| Unsteady flow simulation of the Ahmed reference body using a lattice Boltzmann approach E Fares Computers & fluids 35 (8-9), 940-950, 2006 | 214 | 2006 |
| Numerical simulation of fluidic actuators for flow control applications V Vatsa, M Koklu, I Wygnanski 6th AIAA Flow control Conference, 3239, 2012 | 85 | 2012 |
| Lattice–Boltzmann aeroacoustic analysis of the LAGOON landing-gear configuration D Casalino, AFP Ribeiro, E Fares, S Nölting AIAA journal 52 (6), 1232-1248, 2014 | 84 | 2014 |
| A general one-equation turbulence model for free shear and wall-bounded flows E Fares, W Schröder Flow, turbulence and combustion 73, 187-215, 2005 | 80 | 2005 |
| A differential equation for approximate wall distance E Fares, W Schröder International journal for numerical methods in fluids 39 (8), 743-762, 2002 | 76 | 2002 |
| Unsteady flow simulation of a high-lift configuration using a lattice Boltzmann approach E Fares, S Noelting 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2011 | 68 | 2011 |
| Facing rim cavities fluctuation modes D Casalino, AFP Ribeiro, E Fares Journal of Sound and Vibration 333 (13), 2812-2830, 2014 | 54 | 2014 |
| Validation of a lattice-Boltzmann approach for transonic and supersonic flow simulations E Fares, M Wessels, R Zhang, C Sun, N Gopalaswamy, P Roberts, J Hoch, ... 52nd Aerospace Sciences Meeting, 0952, 2014 | 50 | 2014 |
| Airframe noise prediction of a full aircraft in model and full scale using a lattice Boltzmann approach E Fares, B Duda, MR Khorrami 22nd AIAA/CEAS Aeroacoustics Conference, 2707, 2016 | 41 | 2016 |
| Advanced noise control fan direct aeroacoustics predictions using a Lattice-Boltzmann method A Mann, F Perot, MS Kim, D Casalino, E Fares 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference …, 2012 | 41 | 2012 |
| Numerical Simulation of the Interaction of Wingtip Vortices and Engine Jets in the Near Field E Fares, M Meinke, W Schroder | 41 | 2000 |
| Towards numerical aircraft noise certification: Analysis of a full-scale landing gear in fly-over configuration D Casalino, S Noelting, E Fares, T Van de Ven, F Perot, G Bres 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference …, 2012 | 37 | 2012 |
| Evaluation of airframe noise reduction concepts via simulations using a lattice Boltzmann approach E Fares, D Casalino, MR Khorrami 21st AIAA/CEAS Aeroacoustics Conference, 2988, 2015 | 33 | 2015 |
| Towards Lattice-Boltzmann prediction of turbofan engine noise D Casalino, AF Ribeiro, E Fares, SE Noelting, A Mann, F Perot, Y Li, ... 20th AIAA/CEAS Aeroacoustics Conference, 3101, 2014 | 32 | 2014 |
| Simulation-based airframe noise prediction of a full-scale, full aircraft MR Khorrami, E Fares 22nd AIAA/CEAS aeroacoustics conference, 2706, 2016 | 30 | 2016 |
| Validation of a transonic lattice-Boltzmann method on the NASA common research model B Konig, E Fares 54th AIAA Aerospace Sciences Meeting, 2023, 2016 | 28 | 2016 |
| Comparison of computational and experimental microphone array results for an 18% scale aircraft model DP Lockard, WM Humphreys, MR Khorrami, E Fares, D Casalino, ... International journal of aeroacoustics 16 (4-5), 358-381, 2017 | 24 | 2017 |
| Scale-resolving simulations using a lattice Boltzmann-based approach E Fares, B Duda, AFP Ribeiro, B König CEAS Aeronautical Journal 9 (4), 721-733, 2018 | 22 | 2018 |
| PowerFLOW simulations for the third AIAA high-lift prediction workshop B Konig, E Fares, M Murayama, Y Ito 2018 AIAA Aerospace Sciences Meeting, 1255, 2018 | 21 | 2018 |
| Noise simulations of the high-lift common research model DP Lockard, MM Choudhari, MD O’Connell, BM Duda, E Fares 23rd AIAA/CEAS aeroacoustics conference, 3362, 2017 | 21 | 2017 |
