Calculation of the Flow Properties Up- and Downstream of and Within a Supersonic Turbine Cascade PUBLIC ACCESS

[+] Author Affiliations
O. K. Lawaczeck

Gas Dynamics Institute, Göttingen, Germany

Paper No. 72-GT-47, pp. V001T01A046; 13 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


This paper deals with the flow through cascades, which have a supersonic flow up- and downstream. A theoretical method is described to calculate, under certain conditions, the flow quantities up- and downstream of and within the cascade and to determine the pressure distribution on the blades. The method is compared with experimental results, carried out in the cascade wind tunnel of the Aero dynamische Versuchsanstalt Göttingen (AVA), Germany.

Copyright © 1972 by ASME
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