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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)

(v₁ - v₂)²/2g
(v₁ - v₂)²/g
(v₁² -v₂²)/g
(v₁² -v₂²)/2g

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

0.1%
1.0%
0.5%
5%

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Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

10 kg/cm²
2 kg/cm²
14.7 kg/cm²
6 kg/cm²

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

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

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Compressors, Gas Turbines and Jet Engines
The work-done on a compressor will be minimum if air is taken from

A source at 0° C
A source of high temperature air
The atmosphere
A source of low temperature air

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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