Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows
文献类型:期刊论文
作者 | Hu ZM(胡宗民)2![]() ![]() ![]() |
刊名 | SHOCK WAVES
![]() |
出版日期 | 2008-06-01 |
卷号 | 18期号:1页码:41-51 |
关键词 | Shock Shock Interaction Oscillation Hypersonic Double-wedge Numerical Study |
ISSN号 | 0938-1287 |
DOI | 10.1007/s00193-008-0138-x |
英文摘要 | In this paper, the shock pattern oscillations induced by shock/shock interactions over double-wedge geometries in hypersonic flows were studied numerically by solving 2D inviscid Euler equations for a multi-species system. Laminar viscous effects were considered in some cases. Temperature-dependent thermodynamic properties were employed in the state and energy equations for consideration of the distinct change of the thermodynamic state. It was shown that the oscillation results in high-frequency fluctuations of heating and pressure loads over wedge surfaces. In a case with a relatively lower free-stream Mach number, the shock/shock interaction structure maintains a seven-shock configuration during the entire oscillation process. On the other hand, the oscillation is accompanied by a transition between a six-shock configuration (regular interaction) and a seven-shock configuration (Mach interaction) in a case with a higher free-stream Mach number. Numerical results also indicate that the critical wedge angle for the transition from a steady to an oscillation solution is higher compared to the corresponding value in earlier numerical research in which the perfect diatomic gas model was used. |
WOS关键词 | SHOCK ; VALIDATION ; TUBES |
WOS研究方向 | Mechanics |
语种 | 英语 |
WOS记录号 | WOS:000256662600005 |
其他责任者 | Myong, R. S. |
源URL | [http://dspace.imech.ac.cn/handle/311007/84803] ![]() |
专题 | 力学研究所_力学所知识产出(1956-2008) |
作者单位 | 1.Inst Mech, LHD, Beijing 100080, Peoples R China 2.Gyeongsang Natl Univ, Sch Mech & Aerosp Engn, Res Ctr Aircraft Parts Technol, Jinju 660701, South Korea; |
推荐引用方式 GB/T 7714 | Hu ZM,Myong R S,Wang C,et al. Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows[J]. SHOCK WAVES,2008,18(1):41-51. |
APA | 胡宗民,Myong R S,王春,Cho T H,&姜宗林.(2008).Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows.SHOCK WAVES,18(1),41-51. |
MLA | 胡宗民,et al."Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows".SHOCK WAVES 18.1(2008):41-51. |
入库方式: OAI收割
来源:力学研究所
浏览0
下载0
收藏0
其他版本
除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。