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

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

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Compressors, Gas Turbines and Jet Engines
Intercooling in gas turbines

Increases net output and thermal efficiency both
Decreases net output but increases thermal efficiency
Decreases net output and thermal efficiency both
Increases net output but decreases thermal efficiency

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