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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The mass of gas turbine per kW developed is about ________ as that of an I.C. engine.

One-half
One sixth
One fourth
Same

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Compressors, Gas Turbines and Jet Engines
For minimum work required to compress and deliver a quantity of air by multistage compression

The work-done in each stage should be same
All of the listed here
The compression ratio in each stage should be same
The intercooling should be perfect

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Compressors, Gas Turbines and Jet Engines
In jet engines, for the efficient production of large power, fuel is burnt in an atmosphere of

Atmospheric air
Compressed air
Oxygen alone
Vacuum

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

5 to 8 bar
1 to 5 bar
10 to 15 bar
8 to 10 bar

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Compressors, Gas Turbines and Jet Engines
The ratio of work done per cycle to the swept volume in case of compressor is called

Compression ratio
Compressor efficiency
Mean effective pressure
Compression index

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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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