北京航空航天大學(xué)

導(dǎo)師詳細(xì)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(dòng)力工程學(xué)院

首次聘任導(dǎo)師時(shí)間：2004

現(xiàn)聘任導(dǎo)師一級(jí)學(xué)科名稱：動(dòng)力工程及工程熱物理

現(xiàn)聘任導(dǎo)師二級(jí)學(xué)科名稱：流體機(jī)械及工程

聘任在第二學(xué)科培養(yǎng)博士生專業(yè)名稱：無(wú)

聘任在自主設(shè)置學(xué)科培養(yǎng)博士生專業(yè)名稱：流體與聲學(xué)工程

主要研究方向及特色：（1）氣動(dòng)聲學(xué)理論、數(shù)值與實(shí)驗(yàn)研究（航空發(fā)動(dòng)機(jī)、飛機(jī)機(jī)體與短艙）（2）計(jì)算氣動(dòng)聲學(xué)方法研究（高精度格式、邊界條件與湍流模擬技術(shù)）

電子信箱：lixd@buaa.edu.cn

辦公電話：82338579

辦公地點(diǎn)：新主樓D320室,北配電樓204房間

通信地址：北京航空航天大學(xué)407信箱

個(gè)人簡(jiǎn)介：

1.主要學(xué)術(shù)及社會(huì)兼職

2007年被聘為北航藍(lán)天學(xué)者特聘教授，現(xiàn)為流體與聲學(xué)工程學(xué)科和水聲工程學(xué)科責(zé)任教授

美國(guó)航空航天協(xié)會(huì)(AIAA)Associate Fellow,AIAA氣動(dòng)聲學(xué)技術(shù)委員會(huì)國(guó)際委員,美國(guó)聲學(xué)學(xué)會(huì)會(huì)員，中國(guó)工程熱物理學(xué)會(huì)理事，中國(guó)聲學(xué)學(xué)會(huì)理事，International Journal of Aeroacoustics，《工程熱物理學(xué)報(bào)》與《空氣動(dòng)力學(xué)學(xué)報(bào)》編委。

2.獲獎(jiǎng)情況

1)2013“大涵道比渦扇發(fā)動(dòng)機(jī)排氣系統(tǒng)設(shè)計(jì)技術(shù)研究與試驗(yàn)驗(yàn)證”獲國(guó)防科技進(jìn)步二等獎(jiǎng)；

2）2007入選教育部“新世紀(jì)優(yōu)秀人才”支持計(jì)劃；

3）2006第八屆中國(guó)航空學(xué)會(huì)青年科技獎(jiǎng)；

4）2002獲第八屆霍英東基金會(huì)青年教師研究類三等獎(jiǎng)；

5）2002“特種功能蜂窩膠接結(jié)構(gòu)制造技術(shù)”獲國(guó)防科工委科技進(jìn)步三等獎(jiǎng)。

3.科研項(xiàng)目情況

近二十年來(lái)，李曉東教授先后主持了1項(xiàng)973課題和1項(xiàng)973子課題、8項(xiàng)國(guó)家自然科學(xué)基金(1項(xiàng)重大項(xiàng)目子項(xiàng)目、6項(xiàng)面上項(xiàng)目和1項(xiàng)青年基金）、2項(xiàng)博士點(diǎn)基金、1項(xiàng)武器裝備預(yù)研基金、4項(xiàng)航空基礎(chǔ)科學(xué)基金、1項(xiàng)航空支撐科技基金、10多項(xiàng)來(lái)自國(guó)內(nèi)科研院所和國(guó)際合作課題的資助。多年來(lái)與歐美多所大學(xué)的課題組在氣動(dòng)聲學(xué)領(lǐng)域保持密切的合作交流與研究生交換關(guān)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(xiàn).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(chǔ)聲學(xué)（碩士生，48學(xué)時(shí)）

2）計(jì)算氣動(dòng)聲學(xué)（碩士生，32學(xué)時(shí)）

3）氣動(dòng)聲學(xué)和噪聲控制（本科生，32學(xué)時(shí)）

6.人才培養(yǎng)情況

在讀博士生7人，在讀碩士生3人。已培養(yǎng)博士后2人、博士8人、碩士21人，其中1人被評(píng)為北航優(yōu)秀博士論文，3人被評(píng)為北航優(yōu)秀碩士論文，2人被評(píng)為國(guó)防科工委優(yōu)秀畢業(yè)生。