Air enters a device with a Mach number of (M_{1}=2.0) and leaves with (M_{2}=0.25). The ratio of
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Air enters a device with a Mach number of \(M_{1}=2.0\) and leaves with \(M_{2}=0.25\). The ratio of exit to inlet area is \(A_{2} / A_{1}=3.0\).
(a) Find the static pressure ratio \(p_{2} / p_{1}\).
(b) Determine the stagnation pressure ratio \(p_{t 2} / p_{t 1}\).
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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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