The maximum lift co-efficient for NACA 19584 (chord=2.5m) airfoil is__ – McqOptions

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1.	The maximum lift co-efficient for NACA 19584 (chord=2.5m) airfoil is____
A.	0.15
B.	0.315
C.	0.15N
D.	0.3N
Answer» B. 0.315

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