Feature selection and processing of turbulence modeling based on an artificial neural network Y Yin, P Yang, Y Zhang, H Chen, S Fu Physics of Fluids 32 (10), 2020 | 84 | 2020 |
Supercritical natural laminar flow airfoil optimization for regional aircraft wing design Y Zhang, X Fang, H Chen, S Fu, Z Duan, Y Zhang Aerospace Science and Technology 43, 152-164, 2015 | 77 | 2015 |
Aeroacoustic prediction of a multi-element airfoil using wall-modeled large-eddy simulation Y Zhang, H Chen, K Wang, M Wang AIAA Journal 55 (12), 4219-4233, 2017 | 70 | 2017 |
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 |
Supercritical wing design based on airfoil optimization and 2.75 D transformation T Zhao, Y Zhang, H Chen, Y Chen, M Zhang Aerospace Science and Technology 56, 168-182, 2016 | 50 | 2016 |
Numerical study of an airfoil with riblets installed based on large eddy simulation Y Zhang, H Chen, S Fu, W Dong Aerospace Science and Technology 78, 661-670, 2018 | 48 | 2018 |
Learning the aerodynamic design of supercritical airfoils through deep reinforcement learning R Li, Y Zhang, H Chen AIAA Journal 59 (10), 3988-4001, 2021 | 46 | 2021 |
A low dissipation numerical scheme for implicit large eddy simulation Z Li, Y Zhang, H Chen Computers & Fluids 117, 233-246, 2015 | 40 | 2015 |
Improvement to patched grid technique with high-order conservative remapping method Y Zhang, H Chen, S Fu Journal of aircraft 48 (3), 884-893, 2011 | 40 | 2011 |
Pressure distribution guided supercritical wing optimization LI Runze, D Kaiwen, Y Zhang, C Haixin Chinese Journal of Aeronautics 31 (9), 1842-1854, 2018 | 39 | 2018 |
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 | 35 | 2006 |
Performance prediction of conical nozzle using navier–stokes computation Y Zhang, H Chen, M Zhang, M Zhang, Z Li, S Fu Journal of Propulsion and Power 31 (1), 192-203, 2015 | 33 | 2015 |
Aerodynamic prediction of iced airfoils based on modified three-equation turbulence model H Li, Y Zhang, H Chen AIAA Journal 58 (9), 3863-3876, 2020 | 29 | 2020 |
Transonic nacelle aerodynamic optimization based on hybrid genetic algorithm X Fang, Y Zhang, S Li, H Chen 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 3833, 2016 | 29 | 2016 |
Drag prediction method of powered-on civil aircraft based on thrust drag bookkeeping Y Zhang, H Chen, S Fu, M Zhang, M Zhang Chinese Journal of Aeronautics 28 (4), 1023-1033, 2015 | 29 | 2015 |
Numerical study of a supercritical airfoil/wing with variable-camber technology NIU Wei, Y Zhang, C Haixin, M Zhang Chinese Journal of Aeronautics 33 (7), 1850-1866, 2020 | 24 | 2020 |
A Karman-Vortex Generator for passive separation control in a conical diffuser YF Zhang, HX Chen, S Fu Science China Physics, Mechanics and Astronomy 55, 828-836, 2012 | 24 | 2012 |
U or V shape: Dissipation effects on cylinder flow implicit large-eddy simulation H Chen, Z Li, Y Zhang AIAA Journal 55 (2), 459-473, 2017 | 23 | 2017 |
Numerical study of iced airfoils with horn features using large-eddy simulation M Xiao, Y Zhang, F Zhou Journal of Aircraft 56 (1), 94-107, 2019 | 22 | 2019 |