28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
THE METHOD FOR NONLINEAR ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH
R. Zhang, D. Cui*, H. Du, Q. Xiong
Beihang Univ. (BUAA), China; *AVIC, China
Keywords: nonlinear analysis; aircraft and systems integration; multidisciplinary optimization
This paper introduces a method that utilizes the response surface methodology into genetic algorithm to solve the aeronautical nonlinear optimization problem. This method is used in a transonic flutter optimization of a horizontal tail and the analysis result shows that this method can be used in aeronautical nonlinear multidisciplinary optimization.
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