摘要
迎风型TVD格式在高速进气道粘性流动模拟中的应用刘晶昌,徐建中(中国科学院工程热物理研究所北京100080)邢君波(航天部31所北京100080)关键词超音速进气道,数值模拟,Navier-Stokes方程1前言高速进气道流动做为一种非常复杂的流动,...
In this paper,two dimensional compressible Navier-Stokes equations are solved to simulate two kinds of supersonic inlets by an upwind TVD scheme.Numercal results show that the very complicated shocks in different supersonic inlets can be captured well.The scheme can be used to simulate internal flow.
出处
《工程热物理学报》
EI
CAS
CSCD
北大核心
1996年第4期442-445,共4页
Journal of Engineering Thermophysics