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A Unified Variable-Domain Variational Approach to Hybrid Problems of Compressible Blade-to-Blade Flow PUBLIC ACCESS

[+] Author Affiliations
Gao-Lian Liu, Shan Yan

Shanghai Institute of Mechanical Engineering, Shanghai, P. R. China

Paper No. 91-GT-169, pp. V001T01A064; 7 pages
doi:10.1115/91-GT-169
From:
  • ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Orlando, Florida, USA, June 3–6, 1991
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7898-9
  • Copyright © 1991 by ASME

abstract

A unified theory of various hybrid problems for blade-to-blade compressible flow is developed herein via the functional variation with variable domain. Two variational principle (VP) families for three typical hybrid problems are derived, following a systematic approach (Liu, 1990a). Full advantage is taken of the natural boundary condition and suction/blowing along the blade surface are accommodated. This theory is aimed at offering a new theoretical basis for the finite element method (FEM) and various ways for blade design and/or modification, and it also constitutes an important part of optimal cascade theory (Liu,1987b). Based on these VPs, a new FEM with self-adjusting nodes is also suggested, and the numerical tests yield good results.

Copyright © 1991 by ASME
This article is only available in the PDF format.

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