Hypernormal Form at Cubic of a Rectangular Symmetric Cross-ply Laminated Composite Plate

摘要：

　　Based on wings flutter on flying aircraft in this paper,the authors study the mechanical model of the rectangular symmetric cross-ply composite laminated plates.Frist,the method of multiple scales is employed to obtain the four-dimensional averaged equations of the model.Then,the method of new grading function and multiple Lie brackets is utilized to obtain the hypernormal form (simplest normal form,unique normal form) at cubic of above averaged equations.

关键词： Laminated Plate Hypernormal Form New Grading Function Multiple Lie Brackets

作者: Wenyuan Jia Jing Li Bin He

作者单位: The College of Applied Sciences, Beijing University of Technology, Beijing, 100124, P.R.China

会议类型: 国际会议

会议名称: 2012 International Conference on Chemical Engineering,Metallurgical Engineering and Metallic Materials(2012化工、冶金和金属材料国际会议(CMMM2012))

会议地点: 昆明

会议语种:英文

页码: 641-644

在线出版日期: 2012-10-12（万方平台首次上网日期，不代表论文的发表时间）