23rd Congress of International Council of the Aeronautical Sciences, 8-13 September, 2002, Toronto, Canada
Paper ICAS 2002-1.10.4

NUMERICAL OPTIMIZATION DESIGN OF WINGS BY SOLVING ADJOINT EQUATIONS

Z. Qiao, X. D. Yang, X. L. Quin, B. Zhu
Northwestern Polytechnical University, PRC

Keywords: wing design, adjoint equations, numerical optimization, euler equation

A numerical optimization method of wing design by solving adjoint equations based on Euler equations is studied for better considering performance requirements of wing design by given requirements of aerodynamic performance and the given desired pressure distribution respectively.

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