The Turbine Regime of a Rear Axial Compressor Stage PUBLIC ACCESS

[+] Author Affiliations
Václav Cyrus

The National Research Institute for Machine Design (SVUSS), Bechovice, Czechoslovakia

Paper No. 90-GT-074, pp. V001T01A025; 8 pages
  • 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


A detailed investigation of three-dimensional flow has been carried out in a low speed rear axial compressor stage with aspect ratio of 1 at the extreme off-design condition-turbine regime. Measurements were performed by means of both stationery and rotating pressure probes. The mechanism of flow in the rotor and stator blade row in the turbine regime is analysed. Comparison is made with flow mechanism at the design condition.

Copyright © 1990 by ASME
Topics: Compressors , Turbines
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