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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 [9]
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Creator:yangguowei分杨国伟
Language:英语
Community:高温气体动力学国家重点实验室
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Surrogate Based Optimization of Aerodynamic Noise for Streamlined Shape of High Speed Trains
期刊论文
APPLIED SCIENCES-BASEL, 2017, 卷号: 7, 期号: 2
Authors:
Sun ZX(孙振旭)
;
Zhang Y
;
Yang GW(杨国伟)
;
Sun, ZX (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
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Submit date:2017/07/24
Aerodynamic Noise
Nlas
Kriging Model
Cross Validation
Equivalent Continuous Spl
Time efficient aeroelastic simulations based on radial basis functions
期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2017, 卷号: 330, 页码: 810-827
Authors:
Liu W(刘文)
;
Huang CD(黄程德)
;
Yang GW(杨国伟)
;
Liu, W (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2017/04/26
INVESTIGATION OF OBSTACLE EFFECTS ON THE AERODYNAMIC PERFORMANCE OF FLAPPING WINGS
会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
Authors:
Yin B(银波)
;
Yang GW(杨国伟)
;
Yin, B (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.
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Submit date:2018/01/16
Immersed-boundary Method
Micro-air Vehicles
Insect Flight
Vortices
Forces
Flows
Reconstruction of structural damage based on reflection intensity spectra of fiber Bragg gratings
期刊论文
MEASUREMENT SCIENCE & TECHNOLOGY, 2014, 卷号: 25, 期号: 12, 页码: 125109
Authors:
Huang GJ(黄国君)
;
Wei CB
;
Chen SY
;
Yang GW(杨国伟)
;
Huang, GJ (reprint author), Chinese Acad Sci, Inst Mech, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2015/01/04
Damage Reconstruction
Fiber Bragg Grating
Reflection Intensity Spectrum
Transfer Matrix
Genetic Algorithm
Finite Element Method
Train model acceleration and deceleration
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 3, 页码: 642-647
Authors:
Yang QS(杨乾锁)
;
Song JH(宋军浩)
;
Li D(李多)
;
Zhang J(张杰)
;
Yang GW(杨国伟)
;
Yang, QS (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/03/25
Moving Train Model
Acceleration
Deceleration
Magnetic Braking
Air Gun
Compressed Air
Interaction of shock wave with multi-fluids interface using quadrilateral-based adaptive mesh
期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2012, 卷号: 23, 期号: 5, 页码: 1250033
Authors:
Zheng HW(郑洪伟)
;
Li XJ(李现今)
;
Yang GW(杨国伟)
;
Shu C
;
Zheng, HW
;
Chinese Acad Sci, Inst Mech, LHD, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2013/01/18
Shock
Multi-fluids
Interface
Unstructured
Adaptive Mesh Refinement
Quadrilateral
Instability Driven
A numerical study on aerodynamic noise sources of high-speed train
会议论文
1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011
Authors:
Yang Y(杨焱)
;
Yang GW(杨国伟)
;
Yang Y(杨焱)
Adobe PDF(533Kb)
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Submit date:2013/02/06
High-speed Train
Aerodynamic Noise
Noise Source Generation
Cfd
Caa
Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing
期刊论文
Journal of Aircraft, 2009, 卷号: 46, 期号: 4, 页码: 1444-1450
Authors:
Yang GW(杨国伟)
;
Chen DW(陈大伟)
;
Cui K(崔凯)
;
Yang GW
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View/Download:899/203
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Submit date:2009/08/03
Navier-stokes Solver
Aircraft
Numerical analyses of discrete gust response for a flexible aircraft
会议论文
21st AIAA Applied Aerodynamics Conference 2003, Orlando, FL, United states, June 23, 2003 - June 26, 2003
Authors:
Yang GW(杨国伟)
;
Obayashi S
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View/Download:210/87
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Submit date:2017/06/01
Direct-coupling Method
Dynamic Equations Of Motion
Flexible Aircraft
Flexible Airplane
Freedom Of Motion
One-minus-cosine Gust
Quasi-steady Model
Supersonic Transport