Low-Cycle Fatigue, Fractography and Life Assessment of EN AW 2024-T351 under Various Loadings
Author:
Funder
Ministerstvo Školství, Mládeže a Tělovýchovy
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/article/10.1007/s40799-018-0263-0/fulltext.html
Reference39 articles.
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2. Billy F, Hénaff G, Benoit G, Van der Veen S (2014) Residual fatigue properties of a 2024-T351 aluminium alloy from the teardown of AIRBUS A320 wing panels after service. Adv Mater Res 891–892:621–626
3. Jurcevic R, DuQuesnay DL, Topper TH, Pompetzki MA (1990) Fatigue damage accumulation in 2024-T351 aluminium subjected to periodic reversed overloads. Int J Fatigue 12(4):259–266
4. Rodopoulos CA, Choi J-H, De los Rios ER, Yates JR (2004) Stress ratio and the fatigue damage map—part II: the 2024-T351 aluminium alloy. Int J Fatigue 26(7):747–752
5. Lee EU, Vasudevan AK, Glinka G (2009) Environmental effects on low cycle fatigue of 2024-T351 and 7075-T651 aluminum alloys. Int J Fatigue 31(11–12):1938–1942
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