
谭剑锋,男,博士,教授、硕士生导师,江苏省高校“青蓝工程”优秀青年骨干教师,现任机械与动力工程学院院长助理、应急装备技术与工程系主任、中国航空学会直升机分会委员、江苏省能源研究会风能利用专业委员会委员、江苏省力学学会能源结构力学专业委员会委员、“Aerospace Science and Technology”“Journal of Aircraft”“Chinese Journal of Aeronautics”“Applied Mathematics and Mechanics”“Advances in Mechanical Engineering”“Shock and Vibration”“Applied Acoustics”“Physics of Fluids”《航空学报》《北京航空航天大学学报》等期刊审稿专家。
一、教育工作经历:
2017 -2018 University of Glasgow, UK,荣誉副研究员;
2013.08 -至今南京工业大学,机械与动力工程学院;
2009.9-2013.7清华大学航空宇航科学与技术,获得工学博士学位;
2007.9-2009.6南京航空航天大学飞行器设计,获得工学硕士学位;
2003.9-2007.6 南京航空航天大学飞行器设计与工程,获得工学学士学位。
二、研究方向:
主要从事eVTOL/多旋翼飞行器/风力机设计、空气动力学、智能流体力学、复杂环境力学、风沙/气液两相流、结构动力学、战场结构损伤与修复、智能应急无人装备、人工智能研究。
三、主持与参与项目:
主持基础加强重点项目课题、某装备专项项目、“十四五”预研专用项目、“十三五”预研专用项目、装备预研国防重点实验室基金、国家自然科学基金面上项目和青年项目、江苏省自然科学基金面上项目、旋翼空气动力学重点实验室基金、江苏省高校自然科学基金面上项目等10余项,主持参与国家自然科学基金、973项目、航空基金、校部、校际、校企合作等项目14项。发表学术论文40余篇,其中SCI源刊近20篇,EI源刊20余篇。主持江苏省高等教育教改重点课题和一般课题2项,发表教改论文5篇。
四、教学获奖
江苏省教育教学成果一等奖;
江苏省第四届青年教师授课竞赛二等奖;
中国石油和化工教育教学优秀成果奖一等奖;
南京工业大学教育教学成果奖特等奖;
南京工业大学第十一届青年教师授课竞赛特等奖;
南京工业大学优秀共产党员称号;
南京工业大学“教书育人”竞赛先进个人称号;
南京工业大学“南工晨星奖教金”。
五、近年代表性论文:
[1]Tan J F, Yan Y Z, Xu S G, Zhang W G, Wang C, Fan F. Numerical Investigation of Blade Erosion in Helicopter Brownout.Journal of Aircraft, 2025.
[2]Tan J F, Liu M H, Li G Q, Zhang W G, Yu Z H. Numerical Investigation of the Flow Field around a rotor above an Obstacle Using a Panel-LBM Hybrid Method.Journal of Aerospace Engineering, 2025, 38(4): 04025036.
[3] Xing X B,Tan J F, Yang Y X, Yu L J, Zhou Y. An Efficient Analysis Method of Aluminum Alloy Helicopter Fuselage Projectile Damage Based on Projectile Breakdown Theory.Aerospace, 2024, 11,500.
[4]Tan J F, Yon T, He L, Yu L J, Wang C, Accelerated Method of Helicopter Brownout with Particle-Particle Collisions.Aerospace Science and Technology, 2022, 124: 107511.
[5] Tan J F, Ge Y Y, Zhang W G, Cui Z, Wang H W. Numerical Study on Helicopter Brownout with Crosswind.Aerospace Science and Technology, 2022, 131: 107965 (IF=5.4).
[6]Tan J F, Yon T, He L, et al. Accelerated Method of Helicopter Brownout with Particle-Particle Collosons.Aerospace Scinence and Technology, 2022, 124: 107511 (IF=5.4).
[7]Jian FengTan, Jin er Gao, George N. Barakos, Chang Liang Lin, Wei Guo Zhang, Ming Qi Huang. Novel Approach to Helicopter Brownout Based on Vortex and Discrete Element Methods.Aerospace Science and Technology, 2021, 116: 106839 (IF=5.1).
[8]Jian Feng Tan, Jian Gang Cai, George N. Barakos, Chang Wang, Ming Qi Huang. Computational Study on the Aerodynamic Interference between Tandem Rotors and Nearby Obstacles.Journal of Aircraft, 2020, 57(3): 456-468.
