中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共38条，第1-10条 帮助

限定条件    
已选(0)清除 条数/页：   排序方式：
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：169/33  |  提交时间：2022/12/20
Rotating detonation wave  Incomplete mixing  Injection parameters  
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：159/36  |  提交时间：2022/05/17
Mach 12 scramjet inlet  High temperature  Non-equilibrium effects  Thermochemical  Inlet performance  
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：234/22  |  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：266/105  |  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：261/57  |  提交时间：2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
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：147/28  |  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：513/62  |  提交时间：2021/08/03
Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency  
Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
作者:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(6382Kb)  |  收藏  |  浏览/下载：216/32  |  提交时间：2021/11/01
Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
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：329/47  |  提交时间：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
Numerical and experimental study on high-speed hydrogen-oxygen combustion gas flow and aerodynamic heating characteristics 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 7, 页码: 11
作者:  Yu JP(于江鹏);  Li JP(李进平);  Wang Q(汪球);  Zhang SZ(张仕忠);  Zhang XY(张晓源)
Adobe PDF(3271Kb)  |  收藏  |  浏览/下载：232/44  |  提交时间：2021/11/01