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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
ISSN1674-7348
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
DOI10.1007/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
被引频次:52[WOS]   [WOS记录]     [WOS相关记录]
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)
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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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