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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Ratio of indicated H.P. and brake H.P. is known as

Adiabatic efficiency
Mechanical efficiency
Volumetric efficiency
Isothermal efficiency

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Compressors, Gas Turbines and Jet Engines
An air receiver is to be placed outside. Should it be placed in

Rain
Sun
Shade
Enclosed room

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

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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

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

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Compressors, Gas Turbines and Jet Engines
The stagnation pressure rise in a centrifugal compressor takes place

In the inlet guide vanes only
In the impeller only
In the diffuser only
In the diffuser and impeller

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Thrust power and propulsive power
Thrust power and fuel energy
Propulsive power and fuel input
Engine output and propulsive power

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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