Numerical and Experimental Validation of a Supersonic Mixing Layer Facility

The design of a supersonic-supersonic mixing layer facility was motivated by the need for a benchmark experimental platform to study the physical phenomena underlying supersonic mixing layers. The facility is an intermittent blowdown wind tunnel characterized by a two-stream design separated by a sp...

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Бібліографічні деталі
Автори: Yudong Li, Li Chen, Hongxun Li, Yungang Wu, Shuang Chen
Формат: Стаття
Мова:English
Опубліковано: MDPI AG 2022-05-01
Серія:Applied Sciences
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Онлайн доступ:https://www.mdpi.com/2076-3417/12/11/5489