(1) 2011-9至2017-11, 南京理工大学, 航空宇航推进理论与工程, 博士, 导师: 韩珺礼 周长省
(2) 2017-1至2017-8, 美国范德堡大学, 流体力学, 联合培养博士生, 导师:Haoxiang Luo
(3) 2007-9至2011-6, 南京理工大学, 武器系统与工程, 学士
Li, Yingkun; Luo, Haoxiang; Chen, Honggang. Fluid–structure coupled simulation of ignition transient in a dual pulse motor using overset grid method, Acta Astronautica, 2021,183: 211–226
Li, Yingkun; Luo, Haoxiang; Chen, Xiong; Xu, Jinsheng; Laminar boundary layer separation over a fluttering panel induced by an oblique shock wave , Journal of Fluids and Structures, 2019, 90: 90-109.
Li, Chunlei; Chen, Xiong; Li, Yingkun*; Musa, Omer; Zhu, Liang; Numeric al investigation on the performance of scramjet combustor with a novel strut configuration , Applied Thermal Engineering, 2019, 159(113): 894-906.
Musa, O.; Chen, Xiong.; Li, Yingkun *.; Li, W.; Liao, W. Unsteady Simulation of Ignition of Turbulent Reactive Swirling Flow of Novel Design of Solid-Fuel Ramjet Motor. Energies 2019, 12, 2513.
Li Yingkun; Chen Xiong; Xu Jinsheng; Zhou Changsheng; Musa Omer; Three dimensional multi-physics coupled simulation of ignition transient in a dual pulse solid rocket motor , Acta Astronautica, 2018, 146: 46-65.
Li Yingkun; Han Jun li; Chen Xiong; Liu Rui; Xu Jin sheng; Numerical study of the internal flow field of a dual pulse solid rocket motor including conjugate heat transfer , Proceedings of the Institution of Mechanical Engineers - Part G: Journal of Aerospace Engineering, 2017, 231(8):1535-1549.
李映坤; 陈雄; 许进升; 基于流固耦合的斜激波冲击作用下曲壁板气动弹性分析, 航空动力学报, 2020, 35(4): 783-792.
李映坤, 韩珺礼, 陈雄, 鞠玉涛. 基于多物理场耦合的双脉冲发动机点火过程数值模拟[J]. 航空学报, 2017, 38(4): 75-86.
李映坤, 韩珺礼, 陈雄, 刘锐. 级间通道构型对双脉冲发动机燃烧室局部受热的影响[J]. 推进技术, 2014,35(11):1503-1510.
李映坤, 韩珺礼, 陈雄, 沈振华. 基于SST湍流模型的模拟SRM内流场数值仿真[J]. 固体火箭技术, 2014,37(5):616-621.
李映坤, 韩珺礼, 陈雄, 周长省, 巩伦昆. 基于嵌套网格的脉冲发动机喷管内流场数值模拟[J]. 固体火箭技术, 2014,37(2):178-183.