Comparison of different lobe-injectors on fuel mixing characteristics of single jet at the supersonic combustion chamber

被引：0
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作者：
Fan, Guangli [1 ]
Anjal, Hassan Abdulwahab [2 ]
Qahiti, Raed [3 ]
Abu-Hamdeh, Nidal H. [4 ]
Abusorrah, Abdullah M. [5 ]
Xu, Jin [1 ]
Zhang, Hailong [1 ]
Li, Zhixiong [6 ]
机构：
[1] Xijing University, Xi'an,Shaanxi,710123, China
[2] College of Engineering, Petroleum Engineering Department, Knowledge University, kurdistan Region, Iraq
[3] Department of Mathematics, Faculty of Science, Jazan University, Saudi Arabia
[4] Center of Research Excellence in Renewable Energy and Power Systems, Department of Mechanical Engineering, Faculty of Engineering, K. A. CARE Energy Research and Innovation Center, King Abdulaziz University, Jeddah, Saudi Arabia
[5] Center of Research Excellence in Renewable Energy and Power Systems, Department of Electrical and Computer Engineering, Faculty of Engineering, K. A. CARE Energy Research and Innovation Center, King Abdulaziz University, Jeddah, Saudi Arabia
[6] Yonsei Frontier Lab, Yonsei University, 50 Yonsei-ro, Seodaemun-gu,Seoul,03722, Korea, Republic of
来源：
Aerospace Science and Technology | 2021年 / 119卷
关键词：
Compendex;
D O I：
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摘要：
Orifices - Air - Fuels - Supersonic aerodynamics - Ramjet engines - Residence time distribution - Hydrogen - Mixing - Efficiency - Computational fluid dynamics
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