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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

0.99
0.9
0.75
0.85

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Compressors, Gas Turbines and Jet Engines
Ratio of indicated h.p. to shaft h.p. in known as

Volumetric efficiency
Compressor efficiency
Mechanical efficiency
Isothermal efficiency

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

Is used when gas is to be burnt
Provides lesser flexibility
In never used
Provides greater flexibility

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Compressors, Gas Turbines and Jet Engines
In jet engines the products of combustion after passing through the gas turbine are discharged into

Atmosphere
Back to the compressor
Vacuum
Discharge nozzle

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