李文丰


的个人主页 http://teacher.nwpu.edu.cn/wenfeng

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基本信息 The basic information

李文丰

航空学院

博士研究生毕业

工学博士

教授

力学-流体力学,力学-空气动力学

w.li@nwpu.edu.cn

工作经历 Work Experience

2017.09-2020.04,德国亚琛工业大学,空气动力学所,Research Scientist;

2020.06-2022.06,西北工业大学,航空学院,F1岗辅导员;

2020.06-至今,西北工业大学,航空学院,副教授;

2022.06-至今,西北工业大学,航空学院,副教授,博士生导师

教育经历 Education Experience

2006.09-2010.06,西北工业大学,航空学院,本科

2010.09-2013.04,西北工业大学,航空学院,硕士

2012.11-2017.08,德国亚琛工业大学,机械学院,博士


教育教学 Education And Teaching

1. 硕士研究生招生

    每年招收飞行器设计和流体力学学科硕士研究生3名。

2. 博士研究生招生

    每年招收航空宇航科学技术、流体力学博士研究生2名。

长期招收博士后、待遇除学校规定外,额外给予导师配套+奖励绩效+其他项目,具体可面谈;


请联系Email:w.li@nwpu.edu.cn

教学:

1. 空气动力学基础(双语)

2. 空气动力学实验(英语)

3. 悉心指导本科、硕士生17名,目前毕业学生分布于各大航空航天等主机所,美国密歇根大学、南加州大学,瑞典皇家工学院,德国亚琛工业大学、慕尼黑工业大学,清华大学,日本东京大学等世界名校。

4. 指导省级大学生创新创新项目四项,顶峰计划三人


部分学生论文:

[1] Simon. E. Experimental investigation of spatially developing turbulent boundary layers over longitudinal grooves. Bachelor thesis, INSA Lyon/RWTH Aachen University, 2019, 法国INSA Lyon大学本科生,现慕尼黑工业大学读研

[2] Lu. F. Amplitude Modulation in Turbulent Boundary Layers above Riblets. Internship thesis, Michigan State University, 2019, 美国密歇根州立大学本科生,实习论文,现UCLA读研

[3] Paakkari. V. Experimental investigation of friction drag reduction in a pulsating turbulent boundary layer via spanwise traveling surface wave motion. Master thesis, RWTH Aachen University, 2018, 芬兰Aalto大学硕士生

[4] Wang. Z. Transitional boundary layer under active excitation of a spanwise traveling surface wave. Internship thesis, Michigan State University, 2018, 美国密歇根州立大学本科生

[5] Martínez Micó. T. A. Friction drag reduction in a turbulent boundary layer using active flow control with unsteady inflow, Bachelor thesis, INSA Lyon/RWTH Aachen University, 2017, 法国INSA Lyon大学本科生

[6] Hecken. T. Parametric investigation of active friction drag reduction by spanwise traveling surface wave with wall-deformation. Master thesis, RWTH Aachen University, 2016, 亚琛工业大学硕士生,现德国宇航院

[7] Lei. Z. Turbulent drag reduction by spanwise traveling wave motion on riblet surface. Bachelor thesis, RWTH Aachen University, 2014, 西北工业大学本科生

[8] Pan. T. and vor der Bruck. C. Long-distance Micro-PIV/PTV wind tunnel investigations on smooth and riblet surfaces. Project thesis, RWTH Aachen University, 2014, 亚琛工业大学本科生

荣誉获奖 Awards Information

2021年入选国家海外高层次人才引进计划(青年项目);

2020、2021年连续两年学院年终考核先进个人;

2021年学校社会实践优秀指导教师;

2015, Student-presenter Award, the 3rd Symposium on Fluid-Structure-Sound Interactions and Control, Perth, Australia.

