1) Wang Q., Gao, J.H., The drag-adjoint field of a circular cylinder wake at Reynolds numbers 20, 100 and 500, Journal of Fluid Mechanics, Vol.730, 2013, pp.145-161.
2) Gao, J.H., A block interface flux reconstruction method for numerical simulation with high order finite difference scheme, Journal of Computational Physics, Vol. 241, 2013, pp.1--17.
3) Gao, J.H., Yang, Z.G., and Li, X.D., An Optimized Spectral Difference Scheme for CAA Problems, Journal of Computational Physics, Vol. 231, 2012, pp.4848--4866.
4) Gao, J.H. and Li, X.D., Large Eddy Simulation of Supersonic Jet Noise from a Circular Nozzle, International Journal of Aeroacoustics, Vol. 10(4), 2011, pp.465--474.
5) 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.
6) 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.
7) Li, X.D. and Gao, J.H., “Numerical Simulation of the Generation Mechanism of Axisymmetric Supersonic Jet Screech Tones,” Physics of Fluids, Vol.17, 085105-1-8, 2005.
8) Gao, J.H. and Li, X.D., “Large Eddy Simulation of the Noise from a Subsonic Jet-Edge System,” AIAA Paper 2010-4014, June 2010.
9) Gao, J.H. and Li, X.D., “Numerical Simulation of Broadband Shock-Associated Noise from A Circular Supersonic Jet,” AIAA Paper 2010-0275, 2010.