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Fuzzy corrosion fatigue model for aging aircraft structure reliability

conference contribution
posted on 2024-10-31, 08:57 authored by Yunxiang Che, He Ren, Xu WangXu Wang
The integrity and safety of aircraft structure are greatly degraded because of corrosion and corrosion fatigue. The failure mechanism of corrosion and fatigue is very complicated and combined with randomness and fuzziness. For precisely describing the corrosion fatigue life of aircraft structure, based on the obtained investigating service data of the again aircraft, a fuzzy reliability approach is proposed in this paper. Meanwhile, the effects of the pit aspect ratio, the crack aspect ratio and all fuzzy factors on corrosion fatigue life of aircraft structure are discussed as well. Application was proved this methodology is working well in accessing the corrosion fatigue reliability of aging aircraft structure.

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Related Materials

  1. 1.
    ISBN - Is published in 9780980321555 (urn:isbn:9780980321555)

Start page

1

End page

9

Total pages

9

Outlet

Proceedings of the thirteenth Australian International Aerospace Congress

Editors

Waldron Smith Management

Name of conference

Thirteenth Australian International Aeronautical Conference

Publisher

John Wiley and Sons

Place published

Melbourne, Australia

Start date

2009-03-09

End date

2009-03-12

Language

English

Copyright

Copyright © 2006 John Wiley & Sons, Ltd.

Former Identifier

2006009671

Esploro creation date

2020-06-22

Fedora creation date

2011-09-09

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