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Compressors, Gas Turbines and Jet Engines

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

Constant pressure
None of the listed here
Constant temperature
Constant volume

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
The air-fuel ratio in gas turbines is of the order of

30: 1
15: 1
7: 1
50: 1.

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Compressors, Gas Turbines and Jet Engines
The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)

(v₁ - v₂)²/2g
(v₁² -v₂²)/g
(v₁ - v₂)²/g
(v₁² -v₂²)/2g

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

Increase efficiency
Control temperature
Control output of turbine
Control fire hazards

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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