国产材料疲劳寿命分布参数α的初步估计

被引:12
作者
周希沅
机构
[1] 飞机结构热强度研究所
关键词
国产材料; 疲劳寿命分布参数α; 估计;
D O I
暂无
中图分类号
学科分类号
摘要
<正> The fatigue-tested data of home-made materials and simple structure data are collected, which consist of 488 groups of 2705 specimens for aluminum alloys ; 313 groups of 1798 specimens for alloy steels) 79 groups of 389 specimens for titanium alloys. The shape parameter a of two-parameter Weibull distribution is estimated with maximum-likelihood estimation method and the preliminary estimation of a is given. In this study, the estimated parameters of home-made materials coincide with the parameters of overseas materials and the parameters a suggested by the literature can be applied to home-made material, too. This work also studies the effects of stress concentration factor ranges of fatigue life and tensile strength of materials on the values of a.
引用
收藏
页码:488 / 491
页数:4
相关论文
共 1 条
[1]   TC4钛合金旋转弯曲疲劳数据的回归分析 [J].
鞠静敏 ;
陆盘金 .
航空材料, 1988, (01) :29-32