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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Mechanical efficiency of gas turbines as compared to I.C engines is

Higher
None of these
Same
Lower

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Compressors, Gas Turbines and Jet Engines
Only rocket engines can be propelled to space because

They can generate very high thrust
They have high propulsion efficiency
These engines can work on several fuels
They are not air breathing engines

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

None of these
Axial flow
Radial flow
Centrifugal

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Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

2.2 kg
1.0 kg
1.3 kg
0.5 kg

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

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

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Compressors, Gas Turbines and Jet Engines
The ratio of specific weight/h.p. of gas turbine and I.C engines may be typically of the order of

0.042361111111111
0.16736111111111
0.045833333333333
0.084027777777778

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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