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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 [20]
范学军 [17]
吴坤 [6]
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Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
Development and application of ANN model for property prediction of supercritical kerosene
期刊论文
Computers and Fluids, 2020, 卷号: 209, 期号: 2020, 页码: 1-18
Authors:
Li B(李波)
;
Lee YC(李亚超)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(10546Kb)
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Submit date:2020/08/27
Artificial Neural Network (Ann)
Principle Of Extended Corresponding State (Ecs)
Rp-3 Kerosene
Superitical Pressure
Openfoam
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
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)
Adobe PDF(2427Kb)
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Submit date:2018/10/19
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
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)
Adobe PDF(807Kb)
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Submit date:2018/07/17
Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion
期刊论文
ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Fan XJ(范学军)
Adobe PDF(1388Kb)
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Submit date:2018/12/27
Combustion Condition
Combustor Efficiency
Improved Delayed Detached Eddy Simulations
Initial Temperatures
Laminar Flame Speed
Scramjet Combustors
Supersonic Combustion
Turbulence-chemistry Interactions
Numerical investigation of characteristic frequency excited highly underexpanded jets
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
Authors:
Li XP
;
Fan E
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
;
Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Submit date:2017/07/24
Fuel Jets
Underexpanded Jets
Jet Mixing Control
Excited Jets
Large Eddy Simulation
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)
Adobe PDF(1377Kb)
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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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View/Download:437/111
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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