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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work ratio of simple gas turbine cycle depends on

All of these
Minimum cycle temperature
Maximum cycle temperature
Pressure ratio

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Compressors, Gas Turbines and Jet Engines
Water is injected in gas turbine cycle to

Control temperature
Control fire hazards
Increase efficiency
Control output of turbine

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Compressors, Gas Turbines and Jet Engines
The ratio of work done per cycle to the swept volume in case of compressor is called

Compression index
Compressor efficiency
Mean effective pressure
Compression ratio

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

All of these
Decreased discharge temperature
Lower power consumption per unit of air delivered
Higher volumetric efficiency

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Compressors, Gas Turbines and Jet Engines
The following property is most important for material used for gas turbine blade

Creep
Toughness
Fatigue
Corrosion resistance

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Decrease of thermal efficiency
Decrease of work ratio
Increase of work ratio
Both (A) and (B) above

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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