SELLITTO, Andrea
 Distribuzione geografica
Continente #
EU - Europa 8.400
AS - Asia 3.535
NA - Nord America 3.495
SA - Sud America 667
AF - Africa 71
OC - Oceania 18
Continente sconosciuto - Info sul continente non disponibili 3
Totale 16.189
Nazione #
RU - Federazione Russa 5.875
US - Stati Uniti d'America 3.395
SG - Singapore 1.328
IE - Irlanda 872
CN - Cina 738
IT - Italia 579
HK - Hong Kong 567
BR - Brasile 561
VN - Vietnam 352
GB - Regno Unito 269
DE - Germania 231
KR - Corea 153
UA - Ucraina 132
IN - India 105
FR - Francia 93
FI - Finlandia 64
GR - Grecia 64
CA - Canada 60
TR - Turchia 52
SE - Svezia 50
AR - Argentina 47
NL - Olanda 40
ID - Indonesia 36
JP - Giappone 33
IQ - Iraq 29
EC - Ecuador 27
MX - Messico 24
BD - Bangladesh 21
ES - Italia 20
IR - Iran 20
AU - Australia 17
BE - Belgio 17
PL - Polonia 17
AT - Austria 15
MA - Marocco 15
PK - Pakistan 14
RO - Romania 14
ZA - Sudafrica 14
MY - Malesia 10
TW - Taiwan 10
CH - Svizzera 9
CO - Colombia 9
EG - Egitto 9
UZ - Uzbekistan 9
PT - Portogallo 8
TN - Tunisia 8
CL - Cile 6
CZ - Repubblica Ceca 6
KE - Kenya 6
SA - Arabia Saudita 6
UY - Uruguay 6
AZ - Azerbaigian 5
DZ - Algeria 5
LT - Lituania 5
OM - Oman 5
AL - Albania 4
AM - Armenia 4
CR - Costa Rica 4
CY - Cipro 4
ET - Etiopia 4
IL - Israele 4
PS - Palestinian Territory 4
TH - Thailandia 4
VE - Venezuela 4
DO - Repubblica Dominicana 3
GE - Georgia 3
JM - Giamaica 3
KG - Kirghizistan 3
LK - Sri Lanka 3
LV - Lettonia 3
PY - Paraguay 3
CG - Congo 2
EU - Europa 2
HN - Honduras 2
JO - Giordania 2
KZ - Kazakistan 2
LB - Libano 2
NO - Norvegia 2
NP - Nepal 2
PE - Perù 2
RS - Serbia 2
SY - Repubblica araba siriana 2
TG - Togo 2
TT - Trinidad e Tobago 2
AE - Emirati Arabi Uniti 1
AO - Angola 1
BG - Bulgaria 1
BH - Bahrain 1
BO - Bolivia 1
BY - Bielorussia 1
CM - Camerun 1
DK - Danimarca 1
GA - Gabon 1
GT - Guatemala 1
HR - Croazia 1
HU - Ungheria 1
LU - Lussemburgo 1
LY - Libia 1
MD - Moldavia 1
MT - Malta 1
Totale 16.181
Città #
Moscow 2.143
Dublin 872
Singapore 613
Santa Clara 573
Hong Kong 557
Chandler 357
San Jose 342
Jacksonville 263
Ashburn 166
Beijing 163
Ho Chi Minh City 134
Seoul 129
Dallas 111
Princeton 110
Roxbury 106
Hefei 93
Ann Arbor 82
Cambridge 80
Munich 64
Hanoi 57
New York 51
Naples 50
The Dalles 46
Medford 44
Los Angeles 37
Rome 37
Wilmington 36
Woodbridge 36
Des Moines 35
Bengaluru 34
Falkenstein 34
Milan 34
São Paulo 34
Caserta 22
Montreal 21
Redwood City 21
Boardman 19
Da Nang 19
Turin 19
Zhengzhou 19
Belo Horizonte 18
Nanjing 18
Turku 18
Amsterdam 16
Dong Ket 16
Shanghai 16
Brooklyn 15
Frankfurt am Main 15
Phoenix 14
Rio de Janeiro 14
Seattle 14
Aversa 13
Atlanta 12
Brussels 12
Chennai 12
Kaiserslautern 12
Orem 12
Ottawa 12
San Francisco 12
Columbus 11
Haiphong 11
Helsinki 11
London 11
Baghdad 10
Nuremberg 10
Vienna 10
Brasília 9
Council Bluffs 9
Guayaquil 9
Houston 9
Louisville 9
Tashkent 9
Vitulazio 9
Warsaw 9
Afragola 8
Biên Hòa 8
Controguerra 8
Denver 8
Düsseldorf 8
Istanbul 8
Johannesburg 8
Magelang 8
Napoli 8
Norwalk 8
Piscataway 8
Bremen 7
Juiz de Fora 7
Mexico City 7
Quito 7
Taipei 7
Thái Bình 7
Auburn Hills 6
Boston 6
Buenos Aires 6
Casablanca 6
Changsha 6
Chicago 6
Chongqing 6
Cluj-Napoca 6
Guangzhou 6
Totale 8.264
Nome #
Cohesive Zone Material model in ANSYS: a sensitivity analysis on a DCB test case 327
Robustness of XFEM method for the simulation of cracks propagation in fracture mechanics problems 206
A FEASIBILITY STUDY ON ADDITIVE MANUFACTURED HYBRID METAL/COMPOSITE SHOCK ABSORBER PANELS 190
3D global-local analysis using mesh superposition method 187
Methodological Approaches for Kinematic Coupling of non-matching Finite Element meshes 181
A robust cumulative damage approach for the simulation of delamination under cyclic loading conditions 175
Buckling analysis of a delaminated panel by using a kinematic global-local coupling approach 172
Predictors of in-hospital mortality of COVID-19 patients and the role of telemetry in an internal medicine ward during the third phase of the pandemic 166
Kinematic Approach for a Global-Local Coupling: Compressive Behaviour of a Delaminated Panel 164
A Computational Cost-effective numerical methodology for the simulation of the fatigue behaviour in composite materials. 162
A robust numerical methodology for fatigue damage evolution simulation in composites 161
A Numerical Study on the Bird Strike of a Crashworthy composite wing by a Coupled Eulerian-Lagrangian (CEL) approach 160
