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-   -   NACA 0012 FLAP experimental data (http://www.cfd-online.com/Forums/main/117012-naca-0012-flap-experimental-data.html)

ferra89 April 30, 2013 10:14

NACA 0012 FLAP experimental data
 
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?

Thanks

Aeronautics El. K. May 1, 2013 11:08

1. Theory of wing sections
2. nasa's website


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