A study of the flow structure and transition for typical shock reflection in the design of the scramjet engine

摘要：

Researching the structure of the shock-train signify much in the design of the scramjet engine. The shocktrain is composed of regular shock reflection and Mach shock reflection. In this paper, we study the wave structures and wave interactions of Mach reflection in two dimensional flows. The fine structure of the transition from regular to Mach reflection due to the influence of an upstream disturbance is also studied.

关键词： shock Mach reflection transition

作者: B.Gao L.Zhu Y.Y.Wu X.J.Yang P.Jiang

作者单位: China Academy of Launch Vehicle Technology Systems Engineer Division, Beijing, P.R. China, 100076

会议类型: 国际会议

会议名称: The 8th Sino-Russia High-speed Flow Conference(第八届中俄高超声速流体力学研讨会)

会议地点: 上海

会议语种:英文

页码: 235-242

在线出版日期: 2011-11-21（万方平台首次上网日期，不代表论文的发表时间）