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Linking bilinear traction law parameters to cohesive zone length for laminated composites and bonded joints
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  • Linking bilinear traction law parameters to cohesive zone length for laminated composites and bonded joints
  • Linking bilinear traction law parameters to cohesive zone length for laminated composites and bonded joints
저자명
Li. Gang,Li. Chun
간행물명
Advances in aircraft and spacecraft science
권/호정보
2014년|1권 2호|pp.177-196 (20 pages)
발행정보
테크노프레스
파일정보
정기간행물|ENG|
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기타
이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
서지반출

기타언어초록

A theoretical exploration for determining the characteristic length of the cohesive zone for a double cantilever beam (DCB) specimen under mode I loading was conducted. Two traction-separation laws were studied: (i) a law with only a linear elastic stage from zero to full traction strength; and (ii) a bilinear traction law illustrating a progressive softening stage. Two analytical solutions were derived for the first law, which fit well into two existing solution groups. A transcendental equation was derived for the bilinear traction law, and a graphical method was presented to identify the resultant cohesive zone length. The study using the bilinear traction law enabled the theoretical investigation of the individual effects of cohesive law parameters (i.e., strength, stiffness, and fracture energy) on the cohesive zone length. Correlations between the theoretical and finite element (FE) results were assessed. Effects of traction law parameters on the cohesive zone length were discussed.