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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 [10]
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Community:高温气体动力学国家重点实验室
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Community:流固耦合系统力学重点实验室
Language:英语
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Design of a milli-newton force balance for hypersonic rarefied wind tunnel
期刊论文
MEASUREMENT, 2021, 卷号: 185, 页码: 7
Authors:
Wu CW(吴臣武)
;
Liu C(刘聪)
;
Hu DL(胡灯亮)
;
Liu HL(刘宏立)
;
Huang HJ(黄河激)
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Submit date:2021/11/15
Strain
Balance
Milli-newton
Design
Calibration
Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition
期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 卷号: 21, 期号: 2, 页码: 347-362
Authors:
Wang RX(王睿星)
;
Wang, ZW
;
Zheng HW(郑洪伟)
;
Song HW(宋宏伟)
Adobe PDF(4182Kb)
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Submit date:2020/06/22
Coupled flow-thermal analysis
Thermal protection system
Basic direct correction method (BDCM)
Improved DCM (IDCM)
Iteration solution method (ISM)
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
A moving model rig with a scale ratio of 1/8 for high speed train aerodynamics
期刊论文
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2016, 卷号: 152, 页码: 50-58
Authors:
Yang QS(杨乾锁)
;
Song JH(宋军浩)
;
Yang GW(杨国伟)
;
Yang, QS
Adobe PDF(4665Kb)
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Submit date:2017/09/04
Influences of affiliated components and train length on the train wind
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 2, 页码: 191-205
Authors:
Guo DL(郭迪龙)
;
Shang KM
;
Zhang Y
;
Yang GW(杨国伟)
;
Sun ZX(孙振旭)
;
Guo, DL
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Submit date:2017/09/04
A modified multi-objective sorting particle swarm optimization and its application to the design of the nose shape of a high-speed train
期刊论文
ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS, 2015, 卷号: 9, 期号: 1, 页码: 513-527
Authors:
Yao SB(姚栓宝)
;
Guo DL(郭迪龙)
;
Sun ZX(孙振旭)
;
Yang GW(杨国伟)
;
Sun, ZX
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Submit date:2018/07/06
Study on the critical diameter of the subway tunnel based on the pressure variation
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2014, 卷号: 57, 期号: 10, 页码: 2037-2043
Authors:
Sun ZX(孙振旭)
;
Yang GW(杨国伟)
;
Zhu L
;
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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View/Download:684/188
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Submit date:2014/11/27
Tunnel Pressure Waves
Airtight Index
Aural Discomfort
Blockage Ratio
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
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View/Download:214/71
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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