Aerospace Engineering > GATE 2013 > Engine Efficiency
For a given inlet condition, if the turbine inlet temperature is fixed, what value of compressor efficiency given below leads to the lowest amount of fuel added in the combustor of a gas turbine engine?
A
1
B
0.95
C
0.85
D
0.8

Correct : a

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Related Topics

compressor efficiency gas turbine engine gas turbine engine combustor GATE Aerospace Engineering 2013 turbine inlet temperature fuel added in combustor aerospace engineering gate gas turbine efficiency lowest fuel added

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