For =5 , A0=1 and A1=-2 total circulation for a thin cambered airfo – McqOptions

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1.	For =5 , A₀=1 and A₁=-2 total circulation for a thin cambered airfoil equals______
A.	0
B.	2 cV<sub> </sub>
C.	cV<sub> </sub>
D.	2.5 cV<sub> </sub>
Answer» B. 2 cV<sub> </sub>

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