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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
0.9
0.99
0.85

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency is

Index of compressor performance
The ratio of stroke volume to clearance volume
Reciprocal of compression ratio
The ratio of the air actually delivered to the amount of piston displacement

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

Less
More
Zero
Same

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Cools the delivered air
Results in saving of power in compressing a given volume to given pressure
Enables compression in two stages
Is the standard practice for big compressors

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Compressors, Gas Turbines and Jet Engines
Diffuser in a compressor is used to

Make the flow streamline
Convert pressure energy into kinetic energy
Convert kinetic energy into pressure energy
Increase velocity

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

0.41736111111111
0.83402777777778
2.5006944444444
0.62569444444444

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