Compressors, Gas Turbines and Jet Engines - Mechanical Engineering Questions and Answers

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

Increases

Decreases

First increases and then decreases

First decreases and then increases

Answer : Option A

Explanation :

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

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