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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

More
Same
Zero
Less

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Compression of inlet air
Increasing speed of incoming air
Reduction of speed of incoming air and conversion of part of it into pressure energy
Lost work

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Compressors, Gas Turbines and Jet Engines
The process, which causes the air to enter the impeller blades of a centrifugal compressor at ________ velocity (without effecting the mass of air to flow and velocity of flow) is known as prewhirl.

None of these
Reduced
Increased
Zero

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

16 bar
1 bar
64 bar
256 bar

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Propulsive power and fuel input
Thrust power and propulsive power
Thrust power and fuel energy
Engine output and propulsive power

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

200°C
700°C
1000°C
500°C

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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