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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work-done on a compressor will be minimum if air is taken from

A source of high temperature air
A source at 0° C
A source of low temperature air
The atmosphere

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

Work ratio
Pressure ratio
None of these
Compression ratio

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

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

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Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Increases/decreases depending on compressor capacity
Decreases
Remains same
Increases

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Compressors, Gas Turbines and Jet Engines
In turbo fan engine, the jet velocity as compared to turbojet engine is

Same
More
Less
May be less or more depending upon speed

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Compressors, Gas Turbines and Jet Engines
The efficiency of jet engine is

Same at all altitudes
Lower at low speed
Higher at high speed
Higher at high altitudes

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