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http://repository.hneu.edu.ua/handle/123456789/28282
Полная запись метаданных
Поле DC | Значение | Язык |
---|---|---|
dc.contributor.author | Smetankina N. V. | - |
dc.contributor.author | Misura S. Yu. | - |
dc.contributor.author | Misiura Ie. Iu. | - |
dc.date.accessioned | 2022-12-14T11:00:21Z | - |
dc.date.available | 2022-12-14T11:00:21Z | - |
dc.date.issued | 2022 | - |
dc.identifier.citation | Smetankina N. V. Mathematical and computer simulation of the response of aircraft composite elements to impact loading / N. V. Smetankina, S. Yu. Misura, Ie. Iu. Misiura // XХХ international scientific-practical conference MicroCAD-2022. – Kharkiv, October 19 – 21. – 2022. – P. 328. | ru_RU |
dc.identifier.uri | http://repository.hneu.edu.ua/handle/123456789/28282 | - |
dc.description.abstract | The present work suggests an analytical approach to investigating vibrations of laminated orthotropic elements of aircraft structures under impact by hail. The aircraft elements as non-closed cylindrical shells with a complicated form in the plan view are considered. Impact loading of a shell is carried out by an indenter, which is dropped on the shell from a certain height. The dynamic behaviour of the shells is described by the first-order theory accounting for transverse shear strain, thickness reduction and normal element rotation inertia in each layer. The method potentialities are demonstrated by calculating stresses in three-layer and five-layer orthotropic shells with different boundary conditions. A good match of results obtained by different methods confirms the feasibility and effectiveness of the method offered. | ru_RU |
dc.language.iso | en | ru_RU |
dc.subject | aircraft composite elements | ru_RU |
dc.subject | method potentialities | ru_RU |
dc.title | Mathematical and computer simulation of the response of aircraft composite elements to impact loading | ru_RU |
dc.type | Article | ru_RU |
Располагается в коллекциях: | Статті (ЕММ) |
Файлы этого ресурса:
Файл | Описание | Размер | Формат | |
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Zbirnik-tez-MicroCAD-2022_МісюраЄЮ_328с.pdf | 174,61 kB | Adobe PDF | Просмотреть/Открыть |
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