| Investigation of turbulence models with compressibility corrections for hypersonic boundary flows | |
| Tang, Han; Gao, Zhenxun | |
| 刊名 | ADVANCES IN MECHANICAL ENGINEERING
 |
| 2015 | |
| 卷号 | 7 |
| 关键词 | Turbulence models compressibility corrections hypersonic flat plate boundary layer compression corners shock wave boundary layer interaction |
| ISSN号 | 1687-8132 |
| DOI | 10.1177/1687814015620319 |
| URL标识 | 查看原文 |
| 收录类别 | SCIE |
| WOS记录号 | WOS:000367549200027 |
| 内容类型 | 期刊论文 |
| URI标识 | http://www.corc.org.cn/handle/1471x/6541480 |
| 专题 | 北京航空航天大学 |
| 推荐引用方式 GB/T 7714 | Tang, Han,Gao, Zhenxun. Investigation of turbulence models with compressibility corrections for hypersonic boundary flows[J]. ADVANCES IN MECHANICAL ENGINEERING,2015,7. |
| APA | Tang, Han,&Gao, Zhenxun.(2015).Investigation of turbulence models with compressibility corrections for hypersonic boundary flows.ADVANCES IN MECHANICAL ENGINEERING,7. |
| MLA | Tang, Han,et al."Investigation of turbulence models with compressibility corrections for hypersonic boundary flows".ADVANCES IN MECHANICAL ENGINEERING 7(2015). |
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