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Effects of injection parameters on propagation patterns of hydrogen-fueled rotating detonation waves 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2022, 卷号: 47, 期号: 91, 页码: 38811-38822
作者:  Yao KP(姚克鹏);  Yang PF(杨鹏飞);  Teng, Honghui;  Chen, Zheng;  Wang C(王春)
Adobe PDF(3824Kb)  |  收藏  |  浏览/下载：168/33  |  提交时间：2022/12/20
Rotating detonation wave  Incomplete mixing  Injection parameters  
Advances in Plasma Diagnostics and Applications 专著
Beijing:MDPI, 2022
作者:  Editors：Chen ZT;  Attri P;  Wang Q(汪球)
Adobe PDF(20682Kb)  |  收藏  |  浏览/下载：405/1  |  提交时间：2022/12/03
Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 193, 页码: 237-254
作者:  Dai, Chunliang;  Sun, Bo;  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yue LJ(岳连捷)
Adobe PDF(13791Kb)  |  收藏  |  浏览/下载：155/34  |  提交时间：2022/05/17
Mach 12 scramjet inlet  High temperature  Non-equilibrium effects  Thermochemical  Inlet performance  
Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
作者:  Jiang ZL(姜宗林);  Teng, Honghui
Adobe PDF(13641Kb)  |  收藏  |  浏览/下载：101/2  |  提交时间：2023/03/23
Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
作者:  Zhang WS(张文硕);  Zhang, Zijian;  Jiang ZL(姜宗林);  Han X(韩信);  Liu, Yunfeng;  Wang, Chun
Adobe PDF(15045Kb)  |  收藏  |  浏览/下载：232/22  |  提交时间：2022/01/24
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
作者:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  收藏  |  浏览/下载：263/105  |  提交时间：2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
作者:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
Adobe PDF(2954Kb)  |  收藏  |  浏览/下载：256/54  |  提交时间：2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
Special Topic on Selected Papers from the 11th National Congress on Fluid Mechanics of China 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 2
作者:  Liu, Hua;  Zhou, Jifu;  Wan, Minping
Adobe PDF(348Kb)  |  收藏  |  浏览/下载：131/25  |  提交时间：2022/03/05
Near-field relaxation subsequent to the onset of oblique detonations with a two-step kinetic model 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 11
作者:  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Wang, Kuanliang
Adobe PDF(5463Kb)  |  收藏  |  浏览/下载：144/27  |  提交时间：2022/01/13
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
作者:  Fang SH(方思晗);  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Li RJ(李仁杰);  Li, Jing;  Zhang, Zhedian;  Liu, Yan;  Yu XL(余西龙)
Adobe PDF(4367Kb)  |  收藏  |  浏览/下载：507/60  |  提交时间：2021/08/03
Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency