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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compressor performance at higher altitude compared to sea level will be

Dependent on other factors
Lower
Same
Higher

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Compressors, Gas Turbines and Jet Engines
Out of the following, from where you will prefer to take intake for air compressor

From coal yard side
From outside atmosphere at 1°C
From an air conditioned room maintained at 20°C
From a side where cooling tower is located nearby

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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

0.16736111111111
0.045833333333333
0.084027777777778
0.042361111111111

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Compressors, Gas Turbines and Jet Engines
A 3 m³/min compressor means that it

Delivers 3 m³/ min of compressed air
Compresses 3 m³/ min of free air
Delivers 3 m³/ min of compressed air at delivery pressure
Compresses 3 m³/min of standard air

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Compressors, Gas Turbines and Jet Engines
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Slip factor
Degree of reaction
Pressure coefficient
Work factor

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Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

Increase
None of these
Remain same
Decrease

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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