中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
DNS of shock/boundary layer interaction flow in a supersonic compression ramp

文献类型:会议论文

作者Li XL(李新亮); Fu DX(傅德薰); Ma YW(马延文); Liang X(梁贤)
出版日期2011
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
通讯作者邮箱lixl@imech.ac.cn; fudx@lnm.imech.ac.cn; fudx@lnm.imech.ac.cn; liangx@imech.ac.cn
关键词TURBULENT-BOUNDARY-LAYER DIRECT NUMERICAL-SIMULATION
页码729-737
通讯作者Li, XL (reprint author), CAS, Inst Mech, LHD, Beijing 100190, Peoples R China
中文摘要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.
收录类别CPCI
产权排序[Li, Xin-Liang; Fu, De-Xun; Ma, Yan-Wen; Liang, Xian] CAS, Inst Mech, LHD, Beijing 100190, Peoples R China
会议网址http://dx.doi.org/10.1007/978-3-642-17884-9_93
会议录COMPUTATIONAL FLUID DYNAMICS 2010
会议录出版者SPRINGER-VERLAG BERLIN
学科主题Mathematics ; Interdisciplinary Applications; Mechanics; Physics ; Fluids & Plasmas
会议录出版地HEIDELBERGER PLATZ 3, D-14197 BERLIN, GERMANY
语种英语
ISBN号978-3-642-17883-2
源URL[http://dspace.imech.ac.cn/handle/311007/46806]  
专题力学研究所_高温气体动力学国家重点实验室
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]. 见:6th International Conference on Computational Fluid Dynamics. St Petersburg, RUSSIA. JUL 12-16, 2010.http://dx.doi.org/10.1007/978-3-642-17884-9_93.

入库方式: OAI收割

来源:力学研究所

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