Design of Composite Structures for Improved Aeroelastic Performance

نویسنده

  • G. A Vio
چکیده

Despite the benefits of composite structures, it is only recently that the main load bearing structures in large aircraft such as the Boeing 787 and Airbus A350 have started to be manufactured using carbon fibre composites. Even then, the unique directionality properties of composite laminates and design possibilities have yet to be exploited to improve the aircraft performance. In this study a typical composite commercial aircraft wing structure is optimised using evolutionary algorithms with the aim of improving the aeroelastic response, concentrating on gust loads. Conclusions are drawn based on the performance gains that can be achieved using aeroelastic tailoring and new design idea whilst taking into account flutter and divergence constraints.

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تاریخ انتشار 2012