Influence of Composite Lay-Up on the Stability of Channel-Section Profiles Weakened by Cut-Outs – A Numerical Investigation
Artykuł w czasopiśmie
MNiSW
100
Lista 2023
Status: | |
Autorzy: | Falkowicz Katarzyna, Valvo Paolo S. |
Dyscypliny: | |
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Rok wydania: | 2023 |
Wersja dokumentu: | Drukowana | Elektroniczna |
Język: | angielski |
Numer czasopisma: | 1 |
Wolumen/Tom: | 17 |
Strony: | 108 - 115 |
Impact Factor: | 1,0 |
Web of Science® Times Cited: | 7 |
Scopus® Cytowania: | 7 |
Bazy: | Web of Science | Scopus | BazTech |
Efekt badań statutowych | NIE |
Finansowanie: | The project/research was financed in the framework of the project Lublin University of Technology-Regional Excellence Initiative, funded by the Polish Ministry of Science and Higher Education (contract no. 030/RID/2018/19). The first Author gratefully acknowledges financial support from the University of Pisa, Italy, through the Visiting Fellows Programme 2022. |
Materiał konferencyjny: | NIE |
Publikacja OA: | TAK |
Licencja: | |
Sposób udostępnienia: | Otwarte czasopismo |
Wersja tekstu: | Ostateczna wersja autorska |
Czas opublikowania: | W momencie opublikowania |
Data opublikowania w OA: | 1 lutego 2023 |
Abstrakty: | angielski |
This paper presents a numerical study on the stability of composite channel-section profiles weakened by cut-outs. Profiles were made from carbon fibre-reinforced polymer (CFRP) laminates and subjected to compression load. Numerical analysis carried out in the Abaqus software allowed us to determine the value of the buckling load and the corresponding buckling form. Four different laminate lay-ups were chosen to study their effects on the buckling behaviour of the profiles. Obtained results help identify the best laminate lay-up to get the highest critical buckling load for perforated columns. The performed analysis shows that [45/-45/90/0]s and [90/-45/45/0]s composite lay- ups have the greatest impact on the buckling load. Moreover, the introduced perforation caused a change in the buckling form and a decrease in the critical load value. |