袁化成
个人信息Personal Information
教授 博士生导师
招生学科专业:
动力工程及工程热物理 -- 【招收硕士研究生】 -- 能源与动力学院
航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 能源与动力学院
能源动力 -- 【招收博士、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:南京航空航天大学
学位:工学博士学位
所在单位:能源与动力学院
办公地点:A10-634
电子邮箱:
扫描关注
- [1]袁化成,袁化成.Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC:International Journal of turbo & jet engines,2021
- [2]袁化成,袁化成.一种小长高比组合发动机喷管气动设计及性能分析:实验流体力学,2020
- [3]袁化成,.几何参数对S弯进气道气动特性的影响研究:机械制造与自动化,2020
- [4]袁化成,.一种二元混压式可调进气道的抽吸影响规律研究及方案设计:重庆理工大学学报(自然科学),2020
- [5]袁化成,.一种小长高比组合发动机喷管气动设计及性能分析:实验流体力学,2020
- [6]袁化成,袁化成,Zhang, Jin-Sheng,Lu, Jie,黄国平.Effects of Wall Roughness on Aerodynamic Performance of Hypersonic Inlet:Tuijin Jishu,2018
- [7]袁化成,袁化成,李蔚霆,郭荣伟.一种曲面压缩的定几何宽速域进气道设计研究:机械制造与自动化,2019
- [8]袁化成,袁化成,陈文芳,刘君,华正旭.Design and Performance Analysis of Hypersonic Forebody Based on Conic Section:Tuijin Jishu,2017
- [9]袁化成,袁化成,华正旭,王金刚,陈文芳.Effects of Swept Lip on Starting Characteristics of 2-D Hypersonic Inlet:Tuijin Jishu,2017
- [10]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
- [11]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
- [12]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
- [13]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
- [14]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
- [15]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
- [16]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
- [17]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
- [18]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
- [19]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
- [20]袁化成,.Unsteady supercritical/critical dual flowpath inlet flow and its control methods:CHINESE JOURNAL OF AERONAUTICS,2017