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Compressors, Gas Turbines and Jet Engines

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

Increase efficiency
Control output of turbine
Control temperature
Control fire hazards

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Compressors, Gas Turbines and Jet Engines
The maximum compression ratio in an actual single stage axial flow compressor is of the order of

0.048611111111111
0.00070833333333333
0.045138888888889
0.043055555555556

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Isothermal
Adiabatic
None of these
Polytropic

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

Corrosion resistance
Toughness
Fatigue
Creep

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Compressors, Gas Turbines and Jet Engines
The ratio of work-done per cycle to the stroke volume of the compressor is known as

Compressor capacity
Compression ratio
Compressor efficiency
Mean effective pressure

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Compressors, Gas Turbines and Jet Engines
Mining industry usually employs following motive power

Petrol engine
Diesel engine
C. electric motor
Compressed air

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