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A Design Method and the Performance of Two-Dimensional Turbine Cascades for High Subsonic Flow FREE

[+] Author Affiliations
A. Uenishi

Hitachi Ltd., Hitachi, Ibaraki, Japan

Paper No. 71-GT-34, pp. V001T01A034; 12 pages
doi:10.1115/71-GT-34
From:
  • ASME 1971 International Gas Turbine Conference and Products Show
  • ASME 1971 International Gas Turbine Conference and Products Show
  • Houston, Texas, USA, March 28–April 1, 1971
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7982-5
  • Copyright © 1971 by ASME

abstract

This paper deals with a hodograph method for design of turbine cascades in high subsonic flow and an approximate solution to a gas, specific heat ratio γ = −1 (the Karman-Tsien approximation) and γ > 1 (the gas obeying the adiabatic law). Numerical examples and a comparison of theoretical and measured pressure distribution for profiles designed by this method are given. Further, a better criterion for design to improve cascade efficiency is also presented.

Copyright © 1971 by ASME
This article is only available in the PDF format.

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