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姚卫 [8]
范学军 [7]
陆阳 [4]
李亚超 [3]
李波 [3]
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Creator:姚卫
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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
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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Submit date:2021/02/01
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
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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Submit date:2019/09/09
Heat flux measurement
Kerosene
Supersonic combustion
Scramjet
Heat flux sensor
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
Authors:
Li B
;
Lee YC(李亚超)
;
Yao W(姚卫)
;
Lu Y(陆阳)
;
Fan XJ(范学军)
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Submit date:2018/12/26
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio., July 9-11, 2018
Authors:
Li B(李波)
;
Lee YC(李亚超)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2020/08/27
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor
会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
Authors:
Cheng D(程迪)
;
Wang J(王晶)
;
Gong J
;
Lu Y(陆阳)
;
Yao W(姚卫)
;
Li L(李龙)
;
Fan XJ(范学军)
;
Fan, Xuejun (xfan@imech.ac.cn)
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Submit date:2017/05/05
Equivalence Ratios
Heat Flux Distributions
Heat Transfer Characteristics
Scramjet
Supercritical Kerosenes
Supersonic Combustion
Supersonic Combustors
Total Temperatures
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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Submit date:2016/01/08
Hydrocarbons
Combustors
Cooling
Heat Transfer