北京航空航天大学能源与动力工程学院流体机械及工程导师介绍：李晓东

导师详细信息

姓名：李晓东

性别：男

出生年份：1967

职称：教授

院系：能源与动力工程学院

首次聘任导师时间：2004

现聘任导师一级学科名称：动力工程及工程热物理

现聘任导师二级学科名称：流体机械及工程

聘任在第二学科培养博士生专业名称：无

聘任在自主设置学科培养博士生专业名称：流体与声学工程

主要研究方向及特色：（1）气动声学理论、数值与实验研究（航空发动机、飞机机体与短舱）（2）计算气动声学方法研究（高精度格式、边界条件与湍流模拟技术）

电子信箱：lixd@buaa.edu.cn

办公电话：82338579

办公地点：新主楼D320室,北配电楼204房间

通信地址：北京航空航天大学407信箱

个人简介：

1.主要学术及社会兼职

2007年被聘为北航蓝天学者特聘教授，现为流体与声学工程学科和水声工程学科责任教授

美国航空航天协会(AIAA)Associate Fellow,AIAA气动声学技术委员会国际委员,美国声学学会会员，中国工程热物理学会理事，中国声学学会理事，International Journal of Aeroacoustics，《工程热物理学报》与《空气动力学学报》编委。

2.获奖情况

1)2013“大涵道比涡扇发动机排气系统设计技术研究与试验验证”获国防科技进步二等奖；

2）2007入选教育部“新世纪优秀人才”支持计划；

3）2006第八届中国航空学会青年科技奖；

4）2002获第八届霍英东基金会青年教师研究类三等奖；

5）2002“特种功能蜂窝胶接结构制造技术”获国防科工委科技进步三等奖。

3.科研项目情况

近二十年来，李晓东教授先后主持了1项973课题和1项973子课题、8项国家自然科学基金(1项重大项目子项目、6项面上项目和1项青年基金）、2项博士点基金、1项武器装备预研基金、4项航空基础科学基金、1项航空支撑科技基金、10多项来自国内科研院所和国际合作课题的资助。多年来与欧美多所大学的课题组在气动声学领域保持密切的合作交流与研究生交换关系。

4.代表性论著情况

1)Li, X.D., Jiang, M., Gao, J.H., Lin, D.K., Liu, L. and Li, X.Y., “Recent Advances of Computational Aeroacoustics,”Applied Mathematics and Mechanics, Vol.36, Issue 1, 2015, pp.131-140.

2)Liu, Li., Li, X.D. and Hu, F.Q., “Nonuniform-time-step explicit Runge-Kutta scheme for high-order finite difference method，”Computers and Fluids, Vol.105, 2014, pp.166-178.

3)Hu, F.Q., Li, X.D., Li, X.Y. and Jiang, M., “Time Domain Wave Packet Method and Suppression of Instability Waves in Aeroacoustic Computations,” Journal of Fluids Engineering, Vol.136, No.6, 2014.

4)Gao, J.H., Yang, Z.G. and Li, X.D., “An Optimized Spectral Difference Scheme for CAA Problems,” Journal of Computational Physics, Vol. 231, Issue 14, 2012, pp.4848-4866.

5) Li, X.Y., Li, X.D. and Tam, C.K.W., “An Improved Multi-pole Broadband Time Domain Impedance Boundary Condition,” AIAA Journal, Vol. 50, No.4, 2012, pp.980-984.

6）Gao, J.H. and Li, X.D.,“Large Eddy Simulation of Supersonic Jet Noise from a Circular Nozzle,” International Journal of Aeroacoustics, Vol. 10, No. 4, 2011, pp.465-474.

7)Jiang, M., Li, X.D. and Zhou, J.J., “Experimental and Numerical Investigation on Sound Generation from Airfoil-Flow Interaction,” Applied Mathematics and Mechanics, Vol. 32, No. 6, 2011, pp.765-776.

