IMECH-IR  > 高温气体动力学国家重点实验室
局部收缩比处处一致的变截面高超声速内转式进气道设计方法
肖雅彬; 岳连捷; 高占彪; 陈立红; 张新宇
Source Publication高温气体动力学研究进展
2012
Pages208-217
Conference NameLHD2012夏季学术研讨会
Conference Date2012
Conference Place吉林延吉
Abstract超声速流场在变截面的过程中以及出口流动尽量均匀,将三维流场分解成若有限根流管,所有流管的收缩比相等,对这些流管分别进行设计,再将他们重新组合起来。应用该方法设计了收缩比为3.67的高超声速进气道,设计点来流马赫数5.4,雷诺数4.885e6 时的捕获率达到0.995,隔离段出口的压比为11.73,总压恢复为0.520; 来流马赫数3.5,雷诺数1.297e7 时的捕获率达到0.952,隔离段出口的压比为12.26,总压恢复为0.684。进气道表现出良好的设计点和亚设计点性能已经较好的流动均匀性。
DepartmentLHD高超声速推进技术
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/48002
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
肖雅彬,岳连捷,高占彪,等. 局部收缩比处处一致的变截面高超声速内转式进气道设计方法[C]高温气体动力学研究进展,2012:208-217.
Files in This Item: Download All
File Name/Size DocType Version Access License
LhdCA2012-208.pdf(2046KB) 开放获取--View Download
Related Services
Recommend this item
Bookmark
Usage statistics
Export to Endnote
Google Scholar
Similar articles in Google Scholar
[肖雅彬]'s Articles
[岳连捷]'s Articles
[高占彪]'s Articles
Baidu academic
Similar articles in Baidu academic
[肖雅彬]'s Articles
[岳连捷]'s Articles
[高占彪]'s Articles
Bing Scholar
Similar articles in Bing Scholar
[肖雅彬]'s Articles
[岳连捷]'s Articles
[高占彪]'s Articles
Terms of Use
No data!
Social Bookmark/Share
File name: LhdCA2012-208.pdf
Format: Adobe PDF
This file does not support browsing at this time
 

Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.