Aerospace Engineering > GATE 2010 > Engine Performance
How does the specific thrust, at constant turbine inlet temperature, produced by a turbofan engine
change with an increase in compressor pressure ratio?
A
Increases
B
Decreases
C
First increases and then decreases
D
First decreases and then increases

Correct : c

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Related Topics

GATE Aerospace Engineering 2010 GATE AE 2010 Q21 turbofan engine specific thrust compressor pressure ratio turbine inlet temperature aircraft propulsion specific thrust vs pressure ratio

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