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
ηtctn
B
ηttcn
C
ηctin
D
ηcttn

Correct : c

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