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Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor 期刊论文
AIAA JOURNAL, 2022, 页码: 7
作者:  Zhang X(张旭);  Zhang QF(张启帆);  Wu ZJ(吴振杰);  Yue LJ(岳连捷);  Gao ZB(高占彪);  Luo WH(罗苇航);  Chen H(陈昊)
Adobe PDF(1382Kb)  |  收藏  |  浏览/下载：152/27  |  提交时间：2022/03/22
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
作者:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
Adobe PDF(4108Kb)  |  收藏  |  浏览/下载：331/48  |  提交时间：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
作者:  Xue, Rui;  Zheng, Xing;  Yue LJ(岳连捷);  Zhang, Qian;  He, Xin;  Yang, Jing;  Weng, Chao;  Li, Zhihao
Adobe PDF(5483Kb)  |  收藏  |  浏览/下载：127/42  |  提交时间：2022/10/25
Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
Adobe PDF(3937Kb)  |  收藏  |  浏览/下载：189/45  |  提交时间：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
作者:  Xue R(薛瑞);  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3251Kb)  |  收藏  |  浏览/下载：339/111  |  提交时间：2020/07/06
Compressible boundary layer combustion  Skin-friction reduction  Shock train/flame interaction  
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
作者:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
浏览  |  Adobe PDF(3862Kb)  |  收藏  |  浏览/下载：332/115  |  提交时间：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
隔离段抽吸引起的激波迟滞现象研究 期刊论文
推进技术, 2017, 卷号: 38, 期号: 04, 页码: 732-739
作者:  马生虎;  岳连捷;  贾轶楠;  肖雅彬;  张新宇
浏览  |  Adobe PDF(1677Kb)  |  收藏  |  浏览/下载：255/68  |  提交时间：2017/12/22
超燃冲压发动机  隔离段  激波反射迟滞  边界层分离迟滞  
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：260/90  |  提交时间：2018/01/16
Spacecraft  
The effects of air vitiation on the supersonic turbulent channel flow using direct numerical simulation 会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
作者:  Chen XP;  Li XP(李晓鹏);  Dou HS
浏览  |  Adobe PDF(1216Kb)  |  收藏  |  浏览/下载：219/75  |  提交时间：2017/05/05
Mass Fraction  Mean Velocities  Nondimensional  Reynolds Analogy  Static Temperature  Statistical Characteristics  Temperature Correlation  Turbulent Channel Flows  
H_2O/CO_2污染对RP-3航空煤油着火特性的影响 期刊论文
推进技术, 2015, 卷号: 36, 期号: 3, 页码: 336-344
作者:  梁金虎;  王苏;  张灿;  张胜涛;  岳连捷;  范秉诚;  张新宇;  崔季平
浏览  |  Adobe PDF(1583Kb)  |  收藏  |  浏览/下载：241/64  |  提交时间：2015/12/25
污染效应  着火延时  煤油  H2o  Co2  激波管