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Compressors, Gas Turbines and Jet Engines

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

50 bar
20 bar
10 bar
30 bar

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

Axial flow
Centrifugal
Radial flow
None of these

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

16 bar
256 bar
64 bar
1 bar

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Compressors, Gas Turbines and Jet Engines
The combustion efficiency of a gas turbine using perfect combustion chamber is of the order of

0.75
0.85
0.9
0.99

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

Higher
Lower
Dependent on other factors
Same

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Compressors, Gas Turbines and Jet Engines
The clearance volume of the air compressor is kept minimum because

It permits isothermal compression
It allows maximum compression to be achieved
It results in minimum work
It greatly affects volumetric efficiency

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