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Analysis of Three-Dimensional Turbomachinery Flows on C-Type Grids Using an Implicit Euler Solver PUBLIC ACCESS

[+] Author Affiliations
K. F. Weber, D. W. Thoe, R. A. Delaney

General Motors Corporation, Indianapolis, IN

Paper No. 89-GT-85, pp. V001T01A051; 9 pages
doi:10.1115/89-GT-85
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

A 3-D Euler analysis for turbomachinery flows on a C-type grid is presented. The analysis is based on the Beam and Warming implicit algorithm for solution of the unsteady Euler equations and is derived from the ARC3D code developed by Pulliam at NASA Ames Research Center. Modifications made to convert this code from external flow applications to internal turbomachinery flows are given in detail. These changes include the addition of inflow, outflow, and periodic boundary point calculation procedures. Also presented are the C-grid construction procedures. Finally, results of code experimental verification studies for 3-D compressor cascade and rotor flows are presented.

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

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