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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
A rocket engine uses __________ for the combustion of its fuel.

Its own oxygen
Surrounding air
Compressed atmospheric air
None of these

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Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

Axial compressor
Centrifugal compressor
All of these
Pumps

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Other factors control it
Remain unaffected
Decrease
Increase

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Compressors, Gas Turbines and Jet Engines
Phenomenon of choking in compressor means

Fixed mass flow rate regardless of pressure ratio
Increased inclination of chord with air steam
Reducing mass flow rate with increase in pressure ratio
No flow of air

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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