Plot (p_{2} / p_{1}, T_{2} / T_{1}, p_{02} / p_{01}, T_{02} / T_{01}), and (M_{2}) from (M_{1}=1)
Question:
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
Fundamentals Of Aerodynamics ISE
ISBN: 9781266076442
7th Edition
Authors: John D. Anderson, Jr, Christopher P Cadou
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