谭剑锋，男，博士，副教授、硕士生导师，“Aerospace Science and Technology”、“Journal of Aircraft”、“Chinese Journal of Aeronautics”、“Applied Mathematics and Mechanics”、“Advances in Mechanical Engineering”、“Shock and Vibration”、《航空学报》、《北京航空航天大学学报》等期刊审稿专家。
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。


一、研究方向：
主要从事旋翼/风力机叶片设计、空气动力学、计算流体力学、声学及流动控制技术研究。
二、主持与参与项目：
主持国家自然科学青年基金、江苏省自然科学基金面上项目、装备预研国防重点实验室基金、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5项，主持参与国家自然科学基金、国防973、航空基金、校部、校际、校企合作等项目8项。发表学术论文24篇，其中SCI源刊8篇，EI源刊14篇。
三、近年论文：
[1]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.
[2]Tan, J. F., Sun, Y. M., Zhou, T. Y.,Barakos, G. N.andGreen, R. B.Simulation of the aerodynamic interaction between rotor and ground obstacle using vortex method.CEAS Aeronautical Journal,2019.
[3]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.
[4]J. F. Tan, Y. M. Sun, T. Y. Zhou, G. N. Barakos, R. B. Green. Unsteady Aerodynamic Interaction between Rotor and Ground Obstacle. The 44th European Rotorcraft Forum, 18-21th, Sep, 2018, Delft, Nethelands.
[5]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.
[6]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.
[7]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 74th Annual Forum & Technology Display, Phoenix, Arizona, USA, May 14-17, 2018.
[8]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.
[9]Jianfeng Tan, Haowen Wang. Highly Efficient Unsteady Panel Time-Marching Free Wake for Aerodynamics of Rotorcraft. Journal of Aircraft, 51(1): 54-61, 2014.
[10]Jian-feng Tan, Hao-wen Wang. Simulating Unsteady Aerodynamics of Helicopter Rotor with Panel/Viscous Vortex Particle Method. Aerospace Science and Technology, 30: 255-268, 2013.
[11]Tan Jianfeng, Wang Haowen. Panel/Full-Span Free-Wake Coupled Method for Unsteady Aerodynamics of Helicopter Rotor Blade. Chinese Journal of Aeronautics, 26 (3): 535-543, 2013.
[12] Sun Tao,Tan Jianfeng, Wang Haowen. Investigation of Rotor Control System Loads. Chinese Journal of Aeronautics, 26 (5): 1114-1124, 2013.
[13]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.
[14]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.
[15]谭剑锋，吴超，王浩文，林长亮.旋翼/平尾气动干扰对直升机配平特性的影响分析,北京航空航天大学学报, 2016, 42(11): 2349-2357.
[16]谭剑锋.直升机旋翼对尾桨非定常气动载荷的影响,航空学报,2015,36(10): 3228-3240.
[17]吴超,王浩文,张玉文,谭剑锋,倪先平.基于LADRC的无人直升机轨迹跟踪.航空学报, 2015, 36(2): 473-483.
[18]王俊超，谭剑锋，李建波，徐明.基于自由尾迹方法的自转旋翼气动特性研究,航空学报, 2015, 36(11): 3540-3548.
[19]谭剑锋，王浩文，吴超，林长亮.基于非定常面元/粘性涡粒子混合法的旋翼/平尾非定常气动干扰研究.航空学报, 2014, 35(3): 643-656.
[20]吴超,谭剑锋,王浩文,倪先平.基于GA/LM混合优化的直升机全机配平算法.飞行力学, 2014, 32(1): 5-10.
[21]谭剑锋,王浩文.直升机旋翼/机身非定常气动干扰数值分析.空气动力学学报，2014, 35(3): 643-656.
[22]谭剑锋,王浩文,林长亮.基于升力面自由尾迹的直升机旋翼悬停性能参数影响研究.航空学报, 33(2): 249-257, 2012.
[23]邓景辉，谭剑锋，张呈林.基于时间步进自由尾迹的旋翼总距突增气动响应分析.空气动力学学报, 29(2): 217-221, 2011.
[24]孙韬,谭剑锋,王浩文.典型飞行状态下的旋翼振动载荷计算与分析.南京航空航天大学学报, 43(3): 302-307, 2011.
四、联系方式：
Email:Jianfengtan@njtech.edu.cn