Failure Prediction of Composite Single Lap Bonded Joints

복합재료 Single Lap 접합 조인트의 파손 예측

  • 김광수 (한국항공우주연구원 구조그룹) ;
  • 장영순 (한국항공우주연구원 구조그룹) ;
  • 이영무 (한국항공우주연구원 구조그룹)
  • Published : 2004.10.01

Abstract

Failure predictions of composite single-lap bonded joints were performed considering both of composite adherend failure and bondline failure. An elastic-perfectly plastic model of adhesive and a delamination failure criterion are used. The failure prediction results such as failure mode and strength have very good agreements with the test results of joint specimens with various bonding methods and parameters. The influence of variations in the effective strength (that is, adhesion performance) and plastic behavior of adhesive on the failure characteristics of composite bonded joints are investigated numerically. The numerical results show that optimal joint strength is archived when adhesive and delamination failure occur in the same time.

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