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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Isentropic compression
None of the listed here
Polytropic compression
Isothermal compression

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

Fatigue
Creep
Toughness
Corrosion resistance

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor

Decreases with decrease in compression ratio
Increases with decrease in compression ratio
Decreases with increase in compression ratio
Increases with increase in compression ratio

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

Control output of turbine
Control temperature
Increase efficiency
Control fire hazards

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is 5 m/min refers to

Compressed air
Standard air
Compressed air at delivery pressure
Free air

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Compressors, Gas Turbines and Jet Engines
Ramjet engine

Produces a jet consisting of plasma
Requires no air for its operation
Is self operating at zero flight speed
Is not self operating at zero flight speed

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