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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...
| Autores principales: | , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
MDPI
2022
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| 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 |