Аннотация
Time-and-space localized disturbances (wave packets), created by pulsed electric discharges in a supersonic boundary layer, were visualized using hot-wire anemometry. Experimental studies were performed on a flat plate model with a sharp leading edge at Mach number M = 2. The evolution of localized artificial disturbances generated by discharges of different duration and power was studied. The velocity of propagation of the wave packets was also determined.
Язык оригинала | английский |
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Страницы (с-по) | 549-557 |
Число страниц | 9 |
Журнал | Journal of Visualization |
Том | 20 |
Номер выпуска | 3 |
DOI | |
Состояние | Опубликовано - 1 авг. 2017 |
Опубликовано для внешнего пользования | Да |