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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be

Radial
Forward curved
None of the listed here
Backward curved

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Diffuser inlet radius
Diffuser outlet radius
Impeller inlet radius
Impeller outlet radius

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Lower volumetric efficiency
Less power requirement
Less loss of air due to leakage past the cylinder
Better mechanical balance

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

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

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

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Compressors, Gas Turbines and Jet Engines
If V, U and Vr represent the absolute velocity of fluid, velocity of blade, and relative velocity of fluid, and suffix ‘I’ and ‘o’ stand for entry and exit conditions, then in a rotary machine whose degree of reaction is unity

Vi = Vo
U < Vo
V = Uo
Vt > Vo

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