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统一分区加强解算法解物体穿越激波非定常流场
引用本文:江娟,周伟江,马汉东. 统一分区加强解算法解物体穿越激波非定常流场[J]. 宇航学报, 2003, 24(4): 384-388
作者姓名:江娟  周伟江  马汉东
作者单位:北京空气动力研究所,北京,100074
基金项目:国防科技预研基金 (项目编号 :0 0 J13 .2 .1HT710 2 )
摘    要:使用统一分区加强解算法求解非定常可压缩Navier-Stokes方程,模拟了物体分别以超音速和亚声速穿越与之同向运动激波的全过程,并且通过和单区计算结果的详细对比,说明统一分区加强解算法能够简便、有效的处理复杂几何外形和提高网格分辨率。

关 键 词:统一分区加强解算法 数值模拟 超声速穿越 亚声速穿越
文章编号:1000-1328(2003)04-0384-05
修稿时间:2002-10-25

The unified zonal fortified solution of the unsteady flows induced by a body overtaking a shock wave
JIANG Juan,ZHOU Wei jiang,MA Han dong. The unified zonal fortified solution of the unsteady flows induced by a body overtaking a shock wave[J]. Journal of Astronautics, 2003, 24(4): 384-388
Authors:JIANG Juan  ZHOU Wei jiang  MA Han dong
Abstract:Numerical simulations of the flow fields around a body overtaking a shock wave are carried out with the two dimensional unsteady compressible Navier Stokes equations.A domain decomposition method and the FSA(Fortified Solution Algorithm) are employed to reach sufficient grid resolution.Two test cases,the supersonic overtaking and the subsonic overtaking are considered.By the contrast with the results obtained by original method,the FSA is a good tool which can handle the complicated configuration and improve the grid resolution simply and usefully.
Keywords:FSA  Numerical simulation  Supersonic overtaking  Subsonic overtaking
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