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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The air is delivered ________ in one revolution in case of a three lobbed rotor.

Three times
Four times
Six times
Two times

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

One fourth
One sixth
One-half
Same

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

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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

Axial
Reciprocating
Centrifugal
Screw

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Compressors, Gas Turbines and Jet Engines
The compression ratio in a gas turbine is of the order of

0.33402777777778
0.50069444444444
0.20902777777778
3.5 : 1

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Compressors, Gas Turbines and Jet Engines
The efficiency of jet engine is

Same at all altitudes
Lower at low speed
Higher at high altitudes
Higher at high speed

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