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http://dx.doi.org/10.12985/ksaa.2012.20.3.051

Matrix Structure Reliability Analysis using AFORM  

Lee, Seung-Gyu (한국항공우주연구원)
Kim, Tae-Uk (한국항공우주연구원)
Kim, Sung-Chan (한국항공우주연구원)
Ahn, Lee-Ki (한국항공우주연구원)
Publication Information
Journal of the Korean Society for Aviation and Aeronautics / v.20, no.3, 2012 , pp. 51-56 More about this Journal
Abstract
The wing is a framework composed chiefly of skin, spars, ribs and can be simplified by matrix structure. In this paper, a displacement reliability of matrix structure is analysed by AFORM(Advanced First Order Reliability Method) and applicability is assessed.
Keywords
Reliability Assessment; AFORM; Matrix Structure;
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  • Reference
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