The diverging section of a supersonic nozzle is formed from the frustum of a cone. When operating
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The diverging section of a supersonic nozzle is formed from the frustum of a cone. When operating at its third critical point with nitrogen, the exit Mach number is 2.6 . Compute the operating pressure ratio that will locate a normal shock as shown in Figure P6.11.
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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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