and drag coefficients that matches experiment data. I'm running for Angle of attack of 0 degrees and at reynolds number 1 million. what parameters did you guys use?

Cheerios Rif
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