李祝飞 副教授 |
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个人简介：
李祝飞，1986年生，博士，副教授，博士生导师，“仲英青年学者”。长期从事高超声速空气动力学、激波干扰、激波风洞实验技术等方面的教学和科研工作。主持国家重大专项课题1项、国家自然科学基金项目3项、关键技术攻关项目4项、航空航天领域横向课题10余项；合著《高超声速流动中的激波及相互作用》；在Journal of Fluid Mechanics、Physics of Fluids、AIAA Journal、Chinese Journal of Aeronautics等国内外重要期刊发表论文60余篇；获得国家专利授权8项、软件著作权1项。现为中国空气动力学会理事、高超声速专业委员会委员、中国航天第三专业信息网进排气技术专业委员会委员，《空天技术》、《气动研究与试验》副主编，《实验流体力学》编委，《推进技术》青年编委。
教育经历：
2004—2008年，中国科学技术大学，近代力学系，获理学学士学位
2008—2013年，中国科学技术大学，近代力学系，获工学博士学位
工作经历：
2013—2016年，中国科学技术大学，博士后
2016—2020年，中国科学技术大学，特任副研究员
2020年4月至今，中国科学技术大学，近代力学系，副教授
主要研究方向:
面向国家航空航天重大科技工程中的关键科学与技术问题，开展空天飞行器内外流耦合复杂激波干扰机理与流动控制、气动力/热特性预测、先进流场观测方法等方面的研究工作。
近期代表性论著：
1. Huang Q, Hong YT, Li ZF. Scaling of Upstream Influence Line Induced by Shock Sweeping Concave Half-Cylinder. AIAA Journal, published online. https://doi.org/10.2514/1.J063924
2. Si DX, Li ZF.Kinks on elliptical convergent shock waves in hypersonic flow. Journal of Fluid Mechanics, 2023, 977: A12.https://doi.org/10.1017/jfm.2023.939
3. Zhou BK, Yi XY, Wang ZW, Li ZF. Aerothermal Heating Correlations at Stagnation Point/Line in Low-Enthalpy Hypersonic Flow. AIAA Journal, 2023, 61(3): 1435-1439. https://doi.org/10.2514/1.J062455
4. Ma YK, Li ZF, Yang JM. Planar laser scattering visualization of streamwise vortex pairs in a Mach 6 flow. Chinese Journal of Aeronautics, 2023, 36(1): 166–177. https://doi.org/10.1016/j.cja.2022.03.011
5. Ji JZ, Li ZF, Zhang EL, Si DX, Yang JM. Intensification of non-uniformity in convergent near-conical hypersonic flow. Journal of Fluid Mechanics, 2022, 931: A8. https://doi.org/10.1017/jfm.2021.943
6. Zhang YJ,Wang J, Li ZF. Shock-induced heating loads on V-shaped leading edges with elliptic cross section. AIAA Journal, 2022, 60(12): 6958-6962. https://doi.org/10.2514/1.J062013
7. Zhang ZY, Li ZF, Yang JM. Transitions of shock interactions on V-shaped blunt leading edges. Journal of Fluid Mechanics, 2021, 912: A12. https://doi.org/10.1017/jfm.2020.1117
8. Zhang EL, Li ZF, Ji JZ, Si DX, Yang JM. Converging near-elliptic shock waves. Journal of Fluid Mechanics, 2021, 909: A2. https://doi.org/10.1017/jfm.2020.910
9. Wang J, Li ZF, Yang JM. Shock-induced pressure/heating loads on V-shaped leading edges with nonuniform bluntness. AIAA Journal, 2021, 59(3): 1114-1118. https://doi.org/10.2514/1.J059990
10. Hong YT, Li ZF, Yang JM. Scaling of interaction lengths for hypersonic shock wave/turbulent boundary layer interactions. Chinese Journal of Aeronautics, 2021, 34(5): 504-509. https://doi.org/10.1016/j.cja.2020.12.028
11. Li YM, Li ZF, Yang JM. Tomography-like flow visualization of a hypersonic inward-turning inlet. Chinese Journal of Aeronautics, 2021, 34(1): 44-49. https://doi.org/10.1016/j.cja.2020.10.012
12. Wang J, Li ZF, Zhang ZY, Yang JM. Shock interactions on V-shaped blunt leading edges with various conic crotches. AIAA Journal, 2020, 58(3):1407-1411. https://doi.org/10.2514/1.J059067
13. Zhang ZY, Li ZF, Huang R, Yang JM. Experimental investigation of shock oscillations on V-shaped blunt leading edges. Physics of Fluids, 2019, 31(2): 026110. https://doi.org/10.1063/1.5084184
14. Zhang EL, Li ZF, Li YM, Yang JM. Three-dimensional shock interactions and vortices on a V-shaped blunt leading edge. Physics of Fluids, 2019, 31(8): 086102. https://doi.org/10.1063/1.5101031
15. Li ZF, Zhang ZY, Wang J, Yang JM. Pressure-heat flux correlations for shock interactions on V-shaped blunt leading edges. AIAA Journal, 2019, 57(10):4588-4592. https://doi.org/10.2514/1.J058538
16. Huang R, Li ZF, Yang JM. Engineering prediction of fluctuating pressure over incident shock/turbulent boundary-layer interactions. AIAA Journal, 2019, 57(5):2209-2213. https://doi.org/10.2514/1.J057903
17. Xiao FS, Li ZF, Zhang ZY, Zhu YJ, Yang JM. Hypersonic shock wave interactions on a V-shaped blunt leading edge. AIAA Journal, 2018, 56(1):356-367. https://doi.org/10.2514/1.J055915
18. Wang DX, Li ZF, Zhang ZY, Liu NS, Yang JM, Lu XY. Unsteady shock interactions on V-shaped blunt leading edges. Physics of Fluids, 2018, 30(11): 116104. https://doi.org/10.1063/1.5051012
19. Li ZF, Huang R, Li YM, Yang JM. Sliding-plug approach for inlet self-starting ability test in shock tunnel. AIAA Journal, 2018, 56(9):3785-3790. https://doi.org/10.2514/1.J056723
20. Zhan DW, Li ZF, Yang JT, Zhu YJ, Yang JM. A contraction channel design for planar shock wave enhancement. Review of Scientific Instruments. 2018, 89(5): 056104. https://doi.org/10.1063/1.5025223