IMECH-IR  > 力学所知识产出(1956-2008)
Research on three-dimensional scramjet inlet
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)
2007
Conference Name14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006
Conference Date20-23 April 2006
Conference PlaceBeijing, China
AbstractThe 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.
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Language英语
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/55315
Collection力学所知识产出(1956-2008)
Recommended Citation
GB/T 7714
Yue LJ,Xiao YB,Chen LH,et al. Research on three-dimensional scramjet inlet[C],2007.
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