HCF notch predictions based on weakest-link failure models

被引:39
|
作者
Lanning, DB
Nicholas, T
Palazotto, A
机构
[1] Embry Riddle Aeronaut Univ, Coll Engn, Prescott, AZ 86301 USA
[2] AFIT, ENY, Wright Patterson AFB, OH 45433 USA
关键词
high cycle fatigue; notches; Ti-6Al-4V; weakest link; Weibull distribution;
D O I
10.1016/S0142-1123(03)00156-7
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Weakest-link models for the prediction of the high cycle fatigue (HCF) limit stress of notched components were investigated. The models employed surface area elements in the high-stress region surrounding the root of a notch. Statistical descriptions of unnotched specimen experimental data were developed using Weibull distributions and median ranking, and incorporated into some of the weakest-link notch formulations. The predictions from each of the failure models were compared to the experimental 10(6) cycle fatigue limit stresses. The fatigue limit stresses were estimated using a step-loading technique at stress ratios from R = -1 to 0.8, for five geometries (elastic stress concentration factors of K-t = 2.0, 2.8 and 4.1) of circumferentially notched Ti-6Al-4V specimens. The methods were shown to be modestly successful, although data obtained at R = -1 and R > 0.65 could not be correlated well with data at intermediate values of R. (C) 2003 Elsevier Ltd. All rights reserved.
引用
收藏
页码:835 / 841
页数:7
相关论文
共 50 条