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Compressors, Gas Turbines and Jet Engines

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

Centrifugal
None of these
Axial flow
Radial flow

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

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

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

700°C
2000°C
1000°C
1500°C

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the branch connections from compressed air lines should be taken from

Top side of main
Bottom side of main
Right side of main
Left side of main

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Pumps
All of these
Radial flow compressors
Axial flow compressors

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Compressors, Gas Turbines and Jet Engines
The output of a gas turbine is 300 KW and its efficiency is 20 percent, the heat supplied is

15 KW
600 KW
150 KW
6000 KW

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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