Plot (p_{2} / p_{1}, T_{2} / T_{1}, p_{02} / p_{01}, T_{02} / T_{01}), and (M_{2}) from (M_{1}=1)

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Plot \(p_{2} / p_{1}, T_{2} / T_{1}, p_{02} / p_{01}, T_{02} / T_{01}\), and \(M_{2}\) from \(M_{1}=1\) to \(M_{1}=10\) assuming that the gas is air \((\gamma=1.4)\) and Krypton \((\gamma=1.68)\). What is the effect of changing the specific heat ratio of the gas? How accurate do you think your results at Mach 10 are?

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Related Book For  book-img-for-question

Fundamentals Of Aerodynamics ISE

ISBN: 9781266076442

7th Edition

Authors: John D. Anderson, Jr, Christopher P Cadou

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