宋佳文

副教授 博士生导师 硕士生导师

入职时间：2020-06-05

所在单位：航空航天技术研究院

职务：副教授

学历：研究生(博士)毕业

办公地点：升华后楼711

性别：男

联系方式：songjiawen@csu.edu.cn

学位：博士学位

在职信息：在职

毕业院校：北京航空航天大学

学科：机械工程
航空宇航科学与技术

同专业博导    同专业硕导
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个人简介

宋佳文，1990年6月生，湖南常德人，中共党员，现为中南大学航空航天技术研究院副教授，博士生导师。主要从事空天飞行器、发动机热结构分析与设计研究，研究方向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。主持国家某重大工程课题1项，主持和参与某部委、航天一院、航天三院、航天四院、沈阳飞机设计研究所、中国空气动力研究与发展中心、国防科技大学、西北工业大学等科研项目20余项。以第一作者或通讯作者身份在Energy、Fuel、Applied Thermal Engineering、Aerospace Science and Technology、Chinese Journal of Aeronautics等期刊发表SCI论文20余篇。授权发明专利4项，其中国际专利1项。指导本科生获第四届全国高校航空航天类专业本科毕业设计成果交流会一等奖，指导研究生获第九届中国研究生未来飞行器创新大赛一等奖。


第一作者或通讯作者论文

[1] LUO S, TANG Z, SONG J, 等. Transient numerical investigation on coupled heat transfer of regenerative cooling channels with typical lattice sandwich structures[J/OL]. International Communications in Heat and Mass Transfer, 2025, 169: 109751. DOI:10.1016/j.icheatmasstransfer.2025.109751.

[2] 罗世彬, 郑盛贤, 刘俊, 等. 宽速域高超声速可调进气道研究进展[J/OL]. 空天技术, 2025(1): 1-19. DOI:10.16338/j.issn.2097-0714.20240108.

[3] 罗世彬, 冯彦斌, 刘俊, 等. 航空航天卓越工程师校企深度融合培养模式[C/OL]//第六届全国高等学校航空航天类专业教育教学研讨会. 中国浙江杭州, 2024: 822-829[2025-11-07]. https://doi.org/10.26914/c.cnkihy.2024.088953. DOI:10.26914/c.cnkihy.2024.088953.

[4] 冯彦斌, 罗世彬, 宋佳文, 等. 航空航天工程专业多元化思政教育模式探索[C/OL]//第六届全国高等学校航空航天类专业教育教学研讨会. 中国浙江杭州, 2024: 162-167[2025-11-07]. https://doi.org/10.26914/c.cnkihy.2024.088844. DOI:10.26914/c.cnkihy.2024.088844.

[5] LUO S, SUN Y, LIU J, 等. Research status and development trend of air-breathing high-speed vehicle/engine integration[J/OL]. Aerospace Science and Technology, 2024, 155: 109675. DOI:10.1016/j.ast.2024.109675.

[6] 罗世彬, 岳航, 刘俊, 等. 高超声速变体飞行器宽速域气动特性研究（英文）[J/OL]. Transactions of Nanjing University of Aeronautics and Astronautics, 2024, 41(2): 184-201. DOI:10.16356/j.1005-1120.2024.02.005.

[7] 刘俊, 任杰, 赤丰华, 等. 局部外形参数对高速飞行器的rcs影响[J]. 系统工程与电子技术, 2024, 46(11): 3690-3702.

[8] 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/OL]. 推进技术, 2024, 45(4): 116-129. DOI:10.13675/j.cnki.tjjs.2209059.

[9] 雷超, 刘江, 宋佳文. 矩阵乘法的gpu并行计算时耗模型与最优配置方法[J]. 计算机科学, 2024, 51(S1): 822-829.

[10] YANBIN FENG, SHIBIN LUO, JIAWEN SONG, 等. Numerical investigation on the combustion characteristics of powder fuel under different regulation parameters[J/OL]. Aerospace Science and Technology, 2023, 142: 108608. DOI:10.1016/j.ast.2023.108608.

[11] SHIBIN LUO, YUHANG SUN, JUN LIU, 等. Status and trends in development of hypersonic integration configuration with dorsal intake[J/OL]. Aerospace Science and Technology, 2023, 139: 108369. DOI:10.1016/j.ast.2023.108369.

[12] SHIBIN LUO, YUHANG SUN, JUN LIU, 等. Basic static stability and control characteristics of hypersonic vehicles with dorsal and ventral intake[J/OL]. Aerospace Science and Technology, 2023, 134: 108159. DOI:10.1016/j.ast.2023.108159.

[13] YANBIN FENG, SHIBIN LUO, JIAWEN SONG, 等. Numerical investigation on the combustion characteristics of aluminum powder fuel in a supersonic cavity-based combustor[J/OL]. Applied Thermal Engineering, 2023, 221: 119842. DOI:10.1016/j.applthermaleng.2022.119842.

[14] YANBIN FENG, SHIBIN LUO, JIAWEN SONG, 等. Numerical investigation on flow and mixing characteristics of powder fuel under strong shear and shock wave interaction[J/OL]. Energy, 2023, 263: 126061. DOI:10.1016/j.energy.2022.126061.

[15] SHIBIN LUO, YUHANG SUN, JUN LIU, 等. Performance analysis of the hypersonic vehicle with dorsal and ventral intake[J/OL]. Aerospace Science and Technology, 2022, 131: 107964. DOI:10.1016/j.ast.2022.107964.

[16] JUN LIAO, KUNXIONG XIA, JIAWEN SONG, 等. Influence of structural parameters on fluidization effect of typical fluidization unit of metal powder fuel[J/OL]. Advanced Powder Technology, 2022, 33(11): 103790. DOI:10.1016/j.apt.2022.103790.

