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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Ideal compression
Isothermal compression
Isentropic compression
Adiabatic compression

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Compressors, Gas Turbines and Jet Engines
The effective power of gas turbines is increased by adding the following in compressor

Nitrogen
Hydrogen
Ammonia and water vapour
Carbon dioxide

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

Lower heating value
Heating value
Higher calorific value
Higher heating value

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Compressors, Gas Turbines and Jet Engines
The gas in cooling chamber of a closed cycle gas turbine is cooled at

Constant temperature
Constant pressure
None of the listed here
Constant volume

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Compressors, Gas Turbines and Jet Engines
If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches

Adiabatic
Isothermal
Isochoric
Isentropic

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

Higher at high speed
Same at all altitudes
Lower at low speed
Higher at high altitudes

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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