0
RESEARCH PAPERS

Numerical Solution of Inviscid Two-Dimensional Transonic Flow Through a Cascade

[+] Author and Article Information
J. Fořt

National Research Institute for Machine Design

K. Kozel

Department of Applied Mathematics, ČVUT, Prague, Czechoslovakia

J. Turbomach 109(1), 108-113 (Jan 01, 1987) (6 pages) doi:10.1115/1.3262054 History: Received December 26, 1985; Online November 09, 2009

Abstract

The paper presents a method of numerical solution of transonic potential flow through plane cascades with subsonic inlet flow. The problem is formulated as a weak solution with combined Dirichlet’s and Neumann’s boundary conditions. The numerical procedure uses Jameson’s rotated difference scheme and the SLOR technique to solve a system of difference equations. Numerical results of transonic flow are compared with experimental data and with other numerical results for both compressor and turbine cascades near choke conditions.

Copyright © 1987 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In