| An advanced time approach for acoustic analogy predictions D Casalino Journal of Sound and Vibration 261 (4), 583-612, 2003 | 370 | 2003 |
| A rod-airfoil experiment as a benchmark for broadband noise modeling MC Jacob, J Boudet, D Casalino, M Michard Theoretical and Computational Fluid Dynamics 19, 171-196, 2005 | 343 | 2005 |
| Aircraft noise reduction technologies: A bibliographic review D Casalino, F Diozzi, R Sannino, A Paonessa Aerospace Science and Technology 12 (1), 1-17, 2008 | 244 | 2008 |
| Turbofan broadband noise prediction using the lattice Boltzmann method D Casalino, A Hazir, A Mann AIAA Journal 56 (2), 609-628, 2018 | 184 | 2018 |
| Noise reduction mechanisms of sawtooth and combed-sawtooth trailing-edge serrations F Avallone, WCP Van Der Velden, D Ragni, D Casalino Journal of Fluid Mechanics 848, 560-591, 2018 | 171 | 2018 |
| Prediction of sound generated by a rod–airfoil configuration using EASM DES and the generalised Lighthill/FW-H analogy B Greschner, F Thiele, MC Jacob, D Casalino Computers & fluids 37 (4), 402-413, 2008 | 142 | 2008 |
| Prediction of rod-airfoil interaction noise using the Ffowcs-Williams-Hawkings analogy D Casalino, M Jacob, M Roger AIAA journal 41 (2), 182-191, 2003 | 137 | 2003 |
| Definition of a benchmark for low Reynolds number propeller aeroacoustics D Casalino, E Grande, G Romani, D Ragni, F Avallone Aerospace Science and Technology 113, 106707, 2021 | 134 | 2021 |
| Prediction of aerodynamic sound from circular rods via spanwise statistical modelling D Casalino, M Jacob Journal of Sound and Vibration 262 (4), 815-844, 2003 | 109 | 2003 |
| 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 | 87 | 2014 |
| Aeroacoustic study of a wavy stator leading edge in a realistic fan/OGV stage D Casalino, F Avallone, I Gonzalez-Martino, D Ragni Journal of Sound and Vibration 442, 138-154, 2019 | 83 | 2019 |
| Towards full aircraft airframe noise prediction: lattice Boltzmann simulations MR Khorrami, E Fares, D Casalino 20th AIAA/CEAS aeroacoustics conference, 2481, 2014 | 83 | 2014 |
| Numerical and experimental investigation of flow confinement effects on UAV rotor noise C Nardari, D Casalino, F Polidoro, V Coralic, PT Lew, J Brodie 25th AIAA/CEAS Aeroacoustics Conference, 2497, 2019 | 74 | 2019 |
| Rotorcraft blade-vortex interaction noise prediction using the Lattice-Boltzmann method G Romani, D Casalino Aerospace Science and Technology 88, 147-157, 2019 | 73 | 2019 |
| Performance and noise prediction of low-Reynolds number propellers using the Lattice-Boltzmann method G Romani, E Grande, F Avallone, D Ragni, D Casalino Aerospace Science and Technology 125, 107086, 2022 | 72 | 2022 |
| Noise reduction mechanisms of an open-cell metal-foam trailing edge C Teruna, F Manegar, F Avallone, D Ragni, D Casalino, T Carolus Journal of Fluid Mechanics 898, A18, 2020 | 71 | 2020 |
| Tonal and broadband noise calculations for aeroacoustic optimization of a pusher propeller A Pagano, M Barbarino, D Casalino, L Federico Journal of Aircraft 47 (3), 835-848, 2010 | 69 | 2010 |
| Numerical investigation of leading edge noise reduction on a rod-airfoil configuration using porous materials and serrations C Teruna, F Avallone, D Casalino, D Ragni Journal of Sound and Vibration 494, 115880, 2021 | 68 | 2021 |
| Aeroacoustic investigation of a propeller operating at low Reynolds numbers E Grande, G Romani, D Ragni, F Avallone, D Casalino AIAA Journal 60 (2), 860-871, 2022 | 67 | 2022 |
| Community noise of urban air transportation vehicles D Casalino, WC van der Velden, G Romani AIAA Scitech 2019 Forum, 1834, 2019 | 62 | 2019 |
Dr.-Ing. Ehab Fares (MBA)Chief Engineer Aerodynamics & Director of Attribute Integration at LotusVerified email at eu.lotuscars.com
