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Compressors, Gas Turbines and Jet Engines

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

0.084027777777778
0.045833333333333
0.042361111111111
0.16736111111111

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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
Volumetric efficiency of air compressors is of the order of

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

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Compressors, Gas Turbines and Jet Engines
Ratio of indicated h.p. to shaft h.p. in known as

Mechanical efficiency
Compressor efficiency
Volumetric efficiency
Isothermal efficiency

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

All of these
Axial flow compressors
Pumps
Radial flow compressors

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Compressors, Gas Turbines and Jet Engines
Separators are generally used in air compressor installations

Before the inter-cooler
Before first stage suction
Between the after-cooler and receiver
After the inter-cooler

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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