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

二维双楔外形穿越激波流场特性及其数值分析
引用本文:江娟,周伟江.二维双楔外形穿越激波流场特性及其数值分析[J].空气动力学学报,2002,20(3):260-266.
作者姓名:江娟  周伟江
作者单位:北京空气动力研究所,北京,100074
摘    要:用数值方法求解非定常可压缩Navier-Stokes方程,模拟了双楔外形物体超音速穿越与之同向运动激波以及逆向运动激波两种穿越激波的全过程,给出了穿越过程中流场与运动激波产生剧烈的干扰所形成的复杂波系结构,两种穿越情况的激波干扰都呈现双马赫反射的特征。在追击穿越中,楔形物体追上激波后所受阻力急剧的变小;而在碰撞穿越过程中,物体碰到激波后阻力急剧增加,两种穿越情况楔形物体的气动力都发生的剧烈的改变。

关 键 词:穿越激波  流场特性  非定常流  数值模拟  追击穿越  碰撞穿越  导弹
文章编号:0258-1825(2002)03-0260-07
修稿时间:2001年9月3日

Computational analysis of the unsteady flow induced by adouble-wedge shaped projectile overtaking shock waves
Jiang juan,Zhou Wei-jiang.Computational analysis of the unsteady flow induced by adouble-wedge shaped projectile overtaking shock waves[J].Acta Aerodynamica Sinica,2002,20(3):260-266.
Authors:Jiang juan  Zhou Wei-jiang
Abstract:Numerical simulations of the flow field around a double-wedge shaped p rojectile overtaking shocks are carried out by solving unsteady compressible Nav ier-Stokes equations. Two test cases, the pursuing overtaking and the colliding overtaking are considered, and discussed the complex structure of wave systems, which is induced by the interaction of the flow field and the moving shock wave. The double Mach reflection is observed in both cases. In the case of colliding overtaking, the drag, which is rapidly reduced in pursuing overtaking is greatly increases, after the projectile goes through the shock wave. The aerodynamic fo rces of the projectile show rapid variations.
Keywords:unsteady flow  numerical simulation  pursuing overtaking  colliding o vertaking  
本文献已被 CNKI 维普 万方数据 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