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TECHNICAL BRIEFS

A New Algorithm for the Solution of Turbomachinery Flow Problems

[+] Author and Article Information
R. B. Deshpande

University of Manchester Institute of Science and Technology, Manchester, England

J. Fluids Eng 97(3), 372-374 (Sep 01, 1975) (3 pages) doi:10.1115/1.3447317 History: Received June 03, 1975; Online October 12, 2010

Abstract

A new algorithm, which is a modification of the successive over-relaxation method, has been applied to the inviscid compressible blade-to-blade flow problem. When this procedure was used, an improvement in convergence of the numerical process was obtained with a reduction of computing time by a factor of 2. This technique offers another advantage of obtaining convergence where other methods might have been unsuccessful.

Copyright © 1975 by ASME
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