• 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

• 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

声学

• 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.