[9] Zhou, T.,Tan, J., Cai, J., Shi, R., Xia, Y. Numerical Investigation on the Power Outputs of a Wind Turbine Sited Over the Continuous Hilly Terrain.Transactions of Nanjing University of Aeronautics & Astronautics, 2020, 37(1): 120-128.
[10]Jianfeng Tan, Tianyi Zhou, Yiming Sun, George N. Barakos. Numerical Investigation of the aerodynamic interaction between a tiltrotor and a tandem rotor during shipboard operations.Aerospace Science and Technology, 2019, 87, 62-72 (IF=5.1).
[11]Tan, J. F., Sun, Y. M., Zhou, T. Y., Barakos, G. N. and Green, R. B. Simulation of the aerodynamic interaction between rotor and ground obstacle using vortex method.CEAS Aeronautical Journal, 2019, 10(3): 733-753.
[12]J. F. Tan, Y. M. Sun, et.l. New approach for aerodynamic and aeroacoustic analysis of actively controlled flaps rotor.Journal of Aircraft, 2018, 55(6): 2191-2202.
[13]J. F. Tan, Y. M. Sun, T. Y. Zhou, G. N. Barakos, R. B. Green. Unsteady Aerodynamic Interaction between Rotor and Ground Obstacle. The 44thEuropean Rotorcraft Forum, 18-21th, Sep, 2018, Delft, Nethelands.
[14]Jianfeng Tan, Yimingsun, George N. Barakos. Vortex Approach for Downwash and Outwash of Tandem-Rotor in Ground Effect,Journal of Aircraft, 2018, 55(6): 2491-2509.
[15]Jianfeng Tan, Yimingsun, George N. Barakos. Unsteady Loads for Coaxial Rotors in Forward Flight Computed Using a Vortex Particle Method,Aeronautics Journal, 2018, 122: 693-714.
[16]Jianfeng Tan, Yiming Sun, Tianyi Zhou, George N. Barakos, Richard B. Greeen. Simulation of the Aerodynamic Interaction between Rotor and Ground Obstacle Using Vortex Method, the AHS International 74thAnnual Forum & Technology Display, Phoenix, Arizona, USA, May 14-17, 2018.
[17]Jianfeng Tan, Yimingsun, George N. Barakos. Simulation of Unsteady Aerodynamic Load for Rigid Coaxial Rotor in Forward Flight with Vortex Particle Method, European Rotorcraft Forum, 2017.
[18]夏云松,谭剑锋,韩水等.基于BP神经网络的风力机涡流发生器优化.上海交通大学学报, 2023.
[19]谭剑锋,何龙,于领军,周国臣.基于粘性涡粒子VVPM/沙粒DEM的直升机沙盲建模研究,航空学报, 2022,43(3): 125536.
[20]谭剑锋,韩水,王畅,于领军.基于DEM的直升机沙盲加速计算方法研究,北京航空航天大学学报, 2022.
[21]谭剑锋,邢肖兵,催钊,武杰,张卫国等.舰载直升机主动甲板着舰气动载荷特性研究.北京航空航天大学学报, 2022.
[22]谭剑锋,杨宇霄,张卫国,王世雄,吕琳等.侧风对直升机沙盲特性影响研究.北京航空航天大学学报, 2022.
[23]周天熠,谭剑锋,孙义鸣,蔡建纲.三维连续丘陵对NREL风力机功率特性的影响分析,太阳能学报, 2021,42(04): 359-365.
[24]蔡建纲,谭剑锋,于邻军等,铝合金框架结构的弹体穿击损伤特性,科学技术与工程, 2021,21(21):8757-8764.
[25]谭剑锋,周天熠,王畅,于领军.旋翼地面效应的气动建模与特性研究.航空学报, 2019, 40(6): 122602.
[26]孙义鸣,谭剑锋,周天熠.风轮尺寸与旋向对双风轮风力机功率特性的影响分析.可再生能源, 2019, 37(11):1704-1709.
[37]谭剑锋,孙义明,王浩文,林长亮.共轴刚性双旋翼非定常气动干扰载荷分析,北京航空航天大学学报, 2018, 44(1):50-62.
六、联系方式:
Email:Jianfengtan@njtech.edu.cn
欢迎报考本课题组研究生。