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Compressors, Gas Turbines and Jet Engines

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

Nitrogen
Carbon dioxide
Ammonia and water vapour
Hydrogen

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Propulsive power and fuel input
Thrust power and fuel energy
Engine output and propulsive power
Thrust power and propulsive power

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine works on

Rankine cycle
Ericsson cycle
Carnot cycle
Joule cycle

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Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

Same
Less
More
More/less depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
A rocket works with maximum overall efficiency when air craft velocity is equal to the

Twice the jet velocity
Average of the jet velocity
Half the jet velocity
Jet velocity

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Lost work
Increasing speed of incoming air
Compression of inlet air
Reduction of speed of incoming air and conversion of part of it into pressure energy

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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