What is the lift coefficient over a flat plate at an angle of attack o – McqOptions

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1.	What is the lift coefficient over a flat plate at an angle of attack of 3 degrees in a supersonic flow at Mach 4?
A.	0.0512
B.	0.0541
C.	0.0628
D.	0.0714
Answer» C. 0.0628

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