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The influence of SPAR position on aeroelastic optimization of a large aircraft wing with different materials

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper presented studies on structural sizes optimization and arrangement design of a large aircraft wing with different material. Two three-dimensional finite element models of a high-aspect-ratio wing were built that were a metal model and a composite model, and the influence of the front and rear spar position on the results of the aeroelastic analysis and optimization were studied to improve the wing structure desgin. The most feasible and optimal solutions were effectively obtained by aeroelastic optimization. The position parameter of the front spar has a greater influence on the aeroelastic analysis and optimization than the rear spar.

源语言英语
主期刊名53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012
出版状态已出版 - 2012
活动53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012 - Honolulu, HI, 美国
期限: 23 4月 201226 4月 2012

出版系列

姓名53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012

会议

会议53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012
国家/地区美国
Honolulu, HI
时期23/04/1226/04/12

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