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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The pressure of air at the beginning of the compression stroke is ___ the atmospheric pressure.

More than
Equal to
Less than
None of the listed here

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Higher volumetric efficiency
Decreased discharge temperature
Lower power consumption per unit of air delivered
All of these

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Compressors, Gas Turbines and Jet Engines
The ratio of the discharge pressure to the inlet pressure of air is called

Expansion ratio
Compressor efficiency
Compression ratio
Volumetric efficiency

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Compressors, Gas Turbines and Jet Engines
Stalling of blades in axial flow compressor is the phenomenon of

Air stream not able to follow the blade contour
Air stream blocking the passage
Unsteady periodic and reversed flow
Motion of air at sonic velocity

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Compressor
Cooling chamber
All of these
Heating chamber

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor decreases with ________ in compression ratio.

Does not change
Decrease
Increase
Remain same

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