Design and loss mechanisms analysis of supersonic turbine in turbopump applicationAerospace Science and TechnologyIF5.82026-01-170PRE
A simplified numerical method based on anisotropic porous media model for the precooler of the hypersonic precooled engineAPPLIED THERMAL ENGINEERINGIF6.92024-09-012PRE
Optimization strategies for the design of pre-cooler based on the synergistic air-breathing rocket engineCASE STUDIES IN THERMAL ENGINEERINGIF6.42024-08-010OAAI
Influence of geometric parameters on aerodynamic characteristics of serpentine convergent-divergent nozzleCHINESE JOURNAL OF AERONAUTICSIF5.72024-07-011OAAI
Thermodynamic analysis of key parameters on the performance of air breathing pre-cooled engine吸气预冷发动机关键参数对性能影响的热力学分析APPLIED THERMAL ENGINEERINGIF6.92022-01-0117PRE
个人简介
教育背景
工作经历
荣誉奖项
未登录.png){kind=icon}
未登录个人简介教育背景工作经历荣誉奖项