Computations of Inlet/Isolator for SCRAMjet Engine
文献类型：期刊论文
| 作者 | Wang Xiaodong; Le Jialing |
| 刊名 | JOURNAL OF THERMAL SCIENCE
 |
| 出版日期 | 2000 |
| 卷号 | 9期号:4页码:334，338 |
| 关键词 | Inlet Numerical Simulation Navier-stokes Equations Turbulence Model. |
| 英文摘要 | The inlet/isolator is one of the important parts to the SCRAMjet engine. In the present paper, the flow fields within an inlet and isolator of a SCRAMjet engine have been simulated by the Reynolds-Averaged Navier-Stokes equations with the Baldwin-Lomax algebraic turbulence model. The second order H. C. Yee TVD scheme is used for the inviscid flux terms and a central difference considering the character of flow is used for the diffusion terms. The code was used to simulate the flow field of three types of the inlet/isolator models. The results show that the configuration of the internal compression surface of the inlet and the divergent angle of the isolator have a great important effect on the characteristics of the inlet/isolator. |
| 公开日期 | 2013-03-12 |
| 源URL | [http://ir.etp.ac.cn/handle/311046/53860]  |
| 专题 | 工程热物理研究所_Journal of Thermal Science |
| 推荐引用方式 GB/T 7714 | Wang Xiaodong,Le Jialing. Computations of Inlet/Isolator for SCRAMjet Engine[J]. JOURNAL OF THERMAL SCIENCE,2000,9(4):334，338. |
| APA | Wang Xiaodong,&Le Jialing.(2000).Computations of Inlet/Isolator for SCRAMjet Engine.JOURNAL OF THERMAL SCIENCE,9(4),334，338. |
| MLA | Wang Xiaodong,et al."Computations of Inlet/Isolator for SCRAMjet Engine".JOURNAL OF THERMAL SCIENCE 9.4(2000):334，338. |
入库方式： OAI收割
来源：工程热物理研究所
浏览0
下载0
收藏0
其他版本
除非特别说明，本系统中所有内容都受版权保护，并保留所有权利。