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Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance 期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
Adobe PDF(1524Kb)  |  Favorite  |  View/Download：865/241  |  Submit date：2009/08/03
Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
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：212/79  |  Submit date：2017/06/01
Stagnation Temperatures  Supercritical Kerosene  Supersonic Model Combustors  
乙烯超声速燃烧的数值模拟研究 期刊论文
实验流体力学, 2006, 卷号: 20, 期号: 2, 页码: 55-57,77
Authors:  殷悦;  俞刚
Adobe PDF(169Kb)  |  Favorite  |  View/Download：771/315  |  Submit date：2007/06/15
超声速燃烧  乙烯  Carm  Fluent  Isat  
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)
View  |  Adobe PDF(315Kb)  |  Favorite  |  View/Download：258/68  |  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  
气泡雾化喷嘴液雾特性 期刊论文
推进技术, 2003, 卷号: 24, 期号: 4, 页码: 348-352
Authors:  岳连捷;  俞刚
Adobe PDF(335Kb)  |  Favorite  |  View/Download：890/346  |  Submit date：2007/06/15
气泡  雾化  液雾特性  超音速燃烧  二相流  
Development of the facility for model scramjet testing 会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
Authors:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
View  |  Adobe PDF(872Kb)  |  Favorite  |  View/Download：230/84  |  Submit date：2017/06/01
Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures  
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：201/105  |  Submit date：2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors