|
个人信息Personal Information
副教授 硕士生导师
招生学科专业：
航空宇航科学与技术 -- 【招收硕士研究生】 -- 能源与动力学院
能源动力 -- 【招收硕士研究生】 -- 能源与动力学院
性别：男
毕业院校：南京航空航天大学
学历：博士研究生毕业
学位：工学博士学位
所在单位：能源与动力学院
办公地点：A10-626
电子邮箱：
扫描关注
- [1]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 Pro....[J]:Aerospace,2022,9(685)
- [2]Jun Liu,Huacheng Yuan,Jingzhe Chen.Reynolds number effect on aerodynamic and starting charac-teristics of a two dimensional hyperson....[J]:Aerospace,2022,9(811)
- [3]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
- [4]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
- [5]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 Inl...:INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES,2017
- [6]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
- [7]袁化成,袁化成,刘君,葛宁.The flowfield and performance analyses of turbine-based combined cycle inlet mode transition at c...:AEROSPACE SCIENCE AND TECHNOLOGY,2017
- [8]袁化成,袁化成,陈文芳,刘君,华正旭.基于圆锥截线的高超前体气动设计及特性分析:推进技术,2017
- [9]袁化成,袁化成,刘君,华正旭,陈文芳,葛宁.Preliminary research of terminal shock motion in tandem configuration turbine-based combined cycl...:Aeronautical Journal,2017
- [10]袁化成,袁化成,刘君,葛宁.Turbine based combined cycle inlet mode transition at different operation conditions:Int. Space Planes Hypersonics Technol. Conf.,2017
- [11]袁化成,袁化成,陈文芳,华正旭,刘君.Investigations on flow characteristics of forebody based on spanwise pressure control:Tuijin Jishu,2017
- [12]袁化成,袁化成,王云飞,刘君,华正旭.Aerodynamic design and performance analysis of a two-dimensional variable geometry inlet:Int. Space Planes Hypersonics Technol. Conf.,2017
- [13]袁化成,袁化成,刘君,华正旭,陈文芳,葛宁.Experimental and numerical investigation of smooth turbine-based combined-cycle inlet mode transi...:AEROSPACE SCIENCE AND TECHNOLOGY,2017
- [14]刘君,袁化成.内并联式TBCC进气道模态转换过程流动特性分析:宇航学报,2016
| |