1.

The cl,max for the NACA LS (1) – 0417 is higher than that for the NACA 2412.(a) False(b) TrueThe question was asked in unit test.Query is from Modern Low Speed Airfoils topic in section Incompressible Flow over Airfoils of Aerodynamics

Answer»

Correct option is (b) True

Best EXPLANATION: The new low-speed AIRFOILS had considerably higher maximum LIFT coefficients (around 30% higher) when compared to the standard NACA airfoils.



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