Сериальное издание: AIP Conference Proceedings. 18th International Conference on the Methods of Aerophysical Research (ICMAR2016) (Perm, Russia, 27 June-3 July, 2016)
Страницы: 030031-1-030031-10
Аннотация
Experimental data gained while studying the gas-dynamic structure of a supersonic jet impinging onto a flat plate are reported. The data, obtained for different obstacle inclination angles and flow regimes, comprise the near-wall pressure fields and schlieren images of the flow. The flow pattern in the vicinity of the obstacle and the main elements of the shock-wave structure of the flow observed at various inclination angles are described.
