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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A rotary compressor is driven by an

Engine
Electric motor
None of these
Either (A) or (B)

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

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

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Compressors, Gas Turbines and Jet Engines
The fuel consumption in gas turbines is accounted for by

Higher calorific value
Higher heating value
Heating value
Lower heating value

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

More power
Same power
Less power
More/less power depending on other factors

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

Remains same
Increases
Increases/decreases depending on compressor capacity
Decreases

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Compressors, Gas Turbines and Jet Engines
The output of a gas turbine is 300 KW and its efficiency is 20 percent, the heat supplied is

6000 KW
150 KW
600 KW
15 KW

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