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NACA 0012 FLAP experimental data

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Old   April 30, 2013, 10:14
Default NACA 0012 FLAP experimental data
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Hello everyone,

I'm looking for experimental Cp, Cl, Cd data for the NACA 0012 airfoil to validate simulations that I've run. The Reynolds number is 1e6 and the simulations use 45 -45 flap deflections. Does anyone have any suggestions?

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Old   May 1, 2013, 11:08
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1. Theory of wing sections
2. nasa's website

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