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
Issue11Pages:1379-1382
ISSN2000-6890
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 ByCSCD
Language中文
CSCD IDCSCD:239224
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Document Type期刊论文
Identifierhttp://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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