航空学报 > 1993, Vol. 14 Issue (3): 197-201

疲劳裂纹扩展速率统计分析

王志智, 聂学州, 吴晓峰   

  1. 陕西耀县2号信箱,耀县 727100
  • 收稿日期:1992-07-16 修回日期:1992-09-08 出版日期:1993-03-25 发布日期:1993-03-25

STATISTICAL ANALYSIS OF FATIGUE CRACK GROWTH DATA

Wang Zhi-zhi, Nie Xue-zhou, Wu Xiao-feng   

  1. Box 2, Yao Xian, Shaan Xi, 727100
  • Received:1992-07-16 Revised:1992-09-08 Online:1993-03-25 Published:1993-03-25

摘要: 给出了4种常幅载荷下疲劳裂纹扩展速率的统计处理方法,获得了在规定存活率P下的“P-da/dN-△K”关系,并对LC9中心裂纹试样试验数据进行了统计分析,给出了存活率为0.50、0.90、0.95和0.99时Paris方程中的c和n值。最后对4种方法进行了比较。

关键词: 裂纹扩展速率, 可靠度, 统计分析

Abstract: The four statistical analysis methods for fatigue crack growth rate under constant amplitude loading are given in this paper. The "p-da / dN-ΔK" relationship under given reliability and the c and n values in Paris equation for testing results of LC9 CCT specimen with reliabilities 0.50, 0.90, 0.95 and 0.99 are obtained by using the four methods. Finally, the four methods are compared. It is obviously shown that the lognormal random variable model predicts larger statistical dispersion, and statistically independent Monte Carlo simulation gives much larger statistical dispersion.

Key words: crack growth rate, reliability, statistical analysis