Application of Artificial Neural Networks and Probability Ellipse methods for damage detection using Lamb waves A De Fenza, A Sorrentino, P Vitiello Composite Structures 133, 390-403, 2015 | 133 | 2015 |
Guided wave SHM system for damage detection in complex composite structure A De Luca, D Perfetto, A De Fenza, G Petrone, F Caputo Theoretical and Applied Fracture Mechanics 105, 102408, 2020 | 68 | 2020 |
Guided waves in a composite winglet structure: Numerical and experimental investigations A De Luca, D Perfetto, A De Fenza, G Petrone, F Caputo Composite Structures 210, 96-108, 2019 | 48 | 2019 |
Post-impact damage detection on a winglet structure realized in composite material A De Fenza, G Petrone, R Pecora, M Barile Composite Structures 169, 129–137, 2017 | 28 | 2017 |
Guided-waves in a low velocity impacted composite winglet A De Luca, D Perfetto, G Petrone, A De Fenza, F Caputo Key Engineering Materials 774, 343-348, 2018 | 24 | 2018 |
A sensitivity analysis on the damage detection capability of a Lamb waves based SHM system for a composite winglet A De Luca, D Perfetto, A De Fenza, G Petrone, F Caputo Procedia Structural Integrity 12, 578-588, 2018 | 23 | 2018 |
Conceptual adaptive wing-tip design for pollution reductions E Daniele, A De Fenza, PD Vecchia Journal of intelligent material systems and structures 23 (11), 1197-1212, 2012 | 23 | 2012 |
Skin-spar failure detection of a composite winglet using FBG sensors M Ciminello, A De Fenza, I Dimino, R Pecora Archive of Mechanical Engineering Journal 64 (3), 287-300, 2017 | 22 | 2017 |
Improved elliptical triangulation method for damage detection in composite material structures A Sorrentino, A De Fenza Proceedings of the Institution of Mechanical Engineers, Part C: Journal of …, 2017 | 21 | 2017 |
A modelling technique to investigate the effects of quasi-static loads on guided-wave based structural health monitoring systems D Perfetto, G Lamanna, G Petrone, A De Fenza, A De Luca Forces in Mechanics 9, 100125, 2022 | 20 | 2022 |
Progress in studying passive and active devices for fuselage noise reduction for next generation turboprop M Arena, A De Fenza, M Di Giulio, A Paonessa, F Amoroso CEAS Aeronautical Journal 8 (2), 303-3012, 2017 | 16 | 2017 |
AB Basis Allowable Test Reduction Approach and Composite Generic Basis Strength Values F Abdi, E Clarkson, C Godines, S DorMohammadi, A De Fenza 18th AIAA Non-Deterministic Approaches Conference, 0951, 2016 | 16 | 2016 |
Drop test simulation for an aircraft landing gear via multi-body approach R Di Leo, A De Fenza, M Barile, L Lecce Archive of Mechanical Engineering 61 (2), 287-304, 2014 | 16 | 2014 |
Experimental approach in studying temperature effects on composite material structures realized with viscoelastic damping treatments A De Fenza, E Monaco, F Amoroso, L Lecce Journal of Vibration and Control, 2014 | 12 | 2014 |
Damage Detection in Complex Composite Material Structures by using Elliptical Triangulation Method A SORRENTINO, A DE FENZA Structural Health Monitoring 2017: The 11th International Workshop on …, 2017 | 9 | 2017 |
Numerical simulation of guided waves propagation in loaded composite structures AD Luca, D Perfetto, F Caputo, G Petrone, AD Fenza AIP Conference Proceedings 2309 (1), 2020 | 8 | 2020 |
Experimental evaluation of vibro-acoustic behaviour of composite fuselage structures realized with embedded viscoelastic damping treatments F Amoroso, A De Fenza, E Monaco, R Pecora, L L. 18th International Congress on Sound and Vibration, 2011 | 7 | 2011 |
Experimental application of Lamb wave based SHM system at complex composite material structures A Sorrentino, A De Fenza, F Romano, U Mercurio 9th Workshop on Structural Health Monitoring, Manchester, UK, 2018 | 6 | 2018 |
IMPROVED IMPULSE RESPONSE DECAY METHOD (IRDM) FOR STRUCTURAL DAMPING MEASURE-MENTS F Amoroso, A De Fenza, R Pecora, P Volpe, E Monaco, L Lecce | 6 | 2010 |
Probability ellipse method for damage detection in a composite winglet G Petrone, A De Fenza, D Perfetto, A De Luca, A Sorrentino, F Caputo Key Engineering Materials 827, 67-72, 2020 | 5 | 2020 |