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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

All of these
Compressor
Cooling chamber
Heating chamber

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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

Decrease
Remain unaffected
Other factors control it
Increase

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

Ramjet
Turbo-propeller
Rocket
Turbojet

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Compressors, Gas Turbines and Jet Engines
Rotary compressor is best suited for

Small quantity of air at low pressure
Large quantity of air at low pressure
Large quantity of air at high pressure
Small quantity of air at high pressure

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Compressors, Gas Turbines and Jet Engines
The effective power of gas turbines is increased by adding the following in compressor

Carbon dioxide
Hydrogen
Nitrogen
Ammonia and water vapour

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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