인문학
사회과학
자연과학
공학
의약학
농수해양학
예술체육학
복합학
DBpia AI
AI 에이전트
AI 아이디어
AI 리더
AI 뷰어
Citeasy
크롬 서지관리 다운로드
지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
피인용 0
초록·키워드
Advanced composite material consists of fibers of high specific strength and stiffness embedded in a stabilizing resin matrix of lower stiffness and strength. For composite structure, the longitudinal tension and compression are carried by the fibers. The matrix distributes the load between the fibers for the tension case and it stabilizes and prevents the fibers from buckling for the compression case. The fiber dominates the tensile properties and the matrix dominates the compression and in-plane shear.
The lap shear joint where all of the load in the structural members is transferred through the joining fasteners. This paper presents joint strength for laminate of advanced composite material in the bolted joints. The single lap joints were investigated experimentally with respect to stabilized and unstabilized lap joints. The stabilized single lap joint means joints with out-of-plane rotational constraints. The unstabilized single lap joint is joint without out-of-plane deflection constraints.
The standard angles 0 degree, +45 degree, -45 degree and 90 degree, in the laminate reference system, were used for ply orientation within a laminate. The composite material used in this paper is a carbon/epoxy unidirectional(UD) tape prepreg cured at 350F. A total of 112 single lap joint tests were conducted on specimens from 8 distinct laminates. The ASTM-D-5961M standard was used for stabilized and unstabilized single lap shear joints.
The lap shear joint where all of the load in the structural members is transferred through the joining fasteners. This paper presents joint strength for laminate of advanced composite material in the bolted joints. The single lap joints were investigated experimentally with respect to stabilized and unstabilized lap joints. The stabilized single lap joint means joints with out-of-plane rotational constraints. The unstabilized single lap joint is joint without out-of-plane deflection constraints.
The standard angles 0 degree, +45 degree, -45 degree and 90 degree, in the laminate reference system, were used for ply orientation within a laminate. The composite material used in this paper is a carbon/epoxy unidirectional(UD) tape prepreg cured at 350F. A total of 112 single lap joint tests were conducted on specimens from 8 distinct laminates. The ASTM-D-5961M standard was used for stabilized and unstabilized single lap shear joints.
본문·목차
인공지능 문자 인식 모델을 통해 추출된 텍스트로, 일부 오타나 오류가 포함될 수 있으나 지속적으로 개선 중입니다.
오류를 발견하셨다면 해당 부분을 드래그한 후 ' 를 통해 신고해주세요.
오류를 발견하셨다면 해당 부분을 드래그한 후 ' 를 통해 신고해주세요.
최근 본 자료 전체보기
UCI(KEPA) : I410-ECN-0101-2017-550-002049623
