Nitrogen flows through a converging-diverging nozzle designed to operate at a Mach number of 3.0. If it
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Nitrogen flows through a converging-diverging nozzle designed to operate at a Mach number of 3.0. If it is subjected to an operating pressure ratio of 0.5 :
(a) Determine the Mach number at the exit.
(b) What is the entropy change in the nozzle?
(c) Compute the area ratio at the shock location.
(d) What value of the operating pressure ratio would be required to move the shock to the exit?
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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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