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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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力学所知识产出(19... [2]
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范学军 [10]
姚卫 [4]
李建国 [4]
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Indexed By:EI
Creator:范学军
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Language:英语
Document Type:会议论文
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Experimental Studies of Film Cooling in Supersonic Combustors
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Fan C(樊川)
;
Wang J(王晶)
;
Fan XJ(范学军)
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Submit date:2018/01/16
Combustion
Combustors
Coolants
Kerosene
Spacecraft
Supersonic Aerodynamics
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
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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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
A comparative study of highly underexpanded nitrogen and hydrogenjets using large eddy simulation
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Li XP(李晓鹏)
;
Wu K(吴坤)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2017/05/05
Comparative Studies
Flow Charac
Teristics
High Order Harmonics
High Resolution
Instability Modes
Near
Field Structure
Shock Structure
Under
Expanded Jets
Blowout limits of supercritical kerosene in supersonic combustors
会议论文
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United states, JUL 14-17, 2013
Authors:
Zhang TC(张泰昌)
;
Wang J(王晶)
;
Yuan YM(袁越明)
;
Li JG(李建国)
;
Yu G(俞刚)
;
Fan XJ(范学军)
;
Zhang TC(张泰昌)
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Submit date:2014/02/24
Characteristics of a supersonic model combustor with two-staged injections of supercritical kerosene
会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:
Zhang TC(张泰昌)
;
Yuan YM(袁越明)
;
Li JG(李建国)
;
Fan XJ(范学军)
;
Zhang TC(张泰昌)
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Submit date:2014/02/24
Quasi-1D compressible flow of hydrocarbon fuel
会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:
Cheng D(程迪)
;
Fan XJ(范学军)
;
Yang M(杨猛)
;
Cheng D(程迪)
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Adobe PDF(1018Kb)
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Submit date:2014/02/24
Performance of supersonic model combustors with distributed injection of supercritical kerosene
会议论文
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, United states, July 8, 2007 - July 11, 2007
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Lu XN
;
Sung CJ
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Adobe PDF(423Kb)
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Submit date:2017/06/01
Stagnation Temperatures
Supercritical Kerosene
Supersonic Model Combustors
Flow rate analyses and calibrations of kerosene cracking for supersonic combustion
会议论文
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United states, July 10, 2005 - July 13, 2005
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
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Adobe PDF(315Kb)
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Submit date:2017/06/01
Average Molecular Weight
Chemical Formulae
Cracking Model
Gaseous Products
High Temperature
Ideal Gas Law
Ideal Gas Mixtures
Mass Flow Rate
Mole Fraction
Residence Time
Room Temperature
Sonic Nozzle
Supercritical Condition
Supersonic Combustion
Temperature Dependencies
Thermal Cracking
Three-component