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

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

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Compressors, Gas Turbines and Jet Engines
The assumption made in two stage compression with inter-cooler is that

There is no pressure drop in the inter-cooler
All of the listed here
The suction and delivery of air takes place at constant pressure
The compression in both the cylinders is polytropic

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