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高超声速电离绕流的数值模拟
引用本文:高铁锁,李椿萱,董维中,张巧芸.高超声速电离绕流的数值模拟[J].空气动力学学报,2002,20(2):184-191.
作者姓名:高铁锁  李椿萱  董维中  张巧芸
作者单位:1. 北京航空航天大学,北京,100083
2. 中国空气动力研究与发展中心,四川绵阳,621000
摘    要:本文从三维N-S方程出发,采用稳式L-U分解算法和7组分15个反应的化学模型,数值模拟高超声速电离空气绕流。首先采用对称TVD格式、AUSMPW+格式和Van Leer的矢通量分裂格式计算了高超声速球头绕流,并对它们的计算结果做了对比分析。然后用前两种格式,对RAM-C飞行试验模型三个再入高度(81km、71km、61km)的流场进行了数值模拟,计算的流场电子数密度值和试验测量数据符合较好。

关 键 词:高超声速电离绕流  数值模拟  化学非平衡流动  电子数密度  高超声速飞行器
文章编号:0258-1825(2002)02-0184-08
修稿时间:2001年8月5日

Numerical simulation of hypersonic ionized flows
GAO Tie suo ,LI Chun xuan ,DONG Wei zhong ,ZHANG Qiao yun.Numerical simulation of hypersonic ionized flows[J].Acta Aerodynamica Sinica,2002,20(2):184-191.
Authors:GAO Tie suo  LI Chun xuan  DONG Wei zhong  ZHANG Qiao yun
Institution:GAO Tie suo 1,LI Chun xuan 1,DONG Wei zhong 2,ZHANG Qiao yun 2
Abstract:In this paper, The algorithm of implicit Lower Upper decomposition and chemical model of 7 species 15 reactions are adopted to simulate numerically hypersonic ionized air flow, based on three dimensional Navier Stokes equations.First, symmetric TVD scheme, AUSMPW+ scheme and Van Leer's flux vector splitting scheme are used to calculate the hypersonic flow over a hemi sphere and the computational results corresponding to the three scheme are compared and analyzed. Then the flows over the model for RAM C flight test at three altitudes (81km, 71km and 61km) are numerically simulated with the symmetric TVD and AUSMPW+ scheme, the computed electron number densities in the flowfield compare well with the experimental data.
Keywords:chemical nonequilibrium flows  electron number density  numerical schemes
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