 
            能源与动力学院
通讯地址:
个人邮箱:xiaojun.fan@just.edu.cn
邮政编码:226500
办公地点:长山校区能动楼211
传真:
范小军,男,工学博士研究生,现任 能动学院副教授;主持国家自然科学基金青年基金项目、江苏省自然科学基金青年项目、江苏省高等学校基础科学(自然科学)研究面上项目等科研项目;入选省部级人才项目;一作/通讯发表SCI收录10余篇;一作发表EI核心论文5篇。

1) 国家自然科学基金青年基金项目,2023,30万,主持
2)江苏省自然科学青年基金项目,2022,20万,主持
3) 燃气轮机叶片双层壁冷却设计,上海电气,2023,56万,第二主持
4) 江苏省高等学校基础科学(自然科学)研究面上项目,2022,,5万,主持
5) 江苏省“双创博士”,2021,15万,主持
6)  青年科技创新项目,2021,5万,主持
7)  自制教学仪器设备项目,2021,4.5万,主持

[1]Cai, Yang, Xinzi Liu, Yu Sun,Xiaojun Fan, and Jiao Wang. 2024. Unique Coolant Supply Passage Arrangements to Induce Large-Scale Vortex within Turbine Blade Interior Leading Edge ChambersEnergies17, no. 14: 3404. https://doi.org/10.3390/en17143404
[2]Xiaojun Fan; Numerical research of a new vortex double wall cooling configuration for gas turbine blade leading edge[J]. International Journal of Heat and Mass Transfer, 2022. (SCI)
[3]Xiaojun Fan; Xue yuan; Numerical investigation of nozzle geometry influence on the vortex cooling in an actual gas turbine blade leading edge cooling system[J]. Heat and Mass Transfer, 2021. (SCI)
[4]Fan Xiaojun, Chuangxin He, Lian Gan, Liang Li, Changhe Du. Experimental study of swirling flow characteristicsin a semi cylinder vortex cooling configuration.[J].Experimental Thermal and Fluid Science, 2020.
[5]Fan Xiaojun, Li Liang, Wang Jiefeng, Wu Fan. Heat transfer enhancement for gas turbine blade leading edge cooling using curved double-wall/vortex cooling with various disturbing objects[C].ASME PaperGT2019-90211, 2019.
[6] Fan Xiaojun, Li Liang, Zou Jiasheng, Zhou yuanyuan. Cooling methods for gas turbine blade leading edge: Comparative study on impingement cooling, vortex cooling and double vortex cooling[J].International Communications in Heat and Mass Transfer, 2019, 100: 133-145.
[7]Fan Xiaojun, Li Liang, Zou Jiasheng, Wang Jiefeng, Wu Fan. Local heat transfer of vortex cooling with multiple tangential nozzles in a gas turbine blade leading edge cooling passage[J].International Journal of Heat and Mass Transfer, 2018, 126: 377-389.
[8]Fan Xiaojun, Du Changhe, Li Liang, Li Sen. Numerical simulation on effects of film hole geometry and mass flow on vortex cooling behavior for gas turbine blade leading edge[J].Applied Thermal Engineering, 2017, 112: 472-483.
[9]范小军,杜长河,李亮,李森.气膜孔几何位置对旋流冷却流动与传热特性的影响[J].西安交通大学学报, 2016, 50(7): 32-38.
[10] 范小军,李亮,李森,张翔.平板和静叶表面气流-水膜耦合流动特性的数值研究[J].西安交通大学学报, 2016, 50(11):7-13.
[11]范小军,杜长河,李亮,邹佳生. 4种冷却结构对叶片前缘流动换热影响的比较研究[J].西安交通大学学报, 2017, 51(7):37-43.
[12]范小军,邹佳生,周源远,李亮.喷嘴数目和温比对旋流冷却流动和传热特性影响的研究[J].西安交通大学学报, 2018, 52(3): 19-24.
[13]范小军,杜长河,周源远,李亮,丰镇平.复合冲击和复合旋流冷却特性的对比研究[J].工程热物理学报, 2018, 39(12): 2627-2633.
2015.09-2020.09西安交通大学动力工程及工程热物理博士(硕博连读)
2018.11-2019.05英国杜伦大学School of Engineering联合培养博士生
2011.09-2015.07西安交通大学能源动力系统及自动化学士
本科生教学:
《机械制造基础》
《CAE技术应用》
《热交换器设计》
研究生教学:
《Instrumental Survey of Small Energy Facilities》
《燃气轮机/Gas Turbine》

