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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a jet engine, the air-fuel ratio is

2.5006944444444
1.6673611111111
1.2506944444444
2.0840277777778

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is 5 m/min refers to

Free air
Compressed air
Standard air
Compressed air at delivery pressure

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Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is parallel to its axis, then the compressor is

Centrifugal compressor
Reciprocating compressor
Turbo compressor
Axial flow compressor

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

None of these
Adiabatic
Isothermal
Polytropic

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Compressors, Gas Turbines and Jet Engines
Gas turbines for power generation are normally used

To enable start thermal power plant
To supply peak load requirements
To supply base load requirements
In emergency

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Compressors, Gas Turbines and Jet Engines
For speed above 3000 km/hour, it is more advantageous to use

Ramjet engine
Rockets
Propellers
Turbojet engine

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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