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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compression ratio in a gas turbine is of the order of

0.50069444444444
0.20902777777778
0.33402777777778
3.5 : 1

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

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

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Compressors, Gas Turbines and Jet Engines
Propulsion efficiency of the following order is obtained in practice

0.34
0.5
0.72
0.6

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Compressors, Gas Turbines and Jet Engines
Reciprocating air compressor is best suited for

Large quantity of air at low pressure
Small quantity of air at high pressure
Small quantity of air at low pressure
Large quantity of air at high pressure

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of air compressors is of the order of

60 - 70%
70 - 90%
20 - 30%
40 - 50%

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Compressors, Gas Turbines and Jet Engines
Diffuser in a compressor is used to

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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