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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In three phases
In two phases
In the form of air and water mixture
In a single phase

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

Free air delivery
Compressor capacity
None of the listed here
Swept volume

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in multistage compressors is done

To cool the air during compression
To cool the air at delivery
To enable compression in two stages
To minimize the work of compression

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Compressors, Gas Turbines and Jet Engines
The thermodynamic efficiency of rotary compressor is based on

Isentropic compression
Adiabatic compression
Polytropic compression
Isothermal compression

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

None of these
Radial flow type
Axial flow type
Centrifugal type

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Compressors, Gas Turbines and Jet Engines
In jet engines, paraffin is usually used as the fuel because of its

Ease of atomisation
High calorific value
Low freezing point
Both (A) and (C) above

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