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Mixing in Axial Flow Compressors: Part I — Test Facilities and Measurements in a Four-Stage Compressor FREE

[+] Author Affiliations
Y. S. Li, N. A. Cumpsty

Cambridge University, England

Paper No. 90-GT-038, pp. V001T01A015; 7 pages
doi:10.1115/90-GT-038
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 mechanism of mixing in axial flow compressors has been investigated in two low speed machines. For reasons of length this is described in two parts. Results in a 4-stage compressor are described here in Part I and show that the mixing coefficients across the first and the third stators are of similar magnitude. Part I also describes the background and experimental facilities and techniques used in both parts together with the nomenclature and all the references. Part II describes the results from a large single stage compressor. It also presents measurements of mixing in a simple two-dimensional duct, and presents conclusions for the whole investigation.

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

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