研究领域

• 1、组合动力进气道设计、数值仿真及试验

  2、飞/发一体化及变维度数值仿真方法

论文成果

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• 刘君,袁化成,袁化成,张锦昇,匡正.A Multifidelity Simulation Method for Internal and External Flow of a Hypersonic Airbreathing Propulsion System.[J]:Aerospace,2022,9(685)
• Jun Liu,Huacheng Yuan,Jingzhe Chen.Reynolds number effect on aerodynamic and starting charac-teristics of a two dimensional hypersonic inlet.[J]:Aerospace,2022,9(811)
• 刘君,,袁化成,陈文芳,郭荣伟.Investigation of translation scheme turbine-based combined-cycle inlet mode transition.[J].France:Aerospace Science and Technology,2021,116(2021):106894
• 袁化成,袁化成,刘君,郭荣伟.一种Ma0～4 TBCC进气道气动设计及性能分析:实验流体力学,2018
• 袁化成,袁化成,刘君,姚猛,葛宁.Numerical Simulation of Terminal Shock Oscillation in Over/Under Turbine-Based Combined-Cycle Inlet:INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES,2017
• 袁化成,袁化成,刘君,王云飞,葛宁.Unsteady supercritical/critical dual flowpath inlet flow and its control methods:CHINESE JOURNAL OF AERONAUTICS,2017

专利

• 刘君,袁化成,王云飞,刘甫州,李铮, 超声速进气道自适应试验节流系统及其控制方法
• 袁化成,刘君,张锦昇,李蔚霆,王云飞, 一种平动式内并联组合动力进气道模态转换装置及方法
• 刘君,袁化成,陈文芳,姚猛, 用于组合动力进气道模态转换试验的堵锥及试验装置
• 刘君,周珂玉,袁化成,许凌锋,李东, 一种单变量控制模态转换装置的组合动力进气道
• 刘君,许凌锋,袁化成,李铮,周珂玉, 一种并联式组合动力进气道的调节机构及设计方法

著作成果

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科研项目

• 适用于***航空发动机安装性能分析及进排气系统特性模拟研究,工信部,刘君,袁化成