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Naca 2414 airfoil database3/21/2024 ![]() ![]() The 15 indicates that the airfoil has a 15% thickness to chord length ratio: it is 15% as thick as it is long. National Advisory Committee for Aeronautics airfoils. The NACA 0015 airfoil is symmetrical, the 00 indicating that it has no camber. įor example, the NACA 2412 airfoil has a maximum camber of 2% located 40% (0.4 chords) from the leading edge with a maximum thickness of 12% of the chord.
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