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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The combustion efficiency of a gas turbine using perfect combustion chamber is of the order of

0.75
0.99
0.9
0.85

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Compressors, Gas Turbines and Jet Engines
A machine used to raise the pressure of air is called

Compressor
I.C engine
Air motor
Gas turbine

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Compressors, Gas Turbines and Jet Engines
The mass of gas turbine per kW developed is about ________ as that of an I.C. engine.

One fourth
One sixth
Same
One-half

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Compressors, Gas Turbines and Jet Engines
A closed gas turbine in which fuel is burnt directly in the air is not possible because of

Paucity of O2
High specific volume
High friction losses
Increasing gas temperature

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Compressors, Gas Turbines and Jet Engines
A compressor mostly used for supercharging of I.C. engines is

Roots blower
Reciprocating compressor
Axial flow compressor
Radial flow compressor

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Less power requirement
Lower volumetric efficiency
Less loss of air due to leakage past the cylinder
Better mechanical balance

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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