摘要
本文提出了一种随机耐久性分析方法。该方法从耐久性分析的基本原理出发,考虑损伤发展的随机特性,提出用正态随机变量裂纹扩展方程描述裂纹扩展规律,对随机基础的EIFS分布和给定任意时刻的裂纹尺寸分布给出相应的确定方法和推导公式,进而建立较为完善的随机耐久性分析程序。文中通过对实际飞机结构的耐久性分析评估,证明了该方法的有效性。同时该方法可推广应用于其它类似的大型结构。
This paper develops a stochastic durability analysis method. In view of the basic concept of durability analysis, taking into accounts the stochastics of damage process,with the normal-random-variable crack growth equation describing crack propagation,the evaluation methods of ElFS distributions and the formulas of crack size distributions at any time were proposed, and then a complete stochastic durability analysis program was set up.Through practical applications, the method was proved to be applicable for aircraft structures or any other structure.
出处
《华南理工大学学报(自然科学版)》
EI
CAS
CSCD
1995年第7期142-148,共7页
Journal of South China University of Technology(Natural Science Edition)
关键词
裂纹扩展
随机分析
结构
耐久性
断裂力学
s:durability
crack
crack propagation/crack-exceedance probability