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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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Indexed By:EI
Date Issued:2017
Language:英语
Document Type:会议论文
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A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Lee YC(李亚超)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems
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
A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Yao, Wei(weiyao@imech.ac.cn)
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Submit date:2018/01/16
Computational Fluid Dynamics
Computer Software
Digital Storage
Kinetic Energy
Kinetics
Open Source Software
Open Systems
Runge Kutta Methods
Shock Tubes
Shock Waves
Spacecraft
Turbulence
Two Phase Flow
Development of zone flamelet model for scramjet combustor modeling
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
View
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Adobe PDF(1377Kb)
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View/Download:497/98
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Submit date:2018/11/08
Computational Fluid Dynamics
Digital Storage
Kinetic Energy
Kinetics
Open Source Software
Open Systems
Ramjet Engines
Runge Kutta Methods
Shock Tubes
Turbulence
Two Phase Flow
Bench
Mark Problems
Central
Upwind Scheme
Computational Fluid Dynamics Software
Skew
Symmetric Forms
Temporal Discretization
Turbulence Structures
Unstructured Meshes
Wall Bounded Turbulence
Development of zone flamelet modelfor scramjet combustor modeling
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(832Kb)
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View/Download:290/87
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Submit date:2018/11/08
Combustion
Cost benefit analysis
Costs
Mixtures
Ramjet engines
Supersonic aircraft
Computational costs
Equivalence ratios
Local flow conditions
Scramjet combustors
Statistics approaches
Supersonic combustion
Supersonic combustors
Turbulent combustion
Detailed transitional process of the flames in hot and diluted environments from lifted flames to MILD combustion
会议论文
10th U.S. National Combustion Meeting, College Park, MD, United states, April 23, 2017 - April 26, 2017
Authors:
Liu CY
;
Zhang J(张健)
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Submit date:2018/11/08
Oxygen
Diluted environments
Monotonic trend
Partial premixing
Stabilization mechanisms
Transition process
Transitional flames
Transitional process
Turbulent combustion
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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View/Download:394/95
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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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View/Download:285/89
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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