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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Ideal compression
Isothermal compression
Adiabatic compression
Isentropic compression

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

Less than
None of these
Equal to
More than

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is expressed in

m³/min
kg/m³
m³/kg
kg/m²

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in multistage compressors is done

To enable compression in two stages
To cool the air during compression
To minimize the work of compression
To cool the air at delivery

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Compressors, Gas Turbines and Jet Engines
For minimum work required to compress and deliver a quantity of air by multistage compression

The work-done in each stage should be same
The intercooling should be perfect
The compression ratio in each stage should be same
All of the listed here

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Compressors, Gas Turbines and Jet Engines
Gas turbines use following type of air compressor

Centrifugal type
Lobe type
Reciprocating type
Axial flow type

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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