李晓东



工作经历

  • 1997/1 - 1998/1,德国宇航研究院 客座科学家
  • 1998/2 - 2001/9,柏林工业大学 客座科学家
  • 1995/7 - 1998/6,北京航空航天大学 能源与动力工程学院 讲师
  • 1998/7 - 2002/6,北京航空航天大学 能源与动力工程学院 副教授
  • 2002/7至现在,北京航空航天大学 能源与动力工程学院 教授

学习经历

  • 2002,国防科学技术进步三等奖
  • 2007,教育部新世纪人才支持计划
  • 2009,AIAA Associate Fellow
  • 2013,国防科学技术进步二等奖

代表文章

C. Chen, X. D. Li and F. Thiele, “Numerical study on non-locally reacting behavior of nacelle liners incorporating drainage slots,” Journal of Sound and Vibration, 424, 2018.
J. H., Gao, X. Xu, and X. D. Li, “Numerical simulation of supersonic twin-jet noise with high-order finite difference scheme,” AIAA Journal, 56(1), 2018.
J. H., Gao and X. D. Li, “An improved grid block interface flux reconstruction method for high order finite difference scheme,” AIAA Journal, 53(7), 2015.
L. Liu, X.D. Li and F. Q. Hu, “Nonuniform-time-step explicit Runge-Kutta scheme for high-order finite difference method,” Computers and Fluids, 105, 2014.
J. H. Gao, Z. G. Yang, and X. D. Li, “An optimized spectral difference scheme for CAA problems,” Journal of Computational Physics, 231(14), 2012.
X.Y. Li, X. D. Li and C. K. W. Tam, “An improved multi-pole broadband time domain impedance boundary condition,” AIAA Journal, 50(4), 2012.
L. Liu, X. D. Li and F. Q. Hu, “Nonuniform time-step Runge-Kutta discontinuous Galerkin method for Computational Aeroacoustics,” Journal of Computational Physics, 229(19), 2010.
J. H. Gao and X. D. Li, “A multi-mode screech frequency prediction formula for circular supersonic jets,” Journal of the Acoustical Society of America,  127(3),  2010.
F. Q. Hu,X. D. Li, and D. K. Lin, “Absorbing boundary conditions for nonlinear Euler and Navier-Stokes equations based on the perfectly matched layer technique,” Journal of Computational Physics, 227(9), 2008.
X. D. Li and J. H. Gao, “Numerical simulation of the three dimensional screech phenomenon from a circular jet,” Physics of Fluids, 20(3), 035101, 2008.
X. D. Li,C. Richter, and F. Thiele, “Time-domain impedance boundary conditions for surfaces with subsonic mean flows,” Journal of the Acoustical Society of America, 119(5), 2006.
X. D. Li and J. H. Gao, “Numerical simulation of the generation mechanism of axisymmetric supersonic jet screech tones,” Physics of Fluids, 17(8), 085105, 2005.
X. D. Li,C. Schemel, U. Michel and F. Thiele, “Azimuthal sound mode propagation in axisymmetric flow ducts,” AIAA Journal, 42(10), 2004.
J. Luo and X. D. Li, “An inverse aeroacoustic problem on rotor wake/stator interaction,”Journal of Sound and Vibration, 254(2), 2002.
X. D. Li, and S. Zhou, “Spatial transformation of the discrete sound field from a propeller,” AIAA Journal, 34(6), 1996.