摘要: A series of experiments were performed at Mach 2.5 in a 17 cm diameter circular test section to characterize an impinging/reflected shock wave turbulent boundary layer interaction generated by a cone-cylinder centerbody. The cone-... 展开
作者 | Jonathan Sasson Heath H. Reising David O. Davis Paul J. Barnhart | ||
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作者单位 | |||
文集名称 | Computational fluid dynamics | ||
出版年 | 2023 | ||
会议名称 | AIAA SciTech Forum and Exposition | ||
页码 | 171-219 | 开始页/总页数 | 00000171 / 49 |
会议地点 | Maryland(US) | 会议年 | 2023 |
馆藏号 | P2400086 |