Evaluation of mechanically fastened composite joint with the clamping force

클램핑 포스가 존재하는 복합재료 조인트의 특성 평가

  • 류충오 (경상대학교 기계항공공학부 대학원) ;
  • 유연호 (경상대학교 기계항공공학부 대학원) ;
  • 이영환 (경상대학교 기계항공공학부 대학원) ;
  • 최진호 (경상대학교 기계항공공학부, 항공기부품기술연구소) ;
  • 권진회 (경상대학교 기계항공공학부, 항공기부품기술연구소)
  • Published : 2005.04.29

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 clamping force was applied to the composite joint.

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