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)
Source PublicationActa Mechanica Sinica
1992
Volume8Issue:3Pages:224-230
ISSN0567-7718
AbstractDetailed 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...
KeywordShock Wave Boundary Layer Aerodynamic Heating
Language英语
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/55245
Collection力学所知识产出(1956-2008)
Recommended Citation
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.
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