Dr.-Ing. Ehab Fares (MBA)
Dr.-Ing. Ehab Fares (MBA)
Director of Aerodynamics, Thermal, Acoustics at Lotus
Verified email at
Cited by
Cited by
Unsteady flow simulation of the Ahmed reference body using a lattice Boltzmann approach
E Fares
Computers & fluids 35 (8-9), 940-950, 2006
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
Numerical simulation of fluidic actuators for flow control applications
V Vatsa, M Koklu, I Wygnanski
6th AIAA Flow control Conference, 3239, 2012
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
Towards full aircraft airframe noise prediction: lattice Boltzmann simulations
MR Khorrami, E Fares, D Casalino
20th AIAA/CEAS aeroacoustics conference, 2481, 2014
A differential equation for approximate wall distance
E Fares, W Schröder
International journal for numerical methods in fluids 39 (8), 743-762, 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
Facing rim cavities fluctuation modes
D Casalino, AFP Ribeiro, E Fares
Journal of Sound and Vibration 333 (13), 2812-2830, 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
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
Numerical Simulation of the Interaction of Wingtip Vortices and Engine Jets in the Near Field
E Fares, M Meinke, W Schroder
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
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
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
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
Simulation-based airframe noise prediction of a full-scale, full aircraft
MR Khorrami, E Fares
22nd AIAA/CEAS aeroacoustics conference, 2706, 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
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
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
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
The system can't perform the operation now. Try again later.
Articles 1–20