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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The gas in cooling chamber of a closed cycle gas turbine is cooled at

Constant pressure
Constant temperature
Constant volume
None of the listed here

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Compressors, Gas Turbines and Jet Engines
In jet engines the products of combustion after passing through the gas turbine are discharged into

Discharge nozzle
Vacuum
Atmosphere
Back to the compressor

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Compressors, Gas Turbines and Jet Engines
The material commonly used for air craft gas turbine is

High alloy steel
Duralumin
Timken, Haste alloys
Stainless steel

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Compressors, Gas Turbines and Jet Engines
The maximum propulsion efficiency of a turbojet is attained at around following speed

1700 km/hr
550 km/hr
1050 km/hr
2400 km/hr

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Compressors, Gas Turbines and Jet Engines
Gas turbines use following type of air compressor

Lobe type
Axial flow type
Reciprocating type
Centrifugal type

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Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

4-stroke petrol engine
Gas turbine
4-stroke diesel engine
Multi cylinder engine

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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