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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
Authors:  Huang CD(黄程德);  Zheng GN(郑冠男);  Nie XY(聂雪媛);  Yang GW(杨国伟)
Favorite  |  View/Download：12/0  |  Submit date：2024/05/27
Flutter  Nonlinear energy sink  Equivalent linearization method  Reduced order model  
地效翼的颤振特性研究 期刊论文
振动与冲击, 2023, 卷号: 42, 期号: 17, 页码: 265-274
Authors:  赵奥博;  郑冠男;  黄程德;  杨国伟;  陈玮琪
Adobe PDF(2373Kb)  |  Favorite  |  View/Download：60/20  |  Submit date：2023/10/26
地面效应  计算流体力学/计算结构力学(CFD/CSD)耦合  颤振  
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
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：166/52  |  Submit date：2022/10/25
Free-play  Transonic dip  Flutter  Limit cycle oscillation  Aeroelastic  
含间隙非线性机翼跨声速颤振时滞反馈控制 期刊论文
北京航空航天大学学报, 2020, 卷号: 47, 期号: 10, 页码: 1980-1988
Authors:  聂雪媛;  郑冠男;  杨国伟
Adobe PDF(2883Kb)  |  Favorite  |  View/Download：145/33  |  Submit date：2022/03/16
颤振抑制  时滞系统  反馈控制  跨声速  降阶模型  间隙非线性  
变时滞间隙非线性机翼颤振主动控制方法 期刊论文
北京航空航天大学学报, 2019, 卷号: 46, 期号: 10, 页码: 1899-1906
Authors:  聂雪媛;  郑冠男;  杨国伟
Adobe PDF(1255Kb)  |  Favorite  |  View/Download：266/52  |  Submit date：2020/11/18
颤振抑制  间隙非线性  时滞控制系统  状态观测  时变时延  
几何不确定性区间分析及鲁棒气动优化设计 期刊论文
北京航空航天大学学报, 2019, 页码: 15
Authors:  宋鑫;  郑冠男;  杨国伟;  姜倩
Adobe PDF(914Kb)  |  Favorite  |  View/Download：284/65  |  Submit date：2019/12/16
几何不确定性  非线性区间分析  DFFD(直接操作自由变形)  气动优化设计  鲁棒优化设计  自适应多目标粒子群算法  Kriging代理模型  
A robust aerodynamic optimization design for airfoil based on interval uncertainty analysis 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:  Song X(宋鑫);  Zheng GN(郑冠男);  Yang GW(杨国伟)
Favorite  |  View/Download：127/0  |  Submit date：2020/11/20
Adaptive MOPSO  DFFD  Geometric uncertainty  Interval analysis  Kriging model  Robust design optimization  
Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds 会议论文
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, St. Petersburg, Russia, September 7, 2014 - September 12, 2014
Authors:  Qian W;  Yang GW(杨国伟);  Zheng GN(郑冠男);  Zhang GJ
Adobe PDF(1159Kb)  |  Favorite  |  View/Download：225/77  |  Submit date：2017/05/27
All-movable Horizontal Tail  Flutter Boundaries  Overload Factors  Structure Dynamics  Transonic Flutter  Transonic Speed  Wind Tunnel Tests  Wind-tunnel Testing  
Flutter analyses of complete aircraft based on hybrid grids and parallel computing 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 2, 页码: 398-404
Authors:  Zheng GN(郑冠男);  Yang GW(杨国伟);  Qian W;  Yang, GW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
Adobe PDF(4121Kb)  |  Favorite  |  View/Download：990/219  |  Submit date：2013/03/25
Cfd  Csd  Aeroelasticity  Coupled Method  Flutter  Mpi  
Computational methods and engineering applications of static/dynamic aeroelasticity based on CFD/CSD coupling solution 期刊论文
Science China-Technological Sciences, 2012, 卷号: 55, 期号: 9, 页码: 2453-2461
Authors:  Yang GW(杨国伟);  Zheng GN(郑冠男);  Li GB(李桂波)
Adobe PDF(871Kb)  |  Favorite  |  View/Download：1030/340  |  Submit date：2012/12/07
Navier-stokes Equations  Schemes  Solver  Aeroelasticity  Cfd/csd  Rom  Active Flutter Suppression