Wake Measurements and Loss Evaluation in a Controlled Diffusion Compressor Cascade

[+] Author and Article Information
R. P. Shreeve, Y. Elazar, J. W. Dreon, A. Baydar

Turbopropulsion Laboratory, Naval Postgraduate School, Monterey, CA 93943

J. Turbomach 113(4), 591-599 (Oct 01, 1991) (9 pages) doi:10.1115/1.2929120 History: Received February 07, 1990; Online June 09, 2008


The results of two component laser-Doppler velocimeter (LDV) surveys made in the near wake (to one fifth chord) of a controlled diffusion (CD) compressor blade in a large-scale cascade wind tunnel are reported. The measurements were made at three positive incidence angles from near design to angles thought to approach stall. Comparisons were made with calibrated pressure probe and hot-wire wake measurements and good agreement was found. The flow was found to be fully attached at the trailing edge at all incidence angles and the wake profiles were found to be highly skewed. Despite the precision obtained in the wake velocity profiles, the blade loss could not be evaluated accurately without measurements of the pressure field. The blade trailing edge surface pressures and velocity profiles were found to be consistent with downstream pressure probe measurements of loss, allowing conclusions to be drawn concerning the design of the trailing edge.

Copyright © 1991 by The American Society of Mechanical Engineers
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