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基本信息 The basic information
姓名: 李江

学院: 航天学院


学历: 博士研究生毕业

学位: 工学博士


职称: 教授

职务:


学科: 航空宇航科学-航空宇航推进理论与工程,动力工程及工程热物理-工程热物理


邮箱: lijiang@nwpu.edu.cn




教育经历 Education Experience
1989-1993，西北工业大学，火箭发动机，本科
1993-1998，西北工业大学，航空宇航推进理论与工程，博士




工作经历 Work Experience
1998-2001，中国科学院力学研究所，博士后
2001-2003，西北工业大学，二站博士后
2002至今，西北工业大学航天学院，教师



教育教学 Education And Teaching
主讲本科生课“测试技术”，讲授本科生课“发动机热防护基础”，主讲博士生课“高等计算流体力学”。
主要研究方向：
1. 发动机烧蚀与热结构
2. 新型纳米绝热材料
3. 空气涡轮火箭（ATR）
4. 固体变推力发动机



招生信息 Admission Information
飞行器动力工程，航空宇航推进理论与工程；
动力工程及工程热物理；
材料或化工类专业，对热防护材料研究有兴趣。



荣誉获奖 Awards Information
1. 国家技术发明二等奖，2011，第二
2. 国防科技进步一等奖，2012，第五
3. 国防科技进步二等奖，2009，第八



学术成果 Academic Achievements
1. Li, J., Xi, K., et al (2018). Characteristics and formation mechanism of compact/porous structures in char layers of EPDM insulation materials. Carbon, 127, 498–509.
2. Guo M.F., Li J., et al (2020). Effects of multi-walled carbon nanotubes on char residue and carbothermal reduction reaction in ethylene propylene diene monomer composites at high temperature. Composites Science and Technology, 186, 107916.
3. Li, J., Ma, K., et al (2019). Combustion characteristics of solid propellants under high-temperature dense-particle erosion conditions. Combustion and Flame, 204, 49–57.
4. Li, J., Liu, K., et al (2018). Ablation and erosion characteristics of EPDM composites under SRM operating conditions. Composites Part A, 109, 392–401.
5. Ma, K., Li J., et al (2020). Experimental study on evolution characteristics of plane subsonic-supersonic shear layer. Aerospace Science and Technology, 100, 105791.
6. Li, J., Zhu, G., et al (2019). Experimental investigation on upstream fuel injection technique of RBCC scramjet mode. Applied Thermal Engineering, 154, 450–457.
7. Li J., Zhu, G., et al (2020). Simulated experiment on case overheating failure of solid rocket motor under flight overload condition. Applied Thermal Engineering, 172, 115135.
8. Li, J., Liu, K., et al (2018). Concept and performance study of turbocharged solid propellant ramjet. Acta Astronautica, 147, 431–444.
9. Li, J., Guo, M.F., et al (2018). Erosion characteristics of ethylene propylene diene monomer composite insulation by high-temperature dense particles. Acta Astronautica, 145, 293–303.
10. Li, J., Ma, K., et al (2019). Experimental study on erosion characteristics of char layer of EPDM composite by cold flow. Acta Astronautica, 157, 332–340.
11. Li, J., Liu, K., et al (2018). Combustion Characteristics Experimental Study of Solid Hydrocarbon Propellant for Air-Turbo Rocket. Journal of Propulsion and Power, 34, 1198–1205.
12. Guan, Y.W., Li, J., et al (2018). Reaction kinetics and a physical model of the charring layer by depositing Al2O3 at ultra-high temperatures. Physical Chemistry Chemical Physics, 20, 24418–24426.
13. Xi, K., Li, J., et al (2019). Redeposition and densification of pyrolysis products of polymer composites in char layer. Polymer Degradation and Stability, 166, 238–247.
14. Xi, K., Li, J., et al (2020). Characteristics of chemical vapour deposition in micro pore structure in char layer of polymer composites. Polymer Degradation and Stability, 178, 109222.
15. Ma, K., Li, J., et al (2020). Numerical and experimental investigation of the geometrical scale effect on a confined subsonic-supersonic shear layer. Acta Astronautica, 173, 212–220.
16. Guo, M.F., Li, J., et al (2019). Effect of multi-walled carbon nanotubes on thermal stability and ablation properties of EPDM insulation materials for solid rocket motors. Acta Astronautica, 159, 508–516.
17. Guan, Y.W. Li, J., et al (2018). Influence of different propellant systems on ablation of EPDM insulators in overload state. Acta Astronautica, 145, 141–152.
18. Liu, S.C., Li, J., (2018). Mixing and combustion enhancement of Turbocharged Solid Propellant Ramjet. Acta Astronautica, 143, 193–202.
19. Guan, Y.W. Li, J., et al (2017). Ablation characteristics and reaction mechanism of insulation materials under slag deposition condition. Acta Astronautica, 136, 80–89.
20. Zhang, S.K., Li, J., et al (2016). Numerical investigation of combustion field of hypervelocity scramjet engine. Acta Astronautica, 129, 357-366.
21. Wang, Y.J., Li, J., et al (2015). Study of thermal throat of RBCC combustor based on one-dimensional analysis. Acta Astronautica, 117, 130-141.
22. 李江，郭梦飞等 (2019). 固体发动机绝热材料烧蚀研究进展. 宇航学报，40(10)，1146-1156.
23. 刘凯，李江等 (2018). 涡轮增压固冲发动机（TSPR）爬升方案与性能研究. 推进技术，39(3)，494-500.





社会兼职 Social Appointments
1. 宇航学会会员
2. 航空学会会员



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