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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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Combustion Condition  Combustor Efficiency  Improved Delayed Detached Eddy Simulations  Initial Temperatures  Laminar Flame Speed  Scramjet Combustors  Supersonic Combustion  Turbulence-chemistry Interactions  
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)
View  |  Adobe PDF(735Kb)  |  Favorite  |  View/Download:395/136  |  Submit date:2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
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)
View  |  Adobe PDF(832Kb)  |  Favorite  |  View/Download:343/105  |  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  
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 ([email protected])
View  |  Adobe PDF(2131Kb)  |  Favorite  |  View/Download:404/142  |  Submit date:2017/05/05
Equivalence Ratios  Heat Flux Distributions  Heat Transfer Characteristics  Scramjet  Supercritical Kerosenes  Supersonic Combustion  Supersonic Combustors  Total Temperatures  
Performance of the fuel injector in supersonic combustor 会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
Authors:  Wei Z(卫喆);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Gu SL(顾声龙);  Chang XY(张新宇);  Wei, Z. ([email protected])
View  |  Adobe PDF(167Kb)  |  Favorite  |  View/Download:247/64  |  Submit date:2017/07/14
Concentration Profiles  Engine Design  Fuel Injectors  Fuel-air Mixing  Gas Sampling  Ramp Injector  Scramjet Combustors  Scramjet Test  Supersonic Combustors  
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
View  |  Adobe PDF(423Kb)  |  Favorite  |  View/Download:278/96  |  Submit date:2017/06/01
Stagnation Temperatures  Supercritical Kerosene  Supersonic Model Combustors  
Combustion of kerosene in a supersonic stream 会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
Authors:  Li JG(李建国);  Yu G(俞刚);  Zhang XY(张新宇);  Huang QS
View  |  Adobe PDF(519Kb)  |  Favorite  |  View/Download:256/129  |  Submit date:2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors