Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel

	Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel
	Wang YP(汪运鹏); Hu ZM(胡宗民); Liu YF(刘云峰); Jiang ZL(姜宗林)
会议录名称	22nd AIAA Computational Fluid Dynamics Conference
	2015
会议名称	22nd AIAA Computational Fluid Dynamics Conference, 2015
会议日期	June 22, 2015 - June 26, 2015
会议地点	Dallas, TX, United states
摘要	The starting process of the flow in an expansion nozzle (nominal Mach number 6) with the outlet diameter of 1.5m and the 8.9m length, which is used for a large-scale hypersonic shock tunnel in LHD, was simulated and analyzed at incident Mach number Ms= 3.9. The calculating domains include the driven section (the shock tube end, about 4.8 m length), the nozzle with about 8.9 m length, and the part of test section (more than 3 m). The characteristics of unsteady nozzle flow, including the shock wave patterns in the nozzle inlet region and inside the nozzle, were analyzed numerically in the viscous and inviscid flow regimes, respectively. The pressure and Mach number results were presented and discussed by comparing to the experimental findings, where the simulated results of the reflected shock wave in the shock tube and the transmitted shock wave inside the nozzle, are found to agree well with the test data. Additionally, the case without a contraction section for the throat configuration was also calculated and compared with the case with ones. The effect of the starting flow in these two cases on the flowfield uniformity was discussed in detail in this paper. © 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
关键词	Inviscid Flows Numerical Investigations Outlet Diameters Reflected Shock Waves Simulated Results Starting Process Transmitted Shock Unsteady Nozzle Flow
课题组名称	LHD激波与爆轰物理
ISBN号	9781624103667
收录类别	EI
语种	英语
文献类型	会议论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/60160
专题	高温气体动力学国家重点实验室
推荐引用方式 GB/T 7714	Wang YP,Hu ZM,Liu YF,et al. Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel[C]22nd AIAA Computational Fluid Dynamics Conference,2015.

条目包含的文件		下载所有文件
文件名称/大小	文献类型	版本类型	开放类型	使用许可
Cp2016-045.pdf（5104KB）	会议论文		开放获取	CC BY-NC-SA	浏览下载