[17] DEQUAN XU, SHIBIN LUO, MIAO YANG, 等. Inlet layout effects on the mixing performance with a novel mixing evaluation in a powder-fueled ramjet[J/OL]. Fuel, 2022, 327: 125145. DOI:10.1016/j.fuel.2022.125145.

[18] DEQUAN XU, SHIBIN LUO, JIAWEN SONG, 等. Effects of injection angle and injector mode variation on the fluidization performance of a powder-fueled ramjet[J/OL]. Aerospace Science and Technology, 2022, 129: 107827. DOI:10.1016/j.ast.2022.107827.

[19] JIAWEN SONG, YUNFEI YUAN, JIAN LIU, 等. Heat Transfer Enhancement of Regenerative Cooling Channel with Pyramid Lattice Sandwich Structures[J/OL]. Heat Transfer Engineering, 2022, 0(0): 1-15. DOI:10.1080/01457632.2022.2127049.

[20] SHIBIN LUO, YANBIN FENG, JIAWEN SONG, 等. Powder fuel transport process and mixing characteristics in cavity-based supersonic combustor with different injection schemes[J/OL]. Aerospace Science and Technology, 2022, 128: 107798. DOI:10.1016/j.ast.2022.107798.

[21] SHIBIN LUO, YANBIN FENG, JIAWEN SONG, 等. Progress and challenges in exploration of powder fueled ramjets[J/OL]. Applied Thermal Engineering, 2022, 213: Numerical investigation on flow and mixing characteristics of powder fuel under strong shear and shock wave interaction. DOI:10.1016/j.applthermaleng.2022.118776.

[22] SHIBIN LUO, YUHANG SUN, JIAWEN SONG, 等. Performance analysis of a hybrid pulse detonation engine using liquid hydrogen as fuel[J/OL]. International Journal of Hydrogen Energy, 2022, 47(50): 21537-21551. DOI:10.1016/j.ijhydene.2022.04.278.

[23] JIAWEN SONG, BING SUN, YUYANG XING. Thermo-structural behavior of thermal barrier coatings for thrust chamber applications[J/OL]. International Communications in Heat and Mass Transfer, 2022, 130: 105776. DOI:10.1016/j.icheatmasstransfer.2021.105776.

[24] 罗世彬, 孙雨航, 刘俊, 等. 高超声速乘波前体/进气道一体化设计综述[J/OL]. 空天技术, 2022(6): 24-48. DOI:10.16338/j.issn.2097-0714.20220146.

[25] 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): 7-17.

[26] LIU J, XU M, XI W, 等. Numerical investigations of endwall film cooling design of a turbine vane using four-holes pattern[J/OL]. International Journal of Numerical Methods for Heat & Fluid Flow, 2021, 32(6): 2177-2197. DOI:10.1108/HFF-12-2020-0804.

[27] SHIBIN LUO, DEQUAN XU, JIAWEN SONG, 等. A review of regenerative cooling technologies for scramjets[J/OL]. Applied Thermal Engineering, 2021, 190: 116754. DOI:10.1016/j.applthermaleng.2021.116754.

[28] DEQUAN XU, SHIBIN LUO, JIAWEN SONG, 等. Direct numerical simulations of supersonic compression-expansion slope with a multi-GPU parallel algorithm[J/OL]. Acta Astronautica, 2021, 179: 20-32. DOI:10.1016/j.actaastro.2020.10.047.

[29] SHIBIN LUO, ZHICHAO MIAO, JIAN LIU, 等. Effects of Coolants of Double Layer Transpiration Cooling System in the Leading Edge of a Hypersonic Vehicle[J/OL]. Frontiers in Energy Research, 2021, 9: 530. DOI:10.3389/fenrg.2021.756820.

[30] 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/OL]. 航空工程进展, 2021, 12(06): 13-25. DOI:10.16615/j.cnki.1674-8190.2021.06.02.

[31] DI LIU, BING SUN, TAIPING WANG, 等. Thermo-structural analysis of regenerative cooling thrust chamber cylinder segment based on experimental data[J/OL]. Chinese Journal of Aeronautics, 2020, 33(1): 102-115. DOI:10.1016/j.cja.2019.09.023.

[32] DI LIU, BING SUN, JIAWEN SONG, 等. Effects of thermal and pressure loads on structural deformation of liquid oxygen/methane engine combustion chamber[J/OL]. Journal of Thermal Science and Technology, 2020, 15(3): 19-590. DOI:10.1299/jtst.2020jtst0022.

[33] JIAWEN SONG, BING SUN. Damage localization effects of the regeneratively-cooled thrust chamber wall in LOX/methane rocket engines[J/OL]. Chinese Journal of Aeronautics, 2018, 31(8): 1667-1678. DOI:10.1016/j.cja.2018.05.016.

[34] 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.

[35] JIAWEN SONG, BING SUN. Thermal-structural analysis of regeneratively-cooled thrust chamber wall in reusable LOX/Methane rocket engines[J/OL]. Chinese Journal of Aeronautics, 2017, 30(3): 1043-1053. DOI:10.1016/j.cja.2017.04.007.

[36] JIAWEN SONG, BING SUN. Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors[J/OL]. Acta Astronautica, 2017, 132: 150-160. DOI:10.1016/j.actaastro.2016.12.026.

[37] JIAWEN SONG, BING SUN. Coupled numerical simulation of combustion and regenerative cooling in LOX/Methane rocket engines[J/OL]. Applied Thermal Engineering, 2016, 106: 762-773. DOI:10.1016/j.applthermaleng.2016.05.130.

[38] 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.

[39] 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]  飞行器热结构与热防护

  • [2]  气固两相射流与超声速气流混合机理

  • [3]  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：