Fatigue crack propagation of new aluminum lithium alloy bonded with titanium alloy strap
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference17 articles.
1. Can we accelerate the improvement of energy efficiency in aircraft systems;Lee;Energy Convers Manage,2010
2. Fail-safe design of integral metallic aircraft structures reinforced by bonded crack retarders;Zhang;Eng Fract Mech,2009
3. A modelling technique for calculating stress intensity factors for structures reinforced by bonded straps, Part I: mechanisms and formulation;Boscolo;Eng Fract Mech,2010
4. A modelling technique for calculating stress intensity factors for structures reinforced by bonded straps. Part II: validation;Boscolo;Eng Fract Mech,2010
5. Fracture and damage mechanics modelling of thin-walled structures—an overview;Zerbst;Eng Fract Mech,2009
Cited by 13 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. Effect of synergistic surface treatment on the bonding strength and durability performance of aluminum-lithium alloy adhesive joints;International Journal of Adhesion and Adhesives;2024-06
2. In situ corrosion fatigue life of 2198-T8 Al–Li alloy based on tests and DIC technique;Materials Testing;2022-10-01
3. Tailoring Al–Li Alloy Surface Wettability with a Femtosecond Laser and Its Effect on Bonding Performance;Coatings;2021-08-20
4. Integral Aircraft Wing Panels with Penetration Cracks: The Influence of Structural Parameters on the Stress Intensity Factor;Applied Sciences;2020-06-16
5. Analysis of the Fatigue Damage Behavior of AW2099-T83 Al-Li Alloy under Strain-Controlled Fatigue;Frattura ed Integrità Strutturale;2019-06-25
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