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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

Zero
More
Less
Same

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Compressors, Gas Turbines and Jet Engines
The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

Increases
First increases and then decreases
First decreases and then increases
Decreases

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

Axial flow compressor
Radial flow compressor
Reciprocating compressor
Roots blower

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

Work ratio
Compression ratio
Pressure ratio
None of these

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Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

Remain same
Decreases
First increases and then decreases
Increases

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Compressors, Gas Turbines and Jet Engines
Rotary compressors are suitable for

Low discharge at low pressure
Large discharge at high pressure
Low discharge at high pressure
Large discharge at low pressure

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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