8)Lin, D.K., Li, X.D. and Hu, F.Q., “Absorbing boundary condition for nonlinear Euler equations in primitive variables based on the Perfectly Matched Layer technique,” Computers & Fluids, Vol. 40, 2011, pp. 333-337.

9)Liu, L., Li, X.D. and Hu, F.Q., “Nonuniform Time-step Runge-Kutta Discontinuous Galerkin Method for Computational Aeroacoustics,” Journal of Computational Physics, Vol. 229, Issue 19, 2010, pp.6874-6897.

10)Gao, J.H. and Li, X.D.,“A Multi-Mode Screech Frequency Prediction Formula for Circular Supersonic Jets,” Journal of the Acoustical Society of America, Vol. 127, Issue 3, 2010, pp. 1251-1257.

11)Lin, D.K., Jiang M. And Li, X.D., “A Multi-Time-Step Strategy Based on an Optimized Time Interpolation scheme for Overset Grids,” Journal of Computational Acoustics, Vol.18, No. 2, 2010, pp.131-148.

12)Yu, C., Zhou, Z.F., Zhuang, M., Li, X. D., Thiele, F., “An Effective Far-Field Acoustic Prediction Method and Its CAA Applications,” AIAA Journal, Vol. 47, No.2, 2009, pp.410-417.

13)Li, X.D. and Gao, J.H., “Numerical Simulation of the Three Dimensional Screech Phenomenon from a Circular Jet,” Physics of Fluids, Vol. 20, Issue 3, 035101, 2008.

14)Hu，F.Q., Li, X.D. and Lin, D.K., “Absorbing boundary conditions for nonlinear Euler and Navier-Stokes equations based on the Perfectly Matched Layer Technique,” Journal of Computational Physics , Vol. 227, Issue 9, 2008, pp. 4398-4424.

15)Richter, C., Thiele, F.，Li, X.D. and Zhuang, M., “Comparison of Time-Domain Impedance Boundary Conditions by Lined Axisymmetric Duct Flows,” AIAA Journal, Vol. 45, No.6, 2007, pp.1333-1345.

16)Li, X.D.，Richter, C. and Thiele, F., “Time-Domain Impedance Boundary Conditions for Surfaces with Subsonic Mean Flows,” Journal of the Acoustical Society of America, Vol. 119, No.5, May 2006, pp.2665-2676.

17)Li, X.D. and Gao, J.H., “Numerical Simulation of the Generation Mechanism of Axisymmetric Supersonic Jet Screech Tones,” Physics of Fluids, Vol.17, Issue 8, 085105, 2005.

18)Li, X.D.，Schemel, C., Michel, U. and Thiele, F., “Azimuthal Sound Mode Propagation in Axisymmetric Flow Ducts,” AIAA Journal, Vol. 42, No.10, 2004, pp.2019-2027.

19)Luo, J.and Li, X.D., “An Inverse Aeroacoustic Problem on Rotor Wake/Stator Interaction，”Journal of Sound and Vibration, Vol.254, No.2, 2002, pp.219-229.

20)Li, X.D., and Zhou, S., “Spatial Transformation of the Discrete Sound Field from a Propeller,” AIAA Journal, Vol.34, No.6, 1996, pp.1097-1102.

21)Wang, T.Q., Li, X.D. and Zhou, S., “Some Improvements of Acoustic Near-Field Prediction Model of Multiple Propeller Aircraft,” Science in China (Series A), Vol. 38, No. 3, March 1995, pp.376-384.

5.主讲课程

1）基础声学（硕士生，48学时）

2）计算气动声学（硕士生，32学时）

3）气动声学和噪声控制（本科生，32学时）

6.人才培养情况

在读博士生7人，在读硕士生3人。已培养博士后2人、博士8人、硕士21人，其中1人被评为北航优秀博士论文，3人被评为北航优秀硕士论文，2人被评为国防科工委优秀毕业生。