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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Higher
Can't be compared
Equal
Lower

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

Ammonia and water vapour
Carbon dioxide
Hydrogen
Nitrogen

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

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

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Compressors, Gas Turbines and Jet Engines
The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is

Low
Same
High
Low/high depending on make and type

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

May increase or decrease depending on clearance volume
Increase
Decrease
Remain same

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

Two or more air streams
Solid fuel firing
No air stream
One air stream

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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