| 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 | 65 | 2010 |
| Multi-objective aeroacoustic optimization of an aircraft propeller A Pagano, L Federico, M Barbarino, F Guida, M Aversano 12th AIAA/ISSMO multidisciplinary analysis and optimization conference, 6059, 2008 | 40 | 2008 |
| Validation of CIRA's rotorcraft aerodynamic modelling system with DNW experimental data A Visingardi, A D'Alascio, A Pagano, P Renzoni | 29 | 1996 |
| Helicopter blade morphing strategies aimed at mitigating environmental impact A Pagano, S Ameduri, V Cokonaj, A Prachar, Z Zachariadis, D Drikakis Journal of Theoretical and Applied Mechanics 49 (4), 1233-1259, 2011 | 18 | 2011 |
| Ice accretion prediction on helicopter rotor blade in hover flight G Zanazzi, G Mingione, A Pagano, A Visingardi, R Narducci SAE Technical Paper, 2007 | 15 | 2007 |
| Development of a common European unsteady full potential CFD code for helicopter rotors in hover and forward flight M Costes, JC Le Balleur, L Gasparini, L Vigevano, MHL Hounjet, ... | 15 | 1997 |
| Tonal and broadband noise calculations for aeroacoustic optimization of propeller blades in a pusher configuration A Pagano, M Barbarino, D Casalino, L Federico 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference …, 2009 | 13 | 2009 |
| Aerodynamic and aero-acoustic optimization of modern tilt-rotor blades within the ADYN project T Lefebvre, P Beaumier, S Canard, A Pisoni, A Pagano, A Sorrentino, ... OFFICE NATIONAL D ETUDES ET DE RECHERCHES AEROSPATIALES ONERA-PUBLICATIONS-TP, 2004 | 13 | 2004 |
| GEROS: a European grid generator for rotorcraft simulation methods MHL Hounjet, CR Allen, L Gasparini, L Vigevano, A Pagano National Aerospace Laboratory NLR, 1998 | 13 | 1998 |
| First results of the EROS European unsteady Euler code on overlapping grids A D'Alascio, L Dubuc, D Peshkin, L Vigevano, CB Allen, A Pagano, ... Computational Fluid Dynamics' 98 2, 1998 | 10 | 1998 |
| From a battery-based to a PEM fuel cell-based propulsion architecture on a lightweight full electric aircraft: A Comparative Numerical Study G Marinaro, G Di Lorenzo, A Pagano Aerospace 9 (8), 408, 2022 | 8 | 2022 |
| FLARE: An OPA for technology validation used at the Italian aerospace research center L Vecchione, P De Matteis, A Rispoli, L Pellone, U Mercurio, M Di Donato, ... Society of Flight Test Engineer, 47th Annual International Symposium 8 (11), 2016 | 8 | 2016 |
| Helicopter blade twist control through SMA technology: optimal shape prediction, twist actuator realisation and main rotor enhanced performance computation A Pagano, S Ameduri, V Cokonaj, A Prachar, Z Zachariadis, D Drikakis | 8 | 2009 |
| ROSAA: A European simulatation system for the multidisciplinary numerical prediction of rotor phenomena A Pagano, MHL Hounjet, JV Miller, M Gracey, A Pisoni National Aerospace Laboratory NLR, 2000 | 7 | 2000 |
| Tonal and broadband noise calculations for aeroacoustic optimization of propeller blades in a pusher configuration. 15th AIAA/CEAS Aeroacoustics Conference, no A Pagano, M Barbarino, D Casalino, L Frederico AIAA Paper 3138, 2009 | 6 | 2009 |
| The development of practical Euler methods for aerodynamic design RH Doe, TW Brown, A Pagano ICAS Paper 4, 2, 1986 | 6 | 1986 |
| Optimized synchrophasing system of a turbo-prop aircraft for cabin noise reduction M Barbarino, P Vitiello, R Lombardi, A Pagano INTER-NOISE and NOISE-CON Congress and Conference Proceedings 259 (5), 4752-4759, 2019 | 5 | 2019 |
| Airfoil selection and spanwise placement in aerodynamic design and optimization of tiltrotor blades A Pagano | 5 | 2013 |
| Global launcher trajectory optimization for lunar base settlement A Pagano, E Mooij AIAA/AAS Astrodynamics Specialist Conference, 8387, 2010 | 5 | 2010 |
| ROSAA: The European Solution to Connect Aeroelasticity, Aerodynamics and Acoustics Codes in a Unique User-Friendly Rotorcraft Simulation System JV Miller, M Pidd, A Pagano, H Haverdings, G Bernardini, ... EUROPEAN ROTORCRAFT FORUM 26 (1), 47-47, 2000 | 5 | 2000 |
