Compressors, Gas Turbines and Jet Engines
Axial flow compressor has the following advantage over centrifugal compressor

Larger air handling ability per unit frontal area
Higher pressure ratio per stage
Higher average velocities
Aerofoil blades are used

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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
Bled gas from turbine is heated and readmitted for complete expansion
Heated

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