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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is 5 m/min refers to

Standard air
Free air
Compressed air
Compressed air at delivery pressure

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency, even when running at high speed, can be approached by using

Both (A) and (B) above
Multistage compression
Cold water spray
Fully insulating the cylinder

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Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor, without clearance volume, the work-done is minimum during

None of these
Isentropic compression
Isothermal compression
Polytropic compression

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

All of these
Decreased discharge temperature
Higher volumetric efficiency
Lower power consumption per unit of air delivered

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

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

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Compressors, Gas Turbines and Jet Engines
Only rocket engines can be propelled to space because

They have high propulsion efficiency
These engines can work on several fuels
They can generate very high thrust
They are not air breathing engines

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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