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Compressors, Gas Turbines and Jet Engines

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

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

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

500°C
700°C
1000°C
200°C

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

Same
Zero
Less
More

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Compressors, Gas Turbines and Jet Engines
A turboprop is preferred to turbojet because

It has high power for take off
It can fly at supersonic speeds
It can fly at high elevations
It has high propulsive efficiency at high speeds

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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
Diffuser in a compressor is used to

Convert kinetic energy into pressure energy
Convert pressure energy into kinetic energy
Increase velocity
Make the flow streamline

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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