If (gamma=1.2) and the fluid is a perfect gas, what Mach number will give a temperature ratio
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If \(\gamma=1.2\) and the fluid is a perfect gas, what Mach number will give a temperature ratio of \(T / T_{t}=0.909\) ? What will the ratio of \(p / p_{t}\) be for this flow?
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Related Book For
Fundamentals Of Gas Dynamics
ISBN: 9781119481690
3rd Edition
Authors: Robert D Zucker, Oscar Biblarz
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