Stress Analysis Of Wavy Lap Joint

WAVY LAP JOINT 응력 해석

  • 김위대 (부산대학교 항공우주공학과) ;
  • 양승희 (부산대학교 항공우주공학과)
  • Published : 2000.11.01

Abstract

The adhesive bonded single-lap joint is due to its intrinsic load eccentricity problem, severe peel stresses concentration occur at both end of the joint. In this paper, new lap-joint is designed to avoid the singular peel stress, and to compare the stresses of the middle adhesive layer between the single-lap joint and the wavy-lap joint. Two adherend lay-up, i.e., [90/0/90/0]$_{2s}$ and [0/90/0/90]$_{2s}$ were consider in the study.