| Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack X Li, D Fu, Y Ma Physics of Fluids 22 (2), 2010 | 161 | 2010 |
| Direct numerical simulation of hypersonic boundary layer transition over a blunt cone X Li, D Fu, Y Ma AIAA journal 46 (11), 2899-2913, 2008 | 96 | 2008 |
| Mach-number-invariant mean-velocity profile of compressible turbulent boundary layers YS Zhang, WT Bi, F Hussain, XL Li, ZS She Physical Review Letters 109 (5), 054502, 2012 | 81 | 2012 |
| Direct numerical simulation of compressible turbulent flows XL Li, DX Fu, YW Ma, X Liang Acta Mechanica Sinica 26 (6), 795-806, 2010 | 78 | 2010 |
| Direct numerical simulation of shock/turbulent boundary layer interaction in a supersonic compression ramp XL Li, DX Fu, YW Ma, X Liang Science China Physics, Mechanics and Astronomy 53, 1651-1658, 2010 | 75 | 2010 |
| Direct numerical simulation of a spatially evolving supersonic turbulent boundary layer at Ma= 6 L Xin-Liang, F De-Xun, M Yan-Wen Chinese Physics Letters 23 (6), 1519, 2006 | 66 | 2006 |
| Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp F Tong, X Li, Y Duan, C Yu Physics of Fluids 29 (12), 2017 | 63 | 2017 |
| Direct numerical simulation of supersonic turbulent boundary layer flow G Hui, F De-Xun, M Yan-Wen, L Xin-Liang Chinese Physics Letters 22 (7), 1709, 2005 | 63 | 2005 |
| Effects of wall temperature on boundary layer stability over a blunt cone at Mach 7.99 X Liang, X Li, D Fu, Y Ma Computers & fluids 39 (2), 359-371, 2010 | 62 | 2010 |
| All-speed Roe scheme for the large eddy simulation of homogeneous decaying turbulence X Li, X Li International Journal of Computational Fluid Dynamics 30 (1), 69-78, 2016 | 61 | 2016 |
| Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner: Turning angle effects F Tong, C Yu, Z Tang, X Li Computers & Fluids 149, 56-69, 2017 | 52 | 2017 |
| Optimized sixth‐order monotonicity‐preserving scheme by nonlinear spectral analysis X Li, Y Leng, Z He International Journal for Numerical Methods in Fluids 73 (6), 560-577, 2013 | 50 | 2013 |
| 可压缩湍流直接数值模拟 傅德薰 科学出版社, 2010 | 50 | 2010 |
| Numerical study on wall temperature effects on shock wave/turbulent boundary-layer interaction XK Zhu, CP Yu, FL Tong, XL Li AIAA Journal 55 (1), 131-140, 2017 | 38 | 2017 |
| Wall shear stress and wall heat flux in a supersonic turbulent boundary layer F Tong, S Dong, J Lai, X Yuan, X Li physics of fluids 34 (1), 2022 | 36 | 2022 |
| Effect of wall temperature on the kinetic energy transfer in a hypersonic turbulent boundary layer D Xu, J Wang, M Wan, C Yu, X Li, S Chen Journal of Fluid Mechanics 929, A33, 2021 | 36 | 2021 |
| Acoustic calculation for supersonic turbulent boundary layer flow L Xin-Liang, F De-Xun, M Yan-Wen, G Hui Chinese Physics Letters 26 (9), 094701, 2009 | 35 | 2009 |
| DNS of a spatially evolving hypersonic turbulent boundary layer at Mach 8 X Liang, XL Li Science China Physics, Mechanics and Astronomy 56, 1408-1418, 2013 | 34 | 2013 |
| Compressibility effect in hypersonic boundary layer with isothermal wall condition D Xu, J Wang, M Wan, C Yu, X Li, S Chen Physical Review Fluids 6 (5), 054609, 2021 | 32 | 2021 |
| Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner F Tong, X Li, X Yuan, C Yu Computers & Fluids 198, 104385, 2020 | 32 | 2020 |
