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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The fuel consumption in gas turbines is accounted for by

Heating value
Lower heating value
Higher heating value
Higher calorific value

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Compressors, Gas Turbines and Jet Engines
The ratio of the volume of free air delivery per stroke to the swept volume of the piston, is known as

Isothermal efficiency
Volumetric efficiency
Mechanical efficiency
Compressor efficiency

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

16 kg/cm²
10 kg/cm²
25 kg/cm²
6 kg/cm²

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Compressors, Gas Turbines and Jet Engines
Free air is the air at

15°C and 1 kg/cm²
Atmospheric conditions at any specific location
0°C and standard atmospheric conditions
20°C and 1 kg/cm² and relative humidity of 36%

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Compressors, Gas Turbines and Jet Engines
The compressor capacity with decrease in suction temperature

Increases
Decreases
May increase or decrease depending on compressor capacity
Remain unaffected

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Compressors, Gas Turbines and Jet Engines
A rocket engine uses __________ for the combustion of its fuel.

Surrounding air
None of these
Compressed atmospheric air
Its own oxygen

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