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Federico Fonte
Federico Fonte
Leonardo Helicopters
Verified email at polimi.it
Title
Cited by
Cited by
Year
Gust load alleviation for a regional aircraft through a static output feedback
F Fonte, S Ricci, P Mantegazza
Journal of Aircraft 52 (5), 1559-1574, 2015
692015
Integrated design of a morphing winglet for active load control and alleviation of turboprop regional aircraft
I Dimino, G Andreutti, F Moens, F Fonte, R Pecora, A Concilio
Applied Sciences 11 (5), 2439, 2021
392021
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
362019
Design and wind tunnel test validation of gust load alleviation systems
S Ricci, A De Gaspari, L Riccobene, F Fonte
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017
362017
Design of a wing tip device for active maneuver and gust load alleviation
F Fonte, F Toffol, S Ricci
2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2018
182018
Design, manufacturing and validation of a gust generator for wind tunnel test of a large scale aeroelastic model
F Fonte, L Riccobene, S Ricci, S Adden, M Martegani
30th Congress of the International Council of the Aeronautical Science …, 2016
172016
Wind tunnel system for active flutter suppression research: Overview and insights
S Ricci, F Toffol, A De Gaspari, L Marchetti, F Fonte, L Riccobene, ...
AIAA Journal 60 (12), 6692-6714, 2022
162022
Active flutter suppression analysis and wind tunnel studies of a commercial transport configuration
L Marchetti, A De Gaspari, L Riccobene, F Toffol, F Fonte, S Ricci, ...
AIAA Scitech 2020 Forum, 1677, 2020
152020
An active flutter suppression (AFS) project: Overview, results and lessons learned
S Ricci, L Marchetti, L Riccobene, A De Gaspari, F Toffol, F Fonte, ...
AIAA Scitech 2021 Forum, 0908, 2021
132021
Analytical and Experimental Evaluation of Multivariable Stability Margins in Active Flutter Suppression Wind Tunnel Tests
J Berg, KA Morgansen, E Livne, L Riccobene, F Fonte, F Toffol, ...
AIAA Scitech 2021 Forum, 1261, 2021
72021
Active load control of a regional aircraft wing equipped with morphing winglets
F Fonte, G Iannaccone, N Cimminiello, I Dimino, S Ricci
Smart Materials, Adaptive Structures and Intelligent Systems 51944, V001T04A021, 2018
72018
Gust and Manouvre Loads Alleviation Technologies: Overview, Results and Lesson Learned in the Framework of the Cs2 Airgreen2 Project
F Toffol, L Marchetti, S Ricci, F Fonte, E Capello, S Malisani
19th International Forum on Aeroelasticity and Structural Dynamics (IFASD …, 2023
62023
Recent developments of NeoCASS the open source suite for structural sizing and aeroelastic analysis
F Fonte, S Ricci
18th International Forum on Aeroelasticity and Structural Dynamics (IFASD …, 2019
62019
Active gust alleviation for a regional aircraft through static output feedback
F Fonte
Politecnico di Milano, 2012
62012
Design and Experimental Validation of Gust Load Alleviation Systems based on Static Output Feedback
S Ricci, F Toffol, L Marchetti, A De Gaspari, JV Chardi, L Riccobene, ...
AIAA Scitech 2022 Forum, 0441, 2022
52022
Numerical and experimental investigations on active flutter suppression technologies
F Fonte, A De Gaspari, L Riccobene, F Toffol, S Malik, L Marchetti, S Ricci, ...
18th International Forum on Aeroelasticity and Structural Dynamics (IFASD …, 2019
52019
Development of a wind tunnel model for active flutter suppression studies
S Ricci, F Fonte, A De Gaspari, L Riccobene, P Mantegazza, F Toffol, ...
AIAA Scitech 2019 Forum, 2029, 2019
52019
A recurrent neural network controller for gust load alleviation on a transport aircraft
F Fonte, P Mantegazza
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017
52017
Design of an innovative wing tip device
F Toffol, F Fonte, S Ricci
17th International Forum on Aeroelasticity and Structural Dynamics (IFASD …, 2017
42017
Design and validation of active gust load alleviation systems for aircraft
F Fonte
Politecnico di Milano, 2018
32018
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