| Mid-fidelity approach to aerodynamic simulations of unconventional VTOL aircraft configurations M Tugnoli, D Montagnani, M Syal, G Droandi, A Zanotti Aerospace Science and Technology 115, 106804, 2021 | 81 | 2021 |
| Tiltwing multi-rotor aerodynamic modeling in hover, transition and cruise flight conditions G Droandi, M Syal, G Bower AHS International 74th Annual Forum & Technology Display 1, 46-62, 2018 | 34 | 2018 |
| Mid-fidelity analysis of unsteady interactional aerodynamics of complex vtol configurations D Montagnani, M Tugnoli, F Fonte, A Zanotti, M Syal, G Droandi 45th European Rotorcraft Forum (ERF 2019), 100-110, 2019 | 32 | 2019 |
| Helicopter drag reduction by vortex generators G Gibertini, JC Boniface, A Zanotti, G Droandi, F Auteri, R Gaveriaux, ... Aerospace science and technology 47, 324-339, 2015 | 29 | 2015 |
| Proprotor–wing aerodynamic interaction in the first stages of conversion from helicopter to aeroplane mode G Droandi, G Gibertini, D Grassi, G Campanardi, C Liprino Aerospace Science and Technology 58, 116-133, 2016 | 27 | 2016 |
| Aerodynamic interaction between rotor and tilting wing in hovering flight condition G Droandi, A Zanotti, G Gibertini Journal of the American helicopter Society 60 (4), 1-20, 2015 | 25 | 2015 |
| Analysis of the interactional aerodynamics of the vahana evtol using a medium fidelity open source tool D Montagnani, M Tugnoli, A Zanotti, M Syal, G Droandi VFS Aeromechanics for Advanced Vertical Flight Technical Meeting, 436-451, 2020 | 22 | 2020 |
| Wing rotor aerodynamic interaction in tiltrotor aircraft G Droandi Politecnico di Milano, 2014 | 21 | 2014 |
| Aerodynamic shape optimisation of a proprotor and its validation by means of CFD and experiments G Droandi, G Gibertini The Aeronautical Journal 119 (1220), 1223-1251, 2015 | 19 | 2015 |
| Aerodynamic blade design with multi-objective optimization for a tiltrotor aircraft G Droandi, G Gibertini Aircraft Engineering and Aerospace Technology: An International Journal 87 …, 2015 | 18 | 2015 |
| Experimental investigation of the rotor-wing aerodynamic interaction in a tiltwing aircraft in hover G Droandi, A Zanotti, G Gibertini, D Grassi, G Campanardi The Aeronautical Journal 119 (1215), 591-612, 2015 | 17 | 2015 |
| Perpendicular blade–vortex-interaction over an oscillating airfoil in light dynamic stall G Droandi, G Gibertini, A Zanotti Journal of Fluids and Structures 65, 472-494, 2016 | 14 | 2016 |
| Assessment of a propeller model embedded on a panel method code for aircraft aerodynamics G Droandi, G Gibertini The Journal of Aerospace Science, Technology and Systems 91 (3/4), 98-108, 2012 | 10 | 2012 |
| CFD assessment of the helicopter and ground obstacles aerodynamic interference G Gibertini, G Droandi, D Zagaglia, P Antoniazza, A Oregio Catelan | 8 | 2016 |
| Acoustics and forces from an isolated rotor system J Goldschmidt, H Tingle, PG Ifgu, SA Miller, LS Ukeiley, B Goldman, ... AIAA SCITECH 2022 Forum, 2530, 2022 | 7 | 2022 |
| Experimental investigation of a helicopter rotor with Gurney flaps G Gibertini, A Zanotti, G Droandi, F Auteri, G Crosta The Aeronautical Journal 121 (1236), 191-212, 2017 | 7 | 2017 |
| Wind-tunnel tests of a heavy-class helicopter optimised for drag reduction G Gibertini, A Zanotti, G Droandi, D Grassi, G Campanardi, F Auteri, ... The Aeronautical Journal 120 (1231), 1446-1467, 2016 | 6 | 2016 |
| Wing-rotor interactions on a 1/4-scale tiltrotor half-model G Droandi, G Gibertini, M Lanz, GG Campanardi, D Grassi, S Garbaccio 39th European Rotorcraft Forum, 1-8, 2013 | 6 | 2013 |
| Experimental Investigation on a 1/4 Scaled Model of an High–Performance Tiltwing Aircraft in Hover G Droandi, A Zanotti, G Gibertini, G Campanardi, D Grassi American Helicopter Society 70th Annual Forum, Montreal, Canada, 20-22, 2014 | 5 | 2014 |
| Robustness and limits of vortex generator effectiveness in helicopter drag reduction A Zanotti, G Droandi, F Auteri, G Gibertini, AL Pape Journal of the American Helicopter Society 61 (3), 1-7, 2016 | 3 | 2016 |
Alex ZanottiPolitecnico di Milano在 polimi.it 的电子邮件经过验证
