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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 [11]
范学军 [8]
王晶 [3]
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Language:英语
Author:姚卫
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On the application of dynamic zone flamelet model to large eddy simulation of supersonic hydrogen flame
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 41, 页码: 21940-21955
Authors:
Yao W(姚卫)
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Submit date:2020/09/27
Dynamic zone flamelet model
Supersonic hydrogen jet
Large eddy simulation
Supersonic combustion
Turbulent combustion model
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)
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Submit date:2021/06/11
Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor
期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11
Authors:
Cheng D(程迪)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li L(李龙)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(2651Kb)
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View/Download:419/137
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Submit date:2019/09/09
Heat flux measurement
Kerosene
Supersonic combustion
Scramjet
Heat flux sensor
Influences of Domain Symmetry on Supersonic Combustion Modeling
期刊论文
JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Fan XJ(范学军)
Adobe PDF(862Kb)
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Submit date:2019/04/11
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:
Yao W(姚卫)
;
Li B(李波)
Adobe PDF(1665Kb)
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View/Download:161/50
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Submit date:2020/11/20
Dynamic zone flamelet model
GH2/GO2
Large Eddy Simulation (LES)
Rocket combustor
Turbulence-chemistry interaction
Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios
期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 4, 页码: 975-991
Authors:
Yao W(姚卫)
;
Lu Y(陆阳)
;
Wu K(吴坤)
;
Wang J(王晶)
;
Fan XJ(范学军)
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Adobe PDF(2427Kb)
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Submit date:2018/10/19
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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Adobe PDF(1377Kb)
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View/Download:296/116
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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
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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Adobe PDF(623Kb)
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View/Download:273/94
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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)
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Adobe PDF(1377Kb)
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View/Download:501/101
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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