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Mechanical Engineering · Q54

Compressors, Gas Turbines And Jet Engines

Engineering and GATE · Mechanical Engineering · question 54

Q54

The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio)

A.
B.
C.
Answer
D.

Answer: Option C

Solution

Answer: Option C
Solution:
The overall thermal efficiency of an ideal gas turbine plant is
(Where r = Pressure ratio)
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