摘要
采用混合网格 ,利用DLR所发展的计算软件TAU对X 38高超声速粘性绕流进行了数值计算。网格自适应技术被用来生成有效的计算网格及提高对流场细节的分辨率。
The DLR code TAU is applied to the hypersonic viscous flow computation for X 38, with the hybrid grids produced by CENTAUR. An adaptation method is used in this work in order to produce efficient grids and to get accurate results. The present results agree well with the wind tunnel data and structured results obtained by another DLR code.
出处
《空气动力学学报》
CSCD
北大核心
2002年第1期96-101,共6页
Acta Aerodynamica Sinica