澳门威斯尼斯人_澳门威斯尼斯人wn8336app(www.hestakykki.com)

飞行器设计系
李伟鹏

李伟鹏

职务:特别研究员

办公电话:021-34208076

电子邮件:liweipeng@sjtu.edu.cn

办公地址:澳门威斯尼斯人wn8336appA320室

 

工作经历

时间 任职单位 职务
2016年-至今 澳门威斯尼斯人wn8336app 特别研究员

2012年-2015年

澳门威斯尼斯人wn8336app 特别副研究员

教育背景

时间 毕业院校 学历

2008年-2011年

东京大学      博士
2006年-2008年 哈尔滨工业大学 硕士
2002年-2006年 哈尔滨工业大学 本科

研究方向

(1)飞行器设计;

(2)湍流减阻;

(3)气动噪声;

(4)数据挖掘与机器学习。

主要科研项目

(1) 国家自然科学基金青年项目/面上项目,重大研究计划培育项目/集成项目
(2) 国家数值风洞I期、基础加强、XX共用技术基金等国防纵向课题
(3) 科技部重点研发计划等国家重大课题
(4) 中国商飞、中国商发、中国航发沈阳发动机研究院、509所、802所等科研攻关
(5) 墨尔本大学、KTH、南洋理工大学、香港科技大学等国际合作

