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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of work-done per cycle to the stroke volume of the compressor is known as

Compressor efficiency
Compression ratio
Compressor capacity
Mean effective pressure

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Compressors, Gas Turbines and Jet Engines
The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

First decreases and then increases
First increases and then decreases
Decreases
Increases

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

Compressor capacity
Swept volume
None of the listed here
Free air delivery

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In two phases
In the form of air and water mixture
In three phases
In a single phase

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

Decrease
May increase or decrease depending on clearance volume
Increase
Remain same

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Compressors, Gas Turbines and Jet Engines
In turbo fan engine, the jet velocity as compared to turbojet engine is

Less
More
May be less or more depending upon speed
Same

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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