科学研究 Scientific Research

研究方向:

1实验流体力学,空气动力学

2、流动主/被动控制技术

3、新型气动布局设计

4湍流边界层,高超声速流动

5、基于光学诊断的流动测量技术 (2D-2C/3C-PIV, Tomo-PIV, μ-PTV, Micro pillar shear-stress-sensor )


主持科研项目:

[6]国家自然科学基金“压力梯度湍流边界层主动减阻的实验研究”,2022.01-2024.12,纵向,30万;

[5]翼型、叶栅空气动力学国家级实验室开放课题“基于微圆柱阵列的壁湍流摩擦应力测量及流动机理研究”,2022.01-2024.12,纵向,15万;

[4]中国空气动力学发展中心开放课题“机翼表面小尺度空腔噪声产生机理与控制方法研究”2021.01-2023.12,纵向,8万;

[3]翼型、叶栅空气动力学国家级实验室稳定支持项目“主动与被动耦合控制边界层减阻方法与流动机理研究”2020.6-2022.12,纵向,60万;

[2]航天一院合作项目“xxx飞行平台气动特性仿真与优化研究”2020.10-2021.12,横向,25万;

[1]中央高校基本业务经费,2020.6-2023.6,纵向,20万;


参与科研项目

[7]xxxx民用飞机专项科研项目,纵向,2021.01-2023.12,主要参与人;

[6] 高速和高分辨率PIV的湍流边界层流动控制测量 (High-speed and high-resolution PIV measurements in a turbulent boundary layer with and without flow control), 德国亚琛工业大学、澳大利亚莫纳什大学,2017. 03-2020.04,德方主要负责人;

[5] 壁面展向行波的主动减阻实验研究 (Experimental investigation of friction drag over moving surfaces), 德国科学基金委FOR1779子项目, 亚琛工业大学, 2015. 05-2018.05,主要负责人,Schroeder 教授为项目第一申请人,28.5万欧元;

[4] 基于波状激励壁面的主动减阻 (Active drag Reduction via wavy surface oscillation), 德国科学基金委FOR1779子项目, 亚琛工业大学, 2012. 11-2014. 12,主要负责人,Schroeder 教授为项目第一申请人,25万欧元;

[3] 壁面微小沟槽的被动减阻技术 (Passive friction drag reduction using micro-structured riblets), 亚琛工业大学,2012. 11-2014. 12,主要负责人;

[2] 圆柱绕流的DBD等离子体主动控制, 西北工业大学,2011. 05-2012. 10,主要参与者;

[1] 三角翼大迎角分离涡控制实验研究, 西北工业大学,2010.09 -2012. 10,主要参与者;

学术成果 Academic Achievements

发表论文

[24] Zhang, Yue, Jinsheng Cai, and Wenfeng Li*. "Turbulent Channel Flow With Riblets In Drag Reducing And Drag Increasing Regimes." In AIAA AVIATION 2022 Forum, p. 3851. 2022.

[23] Wong, C. W., Cheng, X., Fan, D., Li, W., & Zhou, Y. (2021). Friction drag reduction based on a proportional-derivative control scheme. Physics of Fluids, 33(7), 075115.

[22] Li, W.*, Roggenkamp, D., Paakkari. V., Klaas, M., Soria, J., & Schroeder, W., Analysis of a drag reduced flat plate turbulent boundary layer via uniform momentum zones. Aerospace Science and Technology, 2020.

[21] Roggenkamp, D., Li, W.*, Klaas, M., & Schroeder, W., Influence of spanwise transversal surface wave on coherent structures in turbulent boundary layers. Aerospace Science and Technology, 86, 387-400, 2019.

[20] Li, W.*, Roggenkamp, D., Jessen, W., Klaas, M., & Schroeder, W., Parametric investigations of friction drag reduction in turbulent flow over a flexible wall undergoing traveling surface wave motions. Experiments in Fluids, 59 (6), 105, 2018.

[19] Li, W. *, Roggenkamp, D., Jessen, W., Klaas, M., & Schroeder, W.,Reynolds number effects on the fluctuating velocity distribution in wall-bounded shear layers. Measurement science and technology, 28(1), 015302, 2016.

[18] Li, W. *, Jessen, W., Roggenkamp, D., Klaas, M., Silex, W., Schiek, M., & Schroeder, W., Turbulent drag reduction by spanwise traveling ribbed surface waves. European Journal of Mechanics-B/Fluids, 53, 101-112, 2015.

[17] Meysonnat, P. S. *, Roggenkamp, D., Li, W., Roidl, B., & Schroeder, W., Experimental and numerical investigation of transversal traveling surface waves for drag reduction. European Journal of Mechanics-B/Fluids, 55, 313-323, 2016.

[16] Roggenkamp, D. *, Jessen, W., Li, W., Klaas, M., & Schroeder, W. Experimental investigation of turbulent boundary layers over transversal moving surfaces. CEAS Aeronautical Journal, 1-14, 2015.

