Refined 3-D Stress Analysis of Composite Wavy-Lap Joint

복합재료 Wavy-Lap Joint의 3-D 상세 응력 해석

  • 신헌 (서울대학교 항공우주공학과 대학원) ;
  • 이창성 (서울대학교 항공우주공학과 대학원) ;
  • 김승조 (서울대학교 항공우주공학과) ;
  • 김위대 (부산대학교 항공우주공학과)
  • Published : 2001.05.01

Abstract

Due to intrinsic load eccentricity, severe peel stress concentration occurs at both ends of the single-lap joint. To avoid load eccentricity as well as the singular tensile peel stress in the joint interface, composite wavy-lap joint is proposed. In this paper, refined 3-D stress analysis of wavy-lap joint is performed by finite element method using parallel mutifrontal solver. Analysis results show that the singular tensile peel stress concentration is totally avoided in wavy-lap joint, and that loads are more evenly transferred over the length of the joint. Therefore, the strength of wavy-lap joint is significantly higher than that of conventional single-lap joint. And it is believed that even higher strengths can be obtained by optimizing the new design configuration.

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