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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:11/0  |  Submit date:2024/11/22
Scramjet  Pilot hydrogen  Dual cavities  Mixing efficiency  Combustion performance  
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:186/41  |  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:386/60  |  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:458/130  |  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:289/103  |  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:251/127  |  Submit date:2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors