Research on three-dimensional scramjet inlet
文献类型：会议论文
| 作者 | Yue LJ(岳连捷) ; Xiao YB(肖雅彬); Chen LH(陈立红); Xiang AY(向安宇); Zhang XY(张新宇)
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| 出版日期 | 2007 |
| 会议名称 | 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006 |
| 会议日期 | 20-23 April 2006 |
| 会议地点 | Beijing, China |
| 中文摘要 | The numerical simulation was conducted to investigate three-dimensional sidewall compression scramjet inlet flow fields. The research also looked into the effects of cowl positions and strut thickness. It is noted that flow separation occurs at the sidewall shock impingement location. Forward cowl results in the growth of the separation region, ultimately inlet unstart for 75mm cowl position. The glancing shock also separates the baseplate boundary layer. The flow is entrained toward the centerline, which is attributed to a low total pressure region in the inlet exit plane. In addition, an increase in the mass capture is obtained as the decrease in the strut thickness, while the total pressure recovery undergoes a process from reducing to increasing, which is attributed to the compromise between shrinking separation and the lengthening inlet. |
| 会议网址 | http://dx.doi.org/10.2514/6.2006-8141 |
| 语种 | 英语 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/55315]  |
| 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,Xiao YB,Chen LH,et al. Research on three-dimensional scramjet inlet[C]. 见:14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006. Beijing, China. 20-23 April 2006.http://dx.doi.org/10.2514/6.2006-8141. |
入库方式： OAI收割
来源：力学研究所
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