宋佳文

个人简介 宋佳文，博士，中南大学航空航天工程系副研究员，主要从事空天飞行器、发动机热结构分析与设计研究，研究兴趣包括推进剂混合燃烧、燃烧室耦合传热、主动冷却结构寿命预估。主持1XX工程课题1项，参与完成基础加强项目1项、XX预研项目1项，在Energy、Fuel、Applied Thermal Engineering、Aerospace Science and Technology、Chinese Journal of Aeronautics等期刊发表学术论文20余篇。 第一作者或通讯作者论文 [1] Feng Y, Luo S, Song J, 等. Numerical investigation on the combustion characteristics of powder fuel under different regulation parameters[J]. Aerospace Science and Technology, 2023, 142: 108608. [2] Luo S, Sun Y, Liu J, 等. Status and trends in development of hypersonic integration configuration with dorsal intake[J]. Aerospace Science and Technology, 2023, 139: 108369. [3] Luo S, Sun Y, Liu J, 等. Basic static stability and control characteristics of hypersonic vehicles with dorsal and ventral intake[J]. Aerospace Science and Technology, 2023, 134: 108159. [4] Feng Y, Luo S, Song J, 等. Numerical investigation on the combustion characteristics of aluminum powder fuel in a supersonic cavity-based combustor[J]. Applied Thermal Engineering, 2023, 221: 119842. [5] Feng Y, Luo S, Song J, 等. Numerical investigation on flow and mixing characteristics of powder fuel under strong shear and shock wave interaction[J]. Energy, 2023, 263: 126061. [6] 廖俊, 夏琨雄, 宋佳文, 等. 粉末燃料典型流化装置流量调节对流化的影响[J]. 推进技术, 2023: 1–17. [7] Luo S, Sun Y, Liu J, 等. Performance analysis of the hypersonic vehicle with dorsal and ventral intake[J]. Aerospace Science and Technology, 2022, 131: 107964. [8] Xu D, Luo S, Yang M, 等. Inlet layout effects on the mixing performance with a novel mixing evaluation in a powder-fueled ramjet[J]. Fuel, 2022, 327: 125145. [9] Liao J, Xia K, Song J, 等. Influence of structural parameters on fluidization effect of typical fluidization unit of metal powder fuel[J]. Advanced Powder Technology, 2022, 33(11): 103790. [10] Xu D, Luo S, Song J, 等. Effects of injection angle and injector mode variation on the fluidization performance of a powder-fueled ramjet[J]. Aerospace Science and Technology, 2022, 129: 107827. [11] Song J, Yuan Y, Liu J, 等. Heat Transfer Enhancement of Regenerative Cooling Channel with Pyramid Lattice Sandwich Structures[J]. Heat Transfer Engineering, Taylor & Francis, 2022, 0(0): 1–15. [12] Luo S, Feng Y, Song J, 等. Powder fuel transport process and mixing characteristics in cavity-based supersonic combustor with different injection schemes[J]. Aerospace Science and Technology, 2022, 128: 107798. [13] Luo S, Feng Y, Song J, 等. Progress and challenges in exploration of powder fueled ramjets[J]. Applied Thermal Engineering, 2022, 213: Numerical investigation on flow and mixing characteristics of powder fuel under strong shear and shock wave interaction. [14] Luo S, Sun Y, Song J, 等. Performance analysis of a hybrid pulse detonation engine using liquid hydrogen as fuel[J]. International Journal of Hydrogen Energy, 2022, 47(50): 21537–21551. [15] 罗世彬, 庙智超, 宋佳文. 高超声速飞行器前缘主动冷却影响因素[J]. 航空学报, 2022, 43(12): 627023–627023. [16] Song J, Sun B, Xing Y. Thermo-structural behavior of thermal barrier coatings for thrust chamber applications[J]. International Communications in Heat and Mass Transfer, 2022, 130: 105776. [17] Luo S, Xu D, Song J, 等. A review of regenerative cooling technologies for scramjets[J]. Applied Thermal Engineering, 2021, 190: 116754. [18] Xu D, Luo S, Song J, 等. Direct numerical simulations of supersonic compression-expansion slope with a multi-GPU parallel algorithm[J]. Acta Astronautica, 2021, 179: 20–32. [19] Luo S, Miao Z, Liu J, 等. Effects of Coolants of Double Layer Transpiration Cooling System in the Leading Edge of a Hypersonic Vehicle[J]. Frontiers in Energy Research, 2021, 9: 530. [20] 袁运飞, 廖俊, 宋佳文, 等. 点阵夹芯主动冷却结构发展现状与展望[J]. 航空工程进展, 2021, 12(06): 13–25. [21] Liu D, Sun B, Wang T, 等. Thermo-structural analysis of regenerative cooling thrust chamber cylinder segment based on experimental data[J]. Chinese Journal of Aeronautics, 2020, 33(1): 102–115. [22] Liu D, Sun B, Song J, 等. Effects of thermal and pressure loads on structural deformation of liquid oxygen/methane engine combustion chamber[J]. Journal of Thermal Science and Technology, Tokyo: Japan Soc Mechanical Engineers, 2020, 15(3): 19–590. [23] Song J, Sun B. Damage localization effects of the regeneratively-cooled thrust chamber wall in LOX/methane rocket engines[J]. Chinese Journal of Aeronautics, 2018, 31(8): 1667–1678. [24] 邢昱阳, 孙冰, 宋佳文. 再生冷却推力室热障涂层系统的热结构分析[J]. 推进技术, 2018, 39(02): 380–387. [25] SONG J, SUN B. Thermal-structural analysis of regeneratively-cooled thrust chamber wall in reusable LOX/Methane rocket engines[J]. Chinese Journal of Aeronautics, 2017, 30(3): 1043–1053. [26] Song J, Sun B. Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors[J]. Acta Astronautica, 2017, 132: 150–160. [27] Song J, Sun B. Coupled numerical simulation of combustion and regenerative cooling in LOX/Methane rocket engines[J]. Applied Thermal Engineering, 2016, 106: 762–773. [28] 孙冰, 宋佳文. 液氧甲烷发动机台阶型冷却通道的耦合传热特性[J]. 航空动力学报, 2016(12): 2972–2978. [29] 孙冰, 宋佳文. 液体火箭发动机推力室壁瞬态加载三维热结构分析[J]. 推进技术, 2016(07): 1328–1333. 教育经历 [1]   2013.9-2018.7 北京航空航天大学 工学博士学位  |  博士研究生毕业 [2]   2008.9-2012.7 北京航空航天大学 工学学士学位  |  大学本科毕业 研究方向 [1]  气固两相射流与超声速气流混合机理 [2]  发动机复杂多相流动加速数值模拟方法 其他联系方式 [6]  邮箱： songjiawen@csu.edu.cn