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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
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：195/53  |  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
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：145/45  |  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
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：246/78  |  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：115/0  |  Submit date：2020/11/20
Flutter  High speed train external windshield  Tight coupling method  Vibration  
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
View  |  Adobe PDF(1159Kb)  |  Favorite  |  View/Download：214/71  |  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：978/214  |  Submit date：2013/03/25
Cfd  Csd  Aeroelasticity  Coupled Method  Flutter  Mpi  
Fast Dynamic Mesh Method and its Application on Aeroelasticity 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:  Yang GW(杨国伟);  Zheng GN(郑冠男);  Nie XY(聂雪媛)
View  |  Adobe PDF(3458Kb)  |  Favorite  |  View/Download：676/239  |  Submit date：2014/03/11
Dynamic Mesh  Rbf  Reduced-point Option  Aeroelasticity  
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：1016/334  |  Submit date：2012/12/07
Navier-stokes Equations  Schemes  Solver  Aeroelasticity  Cfd/csd  Rom  Active Flutter Suppression  
基于混合网格Navier-Stokes方程并行算法的气动弹性研究 学位论文
博士论文，北京: 中国科学院研究生院, 2011
Authors:  郑冠男
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