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Failure load prediction of mechanically fastened composite joint with the clamping force  

Ryu, Choong-O (경상대학교 기계항공공학부 대학원)
Choi, Jin-Ho (경상대학교 기계항공공학부, 항공기부품기술연구소)
Kweon, Jin-Hwe (경상대학교 기계항공공학부, 항공기부품기술연구소)
Publication Information
Composites Research / v.18, no.5, 2005 , pp. 9-14 More about this Journal
Abstract
The design of composite joint is a very important research area because they are often the weakest areas in composite structures. In this paper, the failure load of the mechanically fastened composite joint with the clamping force was predicted by the failure area index method. By the suggested failure area index method, the strength of the mechanically fastened composite joint could be predicted within $22.5\%$ when the clamping force was applied to the composite joint.
Keywords
Failure area index; Clamping force;
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