COMPUTATION OF TRANSONIC AIRFOIL FLOW WITH THE SHOCK BOUNDARY LAYER INTERACTION ADAPTIVELY CONTROLLED

IMECH-IR > 力学所知识产出(1956-2008)

	COMPUTATION OF TRANSONIC AIRFOIL FLOW WITH THE SHOCK BOUNDARY LAYER INTERACTION ADAPTIVELY CONTROLLED
	Ma X(马侠); Jiang JG(蒋金贵); Zhang MC(张绵纯); Xiao LK(肖林奎)
Source Publication	SOME NEW TRENDS ON FLUID MECHANICS AND THEORETICAL PHYSICS
	1993
Conference Name	International Conference on Fluid Mechanics and Theoretical Physics, in Honor of Professor Pei-Yuan Chous 90th Anniversary
Conference Date	JUN 01-03, 1992
Conference Place	BEIJING, PEOPLES R CHINA
WOS ID	WOS:A1993BD18F00047
ISBN	7-301-02070-8
Indexed By	CPCI-S
Language	英语
Citation statistics
Document Type	会议论文
Identifier	http://dspace.imech.ac.cn/handle/311007/59044
Collection	力学所知识产出(1956-2008)
Recommended Citation GB/T 7714	Ma X,Jiang JG,Zhang MC,et al. COMPUTATION OF TRANSONIC AIRFOIL FLOW WITH THE SHOCK BOUNDARY LAYER INTERACTION ADAPTIVELY CONTROLLED[C]SOME NEW TRENDS ON FLUID MECHANICS AND THEORETICAL PHYSICS,1993.

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