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Centrifugal Compressor Impeller Aerodynamics: An Experimental Investigation FREE

[+] Author Affiliations
H. David Joslyn, Robert P. Dring

United Technologies Research Center, East Hartford, CT

Joost J. Brasz

Carrier Corporation, Syracuse, NY

Paper No. 90-GT-128, pp. V001T01A035; 12 pages
doi:10.1115/90-GT-128
From:
  • ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Brussels, Belgium, June 11–14, 1990
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7904-7
  • Copyright © 1990 by ASME

abstract

The ability to acquire blade loadings (surface pressure distributions) and surface flow visualization on an unshrouded centrifugal compressor impeller is demonstrated. Circumferential and streamwise static pressure distributions acquired on the stationary shroud are also presented. Data was acquired in a new facility designed for centrifugal compressor aerodynamic research. Blade loadings calculated with a blade–to–blade potential flow analysis are compared with the measured results. Surface flow visualization reveals some complex aspects of the flow on the surface of the impeller blading and hub. In a companion paper, Dorney and Davis (1990), a state–of–the–art, three–dimensional, time–accurate, Navier Stokes prediction of the flow through the impeller is presented.

Copyright © 1990 by ASME
This article is only available in the PDF format.

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