Author:
Anes V.,Pedro R.S.,Henriques E.,Freitas M.,Reis L.
Subject
General Engineering,Energy Engineering and Power Technology
Reference7 articles.
1. Towards quantitative non-destructive evaluation of aging aircraft;Achenbach,1991
2. Active metal-based corrosion protective coating systems for aircraft requiring no-chromate pretreatment;Bierwagen;Progress in Organic Coatings,2010
3. Cina, B., 1974. Reducing the susceptibility of alloys, particularly aluminium alloys, to stress corrosion cracking. US Patent 3,856,584.
4. Fatigue crack growth from corrosion damage in 7075-t6511 aluminium alloy under aircraft loading;DuQuesnay;International Journal of Fatigue,2003
5. Fatigue modeling for aircraft structures containing natural exfoliation corrosion;Liao;International Journal of Fatigue,2007
Cited by
14 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