首页 | 本学科首页   官方微博 | 高级检索  
     检索      

二元超音速进气道唇口分离流动及其控制
引用本文:何中伟 ,李君山 ,陈金冲.二元超音速进气道唇口分离流动及其控制[J].南京航空航天大学学报,1986(3).
作者姓名:何中伟  李君山  陈金冲
摘    要:本文着重研究了二元超音速进气道几种唇口内侧壁面分离流动控制结构,对进气口流场、几何喉道下游邻近截面的流场及其壁面附面层参数、进气道出口流场和性能的影响。并对唇口分离流吹除和吸除之后,进气口再附着点下游截面上的总压脉动压力均方根值分布及功率谱密度-频率特性进行了比较。

关 键 词:超音速进气道  流场  分离流动  控制问题

Lip Separate Flow and Its Control of the Two-Dimensional Supersonic Inlet
He Zhongwei Li Junshan Chen Jinchong.Lip Separate Flow and Its Control of the Two-Dimensional Supersonic Inlet[J].Journal of Nanjing University of Aeronautics & Astronautics,1986(3).
Authors:He Zhongwei Li Junshan Chen Jinchong
Institution:He Zhongwei Li Junshan Chen Jinchong
Abstract:The effects of lip separate flow and its control on the flow at the entrance of the inlet and the flow field in the section downstream of the geometrical throat of the inlet,and on its wall boundary layer parameters and flow field and inlet characteristics at the exit are mainly investigated.Comparisons of the R.M.S.distribution of the total pressure fluctuation and its power spectrum density downstream of the lip separation reattachment point with and without lip separation blowing and suction are also made in this paper.
Keywords:supersonic inlets  flow fields  separated flow  control problems
本文献已被 CNKI 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号