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Compressors, Gas Turbines and Jet Engines

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

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

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

Impeller channel losses
Diffuser losses
Inlet losses
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

Decreases
First decreases and then increases
Increases
Remain constant

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

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

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Compressors, Gas Turbines and Jet Engines
The air is delivered ________ in one revolution in case of a three lobbed rotor.

Three times
Four times
Six times
Two times

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

All of these
Pumps
Axial flow compressors
Radial flow compressors

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