Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

Remain same
Decrease
None of these
Increase

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Compressors, Gas Turbines and Jet Engines
Which of the following statement is correct as regard to centrifugal compressors?

The flow of air is parallel to the axis of the compressor
The maximum efficiency is higher than multistage axial flow compressors
The impeller rotates at high speeds
The static pressure of air in the impeller increases in order to provide centripetal force on the air

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