舰船电子工程2019，Vol.39Issue(6)：115-118,132,5.DOI:10.3969/j.issn.1672-9730.2019.06.029
基于全解析法的气动弹性剪裁方法研究与软件实现 ∗
Research of Aeroelastic Tailoring Design Method Based on Complete Analytic Method and Software Implementation
摘要
Abstract
Focusing on multi-discipline coupled aeroelastic problem of large aircraft composite wings,stiffness direction and coupling effect of composite laminates are utilized,in order to produce beneficial elastic deformation of wing structure under loading,so then the structural design performance and aeroelastic characteristics can be improved. The function of the aeroelastic tailoring design software is designed and realized on the domestic independent platform. The software includes structural analysis module,optimization design module and pre-and post-processing module. The operation results indicate that this method and software can effectively deal with aeroelastic and optimization problems,and has been applied and verified on real aircrafts structure design.关键词
气动弹性/全解析/优化/软件Key words
aeroelastic/complete analysis/optimization/software分类
信息技术与安全科学引用本文复制引用
李倩,常亮,王晓辉..基于全解析法的气动弹性剪裁方法研究与软件实现 ∗[J].舰船电子工程,2019,39(6):115-118,132,5.基金项目
装备预先研究项目(编号:41406030201)资助. （编号:41406030201）
