| Optimized compact finite difference schemes with maximum resolution JW Kim, DJ Lee AIAA Journal 34 (5), 887-893, 1996 | 356 | 1996 |
| Generalized characteristic boundary conditions for computational aeroacoustics JW Kim, DJ Lee AIAA Journal 38 (11), 2040-2049, 2000 | 329 | 2000 |
| Airfoil noise reductions through leading edge serrations S Narayanan, P Chaitanya, S Haeri, PF Joseph, JW Kim, C Polacsek Physics of Fluids 27 (2), 025109, 2015 | 222 | 2015 |
| On the reduction of aerofoil-turbulence interaction noise associated with wavy leading edges JW Kim, S Haeri, PF Joseph Journal of Fluid Mechanics 792, 526-552, 2016 | 196 | 2016 |
| Performance and mechanism of sinusoidal leading edge serrations for the reductions of turbulence-aerofoil interaction noise P Chaitanya, PF Joseph, S Narayanan, C Vanderwel, JM Turner, JW Kim, ... Journal of Fluid Mechanics 818, 435-464, 2017 | 174 | 2017 |
| Optimised boundary compact finite difference schemes for computational aeroacoustics JW Kim Journal of Computational Physics 225 (1), 995-1019, 2007 | 149 | 2007 |
| Generalized characteristic boundary conditions for computational aeroacoustics, part 2 JW Kim, DJ Lee AIAA Journal 42 (1), 47-55, 2004 | 147 | 2004 |
| The effect of wavy leading edges on aerofoil-gust interaction noise ASH Lau, S Haeri, JW Kim Journal of Sound and Vibration 332 (24), 6234-6253, 2013 | 137 | 2013 |
| Characteristic interface conditions for multiblock high-order computation on singular structured grid JW Kim, DJ Lee AIAA Journal 41 (12), 2341-2348, 2003 | 112 | 2003 |
| Adaptive nonlinear artificial dissipation model for computational aeroacoustics JW Kim, DJ Lee AIAA Journal 39 (5), 810-818, 2001 | 107 | 2001 |
| A large-eddy simulation on a deep-stalled aerofoil with a wavy leading edge R Pérez-Torró, JW Kim Journal of Fluid Mechanics 813, 23-52, 2017 | 86 | 2017 |
| High-order compact filters with variable cut-off wavenumber and stable boundary treatment JW Kim Computers & Fluids 39 (7), 1168-1182, 2010 | 84 | 2010 |
| Efficient parallel computing with a compact finite difference scheme JW Kim, RD Sandberg Computers & Fluids 58, 70-87, 2012 | 83 | 2012 |
| Aeroacoustic source mechanisms of a wavy leading edge undergoing vortical disturbances JM Turner, JW Kim Journal of Fluid Mechanics 811, 582-611, 2017 | 75 | 2017 |
| Landing-gear noise prediction using high-order finite difference schemes W Liu, JW Kim, X Zhang, D Angland, B Caruelle Journal of Sound and Vibration 332 (14), 3517-3534, 2013 | 71* | 2013 |
| An advanced synthetic eddy method for the computation of aerofoil-turbulence interaction noise JW Kim, S Haeri Journal of Computational Physics 287 (1), 1-17, 2015 | 67 | 2015 |
| Broadband noise reduction through leading edge serrations on realistic aerofoils C Paruchuri, N Subramanian, P Joseph, C Vanderwel, J Turner, JW Kim, ... 21st AIAA/CEAS aeroacoustics conference, 2202, 2015 | 58 | 2015 |
| Quasi-disjoint pentadiagonal matrix systems for the parallelization of compact finite-difference schemes and filters JW Kim Journal of Computational Physics 241, 168-194, 2013 | 55 | 2013 |
| Implementation of boundary conditions for optimized high-order compact schemes JW Kim, DJ Lee Journal of Computational Acoustics 5 (02), 177-191, 1997 | 55 | 1997 |
| Leading edge serration geometries for significantly enhanced leading edge noise reductions CC Paruchuri, S Narayanan, P Joseph, JW Kim 22nd AIAA/CEAS Aeroacoustics Conference, 2736, 2016 | 52 | 2016 |
