1.

What is the formula for coefficient of drag over a circular cylinder at hypersonic speed?

A. cd = \(\frac {D}{q_∞ S}\)
B. cd = \(\frac {D}{2q_∞ S}\)
C. cd = \(\frac {2D}{q_∞ S}\)
D. cd = Dq∞S
Answer» B. cd = \(\frac {D}{2q_∞ S}\)


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