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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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杨国伟 [4]
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Date Issued:2015
Community:流固耦合系统力学重点实验室
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An airplane jig shape design method based on high fidelity aeroelastic simulation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 47, 页码: 314-323
Authors:
Yang W
;
Wang QF
;
Zhou L
;
Zheng GN(郑冠男)
;
Liu W
;
Yang, W (reprint author), Commercial Aircraft Corp China Ltd, Beijing Aeronaut Sci & Technol Res Inst, Beijing, Peoples R China.
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Submit date:2016/03/21
Aeroelasticity
Cfd
Csd
Jig Shape
Structural Mesh
An effective CFD approach for marine-vehicle maneuvering simulation based on hybrid reference frames method
期刊论文
Ocean Engineering, 2015, 卷号: 109, 页码: 83–92
Authors:
Wu XC(吴小翠)
;
Wang YW(王一伟)
;
Huang CG(黄晨光)
;
Hu ZQ
;
Yi RW
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Submit date:2016/01/07
Maneuvering Characteristics
Hybrid Reference Frames Method
Rotating Arm Test
Suboff Model
Experiment and numerical simulation on the characteristics of fluid-structure interactions of non-rigid airships
期刊论文
Theoretical and Applied Mechanics Letters, 2015, 卷号: 5, 期号: 6, 页码: 258–261
Authors:
Wu XC(吴小翠)
;
Wang YW(王一伟)
;
Huang CG(黄晨光)
;
Liu YB(刘玉标)
;
Lu LL(路玲玲)
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Submit date:2016/01/07
Fluid–structure Interaction
Non-rigid Airships
Numerical Simulation
Wind Tunnel Test
基于分离涡方法的高速列车横风非定常气动特性
期刊论文
中南大学学报(自然科学版), 2015, 期号: 3, 页码: 1129-1139
Authors:
郗艳红
;
毛军
;
高亮
;
杨国伟
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Submit date:2015/12/25
高速列车
横风
气动力/力矩
功率谱密度
分离涡模拟
基于CFD降阶模型的阵风减缓主动控制研究
期刊论文
航空学报, 2015, 卷号: 36, 期号: 4, 页码: 1103-1111
Authors:
聂雪媛
;
杨国伟
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Submit date:2015/12/25
阵风减缓控制
降阶模型
气动弹性
跨声速
大气紊流
模型预测控制
高速列车的关键力学问题
期刊论文
力学进展, 2015, 卷号: 45, 期号: 1, 页码: 217-460
Authors:
杨国伟
;
魏宇杰
;
赵桂林
;
刘玉标
;
曾晓辉
;
邢云林
;
赖姜
;
张营营
;
吴晗
;
陈启生
;
刘秋生
;
李家春
;
胡开鑫
;
杨中平
;
刘文正
;
王文静
;
孙守光
;
张卫华
;
周宁
;
李瑞平
;
吕青松
;
金学松
;
温泽峰
;
肖新标
;
赵鑫
;
崔大宾
;
吴兵
;
钟硕乔
;
周信
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Adobe PDF(11087Kb)
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View/Download:969/247
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Submit date:2016/01/21
高速列车
空气动力学
弓网关系
车体振动
运行稳定性
轮轨关系
结构可靠性
噪声
High Speed Rails
Aerodynamics
Catenary-pantograph Interaction
Dynamics And Related Issues Of Carbody
Stability Analysis
Rail-wheel Interaction
Reliability Of Key Components
Noise-generation
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)
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View/Download:267/76
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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