| On the vortex-induced oscillations of a freely vibrating cylinder in the vicinity of a stationary plane wall Z Li, W Yao, K Yang, RK Jaiman, BC Khoo Journal of Fluids and Structures 65, 495-526, 2016 | 78 | 2016 |
| Model reduction and mechanism for the vortex-induced vibrations of bluff bodies W Yao, RK Jaiman Journal of Fluid Mechanics 827, 357-393, 2017 | 69 | 2017 |
| Prediction of transonic limit-cycle oscillations using an aeroelastic harmonic balance method W Yao, S Marques AIAA journal 53 (7), 2040-2051, 2015 | 55 | 2015 |
| Feedback control of unstable flow and vortex-induced vibration using the eigensystem realization algorithm W Yao, RK Jaiman Journal of Fluid Mechanics 827, 394-414, 2017 | 38 | 2017 |
| Nonlinear aerodynamic and aeroelastic model reduction using a discrete empirical interpolation method W Yao, S Marques AIAA Journal 55 (2), 624-637, 2017 | 33 | 2017 |
| Reduced-order modeling for limit-cycle oscillation using recurrent artificial neural network W Yao, MS Liou 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference …, 2012 | 26 | 2012 |
| Lock-in mechanism of flow over a low-Reynolds-number airfoil with morphing surface W Kang, M Xu, W Yao, J Zhang Aerospace Science and Technology 97, 105647, 2020 | 25 | 2020 |
| Application of a high-order CFD harmonic balance method to nonlinear aeroelasticity W Yao, S Marques Journal of Fluids and Structures 74, 427-444, 2017 | 25 | 2017 |
| A harmonic balance technique for the reduced-order computation of vortex-induced vibration W Yao, RK Jaiman Journal of Fluids and Structures 65, 313-332, 2016 | 20 | 2016 |
| Aerodynamic shape optimization of co-flow jet airfoil using a multi-island genetic algorithm H Jiang, M Xu, W Yao Physics of Fluids 34 (12), 2022 | 15 | 2022 |
| A reduced-order model for gradient-based aerodynamic shape optimisation W Yao, S Marques, T Robinson, C Armstrong, L Sun Aerospace Science and Technology 106, 106120, 2020 | 15 | 2020 |
| A harmonic balance method for nonlinear fluid structure interaction problems W Yao, S Marques Computers & Structures 201, 26-36, 2018 | 15 | 2018 |
| Stability analysis of the wake-induced vibration of tandem circular and square cylinders W Yao, RK Jaiman Nonlinear Dynamics 95 (1), 13-28, 2019 | 14 | 2019 |
| Flutter analysis for turbomachinery using Volterra series MS Liou, W Yao Turbo Expo: Power for Land, Sea, and Air 45776, V07BT35A004, 2014 | 11 | 2014 |
| A generalised force equivalence-based modelling method for a dry wind-tunnel flutter test system Z Zhang, B Gao, J Wang, D Xu, G Chen, W Yao The Aeronautical Journal 125 (1286), 720-741, 2021 | 8 | 2021 |
| A framework of gradient-based shape optimization using feature-based CAD parameterization L Sun, W Yao, T Robinson, S Marques, C Armstrong AIAA Scitech 2020 Forum, 0889, 2020 | 8 | 2020 |
| Flutter analysis for a fin in hypersonic flow Y Dou, M Xu, X An, W YAO 工程力学 26 (11), 232-237, 2009 | 8 | 2009 |
| Automated mesh deformation for computer-aided design models that exhibit boundary topology changes L Sun, W Yao, TT Robinson, CG Armstrong, SP Marques AIAA Journal 58 (9), 4128-4141, 2020 | 7 | 2020 |
| 涡破裂诱导的垂尾抖振数值模拟 韩冰， 徐敏， 蔡天星， 姚伟刚 航空学报 33 (5), 788-795, 2012 | 7 | 2012 |
| Analysis of the post-flutter aerothermoelastic characteristics of hypersonic skin panels using a CFD-based approach E Quan, M Xu, W Yao, X Cheng Aerospace Science and Technology 118, 107076, 2021 | 6 | 2021 |
S. MarquesUniversity of Surrey在 surrey.ac.uk 的电子邮件经过验证
