个人简历

教育经历\r
2006.9 -- 2012.6 北京航空航天大学 动力工程及工程热物理-热能工程 博士研究生毕业 工学博士学位\r
2000.9 -- 2004.6 北京航空航天大学 动力工程及工程热物理-热能工程 研究生在读 工学学士学位\r
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工作经历\r
2019.10 -- 至今 北京航空航天大学 航空发动机研究院 副研究员\r
2015.6 -- 2019.9 北京航空航天大学 能源与动力工程学院 讲师\r
2012.6 -- 2015.6 北京航空航天大学 航空宇航博士后流动站 博士后

研究领域

燃烧室结构，低污染燃烧技术，驻涡燃烧技术，高温升燃烧技术，涡轮级间燃烧技术，新型替代燃料""

近期论文

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, IF 8.035)\r
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Yang Xingyu, Fan Weijun, Zhang Rongchun*. Experimental investigations on fuel spatial distribution characteristics of aeroengine afterburner with all typical components. Fuel, 2023. SCI(Q1, IF 8.035)\r
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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, IF 4.98)\r
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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, IF 8.857)\r
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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, IF 6.465)\r
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Zhao Wensheng, Fan Weijun, Zhang Rongchun*. Experimental study on flow field characteristics of TBCC multibypass combustor, Aerospace Science and Technology, 2023. SCI(Q1, IF 5.457)\r
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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, IF 5.457)\r
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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, IF 8.035)\r
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Yan Peiliang, Fan Weijun, Qi Shuchan, Zhang Rongchun*, Liu Jie, Bai Naijian, Zhao Wensheng, Yang Xingyu. Numerical investigation on the effect of g-load on high-g ultra-compact combustor. Aerospace Science and Technology, 2022, 121. SCI(Q1, IF 5.457)\r
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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, IF 8.857)\r
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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, IF 8.857)\r
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Zhang Rongchun, Hao Fang, Fan Weijun*. Combustion and stability characteristics of ultra-compact combustor using cavity for gas turbines. Applied Energy, 2018. SCI (Q1, IF 11.446)\r
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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, IF 8.857)\r
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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, IF 8.857)