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A Stream Function Relaxation Method for Solving Transonic S1 Stream Surface With Pre-Determination of the Density PUBLIC ACCESS

[+] Author Affiliations
Ge Manchu

Academia Sinica, Beijing, China

Paper No. 85-GT-164, pp. V001T03A039; 6 pages
doi:10.1115/85-GT-164
From:
  • ASME 1985 International Gas Turbine Conference and Exhibit
  • Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
  • Houston, Texas, USA, March 18–21, 1985
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7938-2
  • Copyright © 1985 by ASME

abstract

On the basis of Prof. Wu’s 3-D flow theory (ref.1, 2, 3, 4, 5), a general streamfunction equation in non-orthogonal curvilinear coordinates is developed. The equation can be used to calculate subsonic or transonic flows on S1 or S2 stream surfaces of turbomachinery. In this paper streamlines coordinates and a mixed difference scheme are adopted in solving the stream function equation. A procedure for pre-determination of the density is developed and used to determine the unique-value of density from the known value of the stream function. Numerical examples are given.

Copyright © 1985 by ASME
This article is only available in the PDF format.

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