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NACA 0012 Experimental Data

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Old   July 8, 2011, 12:50
Default NACA 0012 Experimental Data
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Prasad
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Hello everyone,

I'm looking for experimental pressure coefficient data for the NACA 0012 airfoil to validate simulations that I've run. The Reynolds number is 1e7. Does anyone have any suggestions regarding where I can find such data?

Thanks
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