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A Generalized Numerical Method for Solving Direct, Inverse and Hybrid Problems of Blade Cascade Flow by Using Streamline-Co-Ordinate Equation FREE

[+] Author Affiliations
Chen Nai-Xing, Zhang Feng-Xian

Chinese Academy of Sciences, Beijing, People’s Republic of China

Paper No. 87-GT-29, pp. V001T01A009; 5 pages
doi:10.1115/87-GT-29
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 generalized numerical method for solving direct, inverse and hybrid aerodynamic problems of the blade cascade flow on the stream surface of revolution. The computational method is based on the numerical solution of the streamline-co-ordinate equation by a linear relaxation scheme. Two conventional blade cascades and a tandem blade have been calculated by the present method.

Copyright © 1987 by ASME
This article is only available in the PDF format.

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