Effect of Impact Position on Repaired Composite Laminates Subjected to Multi-Impacts

Because the certification of aircraft structures requires significant costs and time-consuming experimental tests, all the studies carried out are strong contributions to the applicability of repairs based on adhesively bonded fibre composite patches. In this context, the main goal of this study aim...

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Detalles Bibliográficos
Autores principales: Reis, Paulo N. B., Coelho, Sara R. M., Bezazi, Abderrezak
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9693312/
https://www.ncbi.nlm.nih.gov/pubmed/36431523
http://dx.doi.org/10.3390/ma15228039

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9693312/
https://www.ncbi.nlm.nih.gov/pubmed/36431523
http://dx.doi.org/10.3390/ma15228039

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