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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In air breathing jet engine, the jet is formed by expanding

Plasma
Solids
Highly heated atmospheric air
Liquid

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

at the tip
at the base
between ~ to i of the blade height
in the center

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

Decrease
Increase
Remain same
May increase or decrease depending on clearance volume

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio is used in gas turbines

To save fuel
To increase the efficiency
To increase the output
To reduce the exit temperature

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

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

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor

Increases with decrease in compression ratio
Decreases with increase in compression ratio
Decreases with decrease in compression ratio
Increases with increase in compression ratio

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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