钛合金
疲劳极限
极限(数学)
航程(航空)
线性关系
合金
线性回归
耐久性
压力(语言学)
数学
材料科学
结构工程
计算机科学
统计
冶金
数学分析
工程类
复合材料
语言学
哲学
作者
А. А. Скворцов,Evgeniya O. Gnatyuk,Olga Yu Sklemina,Vladimir K. Nikolaev
出处
期刊:Journal of applied research and technology
[Universidad Nacional Autonoma de Mexico]
日期:2023-02-27
卷期号:21 (1): 98-105
标识
DOI:10.22201/icat.24486736e.2023.21.1.2182
摘要
The presented paper is relevant, as it presents the results of fatigue tests of titanium alloy. The purpose of the article is to describe the use of the hypothesis of linear damage summation when processing the results of fatigue tests. In the study, the authors used empirical methods such as indirect observation of the object under study, description, and measurement of technical influences exerted on it by an artificial means. The linear regression analysis to establish the relationship between stress and durability was also used. The endurance limit of the titanium alloy was determined, which lies in the range from 460 to 480 MPa with the number of cycles from 105 to 108. It was concluded that the use of the linear damage summation hypothesis in processing the results of fatigue tests entails a satisfactory practical accuracy of the calculation of endurance limit
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