Samara University Repository
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| Title: | Исследование влияния угла столкновения с птицей на прочность самолета на основе метода сглаженных частиц (SPH) |
| Authors: | Батурин О. В. |
| Keywords: | aircraft bird strike computational programs impact angle LS-DYNA smoothed partial hydrodynamics smoothed particle method SPH method SPH метод structural strength вычислительные программы метод сглаженных частиц прочность конструкции самолеты сглаженная частичная гидродинамика угол столкновения удар птицы |
| Issue Date: | 2025 |
| Citation: | Люй Вэйсюань Исследование влияния угла столкновения с птицей на прочность самолета на основе метода сглаженных частиц (SPH) = Research on the influence of bird strike angle on aircraft strength using the smoothed particle hydrodynamics (SPH) method / Люй Вэйсюань, О. В. Батурин // Перспективы развития двигателестроения : материалы междунар. науч.-техн. конф. им. Н. Д. Кузнецова (18–20 июня 2025 г.) / Самар. нац. исслед. ун-т им. С. П. Королева (Самар. ун-т) ; редкол.: Е. В. Шахматов, А. И. Ермаков. - Самара : Изд-во Самар. ун-та, 2025. - С. 178-179. |
| Abstract: | This study employs the Smoothed Particle Hydrodynamics (SPH) method to simulate the impact of a bird model on aircraft structures at different impact angles. A bird strike model is established using LS-DYNA software to obtain impact force and kinetic energy curves under varying collision angles. By analyzing the graphical trends, it is concluded that the bird strike angle has a non-negligible influence on aircraft structural integrity. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43233 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-178-179.pdf | 487.37 kB | Adobe PDF | View/Open |
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