张荣春，男，副研究员，博士生导师，高超声速强预冷空天动力团队成员。

        学科方向：热能工程、航空宇航推进理论与工程。

        研究方向：航空发动机/冲压发动机燃烧室设计。

        教育和工作经历：获北京航空航天大学热能工程学士学位和博士学位，2012年至2015年，为北京航空航天大学能源与动力工程学院博士后，2014年至2015年赴英国纽卡斯尔大学学术访问1年，2015年入职北航能源与动力工程学院，2019年转入北航航空发动机研究院。

        基础研究方面：针对燃烧室内气流流动过程、液体燃料雾化过程、液体燃料（航空煤油等）/气体燃料（氢、甲烷等）的燃烧过程，开展流动机理、雾化机理、燃烧机理等基础研究。

        应用研究方面：针对航空发动机主燃烧室/加力燃烧室/涡轮级间燃烧室、冲压发动机燃烧室、组合动力发动机燃烧室、氢燃料发动机燃烧室、高温升燃烧器，开展结构设计、性能分析等应用基础研究。

        研究平台：建成功能完善的航空发动机燃烧试验平台，具有大流量、高压/负压连续空气气源，配备先进光学测量设备，可开展航空发动机燃烧室流场、雾化、传热、燃烧等基础性试验及燃烧室部件试验，具备高温高压环境、负压环境、低温环境等模拟能力。

        主持国家重大专项重大项目课题、国家自然科学基金面上项目和青年项目、中国博士后科学基金特别资助项目和面上项目、航发集团项目、航天科技集团项目、航天科工集团项目等二十余项。

        在《Energy》，《Physics of Fluids》、《Aerospace Science and Technology》等重要学术刊物发表论文70余篇，申请/授权国家专利10余项，获全国创新争先奖（团队奖），部级三等奖（排名1），部级一等奖（排名6），入选北京航空航天大学青年拔尖人才支持计划。

        担任Q1区SCI期刊《Scientific Reports》编委， Q3区SCI期刊《International Journal of Aerospace Engineering》编委，《Frontiers in Mechanical Engineering》客座编委；为《Energy》、《Aerospace Science and Technology》、《Fuel》、《Energy&Fuels》、《Journal of Propulsion and Power》、《International Journal of Energy Research》等国际期刊审稿人、国家自然科学基金通讯评议专家、教育部学位与研究生教育发展中心通讯评议专家。

        主讲本科生数学基础课《计算方法》，本科生必修课《燃烧综合实验》、研究生专业基础课《热能利用与节能减排技术》，指导博士研究生、硕士研究生20余人，其中多人获国家奖学金等国家级或校级荣誉。

        课题组每年招收博士后1名、博士研究生1~2名、硕士研究生1~2名，欢迎加入!

        近期发表的代表性论文：

        [1] Yang Xingyu, Fan Weijun, Zhang Rongchun*. Experimental study of fuel distribution and combustion characteristics under subatmospheric pressure in an afterburner, Applied Thermal Engineering, 2025. SCI(Q1)

        [2] Wang Qian, Fan Weijun, Yi Jia, Xu Hanqing, Zhang Rongchun*. Effect of rear blunt body structure and inlet conditions on the flow and combustion characteristics of an advanced vortex combustor for a gas turbine, Applied Thermal Engineering, 2025. SCI(Q1)

        [3] Wang Qian, Fan Weijun, Zhang Rongchun*. Numerical study on the flow and combustion characteristics of an advanced vortex combustor fueled by liquid aviation kerosene, Aerospace Science and Technology, 2025. SCI(Q1)

        [4] Liu Fangbin, Zhang Rongchun*, Zheng Riheng*, Sun Qiang. Influence of injection positions on combustion performance in kerosene-fueled multi-cavity Scramjet combustor, Chinese Journal of Aeronautics, 2025. SCI(Q1)

        [5] Ren Dongliang, Fan Weijun, Zhang Rongchun*. A novel ultra-compact combustor with low flow resistance for the aero-engine, Applied Thermal Engineering, 2025. SCI(Q1)

        [6] Zhao Yulu, Fan Weijun, Zhang Rongchun*. Spray and flame characteristics of an ultra-compact combustor for gas turbines, Applied Thermal Engineering, 2024. SCI(Q1)

        [7] Zhao Yulu, Fan Weijun, Zhang Rongchun*. Study on the fuel/air mixing process in a compact combustor with uneven flame stabilizer wall, Aerospace Science and Technology, 2024. SCI(Q1)

        [8] Dang Zhanquan, Fan Weijun, Zhang Rongchun*. Experimental and numerical studies of the fuel concentration distribution within the near-wall area in a compact space for a gas turbine combustore. Energy, 2024. SCI(Q1)

        [9] Sun Ruzhou, Fan Weijun, Zhang Rongchun*. Influence of complex inlet conditions on the flow field and flow characteristics in compact combustor for gas turbine, Physics of Fluids, 2024. SCI (Q1)

        [10] Peng Jinlou, Fan Weijun, Zhang Rongchun*. A study on liquid film and evaporation characteristics of fuel jet impingement on the scorching wall of evaporation tube for gas turbine, Physics of Fluids, 2024. SCI (Q1)

