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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The process, which causes the air to enter the impeller blades of a centrifugal compressor at ________ velocity (without effecting the mass of air to flow and velocity of flow) is known as prewhirl.

Zero
Reduced
Increased
None of these

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Pressure coefficient
Compressor efficiency
Euler
Isentropic efficiency

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Compressors, Gas Turbines and Jet Engines
The effective power of gas turbines is increased by adding the following in compressor

Hydrogen
Carbon dioxide
Nitrogen
Ammonia and water vapour

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

Surrounding air
None of these
Compressed atmospheric air
Its own oxygen

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

8 to 10 bar
5 to 8 bar
10 to 15 bar
1 to 5 bar

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

Axial flow
Centrifugal
None of these
Radial flow

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