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1. |
The lift per unit span for a thin, cambered airfoil with =5 , A0=0.65, A1=1 is____ |
A. | L = c (V_ ^2 ) <sub> </sub> (1.15) |
B. | L = c (V_ ^2 ) <sub> </sub> (1.65) |
C. | L = c (V_ ^2 ) <sub> </sub> (-0.35) |
D. | L = c (V_ ^2 ) <sub> </sub> (0.15) |
Answer» B. L = c (V_ ^2 ) <sub> </sub> (1.65) | |