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Andrea Sellitto
Andrea Sellitto
University of Campania "Luigi Vanvitelli"
Email verificata su unicampania.it
Titolo
Citata da
Citata da
Anno
Optimum design of ablative thermal protection systems for atmospheric entry vehicles
A Riccio, F Raimondo, A Sellitto, V Carandente, R Scigliano, D Tescione
Applied Thermal Engineering 119, 541-552, 2017
932017
Influence of kinesiologic tape on post-operative swelling after orthognathic surgery
U Tozzi, M Santagata, A Sellitto, GP Tartaro
Journal of maxillofacial and oral surgery 15, 52-58, 2016
632016
Overview and future advanced engineering applications for morphing surfaces by shape memory alloy materials
A Sellitto, A Riccio
Materials 12 (5), 708, 2019
612019
A numerical study on the impact behaviour of natural fibres made honeycomb cores
A Riccio, A Raimondo, S Saputo, A Sellitto, M Battaglia, G Petrone
Composite Structures 202, 909-916, 2018
602018
Numerical investigation of constitutive material models on bonded joints in scarf repaired composite laminates
A Riccio, R Ricchiuto, F Di Caprio, A Sellitto, A Raimondo
Engineering Fracture Mechanics 173, 91-106, 2017
572017
Modelling the damage evolution in notched omega stiffened composite panels under compression
A Riccio, A Sellitto, S Saputo, A Russo, M Zarrelli, V Lopresto
Composites Part B: Engineering 126, 60-71, 2017
522017
Intra-laminar progressive failure analysis of composite laminates with a large notch damage
A Riccio, C Di Costanzo, P Di Gennaro, A Sellitto, A Raimondo
Engineering Failure Analysis 73, 97-112, 2017
482017
Compressive behaviour of a damaged omega stiffened panel: Damage detection and numerical analysis
A Sellitto, A Riccio, A Russo, M Zarrelli, C Toscano, V Lopresto
Composite Structures 209, 300-316, 2019
472019
Multifunctional polypropylene core for aerospace sandwich composite panels
A Riccio, A Raimondo, A Sellitto, V Acanfora, M Zarrelli
Procedia engineering 167, 64-70, 2016
472016
Numerical methodologies for simulating bird-strike on composite wings
A Riccio, R Cristiano, S Saputo, A Sellitto
Composite Structures 202, 590-602, 2018
452018
Development and application of a numerical procedure for the simulation of the “Fibre Bridging” phenomenon in composite structures
A Riccio, A Russo, A Sellitto, A Raimondo
Composite Structures 168, 104-119, 2017
442017
Numerical–experimental correlation of impact-induced damages in cfrp laminates
A Sellitto, S Saputo, F Di Caprio, A Riccio, A Russo, V Acanfora
Applied Sciences 9 (11), 2372, 2019
412019
A fast numerical procedure for the simulation of inter-laminar damage growth in stiffened composite panels
A Riccio, M Damiano, A Raimondo, G Di Felice, A Sellitto
Composite Structures 145, 203-216, 2016
382016
On the crashworthiness behaviour of a composite fuselage Sub-floor component
A Riccio, S Saputo, A Sellitto, F Di Caprio
Composite Structures 234, 111662, 2020
372020
Robustness of XFEM method for the simulation of cracks propagation in fracture mechanics problems
A Riccio, U Caruso, A Raimondo, A Sellitto
American Journal of Engineering and Applied Sciences 9 (3), 599-610, 2016
372016
On the use of selective stitching in stiffened composite panels to prevent skin-stringer debonding
A Riccio, P Linde, A Raimondo, A Buompane, A Sellitto
Composites Part B: Engineering 124, 64-75, 2017
362017
Analysis of the impact dynamics of shape memory alloy hybrid composites for advanced applications
M Guida, A Sellitto, F Marulo, A Riccio
Materials 12 (1), 153, 2019
352019
A numerical-experimental assessment on a composite fuselage barrel vertical drop test: Induced damage onset and evolution
A Riccio, S Saputo, A Sellitto, F Di Caprio, L Di Palma
Composite Structures 248, 112519, 2020
342020
An insight on the crashworthiness behavior of a full-scale composite fuselage section at different impact angles
A Riccio, S Saputo, A Sellitto, A Russo, F Di Caprio, L Di Palma
Aerospace 6 (6), 72, 2019
322019
On the use of global–local kinematic coupling approaches for delamination growth simulation in stiffened composite panels
R Borrelli, A Riccio, A Sellitto, F Caputo, T Ludwig
Composites Science and Technology 115, 43-51, 2015
302015
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
Articoli 1–20