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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches

Isothermal
Adiabatic
Isochoric
Isentropic

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Compressors, Gas Turbines and Jet Engines
A jet engine works on the principle of conservation of

Energy
Mass
Flow
Linear momentum

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Euler
Isentropic efficiency
Compressor efficiency
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

256 bar
16 bar
1 bar
64 bar

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Compressors, Gas Turbines and Jet Engines
The work done per unit mass of air in compression will be least when 'n' is equal to

1.2
1.4
1.3
1

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Compressors, Gas Turbines and Jet Engines
Gas turbine cycle with regenerator

Decreases heat loss is exhaust
Allows high compression ratio
Increases thermal efficiency
Allows operation at very high altitudes

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