尺寸标注
结构工程
铝
低周疲劳
材料科学
压力(语言学)
振动疲劳
疲劳试验
铝合金
疲劳极限
图表
循环计数
计算机科学
工程类
复合材料
哲学
航空航天工程
数据库
语言学
运营管理
作者
M M Jan,Hans‐Peter Gaenser,Wilfried Eichlseder
标识
DOI:10.1177/0954406211422146
摘要
Engineering estimates for the prediction of fatigue life is an important consideration at the design stage of components. Conventional approach of dimensioning against cyclic loading consists of comparing the stress amplitudes against the life time. Similarly, when a component is under high loading, a strain-life methodology is adopted. In both cases, extensive experimental efforts are required for obtaining the stress-life or strain-life curves. Therefore, it is important to develop a methodology for obtaining the fatigue life of a material to obtain a basic fatigue life data for design engineers. This study focuses on the fatigue life of a material in the region of low cycle fatigue. A method is proposed for obtaining an estimate for the fatigue life of material under high loading from the results of the high cycle fatigue and static properties of the material within the stress-based diagram. The concept is applied to a wrought aluminium alloy typically used for cryogenic applications.
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