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Investigation of the Axial Velocity Density Ratio in a High Turning Cascade FREE

[+] Author Affiliations
H. Starken, P. Schimming

Institut für Luftstrahlantriebe, Porz-Wahn, Germany

F. A. E. Breugelmans

von Karman Institute for Fluid Dynamics, Belgium

Paper No. 75-GT-25, pp. V01AT01A024; 14 pages
doi:10.1115/75-GT-25
From:
  • ASME 1975 International Gas Turbine Conference and Products Show
  • Volume 1A: General
  • Houston, Texas, USA, March 2–6, 1975
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7976-4
  • Copyright © 1975 by ASME

abstract

Subsonic cascade tests of a stator blade row are presented. A 48-deg cambered double circular arc blade section has been investigated at different inlet Mach numbers (M1 = 0.5, 0.64, 0.74), different inlet flow angles and various axial velocity density ratios. Optimum cascade performance has been obtained at negative incidence angles and near two-dimensional flow condition. The cascade results are compared with stator tests of the same blade section at corresponding flow conditions.

Copyright © 1975 by ASME
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