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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
Losses in a centrifugal compressor are due to

Diffuser losses
Inlet losses
All of the listed here
Impeller channel losses

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Compressors, Gas Turbines and Jet Engines
Surging is the phenomenon of

Motion of air at sonic velocity
Air stream blocking the passage
Unsteady, periodic and reversed flow
Air stream not able to follow the blade contour

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Compressors, Gas Turbines and Jet Engines
A jet engine has

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

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

Uses compressed atmospheric air
Does not require oxygen
Carries its own oxygen
Uses surrounding air

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Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

4-stroke petrol engine
Gas turbine
Multi cylinder engine
4-stroke diesel engine

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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