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Compressors, Gas Turbines and Jet Engines

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

Ideal compression
Isentropic compression
Adiabatic compression
Isothermal compression

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Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Remain constant
Decreases
First decreases and then increases
Increases

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Compressors, Gas Turbines and Jet Engines
Rotary compressors are used for delivering

Large quantities of air at high pressures
Small quantities of air at high pressures
Small quantities of air at low pressures
Large quantities of air at low pressures

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

More loss of air due to leakage past the cylinder
Air can be cooled perfectly in between
Better lubrication is possible advantages of multistage
Mechanical balance is better

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Compressors, Gas Turbines and Jet Engines
The compressor capacity with decrease in suction temperature

Remain unaffected
Decreases
Increases
May increase or decrease depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
The stagnation pressure rise in a centrifugal compressor takes place

In the impeller only
In the diffuser only
In the inlet guide vanes only
In the diffuser and impeller

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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