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Associate Professor
Supervisor of Doctorate Candidates
Supervisor of Master's Candidates
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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)