A Progressive Damage Model for Mechanically Fastened Joints in Composite Laminates
Author:
Affiliation:
1. Department of Aeronautics, Imperial College of Science, Technology and Medicine, Centre for Composite Materials, Prince Consort Road, London SW7 2BY, UK
Abstract
Publisher
SAGE Publications
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://journals.sagepub.com/doi/pdf/10.1177/002199839903302402
Reference67 articles.
1. The strength of bolted joints in glass fibre/epoxy laminates
2. The strength of bolted joints in multi-directional cfrp laminates
3. Influence of geometric parameters on the stress distribution around a pin-loaded hole in a composite laminate
Cited by 445 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Design optimization and failure analysis of natural composite sandwich T-joints under pulling load conditions;Engineering Failure Analysis;2024-10
2. Mechanical performance of a new stiffened PFRP-steel bolted connection: Experimental and numerical investigations;Journal of Building Engineering;2024-10
3. Progressive failure analysis of laminar composites under compression using smeared crack-band damage model and full layerwise theory;Theoretical and Applied Fracture Mechanics;2024-10
4. Multiscale damage and low-velocity impact study of three-dimensional woven composites;Thin-Walled Structures;2024-09
5. Multi objective optimization of composite laminate repaired by patches in considering static strength and fatigue life;Mechanics of Advanced Materials and Structures;2024-07-31
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3