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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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范学军 [10]
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Creator:范学军
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Document Type:会议论文
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A novel method of cooling channel optimization for active-cooled structure using the calculus of variations
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:
Li X(李轩)
;
Lu Y(陆阳)
;
Wu K(吴坤)
;
Fan XJ(范学军)
Adobe PDF(705Kb)
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Submit date:2020/11/20
Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Lee YC(李亚超)
;
Fan XJ(范学军)
Adobe PDF(1156Kb)
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View/Download:428/0
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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
;
Lee YC(李亚超)
;
Yao W(姚卫)
;
Lu Y(陆阳)
;
Fan XJ(范学军)
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  |  
Adobe PDF(1813Kb)
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View/Download:327/86
  |  
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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  |  
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View/Download:194/68
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Submit date:2020/08/27
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
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)
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  |  
Adobe PDF(805Kb)
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View/Download:412/154
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Submit date:2018/06/06
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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View/Download:469/227
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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
Visualization of flow separation inside cut kerf during laser cutting of thick sections
会议论文
34th International Congress on Applications of Lasers and Electro-Optics (ICALEO), Atlanta, GA, OCT 18-22, 2015
Authors:
Zhang C
;
Wen P
;
Yao ZH
;
Yuan YM(袁越明)
;
Fan XJ(范学军)
;
Wen, P (reprint author), Tsinghua Univ, State Key Lab Tribol, Beijing 100084, Peoples R China.
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View/Download:329/117
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Submit date:2016/06/28
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
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Yao W(姚卫)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li XP(李晓鹏)
;
Fan XJ(范学军)
Adobe PDF(1195Kb)
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View/Download:494/179
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Submit date:2016/07/01
Adiabatic Flame Temperature
Combustion
Directed Graphs
Flow Separation
Heat Flux
Kerosene
Large Eddy Simulation
Musculoskeletal System
Real Time Systems
Sensitivity Analysis
Spacecraft
Transients
Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor
会议论文
AIAA/ASME/SAE/ASEE 40th Joint Propulsion Conference
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Zhang XY(张新宇)
;
Sung CJ
Adobe PDF(1024Kb)
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View/Download:1078/321
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Submit date:2007/12/18