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Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows
Hu ZM(胡宗民)1; Myong R S1; Wang C(王春)2; Cho T H1; Jiang ZL(姜宗林)2
发表期刊SHOCK WAVES
2008-06-01
卷号18期号:1页码:41-51
ISSN0938-1287
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.
关键词Shock Shock Interaction Oscillation Hypersonic Double-wedge Numerical Study
DOI10.1007/s00193-008-0138-x
收录类别SCI
语种英语
WOS记录号WOS:000256662600005
关键词[WOS]SHOCK ; VALIDATION ; TUBES
WOS研究方向Mechanics
WOS类目Mechanics
RpAuthorMyong, R. S.
引用统计
被引频次:25[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/311007/84803
专题力学所知识产出(1956-2008)
作者单位1.Gyeongsang Natl Univ, Sch Mech & Aerosp Engn, Res Ctr Aircraft Parts Technol, Jinju 660701, South Korea;
2.Inst Mech, LHD, Beijing 100080, Peoples R China
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.
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