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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

Back pressure
None of the listed here
Critical pressure
Discharge pressure

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Compressors, Gas Turbines and Jet Engines
Rotary compressor is best suited for

Small quantity of air at low pressure
Large quantity of air at low pressure
Large quantity of air at high pressure
Small quantity of air at high pressure

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

0.1%
1.0%
5%
0.5%

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Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

Velocity coefficient
Slip factor
None of these
Velocity factor

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Compressors, Gas Turbines and Jet Engines
Diffuser in a compressor is used to

Make the flow streamline
Convert kinetic energy into pressure energy
Increase velocity
Convert pressure energy into kinetic energy

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Compressors, Gas Turbines and Jet Engines
Ratio of indicated h.p. to shaft h.p. in known as

Isothermal efficiency
Volumetric efficiency
Mechanical efficiency
Compressor efficiency

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