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Mathematical Formulation of Blade Surfaces in Turbomachinery: Part II — Practical Examples of Determined Surfaces PUBLIC ACCESS

[+] Author Affiliations
M. Rautenberg, A. Engeda

University of Hannover, Hannover, F. R. Germany

W. Wittekindt

KSB, Bremen, F. R. Germany

Paper No. 89-GT-161, pp. V001T01A066; 9 pages
doi:10.1115/89-GT-161
From:
  • ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Toronto, Ontario, Canada, June 4–8, 1989
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7913-9
  • Copyright © 1989 by ASME

abstract

In an attempt to develop a general method for the surface definitions of turbomachinery blades, the powerful tool straight-line-surface structures method has been introduced and practically tested. At a glance the method may seem too complex to qualify for general use. But the accuracies achived, the flexibilities in the method and the exact compatibility for feeding datas directly to a milling machine certifies it as a worthy method.

Copyright © 1989 by ASME
This article is only available in the PDF format.

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