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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
For perfect intercooling in a two stage compressor

p₁ = p3
p₁/p₃ = p₂/p₁
p₁ = p₂ p3
p₂/p₁ = p₃/p₂

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Compressors, Gas Turbines and Jet Engines
With the decrease in compression ratio, the volumetric efficiency

Decreases
Increases
Does not change
First decrease and then increase

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Compressors, Gas Turbines and Jet Engines
Only rocket engines can be propelled to space because

They are not air breathing engines
These engines can work on several fuels
They can generate very high thrust
They have high propulsion efficiency

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Compressors, Gas Turbines and Jet Engines
Fighter bombers use following type of engine

Rocket
Turbojet
Turbo-propeller
Ramjet

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Compressors, Gas Turbines and Jet Engines
For speed above 3000 km/hour, it is more advantageous to use

Propellers
Rockets
Ramjet engine
Turbojet engine

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Compressors, Gas Turbines and Jet Engines
Cylinder clearance in a compressor should be

About 50% of swept volume
As large as possible
As small as possible
About 100% of swept volume

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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