二维超音速激波风洞及其应用

IMECH-IR > 力学所知识产出(1956-2008)

	二维超音速激波风洞及其应用
	王世芬; 王宇; 唐贵明; 李振华; 刘鹏
Source Publication	航空学报
	1994-11-15
Issue	11 Pages:1379-1382
ISSN	2000-6890
Abstract	简述了二维超音速激波风洞的设计要点和性能;并给出在该风洞中低凸台诱导激波和湍流边界层相互作用的实验结果。实践表明：在被驱动段和喷管之间安装一个前缘光滑的矩形剖面短管道；并将二维喷管精加工成型;就能获得实验所需的均匀超音速气流。
Keyword	激波风洞激波干扰分离流压力测量热流
Indexed By	CSCD
Language	中文
CSCD ID	CSCD:239224
Citation statistics
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/72281
Collection	力学所知识产出(1956-2008)
Recommended Citation GB/T 7714	王世芬,王宇,唐贵明,等. 二维超音速激波风洞及其应用[J]. 航空学报,1994,11,:1379-1382.
APA	王世芬,王宇,唐贵明,李振华,&刘鹏.(1994).二维超音速激波风洞及其应用.航空学报(11),1379-1382.
MLA	王世芬,et al."二维超音速激波风洞及其应用".航空学报 .11(1994):1379-1382.

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