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

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1.	For α=5°, A0=1 and A1=-2 total circulation Γ for a thin cambered airfoil equals______
A.	0
B.	2πcV∞
C.	πcV∞
D.	2.5πcV∞
Answer» B. 2πcV∞

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