dafabet黄金手机版 - 歡迎您!

职称:副研究员

电话:86+10+62796709

E-mail address:wangliang12@tsinghua.edu.cn

个人简介

流体力学博士,某领域专家,清华大学跨介质科学校级平台高速部部长,dafabet黄金手机版副研究员。长期致力于从事航空航天领域的流体力学研究,高超声速流动与叶轮机械流动转捩/湍流模拟,高精度高效率气动优化设计方法,人工智能与流体力学交叉研究。发表论文50余篇、专利5项,译著1本,主持国家自然科学基金4项,子课题负责973课题、民机专项6项。参与中欧合作、国家自然科学基金等课题十余项。主讲《流动稳定性理论及其应用》、《湍流模拟及其应用》等。

地址:清华大学dafabet黄金手机版,蒙民伟科技大楼北楼N727,100084,北京

教育背景

2003.9-2008.7,清华大学dafabet黄金手机版,流体力学专业,工学博士

1999.9-2003.7,清华大学dafabet黄金手机版,动力工程及工程热物理专业,工学学士

工作履历

2012.1 -今,清华大学dafabet黄金手机版工程力学系流体力学研究所,讲师、副研究员

2016.11-2017.10,美国普林斯顿大学机械与航空工程系,访问学者

2008.10-2011.12,德国柏林工业大学流体力学与声学研究所,博士后

学术兼职

Journal of Aerospace Science and Technology编委

SN Applied Science编委

《气体物理》编委

《空天技术》编委

社会兼职

国家工信安全中心知识产权鉴定专家

研究领域

高超声速流动失稳与转捩的机理与模式理论;

湍流模式理论、模拟方法以及飞行器边界层减阻、流动控制等;

高精度高效率气动优化设计、降噪方法,人工智能与流体力学交叉研究

奖励与荣誉

2019年,某技术发明进步二等奖

2019年,中国空气动力学会科学技术奖二等奖, 可压缩湍流生成机理与创新应用

学术成果

已发表国际SCI期刊论文20余篇,主要发表在AIAA Journal、Journal of Fluid Mechanics、PRF(3)、Chinese Journal of Aeronautics、Physics of Fluids等航空航天和流体力学等顶级期刊上(* 通讯作者)。

Chen X, Wang L, Fu S. Energy transfer of hypersonic and high¬-enthalpy boundary layer instabilities and transition. Physical Review Fluids, 2022, 7(3), 033901

Huang Y, Wang L, Fu S. Drag reduction in turbulent channel flows by a spanwise traveling wave of wall blowing and suction. Physics of Fluids, 2021, 33(3): 34132.

Zhang BS, Wang L, Fu S, Mao Z Y, Ding, W J. A novel V-shaped layout method for VIV hydrokinetic energy converters inspired by geese flying in a V-Formation. Energy, 2021, 230: 120811.

Chen XL, Wang L, Fu S. Secondary instability of the hypersonic high-enthalpy boundary layers with thermal-chemical nonequilibrium effects. Physics of Fluids, 2021, 33(3): 34132.

Xi YC, Wang L, Fu S, Ren J. Receptivity and stability of hypersonic leading-edge sweep flows around a blunt body. Journal of Fluid Mechanics, R2; PII S0022112021002172

Chen XL, Wang L, Fu S. Parabolized Stability Analysis of Hypersonic Thermal-Chemical Nonequilibrium Boundary-Layer Flows. AIAA Journal, 2021, 59(7): 2382-2395.

Ji JC, Wang C, Wang L*, Fu S.A recursive approach for aeroacoustic phased array measurements in wind tunnels. Journal of the Acoustical Society of America, 2021, 150 (1): 417-427.

Xue Y, Wang L, Wang Z J, Fu S. Gap-induced transition via oblique breakdown at Mach 6. Shock Waves, 2019, 29(8):1181-1190.

Ji JC, Wang L*, Fu S. An intelligent algorithm for coherent sound source localization based on a strong tracking filter. Chinese Journal of Aeronautics, 2019, 32(8): 1895-1902.

Sun WQ, Zhang TH, Wang L, Ju YG. Effects of Low-Temperature Chemistry and Turbulent Transport on Knocking Formation for Stratified Dimethyl Ether/Air Mixtures. Combustion and Flame, 2019, 200: 342-353.

Wang Z, Wang L, Wang QY, Xue SJ, Fu S. Control of crossflow instability over a swept wing using dielectric-barrier-discharge plasma actuators. International Journal of Heat and Fluid Flow, 2018, 73: 209-222.

Xue Y, Wang L*, Fu S. Detached-Eddy Simulation of Supersonic Flow past a Spike-Tipped Blunt Nose. Chinese Journal of Aeronautics, 2018; 31(9): 1815-1821.

Xue Y, Wang L*, Fu S. Drag Reduction and Aerodynamic Shape Optimization for Spike-Tipped Supersonic Blunt Nose. Journal of Spacecraft and Rockets, 2018; 55(3): 552-560.

Wang L, Hu RY, Li LY, Fu S. Detached-Eddy Simulations for Active Flow Control. AIAA Journal, 2018; 56(4): 1447-1462.

Wang L, Fu S. Detached-Eddy Simulation of flow past a pitching NACA 0015 airfoil with pulsed actuation. Aerospace Science and Technology, 2017; 69: 123-135.

Wang Z, Wang L*, Fu S. Control of stationary crossflow modes in swept Hiemenz flows with dielectric barrier discharge plasma actuators. Physics of Fluids, 2017; 29: 094105.

Wang L, Li LY, Fu S. A comparative study of DES type methods for mild flow separation prediction on a NACA0015 airfoil. International Journal of Numerical Methods for Heat and Fluid Flow, 2017; 27(11): 2528-2543.

Wang L, Zhao YX, Fu S. Computational Study of Drag Increase due to Wall Roughness for Hypersonic Flight. Aeronautical Journal, 2017; 121: 395-415.

Wang L, Xiao L, Fu S. A modular RANS approach for modeling hypersonic flow transition on a scramjet-forebody configuration. Aerospace Science and Technology, 2016; 56: 112-124.

Hu RY, Wang L, Fu S. Investigation of the coherent structures in flow behind a backward-facing step. International Journal of Numerical Methods for Heat and Fluid Flow, 2016; 26(3/4): 1050-1068.

Fu S, Wang L. RANS modeling of high-speed aerodynamic flow transition with consideration of stability theory. Progress in Aerospace Sciences, 2013; 58: 36-59.

Wang L*, Fu S, Carnarius A, Mockett C, Thiele F. A modular RANS approach for modeling laminar-turbulent transition in turbomachinery flows. International Journal of Heat and Fluid Flow, 2012; 34: 62-69.

Wang L, Fu S. Development of an intermittency equation for the modeling of the supersonic/hypersonic boundary layer flow Transition. Flow, Turbulence and Combustion, 2011; 87(1): 165-187.

Wang L, Fu S. Modelling flow transition in hypersonic boundary layer with Reynolds-averaged Navier-Stokes approach. Science in China Series G: Physics Mechanics and Astronomy, 2009; 52(5): 768-774.

Wang L, Zhang GH, Fu S. Pattern formation in Rayleigh-Bénard convection: Numerical simulation with a coupled-map-lattice model. Chinese Science Bulletin, 50(5): 399-406, 2005.