Jet Engine Compressor Pressure Ratio Limit: Separation Explained | GATE Aerospace 2011

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Aerospace Engineering > GATE 2011 > Compressor Performance

The pressure ratio in any one stage of a jet engine compressor is limited by

A

entry stagnation temperature in that stage

B

entry Mach number in that stage

C

pressure gradient induced separation in that stage

D

mass flow rate in that stage

Correct : c

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