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1. On the Effect of Area Ruling on Transonic Abrupt Wing Stall

Author

Rodriguez, D.L., Guruswamy, G., Jones, K.D, Platzer, M.F., and Department of Mechanical and Aerospace Engineering

Abstract

IUTAM Symposium Transsonicum IV Ed. Sobieczky., H., Kluwer Academic Publishers, Dordrecht, The Netherlands, 2003, pp. 99-104. Reynolds-averaged Navier-Stokes simulations of the transonic flow over a generic fighter aircraft wing/LEX/body configuration are presented. Data in the pre and post-stall regime are presented, and it is shown that small changes in the cross-sectional area distribution in the aft body has a significant effect on the onset of wing stall, but more systematic computations are needed before the effectiveness of area-ruling can be firmly established.

Published
2003

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