Compressors, Gas Turbines and Jet Engines
The specific output per kg mass flow rate of a gas turbine (having fixed efficiencies of compressor and turbine and fixed higher and lower temperature) with increase in pressure ratio will

Decrease continuously
Increase first at slow rate and then fast
First increase, reach maximum and then decrease
Increase first at fast rate and then slow

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

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

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