Evolution of localized artificial disturbance in 2D and 3D supersonic boundary layers

Aleksey Yatskikh; Yury Yermolaev; Alexander Kosinov; Nikolai Semionov; Alexander Semenov

doi:10.1177/0954410018787120

Evolution of localized artificial disturbance in 2D and 3D supersonic boundary layers

Aleksey Yatskikh, Yury Yermolaev, Alexander Kosinov, Nikolai Semionov, Alexander Semenov

Результат исследования: Научные публикации в периодических изданиях › статья › рецензирование

3 Цитирования (Scopus)

Аннотация

The evolution of a controlled broadband wave packet in flat-plate and swept-wing supersonic boundary layers was experimentally investigated at Mach number M = 2. The wave packet was introduced into the boundary layer by a localized pulse electrical discharge. The structure and evolution downstream of the wave packet were studied by hot-wire measurements. It was found that the wave packet has a symmetric shape in a flat-plate boundary layer, whereas there is asymmetry in case of a swept-wing one. The spectral analysis of the development of different modes of the wave packet was provided.

Язык оригинала	английский
Страницы (с-по)	115-123
Число страниц	9
Журнал	Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Том	234
Номер выпуска	1
DOI	https://doi.org/10.1177/0954410018787120
Состояние	Опубликовано - 1 янв 2020

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10.1177/0954410018787120

Link to publication in Scopus

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abstract = "The evolution of a controlled broadband wave packet in flat-plate and swept-wing supersonic boundary layers was experimentally investigated at Mach number M = 2. The wave packet was introduced into the boundary layer by a localized pulse electrical discharge. The structure and evolution downstream of the wave packet were studied by hot-wire measurements. It was found that the wave packet has a symmetric shape in a flat-plate boundary layer, whereas there is asymmetry in case of a swept-wing one. The spectral analysis of the development of different modes of the wave packet was provided.",

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Evolution of localized artificial disturbance in 2D and 3D supersonic boundary layers. / Yatskikh, Aleksey; Yermolaev, Yury; Kosinov, Alexander; Semionov, Nikolai; Semenov, Alexander.

В: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Том 234, № 1, 01.01.2020, стр. 115-123.

Результат исследования: Научные публикации в периодических изданиях › статья › рецензирование

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