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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Produces uniform torque
Has more efficiency
Can be driven at a very high speed
All of the listed here

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Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Remain constant
Decreases
First decreases and then increases
Increases

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

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

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Compressors, Gas Turbines and Jet Engines
Phenomenon of choking in compressor means

Reducing mass flow rate with increase in pressure ratio
Increased inclination of chord with air steam
No flow of air
Fixed mass flow rate regardless of pressure ratio

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Compressors, Gas Turbines and Jet Engines
Which of the following fuels can be used in turbojet engines?

Liquid hydrogen
Kerosene
Methyl alcohol
High speed diesel oil

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Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.4
0.3
0.5
0.2

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