Casing Treatments on a Supersonic Diffuser for High Pressure Ratio Centrifugal Compressors PUBLIC ACCESS

[+] Author Affiliations
Y. Ribaud

Office National d’Etudes et de Recherches Aérospatiales, Chatillon, France

P. Avram

Office National d’Etudes et de Recherches Aérospatiales, Palaiseu, France

Paper No. 82-GT-85, pp. V001T01A036; 9 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


Centrifugal compressors with high pressure ratios from 7 to 10 often have a very slow mass flow margin. Suitable casing treatments, including large openings at the diffuser throat connected to annular plenums, greatly increase the reduced mass flow range of the diffuser during supersonic inlet operation. In the region of reduced mass flow variation, the reduction of the diffuser flow is associated with a drop of the effectiveness. The use of a backswept centrifugal rotor allows the experiment to overcome this penalty.

Copyright © 1982 by ASME
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