Investigation of Flow Phenomena in a Transonic Fan Rotor Using Laser Anemometry

[+] Author and Article Information
A. J. Strazisar

NASA-Lewis Research Center, Cleveland, Ohio 44135

J. Eng. Gas Turbines Power 107(2), 427-435 (Apr 01, 1985) (9 pages) doi:10.1115/1.3239743 History: Received January 18, 1984; Online October 15, 2009


Several flow phenomena, including flow field periodicity, rotor shock oscillation, and rotor shock system geometry have been investigated in a transonic low aspect ratio fan rotor using laser anemometry. Flow periodicity is found to increase with increasing rotor pressure rise and to correlate with blade geometry variations. Analysis of time-accurate laser anemometer data indicates that the rotor shock oscillates about its mean location with an amplitude of 3–4 percent of rotor chord. The shock surface is nearly two-dimensional for levels of rotor pressure rise at and above the peak efficiency level but becomes more complex for lower levels of pressure rise. Spanwise shock lean generates radial flows due to streamline deflection in the hub-to-shroud streamsurface.

Copyright © 1985 by ASME
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