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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency can be attained by running the compressor

At very slow speed
At average speed
At zero speed
At very high speed

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Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

14.7 kg/cm²
2 kg/cm²
10 kg/cm²
6 kg/cm²

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Compressors, Gas Turbines and Jet Engines
In a jet engine, the air-fuel ratio is

1.6673611111111
2.0840277777778
2.5006944444444
1.2506944444444

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Lost work
Reduction of speed of incoming air and conversion of part of it into pressure energy
Compression of inlet air
Increasing speed of incoming air

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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
Mechanical balance is better
Better lubrication is possible advantages of multistage

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Compressors, Gas Turbines and Jet Engines
Out of the following, from where you will prefer to take intake for air compressor

From outside atmosphere at 1°C
From coal yard side
From an air conditioned room maintained at 20°C
From a side where cooling tower is located nearby

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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