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中国科学院力学研究所机构知识库
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Document Type:会议论文
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High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model
会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors:
Yang L
;
岳连捷
;
张启帆
;
张新宇
Adobe PDF(1289Kb)
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Submit date:2021/01/12
Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model
会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
Authors:
Yao W(姚卫)
;
Chen L(陈留)
Adobe PDF(2272Kb)
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Submit date:2021/06/11
AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL
会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
;
Teng HH(滕宏辉)
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Submit date:2019/04/19
THE MECHANISM OF THREE-DIMENSION STEADY SHOCK WAVE INTERACTION
会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:
Wang C(王春)
;
Yang RX(杨瑞欣)
;
Jiang ZL(姜宗林)
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Submit date:2019/04/19
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, Xuejun(xfan@imech.ac.cn)
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Submit date:2018/01/16
Adiabatic Flame Temperature
Aerodynamics
Boundary Layer Flow
Boundary Layers
Chemical Analysis
Combustion
Computational Chemistry
Directed Graphs
Flow Separation
Mach Number
Principal Component Analysis
Regression Analysis
Sensitivity Analysis
Spacecraft
Supersonic Aerodynamics
Supersonic Aircraft
Transients
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
Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Li GL(李广利)
;
Cui K(崔凯)
;
Xiao Y(肖尧)
;
Xu YZ(徐应洲)
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Adobe PDF(664Kb)
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View/Download:412/102
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Submit date:2018/01/16
Aerodynamics
Angle Of Attack
Angle Of Attack Indicators
Boundary Layers
Drag
Drag Coefficient
High Pressure Effects
Hypersonic Aerodynamics
Hypersonic Flow
Spacecraft
Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Xiao Y(肖尧)
;
Cui K(崔凯)
;
Li GL(李广利)
;
Xu YZ(徐应洲)
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Adobe PDF(639Kb)
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Submit date:2018/01/16
Aerodynamics
Air Engines
Aspect Ratio
Computational Fluid Dynamics
Drag
Engines
Hypersonic Aerodynamics
Lift
Lift Drag Ratio
Propulsion
Spacecraft
Vehicles
Study on Compression Surface Deformation of Waveriders
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Xu YZ(徐应洲)
;
Cui K(崔凯)
;
Li GL(李广利)
;
Xiao Y(肖尧)
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Adobe PDF(461Kb)
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Submit date:2018/01/16
Aerodynamic Configurations
Aerodynamics
Computational Fluid Dynamics
Deformation
Evolutionary Algorithms
Fluid Dynamics
Hypersonic Aerodynamics
Optimization
Spacecraft
Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes
会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
Authors:
Gan JY
;
Shen YQ(申义庆)
;
Zha GC
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Submit date:2017/05/05
Central Differencing
Drag Prediction
Finite Difference Scheme
High
Order Scheme
Line Relaxation
Mesh Refinement
Trailing Edges
Turbulent Models