Experimental and Numerical Research of Delamination Process in CFRP Laminates with Bending-Twisting Elastic Couplings
Artykuł w czasopiśmie
MNiSW
140
Lista 2021
Status: | |
Autorzy: | Rzeczkowski Jakub, Samborski Sylwester |
Dyscypliny: | |
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Rok wydania: | 2022 |
Wersja dokumentu: | Drukowana | Elektroniczna |
Język: | angielski |
Numer czasopisma: | 21 |
Wolumen/Tom: | 15 |
Numer artykułu: | 7745 |
Strony: | 1 - 14 |
Impact Factor: | 3,4 |
Web of Science® Times Cited: | 6 |
Scopus® Cytowania: | 6 |
Bazy: | Web of Science | Scopus |
Efekt badań statutowych | NIE |
Finansowanie: | The 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). |
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: | 3 listopada 2022 |
Abstrakty: | angielski |
This paper aims at experimental and numerical research of delamination process in car- bon/epoxy composite laminates with different fiber orientation angles in stacking sequence exhibiting the bending–twisting elastic couplings. Experimental specimens were subjected to the double can- tilever beam (DCB) tests according to the ASTM D5528 regulations. Values of the mode I strain energy release rates were calculated by using three different data reduction schemes: the modified beam theory, the compliance calibration method and the modified compliance calibration. Determination of delamination initiation point was conducted in twofold way: by visual observation of crack tip using high resolution camera and by utilization of the acoustic emission technique. Numerical analyss were prepared in Abaqus/CAE Software environment by using the virtual crack closure technique (VCCT). The numerical beam model consisted of SC8R continuum shell elements. Obtained out- comes revealed that extensive fiber bridging phenomenon occurring during delamination process pronouncedly affected propagation values of strain energy release rate (GIprop) and numerically obtained load–displacement curves. Nevertheless, in initial stage of delamination, results obtained by using the VCCT were in agreement with experimental data. The greatest value of the mode I fracture toughness equal 0.56 N/mm was obtained for the BT45 laminate. |