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Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download：378/134  |  Submit date：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1112Kb)  |  Favorite  |  View/Download：593/238  |  Submit date：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Interaction of isentropic compression waves with a bow shock 期刊论文
AIAA JOURNAL, 2013, 卷号: 51, 期号: 10, 页码: 2474-2484
Authors:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Xiao YB(肖雅彬);  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(764Kb)  |  Favorite  |  View/Download：786/291  |  Submit date：2014/01/17
Laser induced breakdown spectroscopy for local equivalence ratio measurement of kerosene/air mixture at elevated pressure 期刊论文
OPTICS AND LASERS IN ENGINEERING, 2012, 卷号: 50, 期号: 6, 页码: 877-882
Authors:  Zhang SH(张少华);  Yu XL(余西龙);  Li F(李飞);  Kang GJ;  Chen LH(陈立红);  Zhang XY(张新宇);  Yu, XL;  Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(451Kb)  |  Favorite  |  View/Download：1004/281  |  Submit date：2013/01/18
Laser Induced Breakdown Spectroscopy (Libs)  Equivalence Ratio  Kerosene/air Mixture  Elevated Pressure  Induced Spark  Air  
洛仑兹力控制高超声速进气道边界层分离的数值模拟 期刊论文
推进技术, 2011, 卷号: 32, 期号: 1, 页码: 36-41
Authors:  苏纬仪;  张新宇;  张堃元
Adobe PDF(293Kb)  |  Favorite  |  View/Download：757/196  |  Submit date：2012/04/01
高超声速进气道  Mhd流动控制  激波-边界层相互作用  边界层分离  数值仿真