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Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH;  Jia YN(贾轶南);  Zhang XY(张新宇);  Yue, Lianjie(yuelj@imech.ac.cn)
浏览  |  Adobe PDF(704Kb)  |  收藏  |  浏览/下载：267/93  |  提交时间：2018/01/16
Spacecraft  
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan(yuelj@imech.ac.cn)
Adobe PDF(566Kb)  |  收藏  |  浏览/下载：336/74  |  提交时间：2018/01/16
Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels  
Experimental study of combustion oscillations in a dual-mode scramjet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
作者:  Tian XD;  Chen LH(陈立红);  Gu HB(顾洪斌);  Liu C;  Cheng LW;  Chang XY(张新宇);  Chen, Lihong (lhchen@imech.ac.cn)
Adobe PDF(824Kb)  |  收藏  |  浏览/下载：236/68  |  提交时间：2017/09/04
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)
Adobe PDF(496Kb)  |  收藏  |  浏览/下载：253/74  |  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
Adobe PDF(759Kb)  |  收藏  |  浏览/下载：572/187  |  提交时间：2014/03/11
Combustion Mode  Scramjet  Artificial Neural Network  
Combined TDLAS and OES technique for CO concentration measurement in shock-heated Martian atmosphere 会议论文
2nd International Symposium on Laser Interaction with Matter (LIMIS), Xian, PEOPLES R CHINA, SEP 09-12, 2012
作者:  Lin X(林鑫);  Yu XL(余西龙);  Li F(李飞);  Zhang SH(张少华);  Xin JG;  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(683Kb)  |  收藏  |  浏览/下载：799/279  |  提交时间：2013/12/12
Optical Emission Spectroscopy (Oes)  Tunable Diode Laser Absorption Spectroscopy (Tdlas)  Shock Wave  Temperature  Concentration  
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Chen LH(陈立红);  Zhang XY(张新宇);  Xiao YB(肖雅彬)
Adobe PDF(1674Kb)  |  收藏  |  浏览/下载：442/115  |  提交时间：2014/02/24
Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Chang XY(张新宇);  Zhong FQ(仲峰泉)
Adobe PDF(6469Kb)  |  收藏  |  浏览/下载：432/98  |  提交时间：2014/02/24
Modeling and measurements of heat release distributions in dual-mode scramjet combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Tian L(田璐);  Chen LH(陈立红);  Chen Q(陈强);  Li F(李飞);  Zhang XY(张新宇);  Tian L(田璐)
Adobe PDF(677Kb)  |  收藏  |  浏览/下载：621/198  |  提交时间：2014/02/24
无需压力数据及总温假设的超燃冲压发动机一维分析模 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
作者:  王曦;  仲峰泉;  邢云绯;  陈立红;  张新宇
Adobe PDF(553Kb)  |  收藏  |  浏览/下载：519/224  |  提交时间：2014/01/23
超燃冲压发动机  一维分析模型  燃烧  混合  激波与边界层相互作用