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

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

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

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

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