Gas-kinetic BGK scheme for hypersonic viscous flow

被引：0
|
作者：
Xu, Kun [1 ]
Mao, Meiliang [2 ]
机构：
[1] Hong Kong Univ Sci & Technol, Hong Kong, Hong Kong, Peoples R China
[2] China Aerodynam Res & Dev Ctr, Mianyang, Peoples R China
来源：
COMPUTATIONAL FLUID DYNAMICS 2004, PROCEEDINGS | 2006年
关键词：
D O I：
10.1007/3-540-31801-1_23
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
This paper is about the application of a gas-kinetic scheme based on the Bhatnagar-Gross-Krook (BGK) model for the Navier-Stokes equations in the study of hypersonic viscous flow. In the laminar hypersonic viscous flow computations, complicated flow phenomena, i.e., shock boundary layer interaction, flow separation, and viscous/inviscid interaction, will be encountered. The cases studied include the type IV shock-shock interaction around a circular cylinder and hypersonic flow passing through a double-cone geometry.
引用
收藏
页码：183 / +
页数：2
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