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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...
Zapisane w:
| Wydane w: | Polymers (Basel) |
|---|---|
| Główni autorzy: | , , , |
| Format: | Artigo |
| Język: | Inglês |
| Wydane: |
MDPI
2019
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| Hasła przedmiotowe: | |
| Dostęp online: | 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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