专著：
[1] 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.
[2] Xie K , Chen X , Li J , et al. Fluid Nozzle Throats in Solid Rocket Motors[M],国防工业出版社,2020.
[3] 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] 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.
[2] 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.
[3] 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.
[4] 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.
[5] Han L, Li J*, Zhao D, et al. Study on combustion oscillation characteristics of micron aluminum particles[J]. Powder Technology, 2021, 394: 782-790.
[6] 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.
[7] 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.
[8] 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.
[9] 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. (封面论文)
[10] Song A, Wang N, Li J*, et al. Transient flow characteristics and performance of a solid rocket motor with a pintle valve[J]. Chinese Journal of Aeronautics, 2020, 33(12): 3189-205.
[11] 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.
[12] 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.
[13] 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.
[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] Chen X, Li J*, Feng M, et al. Effects of external heating on flame stability in a micro porous combustor fuelled with heptane[J]. Combustion Science & Technology, 2019:1-14.
[16] Chen X, Li J*, Feng M, et al. Flame stability and combustion characteristics of liquid fuel in a meso-scale burner with porous media[J]. Fuel, 2019, 251:249-259.
[17] 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，2021.(录用待发表)
[18] 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，2021.(录用待发表)
[19] 席运志, 王宁飞, 李军伟,等. 基于旋转阀的固体火箭发动机燃烧室压强振荡特性[J].兵工学报, 2021,42(01):33-44.
[20] 席运志, 李军伟, 陈雪莉,等. 基于旋转阀的固体推进剂压强耦合响应测试方法[J].兵工学报, 2021,42(03):511-20.
[21] 李军伟, 王茹瑶, 宋岸忱等. 丁羟四组元复合推进剂燃烧稳定性机理研究综述[J].火炸药学报， 2021,44(3):284-294.
[22] 王茹瑶, 徐博, 张焱, 李军伟,等. T型燃烧器杯型装药结构设计及试验异常分析[J/OL].固体火箭技术, 2021.(录用待发表)
[23] 黄刚, 李军伟, 王向港,等. 某型号固体火箭发动机高速旋转试验台设计[J].固体火箭技术, 2021,44(4):8.
[24] 马宝印, 李军伟, 张海龙,等. 阻尼环对固体火箭发动机热声振荡的影响[J].兵工学报,2021,42(05):930-943.
[25] 马宝印, 李军伟, 王兴起,等. 针栓变推力固体火箭发动机动态响应特性研究[J].推进技术, 2020,41(10):2161-2172.
