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Supercritical and subcritical aeroelastic behaviors of a three-dimensional wing coupled with a nonlinear energy sink 期刊论文
INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 2024, 卷号: 161, 页码: 17./通讯作者：Huang, Chengde, Zheng, Guannan
Authors:  Huang CD(黄程德);  Zheng GN(郑冠男);  Nie XY(聂雪媛);  Yang GW(杨国伟)
Favorite  |  View/Download：102/0  |  Submit date：2024/05/27
Flutter  Nonlinear energy sink  Equivalent linearization method  Reduced order model  
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)  |  Favorite  |  View/Download：153/47  |  Submit date：2023/09/05
Shock wave  Panel flutter  Subcritical bifurcation  Supercritical bifurcation  Fluid -structure interaction  Limit cycle oscillation  
跨声速翼型颤振数值分析及其抑制研究 学位论文
硕士论文，北京: 中国科学院大学, 2023
Authors:  谈琰
Adobe PDF(6388Kb)  |  Favorite  |  View/Download：196/10  |  Submit date：2023/09/13
Computational Fluid Dynamics, Transonic Flutter, Reduced Order Model, Skin Active Vibration, Energy Diagram  
Research on Panel Flutter Considering the Effect of Convective Active Cooling 期刊论文
APPLIED SCIENCES-BASEL, 2023, 卷号: 13, 期号: 8, 页码: 4925./通讯作者：Zheng, GN
Authors:  Huang J(黄杰);  Lu WS(陆维爽);  Yang GW(杨国伟);  Zheng GN(郑冠男)
Adobe PDF(7523Kb)  |  Favorite  |  View/Download：90/24  |  Submit date：2023/06/15
panel flutter  coolant action  flight stability  flutter suppression  
Time-Domain Aeroelasticity Analysis by a Tightly Coupled Fluid-Structure Interaction Methodology 期刊论文
APPLIED SCIENCES-BASEL, 2021, 卷号: 11, 期号: 12, 页码: 5389./通讯作者：Nie, XY, Zheng, GN, Yang, GW (corresponding author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
Authors:  Liu ZY(刘忠宇);  Nie XY(聂雪媛);  Zheng GN(郑冠男);  Yang GW(杨国伟)
Adobe PDF(5626Kb)  |  Favorite  |  View/Download：345/120  |  Submit date：2022/10/25
CFD  CSD coupling  flutter boundary  computational aeroelasticity  
Three dimensional aeroelastic analyses considering free-play nonlinearity using computational fluid dynamics/computational structural dynamics coupling 期刊论文
JOURNAL OF SOUND AND VIBRATION, 2021, 卷号: 494, 页码: 115896./通讯作者：Yang, GW (corresponding author), Chinese Acad Sci, LMFS Inst Mech, Beijing 100190, Peoples R China., Yang, GW (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
Authors:  Huang CD(黄程德);  Huang J(黄杰);  Song X(宋鑫);  Zheng GN(郑冠男);  Yang GW(杨国伟)
Adobe PDF(4152Kb)  |  Favorite  |  View/Download：411/85  |  Submit date：2022/10/25
Free-play  Transonic dip  Flutter  Limit cycle oscillation  Aeroelastic  
Aeroelastic Simulation Using CFD/CSD Coupling Based on Precise Integration Method 期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 页码: 18./通讯作者：Zheng, Guannan
Authors:  Huang CD(黄程德);  Huang J(黄杰);  Song X(宋鑫);  Zheng GN(郑冠男);  Nie XY(聂雪媛)
View  |  Adobe PDF(5463Kb)  |  Favorite  |  View/Download：283/102  |  Submit date：2020/04/07
Flutter  Static aeroelasticity  CFD  CSD coupling  Precise integration method  
Flutter study on high speed train external windshield by a tight coupling method 会议论文
ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019, San Francisco, CA, United states, July 28, 2019 - August 1, 2019
Authors:  Jiang Q(姜倩);  Zheng GN(郑冠男);  Zhao GL(赵桂林)
Favorite  |  View/Download：189/0  |  Submit date：2020/11/20
Flutter  High speed train external windshield  Tight coupling method  Vibration  
Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230
Authors:  Chen XJ;  Qiu ZP;  Wang XJ;  Li YL;  Wang RX(王睿星)
View  |  Adobe PDF(4860Kb)  |  Favorite  |  View/Download：486/123  |  Submit date：2018/02/08
Uncertain Reduced-order Modeling  Robust Flutter Analysis  Interval Perturbation Method  Uncertain Aeroelastic System  
Investigation on transonic flutter active auppression with CFD-Based ROMs 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 1, 页码: 014701
Authors:  Nie XY(聂雪媛);  Yang GW(杨国伟);  Zhang MF(张明峰)
View  |  Adobe PDF(754Kb)  |  Favorite  |  View/Download：351/97  |  Submit date：2017/08/30
:Reduced Order Model  Aeroelasticity  Linear Quadratic Gaussian Control  Sliding Mode Control  Active Flutter Suppression Keywords Plus:Navier-stokes Equations  Suppression  Identification  Computations  System  
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