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Compressors, Gas Turbines and Jet Engines

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

Isentropic compression
Adiabatic compression
Isothermal compression
Ideal compression

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Compressors, Gas Turbines and Jet Engines
The ratio of work-done per cycle to the stroke volume of the compressor is known as

Mean effective pressure
Compressor efficiency
Compressor capacity
Compression ratio

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Compressors, Gas Turbines and Jet Engines
The compressor performance at higher altitude compared to sea level will be

Dependent on other factors
Same
Higher
Lower

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Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is perpendicular to its axis, then it is a

Centrifugal compressor
Axial flow compressor
Turbo compressor
Reciprocating compressor

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Euler
Compressor efficiency
Isentropic efficiency
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Decrease
Other factors control it
Increase
Remain unaffected

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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