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GATE 2022 AE – Question 44

Propulsion · Intakes and nozzles: non-rotating propulsion components · 2 marks · Multiple select

A convergent nozzle fed from a constant pressure, constant temperature reservoir, is discharging air to atmosphere at 1 bar (absolute) with choked flow at the exit (marked as Q). Flow through the nozzle can be assumed to be isentropic. If the exit area of the nozzle is increased while all the reservoir parameters and ambient conditions remain the same, then at steady state

source diagram and its labels are reproduced in the attached image.
  1. the nozzle will remain choked
  2. the nozzle will be un-choked
  3. the Mach number at section P will increase
  4. the Mach number at section P will decrease

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Correct answer: (A) the nozzle will remain choked; (C) the Mach number at section P will increase

Explanation

**Choked flow in a convergent nozzle.** The exit is choked ($M=1$) as long as the reservoir pressure is high enough compared with the back pressure (here the ratio of the reservoir pressure to 1 bar exceeds about 1.893 for air). The reservoir conditions and the ambient pressure do not change, so the condition for choking is still satisfied.

Answer **A and C**.