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创新资源平台
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李伟鹏(教授)

所属单位:上海交通大学航天航空学院

担任职务:

擅长领域:

联系方式:021-34208076 邮箱:登录后查看

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

主要成就

(1)Li, W., Fan, Y., Modesti, D., and Cheng, C., Decomposition of the mean skin-friction drag in compressible channel flows, Journal of Fluid Mechanics, 2019, accepted.

(2)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, 2019, 870, 1037-1071.

(3)Li, W. and Liu, H., Two-point Statistics of Coherent Structures in Turbulent Flow over Riblet- mounted Surface, Acta Mechanica Sinica, 2019, 35(3), 457-471.

(4)Fan, Y., Cheng, C., and Li, W.(*), Effects of Reynolds number on the mean skin friction decompo- sition in turbulent channel flows, Applied Mathematics and Mechanics, 2019, 40(3), 331-342.

(5)Li, W. and Liu, H., Numerical study of shock-wave/boundary-layer interaction control using a backward facing step, Aerospace Science and Technology, 2019, 284, 1011-1019.

(6)Fan, Y. and Li, W.(*), Review of Far-Field Drag Decomposition Methods for Aircraft Design, Journal of Aircraft, 2019, 56(1), 11-21.

(7)Li, W. and Wang, L., Geometrical structure analysis of the zero-pressure-gradient turbulent boundary layer, Journal of Fluid Mechanics, 2018, 846, 318-340.

(8)Li, W. and Liu, H., Noise Generation in Flow over a Full-span Trailing-edge Flap, AIAA Journal, 55(2), 2017, 561-571.

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, 2018, 26(8), 372-409.

(9)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,2018, 39(1):177-187.

(10)Li, W. Generation of Acoustic Disturbances in Supersonic Laminar Cavity Flows, International Journal of Acoustics and Vibration, 2015. 20(3), pp. 135-142.

(11)Huang, H., Li, W.,(*) and Wang, F., Slat Noise Suppression with Mass Injection, Journal of Aircraft, 52(1), 2015, 31-41.

(12)Wu, X. and Li, W. Effect of Initialized Method on the Three-dimensional Secondary Wake Instability of Elongated Bluff Body, Procedia Engineering, 2015, 126:93-97.

(13)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, 2014: 0954406214532631.

(14)Weipeng Li 3 Li, W., Nonomura, T., and Fujii, K., Mechanism of Controlling Supersonic Cavity Oscillations using Upstream Mass Injections, Physics of Fluids, 25, 2013, 086101.

(15)Li, W., Nonomura, T., and Fujii, K., On the Feedback Mechanism in Supersonic Cavity Flows, Physics of Fluids, 25, 2013, 056101.

(16)Li, W., Nonomura, T., Oyama, A., and Fujii, K., Feedback Mechanism in Supersonic Laminar Cavity Flows, AIAA Journal, 51(1), 2013, 253-257.

(17)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.

(18)Huang, H., Li, W., and Wang, F., Slat Noise Suppression using Upstream Mass Injection, Journal of Shanghai Jiaotong University (Science), 2013, 18(5), 620-629.

(19)Nonomura, T., Li, W., Goto, Y., and Fujii, K., Improvements of Efficiency in Seventh-order Weighted Compact Nonlinear Scheme, CFD Journal, 18(2), 2011, 180-186.

(20)Zhang, Y., Li, W., Wang, F., Experimental Study of Starting Vortex Induced by Atmospheric Dielectric Barrier Discharge Plasma Actuator, Journal of Shanghai Jiaotong University, 2014, 48(8), 1097-1102. (in Chinese).

(21)Bao, W., Li, W., Chang, J., Automatic Optimization of Hypersonic Inlet Using Genetic Algorithm Based on Real-time CFD Flow Solver, Journal of System Simulation, 24(4), 2012, 765-768. (in Chinese).

(22)Bao, W., Li, W., Chang, J., Fu, H., The Closed-loop Control of Distributed Parameter System Based on FLUENT/MATLAB Interface Technique, Journal of System Simulation, 20(11), 2008, 2851-2854. (in Chinese).