Coupled Modal Analysis and Aerodynamics of Rotating Composite Beam
Artykuł w czasopiśmie
MNiSW
140
Lista 2023
Status: | |
Autorzy: | Stachyra Grzegorz, Kłoda Łukasz, Szmit Zofia |
Dyscypliny: | |
Aby zobaczyć szczegóły należy się zalogować. | |
Rok wydania: | 2023 |
Wersja dokumentu: | Drukowana | Elektroniczna |
Język: | angielski |
Numer czasopisma: | 23 |
Wolumen/Tom: | 16 |
Numer artykułu: | 7356 |
Strony: | 1 - 25 |
Impact Factor: | 3,1 |
Web of Science® Times Cited: | 0 |
Scopus® Cytowania: | 1 |
Bazy: | Web of Science | Scopus |
Efekt badań statutowych | NIE |
Finansowanie: | This research was funded in whole or in part by the National Science Centre, Poland 2021/41/B/ST8/03190. For the purpose of Open Access, the author has applied a CC-BY public copyright licence to any Author Accepted Manuscript (AAM) version arising from this submission. The first author would like to acknowledge the financial support of the National Centre for Research and Development under the project POWR.03.02.00-IP.08-00-DOK/16 within the framework of “The International Ph.D. Course in Mechanics”, provided by the Faculty of Mechanical Engineering at Lublin University of Technology, POWR.03.02.00-00-I017/16-00. |
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 listopada 2023 |
Abstrakty: | angielski |
This study primarily focuses on conducting, both experimentally and numerically, a modal analysis of a cantilever composite beam. Through extended numerical simulations, we investigate Campbell diagrams, which, depending on the rotation speed of the structure, comprise natural frequencies and their corresponding modal shapes. Our results are categorized into two main aspects: the classical single-mode behavior and an innovative extension involving linearly coupled modal analysis. One key novelty of our research lies in the introduction of an analytical description for coupled mode shapes, which encompass various deformations, including bending, longitudinal deformations, and twisting. The most pronounced activation of dynamic couplings within the linear regime for a 45◦ preset angle is observed, though the same is not true of the 0◦ and 90◦ preset angles, for which these couplings are not visible. In addition to the modal analysis, our secondary goal is to assess the lift, drag forces, and moment characteristics of a rectangular profile in uniform flow. We provide insights into both the static and dynamic aerodynamic responses experienced by the beam within an operational frequency spectrum. This study contributes to a deeper understanding of the dynamics of composite rotating beams and their aerodynamic characteristics. |