航空学报 > 1991, Vol. 12 Issue (2): 16-21

弹塑性条件下工程小裂纹疲劳扩展试验研究

郑旻仲, 聂学州, 刘晓光   

  1. 飞机结构强度研究所
  • 收稿日期:1990-06-18 修回日期:1990-08-15 出版日期:1991-02-25 发布日期:1991-02-25

AN EXPERIMENTAL STUDY ON FATIGUE CRACK GROWTH FOR ENGINEERING SMALL CRACKS UNDER ELASTO-PLASTIC CONDITION

Zheng Minzhong, Nie Xuezhou, Liu Xiaoguang   

  1. Aircraft Structure Strength Research Institute
  • Received:1990-06-18 Revised:1990-08-15 Online:1991-02-25 Published:1991-02-25

摘要: 本文对在弹塑性条件下工程小裂纹的疲劳扩展规律进行了分析研究。给出了用△J积分作为在弹塑性条件下疲劳裂纹扩展主要控制参数的表达式。对工程小裂纹在缺口循环塑性区中的扩展规律提出了用修正的△J_(eff)积分描述和分析的表达方法,并与试验结果进行了比较。

关键词: 工程小裂纹, 弹塑性条件, 缺口循环塑性区

Abstract: The fatigue crack growth behaviour of engineering small cracks under elasto-plastic condition is studied. The J-integral expression as a main control parameter of fatigue crack growth under elasto-plastic condition is presented.It is suggested that the modified ΔJeft-integral can he used as a main control parameter for engineering cracks in cyclic and plastic area of a notch. The method was verified by the experimental results.

Key words: engineering small crack, elasto-plastic condition, cyclic plastic area of a notch