Compressors, Gas Turbines and Jet Engines
Isothermal compression though most efficient, but is not practicable because

It is impossible in practice
It does not increase pressure much
It requires very big cylinder
Compressor has to run at very slow speed to achieve it

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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
Decrease continuously
Increase first at slow rate and then fast

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