Jacopo Serafini
Jacopo Serafini
Verified email at uniroma3.it
Cited by
Cited by
Adverse rotorcraft pilot couplings—past, present and future challenges
MD Pavel, M Jump, B Dang-Vu, P Masarati, M Gennaretti, A Ionita, ...
Progress in Aerospace Sciences 62, 1-51, 2013
Aeroelastic and biodynamic modelling for stability analysis of rotorcraft-pilot coupling phenomena
J Serafini, M Gennaretti, P Masarati, G Quaranta, O Dieterich
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft
G Bernardini, J Serafini, MM Colella, M Gennaretti
Aerospace Science and Technology 29 (1), 175-184, 2013
Assessment of computational models for the effect of aeroelasticity on BVI noise prediction
G Bernardini, J Serafini, S Lanniello, M Gennaretti
International Journal of Aeroacoustics 6 (3), 199-222, 2007
Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings–A design perspective
MD Pavel, P Masarati, M Gennaretti, M Jump, L Zaichik, B Dang-Vu, L Lu, ...
Progress in Aerospace Sciences 76, 55-89, 2015
Effects of biodynamic feedthrough in rotorcraft/pilot coupling: collective bounce case
M Gennaretti, J Serafini, P Masarati, G Quaranta
Journal of Guidance, Control, and Dynamics 36 (6), 1709-1721, 2013
An investigation of aeroelastic rotorcraft-pilot interaction
P Masarati, G Quaranta, M Gennaretti, J Serafini
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
Aeroservoelastic analysis of rotorcraftpilot coupling: a parametric study
P Masarati, G Quaranta, M Gennaretti, J Serafini
American helicopter society 66th annual forum, 2010
Numerical investigation of aeroservoelastic rotorcraft-pilot coupling
P Masarati, G Quaranta, J Serafini, M Gennaretti
XIX Congresso Nazionale AIDAA, 17-21, 2007
Numerical characterization of helicopter noise hemispheres
M Gennaretti, J Serafini, G Bernardini, A Castorrini, G De Matteis, ...
Aerospace Science and Technology 52, 18-28, 2016
Rotor dynamic wake inflow finite-state modelling
M Gennaretti, R Gori, J Serafini, G Bernardini, F Cardito
33rd AIAA Applied Aerodynamics Conference, Dallas, TX, 2015
A finite-state aeroelastic model for rotorcraft–pilot coupling analysis
J Serafini, MM Colella, M Gennaretti
CEAS Aeronautical Journal 5 (1), 1-11, 2014
Rotorcraft comprehensive code assessment for blade–vortex interaction conditions
M Gennaretti, G Bernardini, J Serafini, G Romani
Aerospace Science and Technology 80, 232-246, 2018
Acoustic prediction of helicopter unsteady manoeuvres, 41st European Rotorcraft Forum ERF 2015
M Gennaretti, G Bernardini, A Anobile, J Serafini, L Trainelli, A Rolando, ...
Munich, Germany, 2015
Evaluation of rotorcraft aeroelastic stability using robust analysis
G Quaranta, A Tamer, V Muscarello, P Masarati, M Gennaretti, J Serafini, ...
Finite-state dynamic wake inflow modelling for coaxial rotors
F Cardito, R Gori, G Bernardini, J Serafini, M Gennaretti
Photogrammetric detection technique for rotor blades structural characterization
C Enei, G Bernardini, J Serafini, L Mattioni, C Ficuciello, V Vezzari
Journal of Physics: Conference Series 658 (1), 012003, 2015
An optimal control approach for alleviation of tiltrotor gust
D Muro, MM Colella, J Serafini, M Gennaretti
The Aeronautical Journal 116 (1180), 651, 2012
A finite-state aeroelastic model for rotorcraft pilot-assisted-oscillations analysis
J Serafini, M Molica Colella, M Gennaretti
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