航空学报 > 1993, Vol. 14 Issue (3): 127-133

含边缘裂纹半无限大加筋板的应力强度因子

黄维扬, 严国林   

  1. 南京航空学院104教研室,南京 210016
  • 收稿日期:1992-07-16 修回日期:1992-09-10 出版日期:1993-03-25 发布日期:1993-03-25

THE STRESS INTENSITY FACTORS FOR EDGE CRACKS IN STIFFENED PLATES

Huang Wei-yang, Yan Guo-lin   

  1. Faculty 104 of Nanjing Aeronautical Institute, Nanjing, 210016
  • Received:1992-07-16 Revised:1992-09-10 Online:1993-03-25 Published:1993-03-25

摘要: 采用交替迭代法及复应力函数与变分原理相结合的方法求解了含边缘裂纹半无限大加筋板的应力强度因子。分析中考虑了铆钉柔度的影响和边加筋条断的情况。对于一些特定的结构参数和3种铆钉柔度,给出了无量纲应力强度因子随裂纹长度的变化曲线。

关键词: 复应力函数, 应力强度因子, 边缘裂纹, 加筋板, 变分原理

Abstract: The stress intensity factors are obtained for a semi-infinite stiffened plate with edge crack by use of the method of alternative iteration and the method of combination of complex stress functions containing unknown coefficients and variational principles. In the course of the analysis, the influence of rivet flexibility and the condition of the broken edge stiffener are taken into consideration. For some cases the curves of non-dimensional stress intensity factors which vary with the crack length are given.

Key words: complex stress function, stress intensity factor, edge crack, stiffened plate, variational principle