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Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
作者:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
Adobe PDF(5176Kb)  |  收藏  |  浏览/下载：252/102  |  提交时间：2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Cheng LW(程柳维);  Zhong FQ(仲峰泉);  Wang ZP(王知溥);  Gu HB(顾洪斌);  Ma SG(马素刚);  Zhang XY(张新宇)
浏览  |  Adobe PDF(517Kb)  |  收藏  |  浏览/下载：310/100  |  提交时间：2018/01/16
Combustors  Cracks  Diesel Engines  Efficiency  Ethylene  Fighter Aircraft  Fuels  High Speed Cameras  Ignition  Kerosene  Luminance  Spacecraft  Stabilization  
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor 期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
作者:  Wang X;  Zhong FQ(仲峰泉);  Gu HB(顾宏斌);  Zhang XY(张新宇);  Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(4711Kb)  |  收藏  |  浏览/下载：296/129  |  提交时间：2016/01/08
Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
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：564/186  |  提交时间：2014/03/11
Combustion Mode  Scramjet  Artificial Neural Network  
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet 期刊论文
Procedia Engineering, 2013, 卷号: 67, 页码: 147-154
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(771Kb)  |  收藏  |  浏览/下载：229/94  |  提交时间：2015/09/24
Scramjet  Artificial Neural Network  
Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
作者:  Gu HB(顾洪斌);  Li Z(李智);  Li F(李飞);  Chen LH(陈立红);  Gu SL(顾声龙);  Zhang XY(张新宇);  Gu HB(顾洪斌)
浏览  |  Adobe PDF(242Kb)  |  收藏  |  浏览/下载：542/204  |  提交时间：2014/02/24