Mechanisms and characteristics of wall skin friction reduction by boundary layer injection under hypervelocity inflow conditions
-
Published:2024-04
Issue:
Volume:106
Page:109269
-
ISSN:0142-727X
-
Container-title:International Journal of Heat and Fluid Flow
-
language:en
-
Short-container-title:International Journal of Heat and Fluid Flow
Author:
Qu ZhenmingORCID,
Li Xinke,
Luo Feiteng,
Long Yaosong,
Chen Wenjuan
Reference42 articles.
1. Hypersonic turbulent boundary-layer fuel injection and combustion: skin-friction reduction mechanisms;Barth;AIAA J.,2013
2. Fifty years of hypersonics: where we’ve been, where we’re going;Bertin;Prog. Aerosp. Sci.,2003
3. RANS investigation of the effect of pulsed fuel injection on scramjet HyShot II engine;Chen;Aerosp. Sci. Technol.,2019
4. Large-eddy Simulation of Compressible Turbulent Boundary Layers with Heat Addition;Denman,2007
5. Denman, A.W., Jacobs, P.A., Mee, D.J., 2005. Compressible, Turbulent Flow with Boundary-Layer Heat Addition, in: 43rd AIAA Aerosp. Sci. Meet. Exhib., Reno, Nevada, 10.2514/6.2005-1097.
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献