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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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姚卫 [10]
范学军 [10]
吴坤 [3]
Lee YC [2]
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Creator:姚卫
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Document Type:会议论文
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Evaluation of the influence of radiation on a GH2/GO2 rocket combustor
会议论文
AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17
Authors:
Li B(李波)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(1358Kb)
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View/Download:166/52
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Submit date:2021/02/01
Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Lee YC(李亚超)
;
Fan XJ(范学军)
Adobe PDF(1156Kb)
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View/Download:436/0
  |  
Submit date:2018/12/26
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Wu K(吴坤)
;
Fan XJ(范学军)
View
  |  
Adobe PDF(805Kb)
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View/Download:417/156
  |  
Submit date:2018/06/06
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)
View
  |  
Adobe PDF(1377Kb)
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Submit date:2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems
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)
View
  |  
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View/Download:444/113
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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)
View
  |  
Adobe PDF(623Kb)
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View/Download:277/96
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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
  |  
Adobe PDF(1377Kb)
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View/Download:506/103
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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)
View
  |  
Adobe PDF(832Kb)
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View/Download:304/92
  |  
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
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
Authors:
Lu Y(陆阳)
;
Wang XZ(王新竹)
;
Li L(李龙)
;
Cheng D(程迪)
;
Yuan T(袁涛)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(445Kb)
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View/Download:474/98
  |  
Submit date:2016/01/08
Hydrocarbons
Combustors
Cooling
Heat Transfer
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Wu K(吴坤)
;
Li XP(李晓鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
View
  |  
Adobe PDF(590Kb)
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View/Download:396/96
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Submit date:2017/05/05
Frequency Spectrum Analysis
High Temporal Resolution
Instantaneous Flow
Noise Generation Mechanisms
Theoretical Modeling
Three
Dimensional Numerical Studies
Transport Mechanism
Under
Expanded Jets