| Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction |
| Zhu XK; Yu ZP(于长平) ; Tong FL; Li XL(李新亮); Li, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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| 发表期刊 | AIAA JOURNAL
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| 2017
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| 卷号 | 55期号:1页码:131-140 |
| ISSN | 0001-1452
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| 摘要 | The effect of wall temperature on the size of the separation bubble in the shock wave/turbulent boundary-layer interaction of a 24 deg compression ramp with Mach 2.9 is numerically investigated. The ratios of wall temperature to recovery temperature T-w/T-r are 0.6, 1.14, 1.4, and 2.0, respectively. To validate the simulation, the statistical results with T-w/T-r = 1.14 are tested and the results show a good agreement with theoretical and experimental results. It is shown that wall temperature has a remarkable effect on the size of the separation bubble and the size increases significantly with the increase of wall temperature. Through theoretical analysis, combined with numerical results, we get a semitheoretical formula L/delta alpha (T-w/T-r )(0.85), in which L and delta are the length of the separation bubble and the thickness of upstream boundary layer, respectively. The turbulent kinetic energy budgets are also analyzed based on the numerical data, and results show that turbulence kinetic energy is chiefly produced both in the buffer layer and near the shock wave, and turbulent dissipation is mainly in the center of the separation bubble as well as in the near-wall region. It is also shown that the intrinsic compressibility effect is not significant in all these cases. |
| DOI | 10.2514/1.J054939
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| URL | 查看原文
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| 收录类别 | SCI
; EI
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| 语种 | 英语
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| WOS记录号 | WOS:000392511000012
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| WOS研究方向 | Engineering
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| WOS类目 | Engineering, Aerospace
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| 项目资助者 | This work was supported by the National Science Foundation of China (91441103, 1372330, 11472279) and National key Research and Development program (2016YFA0401200). The authors thank the National Supercomputer Center in Tianjin, Supercomputing Center of Chinese Academy of Sciences, and Shandong Supercomputing Center for providing computer time. Thanks to Dexun Fu and Yanwen Ma, from the Institute of Mechanics, Chinese Academy of Sciences, for their suggestions. Thanks to the referees for their valuable suggestions and comments
; it is also very helpful to our research.
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| 课题组名称 | LHD可压缩湍流
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| 论文分区 | 一类/力学重要期刊
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| 力学所作者排名 | 1
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| 引用统计 |
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| 文献类型 | 期刊论文
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| 条目标识符 | http://dspace.imech.ac.cn/handle/311007/60109
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| 专题 | 高温气体动力学国家重点实验室
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| 通讯作者 | Li, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China. |
推荐引用方式
GB/T 7714 |
Zhu XK,Yu ZP,Tong FL,et al. Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction[J]. AIAA JOURNAL,2017,55,1,:131-140.
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| APA |
Zhu XK,于长平,Tong FL,李新亮,&Li, XL .(2017).Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction.AIAA JOURNAL,55(1),131-140.
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| MLA |
Zhu XK,et al."Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction".AIAA JOURNAL 55.1(2017):131-140.
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