Effects of interrupted aging T6I4 on hardness and fracture toughness of aeronautic AA7050 alloy
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Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s40430-024-05069-5.pdf
Reference56 articles.
1. Dumont D, Deschamps A, Brechet Y (2003) On the relationship between microstructure, strength and toughness in AA7050 aluminum alloy. Mater Sci Eng A 356:326–336. https://doi.org/10.1016/S0921-5093(03)00145-X
2. Antunes AMBS, Baptista CARP, Barboza MJR et al (2019) Effect of the interrupted aging heat treatment T6I4 on the tensile properties and fatigue resistance of AA7050 alloy. J Brazilian Soc Mech Sci Eng. https://doi.org/10.1007/s40430-019-1821-9
3. Deshpande NU, Gokhale AM, Denzer DK, Liu J (1998) Relationship between fracture toughness, fracture path, and microstructure of 7050 aluminum alloy: part I. quantitative characterization. Metall Mater Trans A Phys Metall Mater Sci 29:1191–1201. https://doi.org/10.1007/s11661-998-0246-3
4. Cavalcante TRF, Pereira GS, Koga GY et al (2021) Fatigue crack propagation of aeronautic AA7050-T7451 and AA2050-T84 aluminum alloys in air and saline environments. Int J Fatigue 154:106519. https://doi.org/10.1016/j.ijfatigue.2021.106519
5. Azarniya A, Taheri AK, Taheri KK (2019) Recent advances in ageing of 7xxx series aluminum alloys: a physical metallurgy perspective. J Alloys Compd 781:945–983. https://doi.org/10.1016/j.jallcom.2018.11.286
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