Associate researcher
Supervisor of Master's Candidates
Date of Employment:2020-06-05
School/Department:Research Institute of Aerospace Technology
Administrative Position:副研究员
Education Level:Postgraduate (Doctoral)
Business Address:升华楼708
Sex:Male
Contact Information:songjiawen@csu.edu.cn
Degree:Doctoral degree
Status:Employed
Alma Mater:北京航空航天大学
Discipline:Aerospace Science and Technology
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。
[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.
