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飞机结构腐蚀数值仿真模拟的研究进展
引用本文:王海涛,韩恩厚.飞机结构腐蚀数值仿真模拟的研究进展[J].装备环境工程,2020,17(2):61-65.
作者姓名:王海涛  韩恩厚
作者单位:中国科学院金属研究所 国家金属腐蚀控制工程技术研究中心,沈阳,110016
基金项目:国家重点研发计划资助项目(2017YFB0702100);中国科学院“十三五”信息化专项(XXH13505-03-212)
摘    要:系统介绍了飞机结构腐蚀数值仿真模拟中应用较为广泛的元胞自动机方法、有限元方法、边界元方法,尤其是它们在点蚀、电偶腐蚀、缝隙腐蚀、晶间腐蚀仿真的研究现状,并对各自方法的优点和缺点与适用的范围进行了阐述,以期对该领域的研究者提供一定的导向作用。

关 键 词:飞机  腐蚀  仿真模拟  元胞自动机  有限元  边界元
收稿时间:2019/7/29 0:00:00
修稿时间:2019/11/6 0:00:00

Research Progress of Numerical Simulation on Corrosion of Aircraft Structure
WANG Hai-tao and HAN En-hou.Research Progress of Numerical Simulation on Corrosion of Aircraft Structure[J].Equipment Environmental Engineering,2020,17(2):61-65.
Authors:WANG Hai-tao and HAN En-hou
Institution:National Engineering Research Center for Corrosion Control, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China and National Engineering Research Center for Corrosion Control, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China
Abstract:The paper systematically introduced the cellular automata model, the finite element method and the boundary element method widely used in the numerical simulation on aircraft structure corrosion, especially the current research situation on their pitting corrosion, galvanic corrosion, crevice corrosion and intergranular corrosion, and illustrated their advantages, disadvantages and the scope of application, in order to provide a guidance for researchers in this field.
Keywords:aircraft  corrosion  numerical simulation  cellular automata  finite element method  boundary element method
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