Compressors, Gas Turbines and Jet Engines
The following is true for an open cycle gas turbine having exhaust heat exchanger. Atmospheric air before entering the compressor is

Bled gas from turbine is heated and readmitted for complete expansion
Compressed air before entering the combustion chamber is heated
Exhaust gases drive the compressor
Heated

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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

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

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