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http://dx.doi.org/10.12985/ksaa.2011.19.4.012

A analysis on the mechanical joint of composite laminate  

Kim, Sung-Joon (한국항공우주연구원 항공구조팀)
Hwang, In-Hee (한국항공우주연구원 항공구조팀)
Publication Information
Journal of the Korean Society for Aviation and Aeronautics / v.19, no.4, 2011 , pp. 12-17 More about this Journal
Abstract
This paper gives a review of finite element model for the analysis of fastening as practical points of view. Different mechanical properties of plate-fastener systems are analyzed. Calculations of the system properties are described as well as the technique of their application in model. Analysis has been performed for calculating the load distribution in multi-joint and the results are compared using the several models. The effects of fastener-hole clearance on the load distribution in multifastener joints are presented. And the stress analysis method have been reviewed for failure analysis of mechanical joint of composite laminate.
Keywords
Joint; Flexibility; Rigidity; Contact; composite laminate;
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