代表性论文专著

(1) Fan, Y., Li, W.(*), and Pirozzoli, S., Energy exchanges in hypersonic flows, Physical Review Fluids, 7, L092601, 2022.
(2) Fan, Y., Vinuesa, R., Gatti, D., Schlatter, P., and Li, W.(*), Decomposition of the mean friction drag on an NACA4412 airfoil under uniform blowing/suction, Journal of Fluid Mechanics, 932, A31, 2022.
(3) Yuan, X., Tong, F., Li, W., Chen, J., and Dong, S.(*), Wall-attached temperature structures in supersonic turbulent boundary layers, Physics of Fluids, in press, 2022. https://doi.org/10.1063/5.0121900
(4) 杨强, 李伟鹏(*). 高精度WCNS格式加权策略改进与数值验证(网络首发). 上海交通大学学报, doi: 10.16183/j.cnki.jsjtu.2022.014.
(5) Fan, Y., Li, W.(*), Spectral analysis of turbulence kinetic and internal energy budgets in hypersonic turbulent boundary layers, Journal of Fluid Mechanics, under review, 2022.
(6) Li, W.(*), Guo, Y., and Liu, W., On the mechanism of acoustic resonances from a leading-edge slat, Aerospace Science and Technology, 113(2), 106711, 2021.
(7) 郑国雨, 李伟鹏(*), 林佳佳, 孙一峰. 外形参数对涡扇发动机冠状喷口气动性能影响. 推进技术, 42(12), 10, 2021.
(8)董思卫, 程诚, 陈坚强, 袁先旭(*), 李伟鹏. 基于聚类连通法的湍流拟序结构研究进展. 力学进展, 51(4): 792-830, 2021.
(9) Cheng, C., Li, W.(*), Lozano-Durán, A., and Liu, H., On the structure of streamwise wall-shear stress fluctuations in turbulent channel flows, Journal of Fluid Mechanics, 903, A29, 2020.
(10) Cheng, C., Li, W.(*), Lozano-Durán, A., and Liu, H., Uncovering Townsend’s wall-attached eddies in low-Reynolds-number wall turbulence, Journal of Fluid Mechanics, 889, A29, 2020.
(11) Fan, Y., Li, W.(*), Atzori, M., Pozuelo, R., Schlatter, P., and Vinuesa, R., Decomposition of the mean friction drag in adverse-pressure-gradient turbulent boundary layers, Physical Review Fluids, 5, 114608, 2020.
(12) Li, W.(*), Turbulence statistics of flow over a drag-reducing and a drag-increasing riblet-mounted surface, Aerospace Science and Technology, 104, 106003, 2020.
(13) Li, W.(*), Three-Dimensional Shock-Wave/Boundary-Layer Interaction in Supersonic Flow Past a Finite-Span Sharp Wedge, International Journal of Aeronautical and Space Sciences, 21, 329–336, 2020.
(14) Fan, Y., Li, W.(*), and Pirozzoli, S., Energy-based decomposition of friction drag in turbulent square-duct flows, International Journal of Heat and Fluid Flow, 86, 108731, 2020.
(15) 张亦知, 程诚, 范钇彤, 李高华, 李伟鹏(*). 基于物理知识约束的数据驱动式湍流模型修正及槽道湍流计算验证. 航空学报, 41(3), 123282, 2020.
(16) Li, W.(*), Fan, Y., Modesti, D., and Cheng, C., Decomposition of the mean skin-friction drag in compressible channel flows, Journal of Fluid Mechanics, 875, 101-123, 2019.
(17) Cheng, C., Li, W.(*), Lozano-Durán, A., and Liu, H., Identity of individual attached eddies in turbulent channel flows with bidimensional empirical mode decomposition, Journal of Fluid Mechanics, 870, 1037-1071, 2019.
(18) Fan, Y., Li, W.(*), and Pirozzoli, S., Decomposition of the mean friction drag in zero-pressure-gradient turbulent boundary layers, Physics of Fluids, 31, 086105, 2019.
(19) Li, W.(*) and Liu, H., Two-point Statistics of Coherent Structures in Turbulent Flow over Riblet-mounted Surface, Acta Mechanica Sinica, 35(3), 457-471, 2019.
(20) Fan, Y., Cheng, C., and Li, W.(*), Effects of Reynolds number on the mean skin friction decomposition in turbulent channel flows, Applied Mathematics and Mechanics, 40(3), 331-342, 2019.
(21) Li, W.(*) and Liu, H., Large-eddy simulation of shock-wave/boundary-layer interaction control using a backward facing step, Aerospace Science and Technology, 84, 1011-1019, 2019.
(22) Fan, Y. and Li, W.(*), Review of Far-Field Drag Decomposition Methods for Aircraft Design, Journal of Aircraft, 56(1), 11-21, 2019.
(23) Xu, S. and Li, W.(*), Reynolds number effect on tonal noise generation from an airfoil, Acta Aerodynamica Sinica, 37(3), 382-392, 2019.
(24) Li, W. and Wang, L.(*), Geometrical structure analysis of the zero-pressure-gradient turbulent boundary layer, Journal of Fluid Mechanics, 846, 318-340, 2018.
(25) 李伟鹏(*), 大型客机增升装置噪声机理与噪声控制综述, 空气动力学报, 36(3), 372-384, 2018.
(26) 魏佳云, 李伟鹏(*), 许思为, 赵克良, 孙一峰, 基于DMD方法的缝翼低频噪声机理分析, 航空学报, 39(1), 121469, 2018.
(27) Li, W.(*) and Liu, H., Noise Generation in Flow over a Full-span Trailing-edge Flap, AIAA Journal, 55(2), 561-571, 2017.
(27) Li, W.(*), Suppression of Supersonic Cavity Oscillations Using Pulsed Upstream Mass Injection, International Journal of Aerospace Engineering, 6702385, 2016.
(29) 张宇轩, 李伟鹏(*), 王福新, 流动线性稳定性分析中切比雪夫谱配置法参数敏感性, 上海交通大学学报, 50(8), 1246-1254, 2016.
(30) Li, W.(*), Nonomura, T., and Fujii, K., Generation of Acoustic Disturbances in Supersonic Laminar Cavity Flows, International Journal of Acoustics and Vibration, 20(3), 135-142, 2015.
(31) Huang, H., Li, W.(*), and Wang, F., Slat Noise Suppression with Mass Injection, Journal of Aircraft, 52(1), 31-41, 2015.
(32) Wu, X. and Li, W.(*), Effect of Initialized Method on the Three-dimensional Secondary Wake Instability of Elongated Bluff Body, Procedia Engineering, 126, 93-97, 2015.
(33) Qiu, S, Liu, H.(*), and Li, W., Turbofan Duct Geometry Optimization for Low Noise using Remote Continuous Adjoint Method, Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 0954406214532631, 2014.
(34) 张屹, 李伟鹏(*), 王福新, 向阳, 李子佳, 大气压下介质阻挡放电等离子体诱导起始涡的实验研究, 上海交通大学学报, 48(8), 1097-1102, 2014.
(35) Huang, H., Li, W.(*), and Wang, F., Slat Noise Suppression using Upstream Mass Injection, Journal of Shanghai Jiaotong University (Science), 18(5), 620-629, 2013.
(36) Li, W., Nonomura, T., and Fujii, K.(*), Mechanism of Controlling Supersonic Cavity Oscillations using Upstream Mass Injections, Physics of Fluids, 25, 086101, 2013.
(37) Li, W., Nonomura, T., and Fujii, K.(*), On the Feedback Mechanism in Supersonic Cavity Flows, Physics of Fluids, 25, 056101, 2013.
(38) Li, W., Nonomura, T., Oyama, A., and Fujii, K.(*), Feedback Mechanism in Supersonic Laminar Cavity Flows, AIAA Journal, 51(1), 253-257, 2013.
(39) Li, W., Nonomura, T., and Fujii, K., Noise Control of Supersonic Cavity Flow with Upstream Mass Blowing, Notes on Numerical Fluid Mechanics and Multidisciplinary Design: Progress in Hybrid RANS/LES Modeling, 117,315-324, 2013.
(40) Nonomura, T., Li, W., Goto, Y., and Fujii, K.(*), Improvements of Efficiency in Seventh-order Weighted Compact Nonlinear Scheme, CFD Journal, 18(2), 180-186, 2011.
(41) 鲍文, 李伟鹏, 常军涛, 基于遗传算法的高超声速进气道自动优化设计, 系统仿真学报,24(4), 29-32, 2012.
(42) 鲍文, 李伟鹏, 常军涛, 基于FLUENT/MATLAB接口的分布参数系统闭环控制仿真, 系统仿真学报, 20(11), 2851-2854, 2008.

 

学术兼职

(1)《空气动力学报》、《实验流体力学》青年编委;

(2) JFM、PRF、POF、航空学报、推进技术等期刊的审稿人;

(3)中国空气动力研究与发展中心气动噪声控制重点实验室,流动专家;

(4)中国商飞大飞机噪声研究与控制联合实验室,学术委员。

 

荣誉奖励

(1)Award of Project Morning Star: Plan B, Shanghai Jiaotong University, 2016.


(2)Young Excellent Teacher Award, Lanxin Li Fund, Shanghai Jiaotong University, 2016.


(3)Best employee, Dept. Aeronautics and Astronautics, Shanghai Jiaotong University, 2015.

(4)Research assistant, GCOE program, University of Tokyo, 2010/04.


(5)Research assistant, Institute of Space and Aeronautical Science/JAXA, 2009/05.


(6)Research assistant, Department of Aeronautics and Astronautics, University of Tokyo, 2008/12.

(7)Excellent Student Example of Colleges, selected one in Aerospace Department, Harbin Institute of Technology,2007/10.

(8)Excellent Graduate Student Scholarship, Harbin Institute of Technology, 2007/07

(9)Champion of Technology Innovation for Undergraduate Students, Harbin Institute of Technology, 20006/05.

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