The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate

V. L. Kocharin, A. D. Kosinov, A. A. Yatskikh, L. V. Afanasev, Yu G. Ermolaev, N. V. Semionov

Результат исследования: Научные публикации в периодических изданияхстатья по материалам конференции

Аннотация

The weak shock waves impact on the flow in the boundary layer of the sweep flat plate at Mach number 2 is studied experimentally. The model was installed at a zero angle of attack. Shock waves in the oncoming flow were generated by a two-dimensional roughness on the side wall of the wind tunnel test section. The data were obtained with a two-dimensional roughness on the wall of the wind tunnel and with a smooth wall at sweep angles (35 and 40 degrees) of the leading edge of the flat blunt plate. The measurements were carried out with a constant temperature anemometer.

Язык оригиналаанглийский
Номер статьи012083
ЖурналJournal of Physics: Conference Series
Том1404
Номер выпуска1
DOI
СостояниеОпубликовано - 6 дек 2019
Событие16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019 - Novosibirsk, Российская Федерация
Продолжительность: 30 сен 20195 окт 2019

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