1.

What is the relation between coefficient of pressure in terms of gamma and Mach number?

A. Cp = \(\frac {1}{γM_∞^2}\)) (1 – \(\frac {p}{p_∞}\))
B. Cp = \(\frac {2}{γM_∞^2}\)(\(\frac {p}{p_∞}\) – 1)
C. Cp = γM\(_∞^2\)(\(\frac {p}{p_∞}\))
D. Cp = \(\frac {γM_∞^2}{2} (\frac {p}{p_∞ – 1})\)
Answer» C. Cp = γM\(_∞^2\)(\(\frac {p}{p_∞}\))


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