Calculation of the Quasi Three-Dimensional Flow in a Turbomachine Blade Row

[+] Author and Article Information
Jean-Pierre Veuillot

Office National d’Etudes et de Recherches Aérospatiales, ONERA, Châtillon, France

J. Eng. Power 99(1), 53-62 (Jan 01, 1977) (10 pages) doi:10.1115/1.3446252 History: Received December 19, 1975; Online July 14, 2010


The equations of the through flow are obtained by an asymptotic theory valid when the blade pitch is small. An iterative method determines the meridian stream function, the circulation, and the density. The various equations are discretized in an orthogonal mesh and solved by classical finite difference techniques. The calculation of the steady transonic blade-to-blade flow is achieved by a time marching method using the MacCormack scheme. The space discretization is obtained either by a finite difference approach or by a finite volume approach. Numerical applications are presented.

Copyright © 1977 by ASME
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