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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

Adiabatic
Isentropic
Isothermal
Isochoric

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Heating chamber
Cooling chamber
All of these
Compressor

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Pumps
Radial flow compressors
Axial flow compressors
All of these

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

Less than
Equal to
None of the listed here
More than

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

Same power
More power
Less power
More/less power depending on other factors

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Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

Remain same
Decrease
None of these
Increase

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