Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction 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(李新亮) | |
发表期刊 | SCIENCE CHINA: Physics, Mechanics & Astronomy |
2010 | |
卷号 | 53期号:9页码:1651-1658 |
ISSN | 1674-7348 |
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 | compression Ramp Shock/turbulent Boundary Layer Interaction Direct Numerical Simulation Shock Oscillation |
学科领域 | 计算流体力学 |
DOI | 10.1007/s11433-010-4034-x |
收录类别 | SCI ; EI ; CSCD |
语种 | 英语 |
WOS记录号 | WOS:000280810000012 |
引用统计 | |
文献类型 | 期刊论文 |
条目标识符 | http://dspace.imech.ac.cn/handle/311007/42444 |
专题 | 高温气体动力学国家重点实验室 非线性力学国家重点实验室 |
通讯作者 | Li XL(李新亮) |
推荐引用方式 GB/T 7714 | Li XL,Fu DX,Ma YW,et al. Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction in a Supersonic Compression Ramp[J]. SCIENCE CHINA: Physics, Mechanics & Astronomy,2010,53,9,:1651-1658. |
APA | Li XL,Fu DX,Ma YW,Liang X,&李新亮.(2010).Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction in a Supersonic Compression Ramp.SCIENCE CHINA: Physics, Mechanics & Astronomy,53(9),1651-1658. |
MLA | Li XL,et al."Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction in a Supersonic Compression Ramp".SCIENCE CHINA: Physics, Mechanics & Astronomy 53.9(2010):1651-1658. |
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