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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum propulsion efficiency of a turbojet is attained at around following speed

1050 km/hr
2400 km/hr
1700 km/hr
550 km/hr

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

More than
None of these
Less than
Equal to

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Compressors, Gas Turbines and Jet Engines
An air receiver is to be placed outside. Should it be placed in

Shade
Rain
Sun
Enclosed room

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

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Compressors, Gas Turbines and Jet Engines
A jet engine has

Propeller in front
Propeller on the top
Propeller at back
No propeller

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Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

2 kg/cm²
14.7 kg/cm²
10 kg/cm²
6 kg/cm²

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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