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受弯脱层层板的局部失稳临界载荷的有限元分析
引用本文:李跃宇,邹振民.受弯脱层层板的局部失稳临界载荷的有限元分析[J].上海力学,1998,19(2):125-129.
作者姓名:李跃宇  邹振民
作者单位:南京航空航天大学飞行器系,南京航空航天大学飞行器系,南京航空航天大学飞行器系 南京 210016,南京 210016,南京 210016
摘    要:含脱层的复合材料层板承受弯曲载荷作用会产生跳跃失稳,还常常引起脱层扩展,从而导致结构失效。本文用基于一阶剪切层板理论的几何非线性有限单元法分析了受弯曲曲载荷作用下含脱层板的人稳的临界载荷。本文指出分叉失稳产生了跳跃失稳,而该跳跃失稳与浅圆拱或薄圆柱壳受向心压力作用下的跳跌 同,在整体平衡路径上没有一个极限点。本文对临界载计算结果比使用能量准则的结果要小,文中给出了原因。

关 键 词:复合材料  层板  脱层  失稳  有限元  临界载荷

A FEM TO PREDICT THE CRITICAL LOAD OF INSTABILITY ANALYSIS OF DELAMNATION IN LAMINATES UNDER BENDING LOAD
Li Yueyu Zou Zhenmin Fan Weixun.A FEM TO PREDICT THE CRITICAL LOAD OF INSTABILITY ANALYSIS OF DELAMNATION IN LAMINATES UNDER BENDING LOAD[J].Chinese Quarterly Mechanics,1998,19(2):125-129.
Authors:Li Yueyu Zou Zhenmin Fan Weixun
Abstract:Local buckling of delaminated laminates subjected to bending loads frequently bring about snap-through buckling, which often causes delamination growth and leads the structure to failure. In this paper, an analysis is made to predict the critical load of instability of the delaminated laminates by the use of a geometrically nonlinear one-dimensional finite element method. It is found that the bifurcation instability produces snap buckling without a limit point on the equilibrium path, which is quite different from the snap buckling of a shallow thin cylindrical shell under concentrated load. However, the results offer lower loads of instbility than that when the energy criterion is used. In the paper, explanation is also given.
Keywords:composite materials  laminates  delamination  instability finite element method  
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