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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

Compressor efficiency
Compressor capacity
Compression ratio
Mean effective pressure

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Compressors, Gas Turbines and Jet Engines
Standard air is the air at ___ and relative humidity of 36 percent.

0.1 bar and 20°C
1 bar and 20°C
0.1 bar and 40°C
1 bar and 40°C

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

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

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Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Ericsson cycle
Rankine cycle
Carnot cycle
Brayton or Atkinson cycle

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Compressors, Gas Turbines and Jet Engines
The air is delivered ________ in one revolution in case of a three lobbed rotor.

Four times
Six times
Two times
Three times

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Compressors, Gas Turbines and Jet Engines
The maximum propulsion efficiency of a turbojet is attained at around following speed

2400 km/hr
1050 km/hr
1700 km/hr
550 km/hr

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