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Mechanical Engineering · Q281

Compressors, Gas Turbines And Jet Engines

Engineering and GATE · Mechanical Engineering · question 281

Q281

As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

A.
Increases
Answer
B.
Decreases
C.
Remain same
D.
First increases and then decreases

Answer: Option A

Solution

Answer: Option A
Solution:
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio Increases