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Dr. Ir. Harinaldi, M.Eng, Dr.Ir budiarso M.Eng.Mechanical Engineering Department

Faculty of Engineering University of Indonesia

CoMPRESSoRAND CENTRIFUGAL FAN

PRE-WHIRL AND INLET GUIDES VANES

MACH NUMBER IN THE DIFFUSER

The absolute Mach number of the fluid leaving the impeller may well be in excess of 1. However, it has been found that as long as the radial flow velocity Cr2 is subsonic, then no loss in efficiency is caused by the formation of shock waves.

The effect of inlet guide vanes on the inlet relaltive velocity:(a) at shroud; (b) at hub

CENTRIFUGAL COMPRESSOR CHARACTERISTIC

The theoretical centrifugal compressor characteristic

SURGING

ROTATING STALL

Rotating stall propagation

CHOCKING

CHARACTERISTIC CURVE

Typical centrifugal compressor characteristic

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