Investigation of Flows in Rectangular Diffusers With Inlet Flow Distortion PUBLIC ACCESS

[+] Author Affiliations
M. M. Al-Mudhafar, M. Ilyas, F. S. Bhinder

The Hatfield Polytechnic, Hatfield, Hertfordshire, UK

Paper No. 82-GT-67, pp. V001T01A025; 5 pages
  • ASME 1982 International Gas Turbine Conference and Exhibit
  • Volume 1: Turbomachinery
  • London, England, April 18–22, 1982
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7956-6
  • Copyright © 1982 by ASME


The results of an experimental study on the influence of severely distorted velocity profiles on the performance of a straight two-dimensional diffuser are reported. The data cover entry Mach numbers ranging from 0.1 to 0.6 and several inlet distortion levels. The pressure recovery progressively deteriorates as the inlet velocity is distorted.

Copyright © 1982 by ASME
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