Mechanical behaviour and failure modes of fibre-metal laminates based on thin-ply composites
Artykuł w czasopiśmie
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brak dyscyplin
| Status: | |
| Autorzy: | Bieniaś Jarosław, Jakubczak Patryk, Droździel-Jurkiewicz Magda, Biruk-Urban Katarzyna |
| Dyscypliny: | |
| Aby zobaczyć szczegóły należy się zalogować. | |
| Rok wydania: | 2026 |
| Wersja dokumentu: | Elektroniczna |
| Język: | angielski |
| Wolumen/Tom: | 391 |
| Numer artykułu: | 120502 |
| Strony: | 1 - 14 |
| Impact Factor: | 7,8 |
| Web of Science® Times Cited: | 0 |
| Scopus® Cytowania: | 0 |
| Bazy: | Web of Science | Scopus |
| Efekt badań statutowych | NIE |
| Finansowanie: | This research was funded by the National Science Centre (Poland), grant number UMO-2023/49/N/ST11/01726. |
| Materiał konferencyjny: | NIE |
| Publikacja OA: | TAK |
| Licencja: | |
| Sposób udostępnienia: | Witryna wydawcy |
| Wersja tekstu: | Ostateczna wersja opublikowana |
| Czas opublikowania: | W momencie opublikowania |
| Data opublikowania w OA: | 26 maja 2026 |
| Abstrakty: | angielski |
| Thin-ply composites are considered a promising route to enhancing the performance of carbon- and glass-fibre reinforced structures due to their numerous advantages. This study investigates the mechanical behavior, microstructural observation and failure mechanisms of aluminium-based fibre-metal laminates (FMLs) incor- porating thin-ply carbon and glass fibre composites. Laminates with different fiber architectures were tested under tensile, compressive, in-plane shear, and interlaminar shear loading and compared with conventional FMLs manufactured using standard ply thickness. The results show that the incorporation of thin-ply composite layers does not significantly influence the in-plane mechanical properties of FMLs. Only unidirectional laminates exhibited a slight increase in tensile strength, while compressive strength and shear properties remained similar to those of conventional laminates. Failure mechanisms were primarily governed by fibre architecture and metal–composite interface behaviour rather than composite ply thickness, with delamination being the dominant damage mode. These findings indicate that the aluminum layers and interfacial characteristics largely control the mechanical response of FMLs, limiting the effect of thin-ply composites on in-plane performance. |
