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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to steam turbine

All of these
Has compressor and combustion chamber
Requires less space for installation
Has less efficiency

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Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

High h.p. and low weight
High speed and high h.p.
Low weight and small frontal area
Small frontal area and high h.p.

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

10 bar
50 bar
30 bar
20 bar

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Compressors, Gas Turbines and Jet Engines
What will be the volume of air at 327°C if its volume at 27°C is 1.5 m³/ mt?

1.5 m³/ mt.
18 m³/ mt.
3 m³/ mt.
6 m³/ mt.

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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