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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Diffuser inlet radius
Diffuser outlet radius
Impeller outlet radius
Impeller inlet radius

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Compressors, Gas Turbines and Jet Engines
In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into

Discharge nozzle
Vacuum
Back to the compressor
Atmosphere

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Compressors, Gas Turbines and Jet Engines
An after-cooler is used to

Reduce volume of air
Remove impurities from air
Cool the air
Cause moisture and oil vapour to drop out

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Compressors, Gas Turbines and Jet Engines
A rocket engine uses __________ for the combustion of its fuel.

Surrounding air
Compressed atmospheric air
None of these
Its own oxygen

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Compressors, Gas Turbines and Jet Engines
In a jet engine, the air-fuel ratio is

2.0840277777778
1.2506944444444
1.6673611111111
2.5006944444444

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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