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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

256 bar
1 bar
64 bar
16 bar

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Adiabatic
None of these
Isothermal
Polytropic

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

10 bar
50 bar
30 bar
20 bar

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Compressors, Gas Turbines and Jet Engines
Ratio of indicated h.p. to shaft h.p. in known as

Compressor efficiency
Volumetric efficiency
Isothermal efficiency
Mechanical efficiency

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Compressors, Gas Turbines and Jet Engines
Which of the following fuels can be used in turbojet engines?

Methyl alcohol
Liquid hydrogen
High speed diesel oil
Kerosene

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Compressors, Gas Turbines and Jet Engines
An after-cooler is used to

Cool the air
Reduce volume of air
Remove impurities from air
Cause moisture and oil vapour to drop out

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