A convergingdiverging nozzle is designed to generate an exit Mach number of 2. The nozzle is supplied
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Question:
A converging–diverging nozzle is designed to generate an exit Mach number of 2. The nozzle is supplied with air from a large reservoir in which the pressure is kept at 6.5 MPa. Assuming one-dimensional isentropic flow, find
a. The maximum back-pressure at which the nozzle will be choked
b. The range of back-pressures over which there will be a shock in the nozzle
c. The design back-pressure
d. The range of back-pressures over which there is supersonic flow on the nozzle exit plane
Related Book For
Thermodynamics An Interactive Approach
ISBN: 978-0130351173
1st edition
Authors: Subrata Bhattacharjee
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