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首页> 外文期刊>Acta Mechanica >Buckling analysis of a plate with built-in rectangular delamination by strip distributed transfer function method
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Buckling analysis of a plate with built-in rectangular delamination by strip distributed transfer function method

机译:条形分布传递函数法分析矩形内藏钢板的屈曲

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摘要

Delamination may reduce the buckling of the laminated plate. In this paper, a semi-analytical, semi-exact method, namely the strip transfer function method based on Mindlin’s first-order shear deformation theory is developed to investigate the buckling of a delaminated plate. First, a composite plate with bulit-in rectangular delamination is divided into two kinds of rectangular super-units, one with a delamination and one without. The variational principle is used to obtain equilibrium equations and boundary conditions. Then, by displacement continuity and force balance of nodes that connect two super-units, the characteristic equation for the buckling analysis of the delaminated plate is derived. Consequently, buckling load and mode are computed. By comparing the results of the plate with through-the–width delamination to the analytic solutions of a beam and the results of the finite element method, the validity of this method is tested. Furthermore, the influence of length, depth and position of the delamination, the boundary condition and the plying angle of the material on the buckling load is analyzed.
机译:分层可以减少层压板的弯曲。本文研究了一种半解析半精确方法,即基于Mindlin的一阶剪切变形理论的带传递函数方法,以研究分层板的屈曲。首先,将带有褶皱状矩形分层的复合板分为两种矩形超级单元,一种是带有分层的矩形超级单元,另一种是没有分层的矩形超级单元。变分原理用于获得平衡方程和边界条件。然后,通过连接两个超单元的节点的位移连续性和力平衡,推导了分层板屈曲分析的特征方程。因此,计算了屈曲载荷和模态。通过将具有全宽度分层的板的结果与梁的解析解以及有限元方法的结果进行比较,测试了该方法的有效性。此外,分析了分层的长度,深度和位置,边界条件和材料的插入角度对屈曲载荷的影响。

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  • 来源
    《Acta Mechanica 》 |2005年第4期| 231-243| 共13页
  • 作者

    D. Li; G. Tang; J. Zhou; Y. Lei;

  • 作者单位

    College of Aerospace and Material Engineering National University of Defense Technology Changsha Hu-Nan Province 410073 P.R. China;

    College of Aerospace and Material Engineering National University of Defense Technology Changsha Hu-Nan Province 410073 P.R. China;

    College of Aerospace and Material Engineering National University of Defense Technology Changsha Hu-Nan Province 410073 P.R. China;

    College of Aerospace and Material Engineering National University of Defense Technology Changsha Hu-Nan Province 410073 P.R. China;

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