Damiano Casalino
Damiano Casalino
Exa Corporation & Delft University of Technology
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Cited by
An advanced time approach for acoustic analogy predictions
D Casalino
Journal of Sound and Vibration 261 (4), 583-612, 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
Aircraft noise reduction technologies: A bibliographic review
D Casalino, F Diozzi, R Sannino, A Paonessa
Aerospace Science and Technology 12 (1), 1-17, 2008
Turbofan broadband noise prediction using the lattice Boltzmann method
D Casalino, A Hazir, A Mann
AIAA Journal 56 (2), 609-628, 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
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
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
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
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
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
Towards full aircraft airframe noise prediction: lattice Boltzmann simulations
MR Khorrami, E Fares, D Casalino
20th AIAA/CEAS aeroacoustics conference, 2481, 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
Rotorcraft blade-vortex interaction noise prediction using the Lattice-Boltzmann method
G Romani, D Casalino
Aerospace Science and Technology 88, 147-157, 2019
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
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
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
Fan tonal and broadband noise simulations at transonic operating conditions using lattice-Boltzmann methods
I Gonzalez-Martino, D Casalino
2018 AIAA/CEAS aeroacoustics conference, 3919, 2018
Facing rim cavities fluctuation modes
D Casalino, AFP Ribeiro, E Fares
Journal of Sound and Vibration 333 (13), 2812-2830, 2014
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
Community noise of urban air transportation vehicles
D Casalino, WC van der Velden, G Romani
AIAA Scitech 2019 Forum, 1834, 2019
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