北京航空航天大學能源與動力工程學院流體機械及工程導師介紹：李曉東

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導師詳細信息

姓名：李曉東

性別：男

出生年份：1967

職稱：教授

院系：能源與動力工程學院

首次聘任導師時間：2004

現聘任導師一級學科名稱：動力工程及工程熱物理

現聘任導師二級學科名稱：流體機械及工程

聘任在第二學科培養博士生專業名稱：無

聘任在自主設置學科培養博士生專業名稱：流體與聲學工程

主要研究方向及特色：（1）氣動聲學理論、數值與實驗研究（航空發動機、飛機機體與短艙）（2）計算氣動聲學方法研究（高精度格式、邊界條件與湍流模擬技術）

電子信箱：lixd@buaa.edu.cn

辦公電話：82338579

辦公地點：新主樓D320室,北配電樓204房間

通信地址：北京航空航天大學407信箱

個人簡介：

1.主要學術及社會兼職

2007年被聘為北航藍天學者特聘教授，現為流體與聲學工程學科和水聲工程學科責任教授

美國航空航天協會(AIAA)Associate Fellow,AIAA氣動聲學技術委員會國際委員,美國聲學學會會員，中國工程熱物理學會理事，中國聲學學會理事，International Journal of Aeroacoustics，《工程熱物理學報》與《空氣動力學學報》編委。

2.獲獎情況

1)2013“大涵道比渦扇發動機排氣系統設計技術研究與試驗驗證”獲國防科技進步二等獎；

2）2007入選教育部“新世紀優秀人才”支持計劃；

3）2006第八屆中國航空學會青年科技獎；

4）2002獲第八屆霍英東基金會青年教師研究類三等獎；

5）2002“特種功能蜂窩膠接結構制造技術”獲國防科工委科技進步三等獎。

3.科研項目情況

近二十年來，李曉東教授先后主持了1項973課題和1項973子課題、8項國家自然科學基金(1項重大項目子項目、6項面上項目和1項青年基金）、2項博士點基金、1項武器裝備預研基金、4項航空基礎科學基金、1項航空支撐科技基金、10多項來自國內科研院所和國際合作課題的資助。多年來與歐美多所大學的課題組在氣動聲學領域保持密切的合作交流與研究生交換關系。

4.代表性論著情況

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.主講課程

1）基礎聲學（碩士生，48學時）

2）計算氣動聲學（碩士生，32學時）

3）氣動聲學和噪聲控制（本科生，32學時）

6.人才培養情況

在讀博士生7人，在讀碩士生3人。已培養博士后2人、博士8人、碩士21人，其中1人被評為北航優秀博士論文，3人被評為北航優秀碩士論文，2人被評為國防科工委優秀畢業生。