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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work done per unit mass of air in compression will be least when 'n' is equal to

1
1.3
1.2
1.4

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

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Compressors, Gas Turbines and Jet Engines
A jet engine works on the principle of conservation of

Linear momentum
Mass
Flow
Energy

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Both (A) and (B) above
Decrease of thermal efficiency
Increase of work ratio
Decrease of work ratio

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Compressors, Gas Turbines and Jet Engines
For supplying intermittent small quantity of air at high pressure, following compressor is best suited

Screw
Reciprocating
Axial
Centrifugal

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

None of the listed here
Compressor capacity
Free air delivery
Swept volume

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