        [11]  Zhao Wensheng, Fan Weijun, Zhang Rongchun*. Influence of a double-mixer configuration on the mixing and combustion characteristics of a multibypass combustor for a turbine-based combined cycle engine. Energy, 2024. SCI(Q1)

        [12]  Tan Tieyi, Fan Weijun, Zhang Rongchun*. A numerical and experimental investigation into the mixing mechanism of hydrogen transverse jets into an air swirl flow, Physics of Fluids, 2024. SCI (Q1)

        [13] Ren Dongliang, Fan Weijun, Zhang Rongchun*. Experimental and numerical study on flow mixing and combustion characteristics of a novel multibypass integrated combustor, Physics of Fluids, 2024. SCI (Q1)

        [14] Yang Xingyu, Fan Weijun, Zhang Rongchun*. Experimental study of the fuel spray and ignition characteristics in an aeroengine afterburner under subatmospheric pressure, Aerospace Science and Technology, 2024. SCI(Q1)

        [15] Zhao Wensheng, Fan Weijun, Zhang Rongchun*. Influence of nonuniform velocity and temperature inlet on the mixing characteristics of TBCC a multibypass combustor with a double-mixer configuration, Aerospace Science and Technology, 2024. SCI(Q1)

        [16] Bai Naijian, Fan Weijun, Zhang Rongchun*. A mixing enhancement mechanism for a hydrogen transverse jet coupled with a shear layer for gas turbine combustion, Physics of Fluids, 2023. SCI (Q1)

        [17] Yang Xingyu, Fan Weijun, Zhang Rongchun*. Experimental investigations on fuel spatial distribution characteristics of aeroengine afterburner with all typical components, Fuel, 2023. SCI(Q1)

        [18] Zhao Wensheng, Fan Weijun, Zhang Rongchun*. Study of the mixing characteristics of a multibypass combustor of a turbine-based combined cycle, Applied Thermal Engineering, 2023. SCI(Q1)

        [19] Zhao Yulu, Fan Weijun, Zhang Rongchun*. Experimental study on the effect of injection schemes on fuel spray and combustion characteristics in a compact combustor, Aerospace Science and Technology, 2023. SCI(Q1)

        [20] Zhao Wensheng, Fan Weijun, Zhang Rongchun*. Experimental study on flow field characteristics of TBCC multibypass combustor, Aerospace Science and Technology, 2023. SCI(Q1)

        [21] Zhao Yulu, Fan Weijun, Zhang Rongchun*. Influence of coupling schemes of radial and circumferential flame stabilization modes on flow and combustion characteristics of compact combustion for gas turbine, Fuel, 2023. SCI(Q1)
        [22] Tan Tieyi, Fan Weijun, Zhang Rongchun*. Study on hydrogen staged combustion for gas turbine, Fuel, 2023. SCI(Q1)

        [23] Yan Peiliang, Fan Weijun, Zhang Rongchun*. Predicting the NOx emissions of low heat value gas rich-quench-lean combustor via three integrated learning algorithms with Bayesian optimization, Energy, 2023. SCI (Q1)

        [24] Bai Naijian, Fan Weijun, Zhu Jiangnan, Miao Hui, Yang Xingyu, Zhao Yulu, Zhao Wensheng, Zhang Rongchun∗. Experimental investigations into the effusion plate wall temperature ofimpingement/effusion cooling systems for gas turbine combustors, Aerospace Science and Technology, 2023. SCI(Q1)

        [25] Yang Xingyu, Fan Weijun, Zhang Rongchun*. Experimental investigations on aviation kerosene multi-jets in high temperature and low pressure air crossflow, Fuel, 2022. SCI(Q1)

        [26] Yan Peiliang, Fan Weijun, Qi Shuchan, Zhang Rongchun*, et al. Numerical investigation on the effect of g-load on high-g ultra-compact combustor, Aerospace Science and Technology, 2022, 121. SCI(Q1)

        [27] Bai Naijian, Fan Weijun,  Zhang Rongchun*, et al. Numerical investigation into the structural characteristics of a hydrogen dual-swirl combustor with slight temperature rise combustion, International Journal of Hydrogen Energy, 2021. SCI (Q1)

        [28] Zhang Rongchun, Bai Naijian, Fan Weijun*, et al. Influence of flame stabilization and fuel injection modes on the flow and combustion,  characteristics of gas turbine combustor with cavity, Energy, 2019. SCI (Q1)

        [29] Zhang Rongchun*, Huang Xiaoyang, Fan Weijun*, et al. Influence of injection mode on the combustion characteristics of slight temperature rise combustion in gas turbine combustor with cavity, Energy, 2019. SCI (Q1)

        [30] Zhang Rongchun, Hao Fang, Fan Weijun*. Combustion and stability characteristics of ultra-compact combustor using cavity for gas turbines, Applied Energy, 2018. SCI (Q1)

        [31] Zhang Rongchun, Bai Naijian, Fan Weijun*, et al. Flow field and combustion characteristics of integrated combustion mode using cavity with low flow resistance for gas turbine engines, Energy, 2018. SCI (Q1)

        [32] Zhang Rongchun, Xu Quanyong*, Fan Weijun. Effect of swirl field on the fuel concentration distribution and combustion characteristics in gas turbine combustor with cavity, Energy, 2018. SCI (Q1)