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超临界态煤油等熵流动和超声速喷注研究 会议论文
第二届高超声速科技学术会议, 中国安徽黄山, 2009-11-02
作者:  仲峰泉;  范学军;  王晶;  李建国;  俞刚
Adobe PDF(2257Kb)  |  收藏  |  浏览/下载:832/186  |  提交时间:2010/11/25
超临界态  超声速  动量比  穿透深度  马赫桶  
超临界煤油的亚/超声速喷注对超声速燃烧性能的影响实验研究 会议论文
第二届高超声速科技学术会议, 中国安徽黄山, 2009-11-02
作者:  王晶;  范学军;  仲峰泉;  李建国;  俞刚
Adobe PDF(775Kb)  |  收藏  |  浏览/下载:846/260  |  提交时间:2010/11/25
航空煤油  超临界态  超声速射流  穿透深度  超声速燃烧  
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
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国)
浏览  |  Adobe PDF(315Kb)  |  收藏  |  浏览/下载:235/60  |  提交时间: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  
Performance of a Supersonic Model Combustor using Vaporized Kerosene Injection 会议论文
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, Florida, July 11-14, 2004, Florida, July 11-14, 2004
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Sun ZR(孙知人);  Fan XJ(范学军)
Adobe PDF(794Kb)  |  收藏  |  浏览/下载:666/126  |  提交时间:2007/12/18
Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor 会议论文
AIAA/ASME/SAE/ASEE 40th Joint Propulsion Conference
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Sung CJ
Adobe PDF(1024Kb)  |  收藏  |  浏览/下载:1057/313  |  提交时间:2007/12/18
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
作者:  Li JG(李建国);  Yu G(俞刚);  Zhang XY(张新宇);  Huang QS
浏览  |  Adobe PDF(519Kb)  |  收藏  |  浏览/下载:180/96  |  提交时间:2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors