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Experimental Research of the Secondary Flow in Rectilinear Turbine Cascades FREE

[+] Author Affiliations
Ye Da-Jun, Zhou Li-Wei

Tsinghua University, Beijing, China

Paper No. 85-IGT-93, pp. V001T02A035; 6 pages
doi:10.1115/85-IGT-93
From:
  • ASME 1985 Beijing International Gas Turbine Symposium and Exposition
  • Volume 1: Aircraft Engine; Turbomachinery
  • Beijing, People’s Republic of China, September 1–7, 1985
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7942-9
  • Copyright © 1985 by ASME

abstract

For studying the secondary flow in a turbine cascade, the flow field is measured in detail. The measurements of pressure and velocity are taken at various axial planes upstream of, within, and downstream of the cascade by a 4-hole probe. The static pressures are taken on the endwall, suction and pressure surfaces. By treating the experiment data the mechanism of the secondary flow field and the loss model are proposed in this paper.

Copyright © 1985 by ASME
This article is only available in the PDF format.

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