The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

Questions › Category: Compressors Gas Turbines and Jet Engines › The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio
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The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

(A) Increases            (Ans)

(B) Decreases

(C) First increases and then decreases

(D) First decreases and then increases

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