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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 [7]
范学军 [6]
吴坤 [2]
李晓鹏 [2]
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Indexed By:EI
Creator:姚卫
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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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View/Download:285/65
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
Reconstruction model for heat release rate based on artificial neural network
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 37, 页码: 19599-19616
Authors:
Li B(李波)
;
Yao W(姚卫)
;
Li YC(李亚超)
;
Fan XJ(范学军)
Adobe PDF(5169Kb)
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Submit date:2022/10/25
Heat release rate (HRR)
Artificial neural network (ANN)
Proper orthogonal -12omposition (POD)
Chemiluminescence
Supersonic hydrogen flame
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
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
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:271/94
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Submit date:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
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:293/87
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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