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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Slip factor
Pressure coefficient
Work factor
Degree of reaction

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Compressors, Gas Turbines and Jet Engines
Efficiency of gas turbine is increased by

Inter cooling
Adding a regenerator
Reheating
All of the listed here

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Compressors, Gas Turbines and Jet Engines
The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is

Low
Low/high depending on make and type
Same
High

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Compressors, Gas Turbines and Jet Engines
An after-cooler is used to

Reduce volume of air
Cool the air
Cause moisture and oil vapour to drop out
Remove impurities from air

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Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

1.0 kg
2.2 kg
1.3 kg
0.5 kg

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Higher
Lower
Can't be compared
Equal

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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