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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Isentropic compression
None of the listed here
Isothermal compression
Polytropic compression

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in gas turbines, is of

Axial flow type
None of the listed here
Centrifugal type
Radial flow type

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the compressed air main line should

Rise gradually towards the point of use
Drop gradually towards the point of use
Be laid exactly horizontally
Be laid vertically

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Compressors, Gas Turbines and Jet Engines
Stalling of blades in axial flow compressor is the phenomenon of

Air stream blocking the passage
Air stream not able to follow the blade contour
Motion of air at sonic velocity
Unsteady periodic and reversed flow

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

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

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Compressors, Gas Turbines and Jet Engines
When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be

Backward curved
Radial
None of the listed here
Forward curved

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