1) 国家自然科学基金青年基金项目,2023,30万,主持
2)江苏省自然科学青年基金项目,2022,20万,主持
3) 燃气轮机叶片双层壁冷却设计,上海电气,2023,56万,第二主持
4) 江苏省高等学校基础科学(自然科学)研究面上项目,2022,,5万,主持
5) 江苏省“双创博士”,2021,15万,主持
6)  青年科技创新项目,2021,5万,主持
7)  自制教学仪器设备项目,2021,4.5万,主持

[1]Cai, Yang, Xinzi Liu, Yu Sun,Xiaojun Fan, and Jiao Wang. 2024. Unique Coolant Supply Passage Arrangements to Induce Large-Scale Vortex within Turbine Blade Interior Leading Edge ChambersEnergies17, no. 14: 3404. https://doi.org/10.3390/en17143404
[2]Xiaojun Fan; Numerical research of a new vortex double wall cooling configuration for gas turbine blade leading edge[J]. International Journal of Heat and Mass Transfer, 2022. (SCI)
[3]Xiaojun Fan; Xue yuan; Numerical investigation of nozzle geometry influence on the vortex cooling in an actual gas turbine blade leading edge cooling system[J]. Heat and Mass Transfer, 2021. (SCI)
[4]Fan Xiaojun, Chuangxin He, Lian Gan, Liang Li, Changhe Du. Experimental study of swirling flow characteristicsin a semi cylinder vortex cooling configuration.[J].Experimental Thermal and Fluid Science, 2020.
[5]Fan Xiaojun, Li Liang, Wang Jiefeng, Wu Fan. Heat transfer enhancement for gas turbine blade leading edge cooling using curved double-wall/vortex cooling with various disturbing objects[C].ASME PaperGT2019-90211, 2019.
[6] Fan Xiaojun, Li Liang, Zou Jiasheng, Zhou yuanyuan. Cooling methods for gas turbine blade leading edge: Comparative study on impingement cooling, vortex cooling and double vortex cooling[J].International Communications in Heat and Mass Transfer, 2019, 100: 133-145.
[7]Fan Xiaojun, Li Liang, Zou Jiasheng, Wang Jiefeng, Wu Fan. Local heat transfer of vortex cooling with multiple tangential nozzles in a gas turbine blade leading edge cooling passage[J].International Journal of Heat and Mass Transfer, 2018, 126: 377-389.
[8]Fan Xiaojun, Du Changhe, Li Liang, Li Sen. Numerical simulation on effects of film hole geometry and mass flow on vortex cooling behavior for gas turbine blade leading edge[J].Applied Thermal Engineering, 2017, 112: 472-483.
[9]范小军,杜长河,李亮,李森.气膜孔几何位置对旋流冷却流动与传热特性的影响[J].西安交通大学学报, 2016, 50(7): 32-38.
[10] 范小军,李亮,李森,张翔.平板和静叶表面气流-水膜耦合流动特性的数值研究[J].西安交通大学学报, 2016, 50(11):7-13.
[11]范小军,杜长河,李亮,邹佳生. 4种冷却结构对叶片前缘流动换热影响的比较研究[J].西安交通大学学报, 2017, 51(7):37-43.
[12]范小军,邹佳生,周源远,李亮.喷嘴数目和温比对旋流冷却流动和传热特性影响的研究[J].西安交通大学学报, 2018, 52(3): 19-24.
[13]范小军,杜长河,周源远,李亮,丰镇平.复合冲击和复合旋流冷却特性的对比研究[J].工程热物理学报, 2018, 39(12): 2627-2633.