Knowledge Management System of Institue of Mechanics, CAS
| Research on three-dimensional scramiet inlet | |
Yue LJ(岳连捷) ; Chen LH(陈立红); Xiao YB; Gong P; Chang XY(张新宇)
| |
| Source Publication | A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference |
| 2006 | |
| Conference Name | 14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference |
| Conference Date | November 6, 2006 - November 9, 2006 |
| Conference Place | Canberra, Australia |
| Abstract | The three-dimensional compression scramjet inlet has been investigated by using surface oil dot visualization and numerical simulation. The research has revealed the details of the internal flow pattern, which included the structure of the shock waves, the spillage, the spatial vortical structures, and the boundary layer separations etc.. These features determined the performance of the inlet, which gave the mass flow capture ratio of 0.86, total pressure recovery of 0.41. The results showed that the arrangement of the shocks is critical for such kind of inlet. More researches have been carried out to investigate the effect of the cowl shape, and the results showed the flow field would be changed little for the cowls with different shapes but the same internal contraction ratios. |
| Keyword | Capture Ratio Mass Flow Surface Oil Dot Visualization Three-dimensional Scramjet Inlet |
| ISBN | 1563478269 |
| Indexed By | EI |
| Language | 英语 |
| Document Type | 会议论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/60292 |
| Collection | 力学所知识产出(1956-2008) |
| Recommended Citation GB/T 7714 | Yue LJ,Chen LH,Xiao YB,et al. Research on three-dimensional scramiet inlet[C]A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference,2006. |
| Files in This Item: | Download All | |||||
| File Name/Size | DocType | Version | Access | License | ||
| CaEi055.pdf（1267KB） | 会议论文 | 开放获取 | CC BY-NC-SA | View Download | ||
Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.
Edit Comment