For a thin airfoil kept at a supersonic flow of Mach number 3 at an i – McqOptions

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1.	For a thin airfoil kept at a supersonic flow of Mach number 3 at an inclination of 2 degrees, what is the coefficient of pressure?
A.	0.47
B.	1.51
C.	1.78
D.	2.83
Answer» E.

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