Supersonic Exit Flow of Two-Dimensional Cascades PUBLIC ACCESS

[+] Author Affiliations
H. J. Lichtfuss, H. Starken

Institut für Luftstrahlantriebe, Porz-Wahn, Germany

Paper No. 72-GT-49, pp. V001T01A048; 18 pages
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • San Francisco, California, USA, March 26–30, 1972
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7981-8
  • Copyright © 1972 by ASME


In this paper the supersonic exit flow field of a two-dimensional cascade is described. Different flow configurations at axial subsonic and supersonic velocities are discussed in detail and calculation methods are presented. The range of possible cascade operation and its dependency of back pressure is evaluated. It is shown that the exit flow field of a double infinite cascade can be simulated behind a semi-infinite cascade.

Copyright © 1972 by ASME
Topics: Flow (Dynamics)
This article is only available in the PDF format.



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