Analysis on capabilities of density-based solvers within OpenFOAM to distinguish aerothermal variables in diffusion boundary layer

机标关键词：experimental data、computational fluid dynamics、diffusion boundary layer、open source、numerical results、compressible flow、Splitting Method、shock wave、heat flux

分类号：O6 ;O29

资助基金：This study was supported by the National Natural Science Foundation of China Grant .51176038,51121004

在线出版日期：2014-01-09（万方平台首次上网日期，不代表论文的发表时间）

页数：共10页

页码：1370-1379