The lift per unit span for a thin, cambered airfoil with =5 , A0=0.65 – McqOptions

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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)

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