Aerospace Engineering > GATE 2023 > Turbojet Engines
In a single-spool aviation turbojet engine, which of the following is the correct relationship between the total work output WT of a 2-stage axial turbine and the total work required Wc by a 6-stage axial compressor, neglecting losses?
A
WT = 2WC
B
WT = 6WC
C
WT = WC
D
WT = 3WC

Correct : c

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