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The Turbomachine Blading Design Achieved by Solving the Inverse Field Problem FREE

[+] Author Affiliations
T. S. Luu, B. Viney

LIMSI (CNRS), France

Paper No. 87-GT-215, pp. V001T01A073; 6 pages
doi:10.1115/87-GT-215
From:
  • ASME 1987 International Gas Turbine Conference and Exhibition
  • Volume 1: Turbomachinery
  • Anaheim, California, USA, May 31–June 4, 1987
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7923-8
  • Copyright © 1987 by ASME

abstract

This paper describes a design procedure for the determination of the geometry of the blading of the turbomachine with prescribed thickness and bound vorticity distribution. The boundary conditions are discussed in order to have a properly posed field problem. Optimised 2D cascade design example is shown. The quasi 3D “S2” - “S1” stream function formulation is developed. The design of guide vanes downstream of a lateral inlet casing is described. A new approach by introducing a potential like function to treat the 3D rotational flow is also formulated.

Copyright © 1987 by ASME
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