Compressors, Gas Turbines and Jet Engines
For minimum work in multistage compression, assuming same index of compression in all stages

Work done in subsequent stages should increase
Work done in subsequent stages should decrease
Work done in all stages should be equal
Work done in first stage should be more

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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

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

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