Corrosion fatigue crack growth of 7475 T7351 aluminum alloy under flight simulation loading (2015)
Source: Procedia Engineering. Conference titles: International Conference on Material and Component Performance under Variable Amplitude Loading (VAL). Unidade: EESC
Subjects: CORROSÃO DOS MATERIAIS, FADIGA DOS MATERIAIS, ALUMÍNIO
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CHEMIN, Aline Emanuelle Albuquerque et al. Corrosion fatigue crack growth of 7475 T7351 aluminum alloy under flight simulation loading. Procedia Engineering. Amsterdam: Escola de Engenharia de São Carlos, Universidade de São Paulo. Disponível em: https://doi.org/10.1016/j.engfracmech.2015.05.038. Acesso em: 25 ago. 2024. , 2015APA
Chemin, A. E. A., Spinelli, D., Bose Filho, W. W., & Ruchert, C. O. F. T. (2015). Corrosion fatigue crack growth of 7475 T7351 aluminum alloy under flight simulation loading. Procedia Engineering. Amsterdam: Escola de Engenharia de São Carlos, Universidade de São Paulo. doi:10.1016/j.engfracmech.2015.05.038NLM
Chemin AEA, Spinelli D, Bose Filho WW, Ruchert COFT. Corrosion fatigue crack growth of 7475 T7351 aluminum alloy under flight simulation loading [Internet]. Procedia Engineering. 2015 ; 101 85-92.[citado 2024 ago. 25 ] Available from: https://doi.org/10.1016/j.engfracmech.2015.05.038Vancouver
Chemin AEA, Spinelli D, Bose Filho WW, Ruchert COFT. Corrosion fatigue crack growth of 7475 T7351 aluminum alloy under flight simulation loading [Internet]. Procedia Engineering. 2015 ; 101 85-92.[citado 2024 ago. 25 ] Available from: https://doi.org/10.1016/j.engfracmech.2015.05.038
