1.

What happens to the pressure behind an oblique shock wave at very high Mach numbers?

A. p2 = \(\frac {2sin^2 β}{γ + 1}\)
B. p2 = \(\frac {γ – 1}{γ + 1}\)
C. p2 = 1 – \(\frac {2sin^2 β}{γ + 1}\)
D. p2 = \(\frac {2sin 2 β}{γ + 1}\)
Answer» B. p2 = \(\frac {γ – 1}{γ + 1}\)


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