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

Decreases
First increases and then decreases
First decreases and then increases
Increases

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Compressors, Gas Turbines and Jet Engines
The mean effective pressure of the compressor is the

None of these
Actual volume of the air delivered by the compressor when reduced to normal temperature and pressure conditions
Volume of air delivered by the compressor
Volume of air sucked by the compressor during its suction stroke

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