期刊
INTERNATIONAL JOURNAL OF FATIGUE
卷 43, 期 -, 页码 54-61出版社
ELSEVIER SCI LTD
DOI: 10.1016/j.ijfatigue.2012.02.005
关键词
Riveted lap joint; Detail fatigue rating method; Fatigue; Reliability
资金
- AVIC Aircraft Strength Research Institute
- Centre for Marine Technology and Engineering
The objective of this paper is to analyse the fatigue reliability of rivet lap joints of aircraft structures based on a fast reliability approach using a newly developed detail fatigue rating method. The existing detail fatigue rating method has been modified for use in analysing aircraft structures with multiple riveted joints subjected to a fatigue environment. The system reliability of aircraft structures is evaluated by the use of a series model. The new detail fatigue rating method, developed here, has been validated through the use of results from fatigue tests and finite element analysis. The modified detail fatigue rating method is confirmed to be more accurate in comparison to the existing traditional one. (C) 2012 Elsevier Ltd. All rights reserved.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据