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Antonio Concilio
Antonio Concilio
Researcher, the Italian Aerospace Research Centre
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Airfoil structural morphing based on SMA actuator series: numerical and experimental studies
S Barbarino, R Pecora, L Lecce, A Concilio, S Ameduri, L De Rosa
Journal of Intelligent Material Systems and Structures 22 (10), 987-1004, 2011
1012011
Design and functional test of a morphing high-lift device for a regional aircraft
R Pecora, S Barbarino, A Concilio, L Lecce, S Russo
Journal of Intelligent Material Systems and Structures 22 (10), 1005-1023, 2011
952011
A novel SMA-based concept for airfoil structural morphing
S Barbarino, R Pecora, L Lecce, A Concilio, S Ameduri, E Calvi
Journal of materials engineering and performance 18, 696-705, 2009
942009
Morphing wings review: Aims, challenges, and current open issues of a technology
S Ameduri, A Concilio
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of …, 2023
872023
Wing shape control through an SMA-based device
S Barbarino, S Ameduri, L Lecce, A Concilio
Journal of Intelligent Material Systems and Structures 20 (3), 283-296, 2009
722009
A shape memory alloy torsion actuator for static blade twist
S Ameduri, A Concilio
Journal of Intelligent Material Systems and Structures 30 (17), 2605-2626, 2019
582019
Actuation system design for a morphing wing trailing edge
I Dimino, D Flauto, G Diodati, A Concilio, R Pecora
Recent Patents on Mechanical Engineering 7 (2), 138-148, 2014
572014
Optimization and integration of shape memory alloy (SMA)-based elastic actuators within a morphing flap architecture
S Ameduri, A Brindisi, B Tiseo, A Concilio, R Pecora
Journal of Intelligent Material Systems and Structures 23 (4), 381-396, 2012
492012
Aero-servo-elastic design of a morphing wing trailing edge system for enhanced cruise performance
M Arena, A Concilio, R Pecora
Aerospace Science and Technology 86, 215-235, 2019
462019
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
Applied Sciences 11 (5), 2439, 2021
402021
Passengers' comfort modeling inside aircraft
A Brindisi, A Concilio
Journal of aircraft 45 (6), 2001-2008, 2008
402008
Load monitoring of aircraft landing gears using fiber optic sensors
A Iele, M Leone, M Consales, GV Persiano, A Brindisi, S Ameduri, ...
Sensors and Actuators A: Physical 281, 31-41, 2018
382018
Seismic performance of a reinforced concrete building retrofitted with self-centering shape memory alloy braces
M Ferraioli, A Concilio, C Molitierno
Earthquake Engineering and Engineering Vibration 21 (3), 785-809, 2022
352022
Design and integration sensitivity of a morphing trailing edge on a reference airfoil: The effect on high-altitude long-endurance aircraft performance
P Della Vecchia, S Corcione, R Pecora, F Nicolosi, I Dimino, A Concilio
Journal of Intelligent Material Systems and Structures 28 (20), 2933-2946, 2017
342017
Shape memory alloys (SMA) for automotive applications and challenges
A Riccio, A Sellitto, S Ameduri, A Concilio, M Arena
Shape Memory Alloy Engineering, 785-808, 2021
332021
Aeroelastic assessments and functional hazard analysis of a regional aircraft equipped with morphing winglets
MC Noviello, I Dimino, A Concilio, F Amoroso, R Pecora
Aerospace 6 (10), 104, 2019
272019
SARISTU: Adaptive trailing edge device (ATED) design process review
A Concilio, I Dimino, R Pecora
Chinese Journal of Aeronautics 34 (7), 187-210, 2021
262021
Morphing wing technologies: Large commercial aircraft and civil helicopters
A Concilio, I Dimino, L Lecce, R Pecora
Butterworth-Heinemann, 2018
232018
Stringer debonding edge detection employing fiber optics by combined distributed strain profile and wave scattering approaches for non-model based SHM
M Ciminello, ND Boffa, A Concilio, V Memmolo, E Monaco, F Ricci
Composite Structures 216, 58-66, 2019
212019
Static and dynamic performance of a morphing trailing edge concept with high-damping elastomeric skin
M Arena, C Nagel, R Pecora, O Schorsch, A Concilio, I Dimino
Aerospace 6 (2), 22, 2019
202019
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