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Compressors, Gas Turbines and Jet Engines

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

Rockets
Propellers
Ramjet engine
Turbojet engine

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In two phases
In the form of air and water mixture
In a single phase
In three phases

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

Same
More
Depends on other factors
Less

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is 5 m/min refers to

Free air
Standard air
Compressed air
Compressed air at delivery pressure

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Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Increases/decreases depending on compressor capacity
Increases
Decreases
Remains same

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Compressors, Gas Turbines and Jet Engines
A rocket engine uses __________ for the combustion of its fuel.

Surrounding air
Compressed atmospheric air
Its own oxygen
None of these

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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