Vincenzo Muscarello
Vincenzo Muscarello
Post Doc Research Fellow, Politecnico di Milano
Verified email at polimi.it
Title
Cited by
Cited by
Year
Linearized aeroservoelastic analysis of rotor-wing aircraft
P Masarati, V Muscarello, G Quaranta
282010
An integrated environment for helicopter aeroservoelastic analysis: the ground resonance case
P Masarati, V Muscarello, G Quaranta, A Locatelli, D Mangone, L Riviello, ...
242011
Rotorcraft aeroelastic stability using robust analysis
G Quaranta, A Tamer, V Muscarello, P Masarati, M Gennaretti, J Serafini, ...
CEAS Aeronautical Journal 5 (1), 29-39, 2014
172014
The role of rotor coning in helicopter proneness to collective bounce
V Muscarello, G Quaranta, P Masarati
Aerospace Science and Technology 36, 103-113, 2014
142014
Multibody analysis of rotorcraft-pilot coupling
V Muscarello, P Masarati, G Quaranta, P Eberhard, P Ziegler
2nd joint international conference on multibody system dynamics, Stuttgart …, 2012
142012
Prediction and simulator verification of roll/lateral adverse aeroservoelastic rotorcraft–pilot couplings
V Muscarello, G Quaranta, P Masarati, L Lu, M Jones, M Jump
Journal of Guidance, Control, and Dynamics 39 (1), 42-60, 2016
132016
Lead-lag damper robustness analysis for helicopter ground resonance
G Quaranta, V Muscarello, P Masarati
Journal of Guidance, Control, and Dynamics 36 (4), 1150-1161, 2013
122013
Aerodynamic models for cycloidal rotor analysis
L Gagnon, M Morandini, G Quaranta, V Muscarello, P Masarati
Aircraft Engineering and Aerospace Technology: An International Journal, 2016
112016
Robust aeroservoelastic stability of helicopters: application to the air/ground resonance
P Masarati, V Muscarello, G Quaranta
67th International Annual Forum American Helicopter Society (AHS), 1191-1201, 2011
102011
Robust aeroservoelastic analysis for the investigation of rotorcraft pilot couplings
V Muscarello, P Masarati, G Quaranta
3rd CEAS Air & Space Conference and 21st AIDAA Congress, 639-650, 2011
92011
Feasibility assessment: a cycloidal rotor to replace conventional helicopter technology
L Gagnon, M Morandini, G Quaranta, V Muscarello, P Masarati, ...
82014
Cyclogyro thrust vectoring for anti-torque and control of helicopters
L Gagnon, M Morandini, G Quaranta, V Muscarello, G Bindolino, ...
70th International Annual Forum American Helicopter Society (AHS), 2381-2394, 2014
72014
Evaluation of rotorcraft aeroelastic stability using robust analysis
G Quaranta, A Tamer, V Muscarello, P Masarati, M Gennaretti, J Serafini, ...
72012
Investigation of adverse aeroelastic rotorcraft-pilot coupling using real-time simulation
V Muscarello, P Masarati, G Quaranta, L Lu, M Jump, M Jones
69th International Annual Forum American Helicopter Society (AHS), 1389-1407, 2013
62013
Anatomy, modelling and prediction of aeroservoelastic rotorcraft-pilot-coupling.
M Gennaretti, MM Collela, J Serafini, BD Vu, P Masarati, G Quaranta, ...
52013
Biodynamic modeling techniques for rotorcraft comfort evaluation
A Tamer, A Zanoni, V Muscarello, A Cocco, G Quaranta, P Masarati
Aerotecnica Missili & Spazio 98 (2), 147-158, 2019
42019
Mulitple input describing function for non-linear analysis of ground and air resonance
V Muscarello, G Quaranta
42011
The role of flight simulation in exposing rotorcraft pilot couplings
M Jones, M Jump, L Lu, D Yilmaz, MD Pavel, P Masarati, G Quaranta, ...
Proceedings of the 39th European Rotorcraft Forum, Moscow, Russia, 2013
32013
Evaluation of vibration reduction devices for helicopter ride quality improvement
A Tamer, V Muscarello, P Masarati, G Quaranta
Aerospace Science and Technology 95, 105456, 2019
22019
Aeroelastic rotorcraft–pilot couplings in tiltrotor aircraft
V Muscarello, F Colombo, G Quaranta, P Masarati
Journal of Guidance, Control, and Dynamics 42 (3), 524-537, 2019
22019
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Articles 1–20