| Analytical models of the wall-pressure spectrum under a turbulent boundary layer with adverse pressure gradient G Grasso, P Jaiswal, H Wu, S Moreau, M Roger Journal of Fluid Mechanics 877, 1007-1062, 2019 | 55 | 2019 |
| Trailing-edge broadband noise prediction of an airfoil with boundary-layer tripping J Winkler, H Wu, S Moreau, T Carolus, RD Sandberg Journal of Sound and Vibration 482, 115450, 2020 | 26 | 2020 |
| Effects of pressure gradient on the evolution of velocity-gradient tensor invariant dynamics on a controlled-diffusion aerofoil at H Wu, S Moreau, RD Sandberg Journal of Fluid Mechanics 868, 584-610, 2019 | 26 | 2019 |
| On the noise generated by a controlled-diffusion aerofoil at Rec= 1.5× 105 H Wu, S Moreau, RD Sandberg Journal of Sound and Vibration 487, 115620, 2020 | 22 | 2020 |
| Direct numerical simulation of the self-noise radiated by the installed controlled-diffusion airfoil at transitional Reynolds number H Wu, M Sanjose, S Moreau, RD Sandberg 2018 AIAA/CEAS Aeroacoustics Conference, 3797, 2018 | 20 | 2018 |
| Adverse-pressure-gradient turbulent boundary layer on convex wall S Pargal, H Wu, J Yuan, S Moreau Physics of Fluids 34 (3), 2022 | 14 | 2022 |
| Numerical study of the installed controlled diffusion airfoil at transitional Reynolds number H Wu, P Laffay, A Idier, P Jaiswal, M Sanjosé, S Moreau Mathematical and Computational Approaches in Advancing Modern Science and …, 2016 | 10 | 2016 |
| Surface pressure spectrum variation with Mach number on a CD airfoil S Shubham, RD Sandberg, S Moreau, H Wu Journal of Sound and Vibration 526, 116762, 2022 | 8 | 2022 |
| Stability characteristics of different aerofoil flows at Rec= 150,000 and the implications for aerofoil self-noise H Wu, RD Sandberg, S Moreau Journal of Sound and Vibration 506, 116152, 2021 | 6 | 2021 |
| On the effect of adverse pressure gradients on wall-pressure statistics in a controlled-diffusion aerofoil turbulent boundary layer A Caiazzo, S Pargal, H Wu, M Sanjosé, J Yuan, S Moreau Journal of Fluid Mechanics 960, A17, 2023 | 4 | 2023 |
| CFD-based prediction of wall-pressure spectra under a turbulent boundary layer with adverse pressure gradient G Grasso, H Wu, S Orestano, M Sanjosé, S Moreau, M Roger CEAS Aeronautical Journal 12, 125-133, 2021 | 4 | 2021 |
| Direct numerical simulation of transitional airfoil noise H Wu, J Winkler, RD Sandberg, S Moreau 23rd AIAA/CEAS Aeroacoustics Conference, 3368, 2017 | 4 | 2017 |
| Shape manipulation of a rotating liquid liner imploded by arrays of pneumatic pistons: Experimental and numerical study NS Mangione, H Wu, C Preston, AMD Lee, S Entezami, R Ségas, ... Fusion Engineering and Design 198, 114087, 2024 | 1 | 2024 |
| Non-equilibrium turbulent boundary layer with adverse pressure gradient and convex wall curvature S Pargal, H Wu, J Yuan, S Moreau APS Division of Fluid Dynamics Meeting Abstracts, Q07-005, 2021 | 1 | 2021 |
| A NURBS-enhanced treatment of curved boundary integrating for the time-accurate upwind scheme with unstructured grids Y Xia, G Wang, CY Loh, T Ji, Y Zheng, H Wu 23rd AIAA Computational Fluid Dynamics Conference, 4298, 2017 | 1 | 2017 |
| A Generalized Corcos model for the prediction of the coherence function in turbulent boundary layers with zero and adverse pressure gradient A Caiazzo, H Wu, S Moreau, M Sanjose AIAA AVIATION 2021 FORUM, 2156, 2021 | | 2021 |