[15] Cai, J. *, Pan, S., Li, W., & Zhang, Z., Numerical and experimental investigations of a nonslender delta wing with leading-edge vortex flap. Computers & Fluids, 99, 1-17, 2014.

[14] Hao, J. *, Tian, B., Wang, Y., Song, Y., Pan, S., & Li, W., Dielectric barrier plasma dynamics for active aerodynamic flow control. Science China Physics, Mechanics and Astronomy, 57(2), 345-353, 2014.

[13] Li, W., Cai, J. *, Hao, J., & Liu, Q., Flow control on a circular cylinder using multi-bipolar plasma actuator. Journal of Experiments in Fluid Mechanics, 27(3), 2013.

[12] Hao, J., Cai, J. *, & Li, W. , Investigation of flow control by using plasma actuator of bipolar electrode. Journal of Experiments in Fluid Mechanics, 26(6), 2012.

[11] Li, W.*, Paakkari, V., Roggenkamp, D., Klaas, M., Soria, J. & Schroeder, W. (2018, 16-19 July). Uniform momentum zones in a turbulent boundary layer with spanwise traveling surface waves. Abstract submitted to the 19th International Symposia on Applications of Laser Techniques to Fluid Mechanics, Lisbon, Portugal.

[10] Li, W.*, Roggenkamp, D., Jessen, W., Klaas, M., & Schroeder, W. (2017, 21-24 August). Friction drag reduction in a wall-bounded pulsating flow using combined active and passive flow control. The 16th European Turbulence Conference, Stockholm, Sweden.

[9] Li, W.*, Roggenkamp, D., Jessen, W., Klaas, M., & Schroeder, W. (2017, 19-21 June). Detection of rare back flow events in zero-pressure gradient turbulent boundary layers using micro-PTV/PIV. The 12th International Symposium on Particle Image Velocimetry, Busan, Korea.

[8] Li, W.*, Roggenkamp, D., Jessen, W., Klaas, M., & Schroeder, W. (2017, 03-04 April). Secondary flow induced by the spanwise traveling surface wave in a turbulent boundary layer. The European Drag Reduction and Flow Control Meeting, MontePorzio Catone, Italy.

[7] Li, W.*, Roggenkamp, D., Jessen, W., Klaas, M., & Schroeder, W. (2016, 21-26 August). Experimental investigations of drag reduction in a turbulent boundary layer using spanwise traveling wave-like surface deformation. The 24th International Congress of Theoretical and Applied Mechanics, Montréal, Canada.

[6] Li, W.*, Roggenkamp, D., Jessen, W., & Klaas, M. (2016, 4-7 July). PIV and μ-PTV investigations of turbulent flow over a flexible wall undergoing traveling surface wave motions. The 18th International Symposia on Applications of Laser Techniques to Fluid Mechanics, Lisbon, Portugal.

[5] Li, W.*, Roggenkamp, D., Jessen, W., Klaas, M., & Schroeder, W. (2016). Turbulent Drag Reduction by Spanwise Traveling Ribbed Surface Waves. In Y. Zhou, A. D. Lucey, Y. Liu & L. Huang (Eds.), Fluid-Structure-Sound Interactions and Control (pp. 363-368): Springer Berlin Heidelberg.

[4] Liu, Y.*,Li, W., Jessen, W., & Schroeder, W. (2015, 10-11 November). Measurements of turbulent flow downstream ribbed surfaces using the micro-pillar shear stress sensor MPS3. Die Deutsche Str?mungsmechanische Arbeitsgemeinschaft, STAB, Goettingen, Germany

[3] Roggenkamp, D.*, Li, W., Jessen, W., Klaas, M., & Schroeder, W. (2015, 25-28 August). Experimental investigation of turbulent boundary layer flow undergoing spanwise traveling transversal surface waves. The 15th European Turbulence Conference 2015, Delft, The Netherlands.

[2] Roggenkamp, D.*, Li, W., Meysonnat, P., Klaas, M., & Schroeder, W. , Experimental analysis of turbulent friction drag reduction due to spanwise transversal surface waves. The 9th Symposium on Turbulence and Shear Flow Phenomena, Melbourne, Australia, 2015, 30 June-3 July.

[1] Jessen, W.*, Li, W., Roggenkamp, D., Klaas, M., & Schroeder, W., Experimental analysis of the near-wall flow structure over moving surfaces. The 4th ICEFM, Beijing, 2014, 12-15 August.