Structural Optimization and Aeroelastic Analysis of a Composite T-tail Configuration

摘要：

　　In this paper,a composite T-tail model is developed,including structural fiinite element model and aeroelastic model,and then structural optimization and aeroelastic analysis are made.Through two steps of structural optimization,and aeroelastic analysis,some valuable conclusions are achieved,which are useful for future composite T-tail design.

关键词： composite T-tail structural optimization aeroelastic analysis

作者: Liang Li Qin Sun

作者单位: Northwestern Polytechnic University,China,Shaanxi,Xian

会议类型: 国际会议

会议名称: 2012 International Conference on Intelligent System and Applied Material(2012智能系统与应用材料国际会议)(GSAM2012)

会议地点: 太原

会议语种:英文

页码: 1125-1128

在线出版日期: 2012-01-13（万方平台首次上网日期，不代表论文的发表时间）