24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-6.4.3

USE OF ADVANCED CFD FOR THE DESIGN OF SNECMA MOTEURS TURBOMACHINE

N. Liamis, F. Bastin, J. Lépine
Snecma Moteurs, Centre de Villaroche, 77550 Moissy Cramayel, France

Keywords: CFD, turbo-machinery, compressor, combustion chamber, turbine

During the last two decades, CFD tools have been a significant source of improvements in the design process of turbomachinery components, leading to higher performances, cost and cycle savings as well as lower associated risks. Several examples of application, at Snecma Moteurs, are presented to illustrate their practical use and compare with experiment.

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