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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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Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230
Authors:
Chen XJ
;
Qiu ZP
;
Wang XJ
;
Li YL
;
Wang RX(王睿星)
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View/Download:375/83
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Submit date:2018/02/08
Uncertain Reduced-order Modeling
Robust Flutter Analysis
Interval Perturbation Method
Uncertain Aeroelastic System
Numerical studies of static aeroelastic effects on grid fin aerodynamic performances
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314
Authors:
Huang CD(黄程德)
;
Liu W(刘文)
;
Yang GW(杨国伟)
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View/Download:323/97
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Submit date:2017/11/29
Aeroelasticity
Fluid-structure Interpolation
Grid Fin
Mesh Deformation
Radial Basis Function
Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:Turning angle effects
期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 149, 页码: 56-69
Authors:
Tong FL(童福林)
;
Yu ZP(于长平)
;
Tang ZG(唐志共)
;
Li XL(李新亮)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
;
Li, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Submit date:2017/10/27
Compression Corner
Low-frequency Oscillation
Coherent Vortex Structure
Power Spectrum
Turbulent Kinetic Energy Budget
Direct Numerical Simulation
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel
期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:
Liu YF(刘云峰)
;
Wang YP(汪运鹏)
;
Yuan CK(苑朝凯)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
;
Liu, YF (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:2017/08/22
Aerodynamic Force And Moment Measurement
10° Half-angle Cone Model
Jf12
Real-gas Effects
Shock Tunnel
Local Piston Theory with Viscous Correction and Its Application
期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
Authors:
Liu W(刘文)
;
Zhang CA(张陈安)
;
Han HQ
;
Wang FM(王发民)
;
Zhang, CA (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:2017/03/28
Hypersonic
Unsteady Aerodynamics
Piston Theory
Aeroelasticity
可压缩流动中间断问题的高分辨率数值求解方法及应用
学位论文
博士论文,北京: 中国科学院大学, 2017
Authors:
刘利
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View/Download:335/11
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Submit date:2019/05/15
Numerical analysis of shock wave and supersonic turbulent boundary interaction between adiabatic and cold walls
期刊论文
JOURNAL OF TURBULENCE, 2017, 卷号: 18, 期号: 6, 页码: 569-588
Authors:
Tong, Fulin
;
Tang, Zhigong
;
Yu ZP(于长平)
;
Zhu, Xingkun
;
Li XL(李新亮)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing, Peoples R China.
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Submit date:2017/09/06
Shock Wave/turbulent Boundary Layer Interaction
Wall Temperature
Turbulence Structure
Shock Motion
Dynamic Mode Decomposition
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp
会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
Authors:
Tong FL(童福林)
;
Li XL(李新亮)
;
Duan, Yanhui
;
Yu ZP(于长平)
;
Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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View/Download:287/116
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Submit date:2018/01/16
Concave Surface Curvature
Adverse Pressure-gradient
Large-eddy Simulation
Reynolds-number
Near-wall
Flows
Separation
Vortices
Models
考虑结构非线性CFD/CSD耦合气动弹性研究
学位论文
博士论文,北京: 中国科学院大学, 2017
Authors:
黄程德
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Submit date:2017/07/07
高速列车参数化方法研究及整车气动外形优化设计
学位论文
博士论文,北京: 中国科学院大学, 2017
Authors:
张业
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Submit date:2017/07/07