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Compressors, Gas Turbines and Jet Engines

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

Control temperature
Control output of turbine
Control fire hazards
Increase efficiency

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

None of the listed here
Constant volume
Constant temperature
Constant pressure

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Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Isothermal H.P./shaft H.R
Total output/air input
Isothermal H.P/indicated H.R
Compression work/motor input

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Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor, without clearance volume, the work-done is minimum during

Polytropic compression
None of these
Isentropic compression
Isothermal compression

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Compressors, Gas Turbines and Jet Engines
The air power of the compressor is also known as

Brake power
Frictional power
Indicated power
None of these

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Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

Remain same
Decreases
Increases
First increases and then decreases

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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