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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 [17]
范学军 [9]
吴坤 [7]
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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
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)
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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
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
Enhancement of combustion performance in a microchannel: Synergistic effects of bluff-body and cavity
期刊论文
FUEL, 2020, 卷号: 265, 页码: 11
Authors:
Zhang Z
;
Wu K(吴坤)
;
Yao W(姚卫)
;
Yuen R
;
Wang J
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Submit date:2020/04/07
Micro-combustor
Bluff-body
Cavity
Combustion performance
Flame-flow interaction
Numerical investigation on the performance of bluff body augmented micro cavity-combustor
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 7, 页码: 4932-4945
Authors:
Zhang Z
;
Wu K(吴坤)
;
Yuen R
;
Yao W(姚卫)
;
Wang J
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Submit date:2020/04/07
Micro combustor
Cavity
Bluff body
Combustion efficiency
Local Damkohler number
Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors:
Yao W(姚卫)
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Submit date:2019/12/17
Kerosene
Supersonic combustion
Large eddy simulation
Skeletal mechanism
Scramjet
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)
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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)
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Submit date:2018/10/19
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)
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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
Flow characteristic of highly underexpanded jets from various nozzle geometries
期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
Authors:
Li XP(李晓鹏)
;
Zhou, Rui
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2017/11/16
Underexpanded Jets
Noncircular Jets
Nozzle Geometry
Large Eddy Simulation