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Effect of pilot hydrogen on the mixing and combustion characteristics in kerosene-fueled scramjet 期刊论文
APPLIED THERMAL ENGINEERING, 2025, 卷号: 258, 页码: 10./通讯作者：Tian, Zhen-Yu
Authors:  Shi, HongQing;  Wang, Du;  Cui NF(崔乃夫);  Zhao, ChenYang;  Lei, JieMing;  Zhu, ZiQiang;  Zhang, YaNing;  Tian, ZhenYu
Favorite  |  View/Download：65/0  |  Submit date：2024/11/22
Scramjet  Pilot hydrogen  Dual cavities  Mixing efficiency  Combustion performance  
Reinforcement Learning for Submodel Assignment in Adaptive Modeling of Turbulent Flames 期刊论文
AIAA JOURNAL, 2024, 页码: 9./通讯作者：Ren, Zhuyin
Authors:  Yang TW(杨天威);  Yin,Yu;  Liu QL(刘起立);  Yu,Tao;  Wang,Yuwang;  Zhou,Hua;  Ren,Zhuyin
Favorite  |  View/Download：52/0  |  Submit date：2024/12/23
Reinforcement Learning  Thermoacoustic Combustion Instabilities  Computational Fluid Dynamics  Artificial Neural Network  Propulsion and Power  Turbulent Reacting Flow  High Performance Computing  Diffusion Flames  Numerical Combustion  
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11./通讯作者：Sun, Mingbo, Zhao, Guoyan
Authors:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui;  Ma, Guangwei;  Wang, Hongbo
Adobe PDF(3841Kb)  |  Favorite  |  View/Download：246/80  |  Submit date：2022/12/20
Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance  
Effect of helical fins on the combustion performance in a micro-step combustor 期刊论文
FUEL, 2022, 卷号: 319, 页码: 13./通讯作者：Yao, Wei
Authors:  Zhang Z(张政);  Shen WBY;  Yao W(姚卫);  Wang Q(汪球);  Zhao W(赵伟)
Adobe PDF(11881Kb)  |  Favorite  |  View/Download：454/100  |  Submit date：2022/05/17
Micro-combustion  Helical fin  Combustion performance  Conjugate heat transfer  Mixing  
Enhancement of combustion performance in a microchannel: Synergistic effects of bluff-body and cavity 期刊论文
FUEL, 2020, 卷号: 265, 页码: 11./通讯作者：Wang, Jian
Authors:  Zhang Z;  Wu K(吴坤);  Yao W(姚卫);  Yuen R;  Wang J
View  |  Adobe PDF(3821Kb)  |  Favorite  |  View/Download：532/178  |  Submit date：2020/04/07
Micro-combustor  Bluff-body  Cavity  Combustion performance  Flame-flow interaction  
Development of the facility for model scramjet testing 会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
Authors:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
View  |  Adobe PDF(872Kb)  |  Favorite  |  View/Download：334/136  |  Submit date：2017/06/01
Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures  
Combustion of kerosene in a supersonic stream 会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
Authors:  Li JG(李建国);  Yu G(俞刚);  Zhang XY(张新宇);  Huang QS
View  |  Adobe PDF(519Kb)  |  Favorite  |  View/Download：309/157  |  Submit date：2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors