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Nanosecond surface sliding discharge in a supersonic flow with oblique shock waveстатья
- Авторы: Mursenkova I., Ivanov I.E., Ulanov P., Liao Yu, Sazonov A.
- Сборник: Proceedings of the 19th Workshop on Magneto-Plasma Aerodynamics Ed. V.A. Bityurin
- Год издания: 2020
- Место издания: Joint Institute for High Temperatures of Russian Academy of Sciences Moscow, JIHT RAS
- Первая страница: 22
- Последняя страница: 27
- Аннотация: The characteristics of a surface sliding discharge of nanosecond duration in a supersonic airflow with an oblique shock wave were investigated in discharge chamber of shock tube. Shadow visualization of the gas dynamics flow after the discharge showed that localized discharge channel in the flow generates a strong shock wave, leading to restructuring the shock-wave structure of the flow and subsequent relaxation to a stationary configuration.
- Добавил в систему: Мурсенкова Ирина Владимировна