Research on three-dimensional scramiet inlet
文献类型：会议论文
| 作者 | Yue LJ(岳连捷) ; Chen LH(陈立红); Xiao YB; Gong P; Chang XY(张新宇)
|
| 出版日期 | 2006 |
| 会议名称 | 14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference |
| 会议日期 | November 6, 2006 - November 9, 2006 |
| 会议地点 | Canberra, Australia |
| 关键词 | Capture ratio Mass flow Surface oil dot visualization Three-dimensional scramjet inlet |
| 中文摘要 | 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. |
| 收录类别 | EI |
| 会议录 | A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference
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| 语种 | 英语 |
| ISBN号 | 1563478269 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/60292]  |
| 专题 | 力学研究所_力学所知识产出(1956-2008) |
| 推荐引用方式 GB/T 7714 | Yue LJ,Chen LH,Xiao YB,et al. Research on three-dimensional scramiet inlet[C]. 见:14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference. Canberra, Australia. November 6, 2006 - November 9, 2006. |
入库方式： OAI收割
来源：力学研究所
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