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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine may be improved by

Increasing the compression work
Increasing the turbine work
Decreasing the compression work
Both (A) and (C) above

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Compressors, Gas Turbines and Jet Engines
The pressure ratio in gas turbines is of the order of

0.16736111111111
0.37569444444444
2.5423611111111
0.084027777777778

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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

16 bar
1 bar
64 bar
256 bar

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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 compressor performance at higher altitude compared to sea level will be

Lower
Same
Higher
Dependent on other factors

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Compressors, Gas Turbines and Jet Engines
Fighter bombers use following type of engine

Ramjet
Turbojet
Rocket
Turbo-propeller

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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