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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

Remain same
Increase
Decrease
May increase or decrease depending on clearance volume

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Compressors, Gas Turbines and Jet Engines
The compressor capacity with decrease in suction temperature

Decreases
Remain unaffected
Increases
May increase or decrease depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
A simple turbojet engine is basically

Ramjet engine
Chemical rocket engine
Gas turbine engine equipped with a propulsive nozzle and diffuse
A propeller system

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitudes will require ___ power.

None of the listed here
More
Same
Less

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Compressors, Gas Turbines and Jet Engines
In jet propulsion power unit, the inlet duct of diverging shape is used in order to

Provide robust structure
Convert kinetic energy of air into pressure energy
Beautify the shape
Collect more air

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Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

Same
None of these
Lower
Higher

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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