Source: Journal of Materials Engineering and Performance. Unidade: EESC
Subjects: CORROSÃO DOS MATERIAIS, LIGAS METÁLICAS, AERONAVES
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MORETO, J. A. et al. Effect of localized corrosion on fatigue–crack growth in 2524-T3 and 2198-T851 aluminum alloys used as aircraft materials. Journal of Materials Engineering and Performance, v. 27, p. 1917–1926, 2018Tradução . . Disponível em: https://doi.org/10.1007/s11665-018-3244-7. Acesso em: 04 nov. 2024.APA
Moreto, J. A., Broday, E. E., Rossino, L. S., Fernandes, J. C. S., & Bose Filho, W. W. (2018). Effect of localized corrosion on fatigue–crack growth in 2524-T3 and 2198-T851 aluminum alloys used as aircraft materials. Journal of Materials Engineering and Performance, 27, 1917–1926. doi:10.1007/s11665-018-3244-7NLM
Moreto JA, Broday EE, Rossino LS, Fernandes JCS, Bose Filho WW. Effect of localized corrosion on fatigue–crack growth in 2524-T3 and 2198-T851 aluminum alloys used as aircraft materials [Internet]. Journal of Materials Engineering and Performance. 2018 ; 27 1917–1926.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1007/s11665-018-3244-7Vancouver
Moreto JA, Broday EE, Rossino LS, Fernandes JCS, Bose Filho WW. Effect of localized corrosion on fatigue–crack growth in 2524-T3 and 2198-T851 aluminum alloys used as aircraft materials [Internet]. Journal of Materials Engineering and Performance. 2018 ; 27 1917–1926.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1007/s11665-018-3244-7