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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Air-fuel ratio in a jet engine will be of the order of

0.41736111111111
2.5006944444444
0.83402777777778
0.62569444444444

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Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

None of these
Same
Lower
Higher

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

Reciprocating compressor
Centrifugal compressor
Axial flow compressor
Turbo compressor

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Compressors, Gas Turbines and Jet Engines
Standard air is the air at ___ and relative humidity of 36 percent.

0.1 bar and 40°C
1 bar and 20°C
1 bar and 40°C
0.1 bar and 20°C

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to steam turbine

Has less efficiency
Has compressor and combustion chamber
Requires less space for installation
All of these

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Compressors, Gas Turbines and Jet Engines
The temperature of air at the beginning of the compression stroke is ________ the atmospheric temperature.

Equal to
None of these
More than
Less than

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