北京航空航天大学学报 ›› 2007, Vol. 33 ›› Issue (01): 50-54.

• 论文 • 上一篇    下一篇

复合材料薄壁梁几何非线性分析

石庆华, 向锦武   

  1. 北京航空航天大学 航空科学与工程学院, 北京 100083
  • 收稿日期:2006-01-09 出版日期:2007-01-31 发布日期:2010-09-19
  • 作者简介:石庆华(1974-),男,安徽安庆人,博士生,jxaabb@etang.com.
  • 基金资助:

    国家自然科学基金资助项目(10272012);教育部新世纪人才 计划资助项目(NCET-04-0169)

Geometry nonlinear analysis of composite thin walled beams

Shi Qinghua, Xiang Jinwu   

  1. School of Aeronautic Science and Engineering, Beijing Universi ty of Aeronautics and Astronautics, Beijing 100083, China
  • Received:2006-01-09 Online:2007-01-31 Published:2010-09-19

摘要: 根据复合材料薄壁梁变形的特点,假设截面有面外翘曲,应变沿薄壁厚度方向 呈二次曲线形式变化,采用9节点平面单元模拟复杂薄壁截面,用27节点体单元模拟面外翘 曲变形.在Hamilton原理基础上,采用非线性有限元理论,用T.L.法,将位移等状态量写成 增量形式后,推导出了任意复杂截面薄壁复合材料梁计入剪切翘曲大变形分析的几何刚度矩 阵,建立了一个新的任意复合材料薄壁截面梁几何非线性分析模型,并进行了算例验证.算 例表明,建立的模型正确,能够进行复合材料薄壁梁几何非线性分析;截面翘曲对复合 材料梁的变形影响明显;与相关文献做比较,说明了模型的优越性.

Abstract: A new geometry nonlinear finite element model for composite thin walle d beams has been developed based on the complex deformation characteristic of th e composite thin walled beams. Supposed the strain quadratic varies along the th in-walled, introducing the complex cross-section of beam was simulated by 9-node pla ne element and the out-of-plane warping displacement was simulated by 27-node so lid element. Based on the Hamilton principle, nonlinear finite element theory an d the Total Lagrange formulation, the geometry stiffness matrix was formed. The analytical model is proved correct through several examples. The model can be used in analysis of thin-walled composite beams, the warping d e formation has evidently affected on composite thin walled beams, compared with r elated literatures numerical results, the advantage of this model has been showe d.

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