The static and total pressures of air downstream of a (30^{circ}) expansion corner are (0.0155 mathrm{~atm}) and
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The static and total pressures of air downstream of a \(30^{\circ}\) expansion corner are \(0.0155 \mathrm{~atm}\) and \(151.8 \mathrm{~atm}\), respectively. What are the Mach number and static pressure upstream of the expansion corner?
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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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