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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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Numerical study on the nonlinear characteristics of shock induced two-dimensional panel flutter in inviscid flow
期刊论文
JOURNAL OF SOUND AND VIBRATION, 2023, 卷号: 564, 页码: 117893./通讯作者:Wang, G (corresponding author), Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China.
Authors:
Zhou, Hao
;
Wang, Gang
;
Li, QuanZheng
;
Liu Y(刘毅)
Adobe PDF(987Kb)
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View/Download:143/41
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Submit date:2023/09/05
Shock wave
Panel flutter
Subcritical bifurcation
Supercritical bifurcation
Fluid -structure interaction
Limit cycle oscillation
Shock oscillation in highly underexpanded jets
期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 9, 页码: 94705
Authors:
Li XP
;
Zhou R
;
Chen XP
;
Fan XJ(范学军)
;
Xie GS
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View/Download:401/136
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Submit date:2018/10/30
highly underexpanded jets
shock oscillation
large eddy simulation
Analysis of the test condition of a shock-expansion tube: JF-16
会议论文
First International Conference on High Temperature Gas Dynamics, Beijing, 2012-10
Authors:
Hu ZM(胡宗民)
;
Wu B(吴波)
;
Jiang ZL(姜宗林)
Adobe PDF(264Kb)
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View/Download:960/294
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Submit date:2013/03/16
Shock-expansion Tube
Computation
Spurious Oscillation
Flus Splliting
Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction in a Supersonic Compression Ramp
期刊论文
SCIENCE CHINA: Physics, Mechanics & Astronomy, 2010, 卷号: 53, 期号: 9, 页码: 1651-1658
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Liang X(梁贤)
;
Li XL(李新亮)
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View/Download:1683/389
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Submit date:2010/10/25
compression Ramp
Shock/turbulent Boundary Layer Interaction
Direct Numerical Simulation
Shock Oscillation
Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows
期刊论文
SHOCK WAVES, 2008, 卷号: 18, 期号: 1, 页码: 41-51./通讯作者:Myong, R. S.
Authors:
Hu ZM(胡宗民)
;
Myong R S
;
Wang C(王春)
;
Cho T H
;
Jiang ZL(姜宗林)
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View/Download:326/137
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Submit date:2020/08/26
Shock
Shock Interaction
Oscillation
Hypersonic
Double-wedge
Numerical Study