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Search: Posts Made By: ferra89
Forum: Main CFD Forum April 30, 2013, 10:14
Replies: 1
Views: 1,743
Posted By ferra89
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...
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