IMECH-IR
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Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism 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
作者:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
浏览  |  Adobe PDF(496Kb)  |  收藏  |  浏览/下载:247/74  |  提交时间:2017/05/05
Combustion Pro  Cess  Directed Relation Graph  Dynamic Evolution  Fuel Injection Velocities  Kinetic Mechanism  Reduced Mechanisms  Temperature Profiles  Temporal And Spatial Evolutions  
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
作者:  Chen Q(陈强);  Chen LH(陈立红);  Gu HB(顾洪斌);  Zhang XY(张新宇);  Wang P
浏览  |  Adobe PDF(759Kb)  |  收藏  |  浏览/下载:565/186  |  提交时间:2014/03/11
Combustion Mode  Scramjet  Artificial Neural Network  
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:179/95  |  提交时间:2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors