The pressure and temperature ratios across a given portion of a shock wave in the air are
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Question:
The pressure and temperature ratios across a given portion of a shock wave in the air are p2/p1 = 4.5 and T2/T1 = 1.687, where 1 and 2 denote conditions ahead of and behind the shock wave, respectively. Calculate the change in entropy in units of
(a) (ft . lb)/(slug . OR)
(b) J/(kg . K).
Related Book For
Thermodynamics for Engineers
ISBN: ?978-1133112860
1st edition
Authors: Kenneth A. Kroos, Merle C. Potter
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