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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
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
A closed cycle gas turbine consists of a

Heating chamber
All of these
Cooling chamber
Compressor

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

500°C
1000°C
700°C
200°C

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Compressors, Gas Turbines and Jet Engines
A rocket works with maximum overall efficiency when air craft velocity is equal to the

Average of the jet velocity
Half the jet velocity
Jet velocity
Twice the jet velocity

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

Methyl alcohol
High speed diesel oil
Liquid hydrogen
Kerosene

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