Equivalent initial damage sizes (EIDS) for type 1C anodised aluminium alloy 7085-T7452 under variable amplitude loading

Author:

Dixon B.,Main B.ORCID,Barter S.ORCID

Funder

Defence Science and Technology Group

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference52 articles.

1. Determination of fatigue related discontinuity state of 7000 series of aerospace aluminum alloys;Merati;Eng. Fail. Anal.,2007

2. Typical fatigue-initiating discontinuities in metallic aircraft structures;Barter;Int. J. Fatigue,2012

3. Microstructure and surface finish influences on AA7085-T7452 small fatigue crack growth rates;Main;Eng. Fail. Anal.,2022

4. R.J.H. Wanhill, Milestone Case Histories in Aircraft Structural Integrity. NLR-TP-2002-521, National Aerospace Laboratory NLR, 2002.

5. C.F. Tiffany, J.P. Gallagher, C.A. Babish, Threats to aircraft structural safety, including a compendium of selected structural accidents/incidents. ASC-TR-2010-5002, Aeronautical Systems Center, Engineering Directorate, Wright-Patterson Air Force Base, 2010.

同舟云学术

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