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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor decreases with ________ in compression ratio.

Decrease
Increase
Does not change
Remain same

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

Better lubrication is possible advantages of multistage
Mechanical balance is better
More loss of air due to leakage past the cylinder
Air can be cooled perfectly in between

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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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Compressors, Gas Turbines and Jet Engines
The compressor performance at higher altitude compared to sea level will be

Same
Higher
Dependent on other factors
Lower

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It is bulky
It is inefficient
None of these
It requires cooling water for its operation

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

Same
More
Less
Depends on other factors

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