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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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| Publicado no: | Polymers (Basel) |
|---|---|
| Main Authors: | , , , |
| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
MDPI
2019
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| Assuntos: | |
| Acesso em linha: | https://ncbi.nlm.nih.gov/pmc/articles/PMC6402028/ https://ncbi.nlm.nih.gov/pubmed/30960064 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.3390/polym11010080 |
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