Aerospace Engineering > GATE 2014 > Engine Performance
The thrust produced by a turbojet engine
A
Increases with increasing compressor pressure ratio
B
Decreases with increasing compressor pressure ratio
C
Remains constant with increasing compressor pressure ratio
D
First increases and then decreases with increasing compressor pressure ratio

Correct : d

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thrust turbojet engine GATE Aerospace Engineering 2014 compressor pressure ratio effect turbojet thrust aerospace engineering gate compressor pressure ratio turbojet engine thrust GATE 2014 Q30

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