Flow structures and unsteadiness in hypersonic shock wave/turbulent boundary layer interaction subject to steady jet

Liu, Q; Xie, W; Luo, ZB; Sun, MB; Cheng, P; Deng, X; Zhou, Y

Luo, ZB (通讯作者)，Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China.

ACTA MECHANICA SINICA, 2023; 39 (12):

Abstract

Direct numerical simulations of Mach 6 hypersonic flow over a 34 degrees compression corner subject to steady jet are conducted. Distributions of skin......

Full Text Link


Links

期刊讨论 | 中国SCI论文 | 期刊主页 | 投稿经验 | 杂志官网 | 投稿链接 | 作者需知 | PMC链接 | Pubmed全文检索