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The thermal efficiency of a simple gas turbine for a given...

This question belongs to Mechanical Engineering Compressors, Gas Turbines And Jet Engines
Compressors, Gas Turbines and Jet Engines
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The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

Answer & Solution
Correct Answer: Option A
The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio Increases
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