The natures of fatigue crack growth under Mode Ⅱ loading are studied. End notched flexure beamspecimens were used. The effects of adherend thickness, rubber modification and adhesive thickness on fatiguecrack growth were examined. The experimental results show that some of these parameters apparently do affectfatigue crack growth. Resistance to ModeⅡ fatigue crack growth are increased by rubber modification. Theeffects of adhesive thickness and rubber content on fatigue crack growth were explained by von Mises'sequivalent stress using BEM analysis. For unmodified epoxy adhesives, the fatigue crack growth propertiesunder Mode Ⅱ loadings were significantly different in all regions. For rubber-modified epoxy adhesives, theywere also different in the first and second regions, but in the third region, they were similar.
목차
Abstract 1. 서론 2. 시험편 및 실험방법 2.1 시험편 2.2 실험방법 3. 실험결과 및 고찰 3.1 da/dN-△GII 관계에 미치는 접착제 층두께 및 CNBR 변성의 영향 3.2 da/dN-△GII 관계에 미치는 접착제 층내의 응력해석 4. 결론 참고문헌
키워드
Epoxy Adhesives(에폭시 접착제)Fatigue Crack Growth(피로균열진전)Adherend Thickness(접착층 두께)Adhesive Thickness(접착두께)Boundary Element Method(경계요소법)