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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

High speeds
High altitudes
Low altitudes
Low speeds

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Compressors, Gas Turbines and Jet Engines
The compression ratio in a gas turbine is of the order of

3.5 : 1
0.50069444444444
0.33402777777778
0.20902777777778

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Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

Radial component
Axial component
Tangential component
None of these

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Produces uniform torque
Has more efficiency
All of the listed here
Can be driven at a very high speed

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Compressors, Gas Turbines and Jet Engines
The compressor capacity with decrease in suction temperature

Increases
Remain unaffected
May increase or decrease depending on compressor capacity
Decreases

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Compressors, Gas Turbines and Jet Engines
The fuel consumption in gas turbines is accounted for by

Higher heating value
Lower heating value
Heating value
Higher calorific value

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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