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Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene 期刊论文
FUEL, 2022, 卷号: 313, 页码: 13
作者:  Shen, Wubingyi;  Huang, Yue;  Yao W(姚卫);  Liu, Hedong;  You, Yancheng
Adobe PDF(9915Kb)  |  收藏  |  浏览/下载：162/35  |  提交时间：2022/05/17
Improved delayed detached eddy simulation  Liquid kerosene  Skeletal reaction mechanism  Equivalence ratio  Cavity-based scramjet combustor  Supersonic combustion  
Stabilization Mechanism of Burner-attached Flames in Laminar Non-premixed Jets 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2022, 卷号: 194, 期号: 14, 页码: 21
作者:  Li D(李丹);  Liu Yu Cheng;  Wang SF(王双峰)
Adobe PDF(10115Kb)  |  收藏  |  浏览/下载：250/60  |  提交时间：2021/05/17
Burner-attached flame  laminar non-premixed jets  flame stabilization  conductive heat transfer  convective heat transfer  
Multispectral infrared absorption spectroscopy for quantitative temperature measurements in axisymmetric laminar premixed sooting flames 期刊论文
CASE STUDIES IN THERMAL ENGINEERING, 2021, 卷号: 28, 页码: 11
作者:  Ma, Liuhao;  Duan, Kun;  Cheong, Kin-Pang;  Yuan CK(苑朝凯);  Ren, Wei
Adobe PDF(5899Kb)  |  收藏  |  浏览/下载：234/59  |  提交时间：2021/11/29
Temperature measurement  Sooting flame  Multispectral infrared absorption spectroscopy  Optical sensing  
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Peng JL(彭锦龙);  Liu, Yan;  Zhang ZL(张泽林);  Fang SH(方思晗);  Yu XL(余西龙)
Adobe PDF(6496Kb)  |  收藏  |  浏览/下载：274/50  |  提交时间：2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
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：268/107  |  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：262/58  |  提交时间：2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
On the Quantification of Boundary Layer Effects on Flame Temperature Measurements Using Line-of-sight Absorption Spectroscopy 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2021, 页码: 18
作者:  Ma, Liuhao;  Cheong, Kin-Pang;  Yang, Min;  Yuan CK(苑朝凯);  Ren, Wei
Adobe PDF(9950Kb)  |  收藏  |  浏览/下载：210/36  |  提交时间：2021/06/21
Flame temperature  Boundary layer effects  Laser absorption spectroscopy  Line-of-sight  
A promising plasma-catalytic approach towards single-step methane conversion to oxygenates at room temperature 期刊论文
APPLIED CATALYSIS B-ENVIRONMENTAL, 2021, 卷号: 284, 页码: 13
作者:  Chawdhury, Piu;  Wang, Yaolin;  Ray, Debjyoti;  Mathieu, Stephanie;  Wang, Ni;  Harding, Jonathan;  Bin F(宾峰);  Tu, Xin;  Subrahmanyam, Ch
Adobe PDF(9051Kb)  |  收藏  |  浏览/下载：208/69  |  提交时间：2021/06/21
Partial oxidation of methane  Non-thermal plasma  Plasma-catalysis  Methanol synthesis  Oxygenates  
Reconstruction model for heat release rate based on artificial neural network 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 37, 页码: 19599-19616
作者:  Li B(李波);  Yao W(姚卫);  Li YC(李亚超);  Fan XJ(范学军)
Adobe PDF(5169Kb)  |  收藏  |  浏览/下载：102/26  |  提交时间：2022/10/25
Heat release rate (HRR)  Artificial neural network (ANN)  Proper orthogonal -12omposition (POD)  Chemiluminescence  Supersonic hydrogen flame  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
作者:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  收藏  |  浏览/下载：278/54  |  提交时间：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test