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Dynamics of an elastically mounted wing in flowстатья
Информация о цитировании статьи получена из
Scopus
Дата последнего поиска статьи во внешних источниках: 10 апреля 2019 г.
- Автор: Selyutskiy Yury D.
- Сборник: AIP Conference Proceedings
- Том: 2046
- Год издания: 2018
- Первая страница: 020085-1
- Последняя страница: 020085-6
- DOI: 10.1063/1.5081605
- Аннотация: Study of aeroelastic systems has a long history. Interest to this problem is stimulated by applications: on the one hand, the flutter phenomenon can lead to reduction of strength or even break of structures; on the other hand, energy of oscillations occurring under flutter conditions can be converted into useful power. In the present work, an elastically mounted wing with asymmetrical profile is considered that has with two degrees of freedom (translational and rotational). Evolution of equilibrium positions and limit cycles of the system depending on parameters is studied. Comparison between symmetrical and non-symmetrical airfoils is performed.
- Добавил в систему: Селюцкий Юрий Дмитриевич