@inproceedings{7d4b0edc8bc3428285699671b0d281fc,
title = "Modeling and Simulation of Wing Skin Structural Pitting Corrosion",
abstract = "Pitting corrosion (PC) significantly affects and reduces the structural integrity of aircraft as they age. This paper details a simulation method for large wing structure with PC damage. It is difficult for integral wing structure to make a corrosion test in the laboratory. The method of modeling and simulation for the wing structure with PC is provided. Firstly, the Finite Element Model of wing structure has been constructed according to a CATIA model of wing structure. Secondly, simulation model of wing structure with PC has been obtained via randomly deleting elements of finite element method. Finally, we discuss the maximum stress distribution of wing structure and mechanical properties of ten wing-fuselage connection joint under different degree of pitting corrosion for wing upper skin. The work in this paper can provide a method of integrated wing PC simulation in order to cut corrosion experiment cost and offer references of aircraft design and corrosion maintenance.",
keywords = "Modeling and simulation, Pitting corrosion, Wing skin",
author = "Xiuping Zhu and Fangyi Wan and Xingliang Yu and Yingnan Guo",
note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018 ; Conference date: 26-10-2018 Through 28-10-2018",
year = "2019",
month = jan,
day = "4",
doi = "10.1109/PHM-Chongqing.2018.00106",
language = "英语",
series = "Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "591--596",
editor = "Ping Ding and Chuan Li and Shuai Yang and Ping Ding and Rene-Vinicio Sanchez",
booktitle = "Proceedings - 2018 Prognostics and System Health Management Conference, PHM-Chongqing 2018",
}