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Compressors, Gas Turbines and Jet Engines

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

More than
None of these
Equal to
Less than

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Compressors, Gas Turbines and Jet Engines
Surging is the phenomenon of

Air stream not able to follow the blade contour
Unsteady, periodic and reversed flow
Air stream blocking the passage
Motion of air at sonic velocity

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the ratio of the ________ to the blade velocity is called slip factor.

Outlet velocity of flow
Outlet whirl velocity
Inlet velocity of flow
Inlet whirl velocity

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Compressors, Gas Turbines and Jet Engines
The following property is most important for material used for gas turbine blade

Fatigue
Creep
Corrosion resistance
Toughness

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

In between isothermal and adiabatic
Better than isothermal and adiabatic
Same as isothermal
Same as adiabatic

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Compressors, Gas Turbines and Jet Engines
The efficiency of the vane blower is (where W₁ = Workdone due to compression, and W₂ = Workdone due to back flow)

W₂/(W₁ + W₂)
(W₁ + W₂)/W₂
(W₁ + W₂)/W₁
W₁/(W₁ + W₂)

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