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| Research Progress of Numerical Simulation on Corrosion of Aircraft Structure |
| Received:July 29, 2019 Revised:November 06, 2019 |
| View Full Text View/Add Comment Download reader |
| DOI：10.7643/issn.1672-9242.2020.02.010 |
| KeyWord:aircraft corrosion numerical simulation cellular automata finite element method boundary element method |
| Author | Institution |
| WANG Hai-tao |
National Engineering Research Center for Corrosion Control, Institute of Metal Research, Chinese Academy of Sciences, Shenyang , China |
| HAN En-hou |
National Engineering Research Center for Corrosion Control, Institute of Metal Research, Chinese Academy of Sciences, Shenyang , China |
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| 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. |
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