Volgen
Jacopo Serafini
Jacopo Serafini
Geverifieerd e-mailadres voor uniroma3.it
Titel
Geciteerd door
Geciteerd door
Jaar
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
762013
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
612013
Aeroelastic and biodynamic modelling for stability analysis of rotorcraft-pilot coupling phenomena
J Serafini, M Gennaretti, P Masarati, G Quaranta, O Dieterich
452008
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
412015
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
402007
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
392018
Numerical characterisation of the aeroacoustic signature of propeller arrays for distributed electric propulsion
G Bernardini, F Centracchio, M Gennaretti, U Iemma, C Pasquali, C Poggi, ...
Applied Sciences 10 (8), 2643, 2020
352020
Control of power generated by a floating offshore wind turbine perturbed by sea waves
L Pustina, C Lugni, G Bernardini, J Serafini, M Gennaretti
Renewable and Sustainable Energy Reviews 132, 109984, 2020
292020
In-flight health monitoring of helicopter blades via differential analysis
J Serafini, G Bernardini, R Porcelli, P Masarati
Aerospace Science and Technology 88, 436-443, 2019
252019
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
252016
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
252013
An investigation of aeroelastic rotorcraft-pilot interaction
P Masarati, G Quaranta, M Gennaretti, J Serafini
252011
Rotorcraft aeroelastic stability using robust analysis
G Quaranta, A Tamer, V Muscarello, P Masarati, M Gennaretti, J Serafini, ...
CEAS Aeronautical Journal 5, 29-39, 2014
222014
Numerical-experimental correlation of hovering rotor aerodynamics in ground effect
C Pasquali, J Serafini, G Bernardini, J Milluzzo, M Gennaretti
Aerospace Science and Technology 106, 106079, 2020
182020
Aeroservoelastic analysis of rotorcraft-pilot coupling: a parametric study
P Masarati, G Quaranta, M Gennaretti, J Serafini
American helicopter society 66th annual forum, 11-13, 2010
182010
Conceptual all-electric retrofit of helicopters: Review, technological outlook, and a sample design
J Serafini, M Cremaschini, G Bernardini, L Solero, C Ficuciello, ...
IEEE Transactions on Transportation Electrification 5 (3), 782-794, 2019
172019
Rotor blade shape reconstruction from strain measurements
G Bernardini, R Porcelli, J Serafini, P Masarati
Aerospace Science and Technology 79, 580-587, 2018
152018
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
15*2015
A finite-state aeroelastic model for rotorcraft–pilot coupling analysis
J Serafini, M Molica Colella, M Gennaretti
CEAS Aeronautical Journal 5, 1-11, 2014
142014
Numerical investigation of aeroservoelastic rotorcraft-pilot coupling
P Masarati, G Quaranta, J Serafini, M Gennaretti
XIX Congresso Nazionale AIDAA, 17-21, 2007
142007
Het systeem kan de bewerking nu niet uitvoeren. Probeer het later opnieuw.
Artikelen 1–20