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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\(_∞^2\)(\(\frac {p}{p_∞}\)) | |