Aerospace Engineering > GATE 2015 > Engine Components Efficiency
Isentropic efficiencies of an aircraft engine operating at typical subsonic cruise conditions with the following components - intake, compressor, turbine and nozzle - are denoted by ηi ηc η, and ηn respectively. Which one of the following is correct?
A
ηt<ηc<ηt<ηn
B
ηt<ηt<ηc<ηn
C
ηc<ηt<ηi<ηn
D
ηc<ηt<ηt<ηn

Correct : c

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Related Topics

Isentropic efficiency aircraft engine efficiency GATE Aerospace Engineering 2015 Q34 Aerospace Engineering GATE engine component efficiency comparison compressor turbine nozzle efficiency subsonic cruise engine

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