固体力学与飞行器总体设计

无限板孔边裂纹问题的高精度解析权函数解

  • 赵晓辰 ,
  • 吴学仁 ,
  • 童第华 ,
  • 徐武 ,
  • 陈勃 ,
  • 胡本润
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  • 1. 中国航发 北京航空材料研究院, 北京 100095;
    2. 上海交通大学 航空航天学院, 上海 200240

收稿日期: 2017-12-29

  修回日期: 2018-03-14

  网络出版日期: 2018-05-15

基金资助

国家自然科学基金(11402249)

Accurate analytical weight function solutions for crack at edge of circular hole in infinite plate

  • ZHAO Xiaochen ,
  • WU Xueren ,
  • TONG Dihua ,
  • XU Wu ,
  • CHEN Bo ,
  • HU Benrun
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  • 1. AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China;
    2. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China

Received date: 2017-12-29

  Revised date: 2018-03-14

  Online published: 2018-05-15

Supported by

National Natural Science Foundation of China (11402249)

摘要

用Wu-Carlsson解析权函数法(WFM)求得了无限板孔边径向单裂纹和对称双裂纹的高精度解析权函数(WF)。分别用Shivakumar-Forman和Newman的解及基于复变函数泰勒级数展开的数值权函数WCTSE法结果,通过对相应格林函数(GF)的逐点比较验证了本文解析权函数的精度。该权函数不但精度高,而且作为裂纹长度的连续函数,能够高效准确地求解任意长度(a/R≤2)裂纹在任意复杂载荷作用下的断裂力学关键参量;且孔边单/双裂纹问题的权函数的形式和推导方法完全相同。作为示例,用该解析权函数计算了孔边裂纹在裂纹嘴楔形载荷、裂纹面幂函数,以及圆孔冷挤压残余应力等多种载荷形式下的应力强度因子。

本文引用格式

赵晓辰 , 吴学仁 , 童第华 , 徐武 , 陈勃 , 胡本润 . 无限板孔边裂纹问题的高精度解析权函数解[J]. 航空学报, 2018 , 39(9) : 221976 -221987 . DOI: 10.7527/S1000-6893.2018.21976

Abstract

Highly accurate Weight Functions (WFs) for the radial crack(s) at a circular hole are derived by using the Wu-Carlsson analytical Weight Function Method (WFM). Accuracy of the WFs proposed is verified and validated point-by-point by using Green's Functions (GFs) of Shivakumar-Forman and Newman, and also the Weight function Complex Taylor Series Expansion (WCTSE) method. It is shown that the WFs proposed are not only highly accurate, but also, as a continuous function for crack length, enable determination of key mechanical parameters of cracks of any length (a/R ≤ 2) under arbitrary loadings with high efficiency and accuracy. A unified approach is adopted for the derivations and expressions of WFs for single/double hole-edge crack(s). The analytical WFs proposed are also used to calculate stress intensity factors for various load cases including wedge-splitting forces at the crack mouth, crack face power stresses, and residual stress fields induced by cold-working of the circular hole.

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