IMECH-IR  > 高温气体动力学国家重点实验室
热流密度峰值最小化的鼻锥钝化设计
屈志朋; 崔凯; 胡守超; 李广利
Source Publication高温气体动力学研究进展
2012
Pages204-207
Conference NameLHD2012夏季学术研讨会
Conference Date2012
Conference Place吉林延吉
Abstract针对旋成体高超声速飞行器,采用一种新的钝化外形。基于CFD 数值模拟分析,完成了新钝化外形和圆锥钝化在气动力方面性能的比较。对三种不同钝化半径/旋成体最大半径(r/R)比1/40、1/20、1/10 比较分析,结果表明,在相同的钝化半径下,钝锥部分阻力系数增加,但对整个旋成体导弹而言,在超过一定的钝化半径或高度时其总阻力才变化较大。
Keyword旋成体 高超声速 钝化半径 阻力
DepartmentLHD气动布局优化与计算方法
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/48001
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
屈志朋,崔凯,胡守超,等. 热流密度峰值最小化的鼻锥钝化设计[C]高温气体动力学研究进展,2012:204-207.
Files in This Item: Download All
File Name/Size DocType Version Access License
LhdCA2012-204.pdf(839KB) 开放获取--View Download
Related Services
Recommend this item
Bookmark
Usage statistics
Export to Endnote
Google Scholar
Similar articles in Google Scholar
[屈志朋]'s Articles
[崔凯]'s Articles
[胡守超]'s Articles
Baidu academic
Similar articles in Baidu academic
[屈志朋]'s Articles
[崔凯]'s Articles
[胡守超]'s Articles
Bing Scholar
Similar articles in Bing Scholar
[屈志朋]'s Articles
[崔凯]'s Articles
[胡守超]'s Articles
Terms of Use
No data!
Social Bookmark/Share
File name: LhdCA2012-204.pdf
Format: Adobe PDF
This file does not support browsing at this time
All comments (0)
No comment.
 

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