[1]陈 雄,鞠玉涛,朱福亚.冲压增程弹用进气道试验与数值研究[J].南京理工大学学报(自然科学版),2007,(04):462-465.
　CHEN Xiong,JU Yu-tao,ZHU Fu-ya.Experimental and Numerical Research on Inlet of Ramjet Assisted Range Projectiles[J].Journal of Nanjing University of Science and Technology,2007,(04):462-465.
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冲压增程弹用进气道试验与数值研究
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《南京理工大学学报》（自然科学版）[ISSN:1005-9830/CN:32-1397/N]

卷:
期数:
2007年04期
页码:
462-465
栏目:
出版日期:
2007-08-30

文章信息/Info

Title:
Experimental and Numerical Research on Inlet of Ramjet Assisted Range Projectiles
作者:
陈 雄;  鞠玉涛;  朱福亚
南京理工大学机械工程学院, 江苏南京210094
Author(s):
CHEN Xiong; JU Yu-tao; ZHU Fu-ya
School of Mechanical Engineering,NUST,Nanjing 210094,China
关键词:
进气道;  风洞试验;  分区算法;  TVD格式;  冲压发动机;  弹丸
Keywords:
in le; t w ind tunnel experimen; t zona lmethod;  TVD schem e;  ram je; t pro ject iles
分类号:
TJ413
摘要:
对某冲压增程弹用超声速双锥进气道流场特性进行研究,在风洞试验中得到合理的流场结构图谱及试验数据。采用块结构网格与二阶精度流场分区求解技术,对该超声速进气道内外流场进行数值研究。通过数值模拟得到了对应于不同出口反压和攻角情况下,超声速进气道内外粘性流场复杂的波系结构,分析了进气道内外流场的形成过程。结果表明:数值模拟得到的流场结构波系图与风洞试验纹影图一致,并且进气道扩压段静压分布以及进气道出口位置的总压分布与试验结果基本一致。
Abstract:
Flow characteristic of superson ic b-i cone inlet o f ram jet assisted range projectiles is studied, and reasonab le flow structures are also achieved through thew ind tunne l experim en.t App lying b lock structure grid and second-order zonal so lver method, the numerica l research on this inlet is presented. Complex w ave structures o f superson ic in le t at different backflow pressure and ang le o f attack are ach ieved by num er ical simu lation. The develop ing prog ress o f in ternal and external flow structure o f inlet is analyzed. R esu lts show that it is a lmost co inc ident o f numerica l flow structure w ith w ind tunne l experimental structure, and the d istribu tion o f static pressure at divergent sect ion o f in let and total pressure at ex it of inlet is also co incident compared w ith exper imenta l results.

参考文献/References:

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[ 3] M icha l T, Ose rM. Im prov ing zonal coupling accuracy and robustness in the w ind code [ R ]. A IAA Paper 2001- 0222, 2001.
[ 4] 陈让福. 三维高超声速无粘定常绕流的数值模拟 [ D]. 北京: 北京大学数学系, 1991.
[ 5] 陈雄. 高速旋转固体火箭冲压发动机进气道工作 过程特性研究[ D]. 南京: 南京理工大学机械工程 学院, 2005.
[ 6] 陈雄, 周长省, 郑亚. 应用TTM 网格研究冲压增程 弹丸进气道内外流场[ J]. 固体火箭技术, 2004, 27( 4): 243- 246.
[ 7] D ionisio F, Stockenstrm A. Aerodynam ic w ind- tunne l test of a ram jet projectile [ A ] . 19 th Internationa l Symposium o f Ballistics [ C ]. Interlaken, Sw itze rland: [ s. n. ], 2001. 529- 536.

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备注/Memo

备注/Memo:
作者简介: 陈雄( 1977- ), 男, 讲师, 博士, 主要研究方向: 计算流体力学及新型推进技术的研究, E-m a il: chenxiongsc@ 163. com。
更新日期/Last Update: 2007-08-30