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DNS of shock/boundary layer interaction flow in a supersonic compression ramp
Li XL(李新亮); Fu DX(傅德薰); Ma YW(马延文); Liang X(梁贤); Li, XL (reprint author), CAS, Inst Mech, LHD, Beijing 100190, Peoples R China
会议录名称COMPUTATIONAL FLUID DYNAMICS 2010
2011
页码729-737
会议名称6th International Conference on Computational Fluid Dynamics
会议日期JUL 12-16, 2010
会议地点St Petersburg, RUSSIA
摘要A direct numerical simulation of the shock/turbulent boundary layer interaction flow in a supersonic 24-degree compression ramp is conducted with the free stream Mach number 2.9. The blow-and-suction disturbance in the upstream wall boundary is used to trigger the transition. Both the mean wall pressure and the velocity profiles agree with those of the experimental data, which validates the simulation. The turbulent kinetic energy budget in the separation region is analyzed. Results show that the turbulent production term increases fast in the separation region, while the turbulent dissipation term reaches its peak in the near-wall region. The turbulent transport term contributes to the balance of the turbulent conduction and turbulent dissipation. Based on the analysis of instantaneous pressure in the downstream region of the mean shock and that in the separation bubble, the authors suggest that the low frequency oscillation of the shock is not caused by the upstream turbulent disturbance, but rather the instability of separation bubble.
关键词Turbulent-boundary-layer Direct Numerical-simulation
课题组名称LHD可压缩湍流
ISBN号978-3-642-17883-2
URL查看原文
收录类别CPCI
语种英语
文献类型会议论文
条目标识符http://dspace.imech.ac.cn/handle/311007/46806
专题高温气体动力学国家重点实验室
通讯作者Li, XL (reprint author), CAS, Inst Mech, LHD, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Li XL,Fu DX,Ma YW,et al. DNS of shock/boundary layer interaction flow in a supersonic compression ramp[C]COMPUTATIONAL FLUID DYNAMICS 2010,2011:729-737.
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