Effect of Thermal Ageing on the Impact and Flexural Damage Behaviour of Carbon Fibre-Reinforced Epoxy Laminates

Most of the composite materials that are used in aerospace structures have been manufactured using a thermostable matrix, as epoxy resin. The region of stability of these polymers is defined by the glass transition temperature (T(g)). However, operating temperatures close and above the T(g) can caus...

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Detalles Bibliográficos
Autores principales: García-Moreno, Irene, Caminero, Miguel Ángel, Rodríguez, Gloria Patricia, López-Cela, Juan José
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2019
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6402028/
https://www.ncbi.nlm.nih.gov/pubmed/30960064
http://dx.doi.org/10.3390/polym11010080

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6402028/
https://www.ncbi.nlm.nih.gov/pubmed/30960064
http://dx.doi.org/10.3390/polym11010080

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