AERODYNAMIC HEATING IN THE REGION OF SHOCK AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY A CYLINDER

IMECH-IR > 力学所知识产出(1956-2008)

	AERODYNAMIC HEATING IN THE REGION OF SHOCK AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY A CYLINDER
	Tang GM(唐贵明); Yu HR(俞鸿儒)
发表期刊	Acta Mechanica Sinica
	1992
卷号	8 期号:3 页码:224-230
ISSN	0567-7718
摘要	Detailed distributions of heat flux in the region of shock wave and turbulent boundary layerinteraction induced by a cylinder were measured in the shock tunnel Oil flow patterns and Schlieren photo-graphs were taken.Empirical relations were given for determining separation shock angle,peaks of h...
关键词	Shock Wave Boundary Layer Aerodynamic Heating
语种	英语
文献类型	期刊论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/55245
专题	力学所知识产出(1956-2008)
推荐引用方式 GB/T 7714	Tang GM,Yu HR. AERODYNAMIC HEATING IN THE REGION OF SHOCK AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY A CYLINDER[J]. Acta Mechanica Sinica,1992,8,3,:224-230.
APA	唐贵明,&俞鸿儒.(1992).AERODYNAMIC HEATING IN THE REGION OF SHOCK AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY A CYLINDER.Acta Mechanica Sinica,8(3),224-230.
MLA	唐贵明,et al."AERODYNAMIC HEATING IN THE REGION OF SHOCK AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY A CYLINDER".Acta Mechanica Sinica 8.3(1992):224-230.