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Time-Split Inflow Boundary Treatment PUBLIC ACCESS

[+] Author Affiliations
Siu Shing Tong

General Electric Company, Schenectady, NY

Paper No. 85-GT-165, pp. V001T03A040; 9 pages
doi:10.1115/85-GT-165
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

This paper describes a new non-reflective inflow treatment for viscous and inviscid internal flow calculations. The method approximates the multi-dimensional governing equations at the inflow boundary in a series of one-dimensional split equations. This treatment allows the artificial inflow boundary to be brought in just in front of the leading edge, while allowing upstream running waves to penetrate without significant reflection. Calculation examples of two dimensional inviscid internal flows are presented. Extension of the method to three-dimensional problems is also discussed.

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

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