Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a M _∞ = 9 hypersonic flow

Hu Z.M.; Myong R.S.; Yang Y.R.; Cho T.H.

首页> 外文期刊>Theoretical and Computational Fluid Dynamics >Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a M _∞ = 9 hypersonic flow

【24h】

Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a M _∞ = 9 hypersonic flow

机译：对M_∞= 9高超音速流中双楔形几何结构上无粘性冲击相互作用和过渡现象的重新考虑

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

Shock polar analysis as well as 2-D numerical computation technique are used to illustrate a diverse flow topology induced by shock/shock interaction in a M _∞ = 9 hypersonic flow. New flow features associated with inviscid shock wave interaction on double-wedge-like geometries are reported in this study. Transition of shock interaction, unsteady oscillation, and hysteresis phenomena in the RR → MR transition, and the physical mechanisms behind these phenomena are numerically studied and analyzed.

机译：激波极性分析和二维数值计算技术用于说明M_∞= 9高超声速流中激波/激波相互作用引起的多种流动拓扑。在这项研究中报告了与双楔形几何形状上无粘性冲击波相互作用相关的新流动特征。对RR→MR跃迁中的冲击相互作用，非稳态振荡和磁滞现象的转变以及这些现象背后的物理机制进行了数值研究和分析。

著录项

来源
《Theoretical and Computational Fluid Dynamics》 |2010年第6期|共14页
作者
Hu Z.M.; Myong R.S.; Yang Y.R.; Cho T.H.;
展开▼
作者单位

展开▼
收录信息
原文格式 PDF
正文语种 eng
中图分类流体力学;
关键词
Double wedge; Hypersonic; Hysteresis; Oscillation; Shock/shock interaction;

机译：双楔形;超人格;迟滞;振动;冲击/冲击相互作用;

相似文献

外文文献
中文文献
专利

1. Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a M _∞ = 9 hypersonic flow [J] . Hu Z.M., Myong R.S., Yang Y.R., Theoretical and Computational Fluid Dynamics . 2010,第6期

机译：对M_∞= 9高超音速流中双楔形几何结构上无粘性冲击相互作用和过渡现象的重新考虑
2. RR-MR transition of a Type V shock interaction in inviscid double-wedge flow with high-temperature gas effects [J] . Xiong W., Li J., Zhu Y., Shock Waves . 2018,第4期

机译：RR-MR转换型V型冲击相互作用，具有高温气体效应
3. NUMERICAL STUDY OF INVISCID SHOCK INTERACTIONS ON DOUBLE-WEDGE GEOMETRIES [J] . Olejniczak J., Candler GV., Wright MJ. Journal of Fluid Mechanics . 1997,第0期

机译：双楔形几何上无粘性激波相互作用的数值研究
4. Computational Studies of Shock Wave Boundary Layer Interactions in Hypersonic Flow Over Double Cone Geometries [C] . Siva Vayala, Ravi K. Peetala International Conference on Applied Mechanical Engineering Research . 2020

机译：双锥形几何上超声波冲击波边界层相互作用的计算研究
5. Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows. [D] . Singh, Dal Jeet. 1989

机译：鼻子过钝和电击-相互作用对粘性高超声速流动中钝体的影响。
6. DSMC Simulation and Experimental Validation of Shock Interaction in Hypersonic Low Density Flow [O] . Hong Xiao, Yuhe Shang, Di Wu -1

机译：高超声速低密度流中冲击相互作用的DSMC模拟和实验验证
7. Laminar/transitional shock-wave/boundary-layer interactions (SWBLIs) in hypersonic flows [O] . Bura Romie Oktovianus 2004

机译：高超声速流中的层流/过渡冲击波/边界层相互作用（sWBLI）
8. Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows [R] . Singh, D. J., Tiwari, S. N. 1990

机译：粘性高超声速流动中钝头和冲击 - 冲击相互作用对钝体的影响

Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a M _∞ = 9 hypersonic flow

摘要

著录项

相似文献

相关主题

期刊订阅