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Compressors, Gas Turbines and Jet Engines

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
Compression ratio
Compressor capacity

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It requires cooling water for its operation
It is inefficient
It is bulky
None of these

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

More
Depends on other factors
Less
Same

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Compressors, Gas Turbines and Jet Engines
Open cycle gas turbine works on

Carnot cycle
Rankine cycle
Brayton or Atkinson cycle
Ericsson cycle

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

30 bar
20 bar
50 bar
10 bar

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Compressors, Gas Turbines and Jet Engines
In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into

Vacuum
Discharge nozzle
Back to the compressor
Atmosphere

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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