Nonstationary phenomena in the region of shock-wave interaction with a boundary layer at transonic flow velocities
- Авторы: Sidorenko A.1, Budovskii A.1, Polivanov P.1, Vishnyakov O.1
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Учреждения:
- Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
- Выпуск: Том 43, № 6 (2017)
- Страницы: 570-573
- Раздел: Article
- URL: https://journals.rcsi.science/1063-7850/article/view/205063
- DOI: https://doi.org/10.1134/S1063785017060268
- ID: 205063
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Аннотация
Nonstationary characteristics of detached flow have been experimentally studied during interaction of the boundary layer with a shock wave that appears on a profiled bump in transonic flow. The experiments were performed with variable shock-wave intensity and position in a T-325 wind tunnel. The flow was studied using methods of schlieren imaging, measuring average pressure and its pulsations on the surface of a model, and determining velocity fields by particle image velocimetry. Analysis of the experimental data showed that the observed shock-wave oscillations and flow pulsations in the detachment zone were related to disturbances present in the oncoming boundary layer.
Об авторах
A. Sidorenko
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
Email: budovsky@itam.nsc.ru
Россия, Novosibirsk, 630090
A. Budovskii
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
Автор, ответственный за переписку.
Email: budovsky@itam.nsc.ru
Россия, Novosibirsk, 630090
P. Polivanov
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
Email: budovsky@itam.nsc.ru
Россия, Novosibirsk, 630090
O. Vishnyakov
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
Email: budovsky@itam.nsc.ru
Россия, Novosibirsk, 630090