Numerical dissipation effects on massive separation around tandem cylinders Z Xiao, J Liu, J Huang, S Fu AIAA journal 50 (5), 1119-1136, 2012 | 84 | 2012 |
Simulation of shock wave buffet and its suppression on an OAT15A supercritical airfoil by IDDES JB Huang, ZX Xiao, J Liu, S Fu Science China Physics, Mechanics and Astronomy 55, 260-271, 2012 | 82 | 2012 |
Improving the k–ω–γ–Ar transition model by the field inversion and machine learning framework M Yang, Z Xiao Physics of Fluids 32 (6), 2020 | 81 | 2020 |
Improved-delayed-detached-eddy simulation of cavity-induced transition in hypersonic boundary layer L Xiao, Z Xiao, Z Duan, S Fu International Journal of Heat and Fluid Flow 51, 138-150, 2015 | 69 | 2015 |
Simulation of wing-body junction flows with hybrid RANS/LES methods S Fu, Z Xiao, H Chen, Y Zhang, J Huang International Journal of Heat and Fluid Flow 28 (6), 1379-1390, 2007 | 68 | 2007 |
Investigation of flows around a rudimentary landing gear with advanced detached-eddy-simulation approaches Z Xiao, J Liu, K Luo, J Huang, S Fu AIAA journal 51 (1), 107-125, 2013 | 66 | 2013 |
Prediction of separation flows around a 6: 1 prolate spheroid using RANS/LES hybrid approaches Z Xiao, Y Zhang, J Huang, H Chen, S Fu Acta Mechanica Sinica 23 (4), 369-382, 2007 | 37 | 2007 |
Study of delayed-detached eddy simulation with weakly nonlinear turbulence model Z Xiao, H Chen, Y Zhang, J Huang, S Fu Journal of aircraft 43 (5), 1377-1385, 2006 | 34 | 2006 |
DDES with adaptive coefficient for stalled flows past a wind turbine airfoil J Liu, W Zhu, Z Xiao, H Sun, Y Huang, Z Liu Energy 161, 846-858, 2018 | 32 | 2018 |
Gas kinetic scheme for turbulence simulation S Tan, Q Li, Z Xiao, S Fu Aerospace Science and Technology 78, 214-227, 2018 | 32 | 2018 |
Numerical investigation of unsteady vortex breakdown past 80/65 double-delta wing J Liu, H Sun, Z Liu, Z Xiao Chinese Journal of Aeronautics 27 (3), 521-530, 2014 | 32 | 2014 |
Distributed roughness induced transition on wind-turbine airfoils simulated by four-equation k-ω-γ-Ar transition model M Yang, Z Xiao Renewable energy 135, 1166-1177, 2019 | 30 | 2019 |
Dynamic response of vortex breakdown flows to a pitching double-delta wing J Liu, K Luo, H Sun, Y Huang, Z Liu, Z Xiao Aerospace Science and Technology 72, 564-577, 2018 | 30 | 2018 |
Direct numerical simulation of hypersonic transition induced by an isolated cylindrical roughness element ZW Duan, ZX Xiao, S Fu Science China Physics, Mechanics & Astronomy 57, 2330-2345, 2014 | 28 | 2014 |
Studies of the unsteady supersonic base flows around three afterbodies Z Xiao, S Fu Acta Mechanica Sinica 25 (4), 471-479, 2009 | 28 | 2009 |
Unsteady Transition Studies over a Pitching Airfoil Using a Transition Model J Liu, Z Xiao, S Fu AIAA Journal 56 (9), 3776-3781, 2018 | 25 | 2018 |
Investigation of spectral characteristics by passive control methods past a supersonic cavity K Luo, W Zhu, Z Xiao, Z Weng, L Deng, D Yang, J Liu AIAA Journal 56 (7), 2669-2686, 2018 | 22 | 2018 |
Improved delayed detached-eddy simulations of sawtooth spoiler control before supersonic cavity K Luo, W Zhe, Z Xiao, S Fu International Journal of Heat and Fluid Flow 63, 172-189, 2017 | 21 | 2017 |
Study of control effects of vortex generators on a supercritical wing JB Huang, ZX Xiao, S Fu, M Zhang Science China Technological Sciences 53, 2038-2048, 2010 | 21 | 2010 |
Improved delayed detached-eddy simulation of massive separation around triple cylinders ZX Xiao, KY Luo Acta Mechanica Sinica 31, 799-816, 2015 | 20 | 2015 |