专著：
[1]李军伟, 魏志军, 隋欣. 固体火箭发动机原理[M], 北京理工大学出版社, 2023.
[2]李军伟, 王宁飞. 固体火箭发动机燃烧不稳定产生机理及评估方法[M], 浙江大学出版社, 2021.
[3]Xie K , Chen X , Li J , et al. Fluid Nozzle Throats in Solid Rocket Motors[M], 国防工业出版社, 2020.
[4]谢侃, 李世鹏, 李军伟,等. 火箭发动机基础[M], 北京理工大学出版社, 2019.
论文：
[1] Chen X, Li J*, He X, et al. Experimental and numerical investigation on the performance of meso-scale burners with novel ordered porous media[J]. Applied Thermal Engineering, 2023, 233: 121103.
[2] Zhou X, Li J*, Chen X, et al. Effects of pulse power on evaporation characteristics of an n-heptane droplet in a microtube[J]. Applied Thermal Engineering, 2023, 120895.
[3] Gu X, Li J*, Han L, et al. Theoretical Study on Heating Process of Micro-Al Particles in Laminar Flame [J], Combustion science and technology, 2021.
[4] Han L, Li J*, Zhao D, et al. Effect analysis on energy conversion enhancement and NOx emission reduction of ammonia/hydrogen fuelled wavy micro-combustor for micro-thermophotovoltaic application[J]. Fuel, 2021, 289: 119755.
[5] Han L, Li J*, Zhao D, et al. Effects of baffle designs on damping acoustic oscillations in a solid rocket motor[J]. Aerospace Science and Technology, 2021, 115: 106827.
[6] Han L, Li J*, Zhao D, et al. Energy and exergy conversion enhancement of a premixed hydrogen-fuelled wavy-combustor for micro-thermophotovolatic application[J]. Applied Thermal Engineering, 2021, 196: 117328.
[7] Han L, Li J*, Zhao D, et al. Study on combustion oscillation characteristics of micron aluminum particles[J]. Powder Technology, 2021, 394: 782-790.
[8] Ma B, Li J*, Zhang Z, et al. Experimental and theoretical studies on thermoacoustic limit cycle oscillation in a simplified solid rocket motor using flat flame burner[J]. Acta Astronautica, 2021, 189: 26-42.
[9] Chen X, Li J*, Zhao D, et al. Effects of porous media on partially premixed combustion and heat transfer in meso-scale burners fuelled with ethanol[J]. Energy, 2021, 224: 120191.
[10] Chen X, Li J*, Zhao D, et al. Experimental investigation on propagation characteristics of n-heptane/air combustion wave in foamed porous media[J]. Fuel, 2021, 306: 121742.
[11] Song A, Qin Z, Li J*, et al. Real-time plume velocity measurement of solid propellant rocket motors using TDLAS technique[J]. Propellants, Explosives, Pyrotechnics, 2021, 46(4): 636-53.
[12] Rashid M, Li J*, Chen X, et al. Flow Boiling and Heat Transfer of N-heptane Flow in a Microtube Heated by Concurrent Microflame[J]. Combustion science & Technology, 2021: 1-29.
[13] Rashid M, Li J*, Chen X, et al. Numerical simulation of evaporation phenomena and heat transfer of liquid Hydrocarbon in a microtube[J]. International journal of Heat & Mass Transfer, 2021, 179: 121734.
[14] Xi Y, Wang N, Li J*, et al. Experimental and numerical study on pressure oscillation in a combustor with rotary valve[J]. Chinese Journal of Aeronautics, 2021, 34(5): 298-314.
[15] Xi Y, Wang N, Li J*, et al. Experimental and numerical study on measuring solid-propellant pressure-coupled response using an improved rotary valve[J]. Acta Astronautica, 2021, 180: 155-69.
[16] 李军伟, 王茹瑶, 陈国锋等. 固体火箭发动机声燃烧不稳定抑制方法综述[J]. 固体火箭技术, 2023, 46(01): 3-15.
[17] 曾佳进, 李军伟, 马宝印等. 火箭发动机燃烧室中燃烧噪声的计算模型[J]. 航空学报, 2023, 44(18): 61-74.
[18] 谭智杰, 李军伟, 张文昊等. 大长径比固体火箭发动机一阶纵向不稳定燃烧判据[J]. 固体火箭技术, 2023, 46(01): 25-31.
[19] 王茹瑶, 宋岸忱, 王立民等. 基于TDLAS技术的喉栓式变推力发动机羽流速度特性[J]. 航空学报, 2023, 44(17): 92-107.
[20] 李泓瑾, 李军伟, 谢侃等. 两相流对固体火箭发动机塞式喷管性能的影响[J]. 航空学报, 2023, 44(16): 27-38.
[21] 田忠亮, 李军伟, 黄刚等. 横向过载下固体火箭发动机内弹道特性研究[J]. 固体火箭技术, 2022, 45(04): 512-521.
[22] 周心远, 李军伟, 陈新建等. 脉冲热激励对液滴蒸发特性影响的实验研究[J]. 推进技术, 2022, 43(11): 226-240.
[23] 田忠亮, 李军伟, 贺业等. 横向过载下锥孔三维药柱的内弹道特性[J]. 兵工学报, 2023, 44(07): 1896-1907.
[24] 覃生福, 李军伟, 张智慧等. 旋转对固体火箭发动机两相流点火过程影响仿真研究[J]. 航空动力学报, 2022, 37(07): 1503-1515.
[25] 田忠亮, 李军伟, 贺业等. 动态横向过载对固体火箭发动机内弹道的影响[J]. 航空动力学报, 2023, 38(02): 504-512.
