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服从不同分布的疲劳寿命分散系数分析
引用本文:贺小帆,刘文珽.服从不同分布的疲劳寿命分散系数分析[J].北京航空航天大学学报,2002,28(1):47-49.
作者姓名:贺小帆  刘文珽
作者单位:北京航空航天大学 飞行器设计与应用力学系
摘    要:民机结构的疲劳寿命服从双参数威布尔分布,其分散系数与战斗机基于对数正态分布的疲劳寿命分散系数存在明显的不同.为分析疲劳寿命服从这两种不同分布时分散系数的区别和联系,导出了疲劳寿命服从双参数威布尔分布时的理论和试验用疲劳寿命分散系数计算公式;并从理论基础和数值计算结果两个方面,对服从对数正态分布和双参数威布尔分布的疲劳寿命分散系数进行了对比,所得的结论对确定民机结构疲劳寿命分散系数提供了重要的技术依据.

关 键 词:疲劳寿命  正态分布  分散系数  威布尔分布
文章编号:1001-5965(2002)01-0047-03
收稿时间:2000-05-16
修稿时间:2000年5月16日

On Scatter Factors of Fatigue Life Obeying Different Distributions
HE Xiao-fan,LIU Wen-ting.On Scatter Factors of Fatigue Life Obeying Different Distributions[J].Journal of Beijing University of Aeronautics and Astronautics,2002,28(1):47-49.
Authors:HE Xiao-fan  LIU Wen-ting
Institution:Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics
Abstract:The fatigue life of civil aircraft structures obeys two parameter Weibull distribution,its scatter factor is significantly different from that obeys logarithm normal distribution .To analyze the difference and relation of these two scatter factors,the scatter factor formulas of fatigue life which obeys two parameter Weibull distribution are presented for theoretical calculation and fatigue testing and the values of scatter factors for different materials are given. Comparison efforts between scatter factors obeying these two distributions are conducted theoretically and numerically. The result provides the important technological approach in determining the fatigue scatter factor of the civil aircraft structures.
Keywords:fatigue life  normal distributions  scatter factor  Weibull distribution
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