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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