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Arrange these nozzle conditions in order of increasing pressure ratio:

1. Unchoked, with subsonic exit flow

2. Just choked, with sonic conditions at the throat

3. Choked and under-expanded, expanding outside the nozzle

4. Highly under-expanded, with a strongly expanding free jet

Select the correct sequence.

  • A.2, 1, 3, 4
  • B.1, 3, 2, 4
  • C.4, 3, 2, 1
  • D.1, 2, 3, 4

Answer: D

Once the throat is sonic the mass flow is fixed and further pressure ratio appears as exit pressure above ambient. Adding a divergent section converts part of that residual pressure into velocity and recovers the thrust it represents.

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