Application to plate components of a kinematic global-local approach for non-matching Finite Element meshes 157
Stiffened panels damage tolerance determination using an optimization procedure based on a linear delamination growth approach 152
A sensitivity analysis on Fibre bridging effects in delaminated composite panels under Flexural Loading Conditions 152
Application of the Mesh Superposition Technique to the Study of Delaminations in Composites Thin Plates 150
A Feasibility Study on Innovative Reinforced Modular Frames for Automotive Applications 149
Low Velocity Impact and Compression After Impact (CAI) Behavior of Natural Fibers based Sandwich Composite Panels 149
FIBREGLASS WIND TURBINE ONE SHOT BLADE®: DAMAGE TOLERANT DESIGN 148
A Prospective, Randomized, Double-Blind, Placebo-Controlled Clinical Trial Comparing the Efficacy of Anti-edema Drugs for Edema Control in Orthognathic Surgery Using Digitizer 3-D to Measure Facial Swelling 147
A numerical study on the impact behaviour of natural fibres made honeycomb cores 146
A Numerical Study on the Influence of Nanosilica-Reinforced Epoxy Resin on the Delamination Behavior of Composite Laminates 145
DEVELOPMENT OF A NUMERICAL METHODOLOGY FOR THE SIMULATION OF THE FATIGUE INDUCED DELAMINATION IN COMPOSITE STRUCTURES 145
Kinematic approach for a global-local coupling: buckling analysis of a delaminated panel 144
A comparative numerical-experimental investigation on the tensile behaviour of bonded, rivetted and hybrid composite joints configurations 143
A Numerical Assessment of Fibre Bridging Influence on Composite Panels Skin-stringer Debonding 143
A customized knee antibiotic-loaded pmma spacer: A preliminary design analysis 143
A new FE Modelling approach to Simulate the Inter-Layer Adherence in Hybrid Sandwich Structures achievable by Additive Manufacturing 140
A Numerical Study on Mode II Fatigue Delamination Growth in Composite Laminates 139
Fatigue driven delamination in composite structures: Definition and assessment of a novel fracture mechanics based computational tool 138
Large Notch Damage Evolution in Omega Stiffened Composite Panels 138
A numerical parametric study on delamination influence on the fatigue behaviour of stiffened composite components 136
An insight on the crashworthiness behavior of a full-scale composite fuselage section at different impact angles 136
EFFECTS OF THERMAL LOADS ON THE MECHANICAL BEHAVIOUR OF BONDED AIRCRAFT SUBCOMPONENTS. 136
A Bistable SMA Actuator: Design and Analysis 136
GARTEUR Structures & Materials Action Group 32 – An European Research Project on Damage Growth in Aerospace Composite Structures 135
Modelling the damage evolution in notched omega stiffened composite panels under compression 135
A numerical-analytical approach for the preliminary design of thin-walled cylindrical shell structures with elliptical cut-outs 135
Shape Memory Alloy Actuators for Controlled Movement of an Automotive Spoiler 134
A NUMERICAL-EXPERIMENTAL STUDY ON THE IMPCAT RESPONSE OF AN ADDITIVE MANUFACTED HYBRID METAL-COMPOSITE STRURCTURE 134
Experimental investigation on 3D printed lightweight sandwich structures for energy absorption aerospace applications 133
Numerical Investigation of the Failure Phenomena in Adhesively Bonded Joints by Means of a Multi-Linear Equivalent Plastic Stress/Strain Approach 133
Experimental and Numerical Study of Composite Omega Stringer - Skin debonding under Flexural Loading Conditions 133
Application of an additive manufactured hybrid metal/composite shock absorber panel to a military seat ejection system 132
Additive manufactured polymeric shock absorbers for automotive applications 131
A numerical model for the simulation of fatigue induced damage onset and evolution 129
Numerical-experimental study on the compressive behaviour of repaired composite panels 128
Development of a combined micro-macro mechanics analytical approach to design shape memory alloy spring-based actuators and its experimental validation 127
A Paris Law Based Mesh Independent Numerical Methodology for the Simulation of Fatigue Driven Delamination in Composites 127
Shape memory alloy-based actuator: Experimental and modelling 125
A Practical Tool for The Preliminary Design of Bonded Composite Repairs 124
A numerical study on multi-terrain impacts of an aeronautical fuselage section 124
A New FE Modelling Approach to Simulate the Inter-Layer Adherence in Hybrid Sandwich Structures Achievable by Additive Manufacturing 123
Experimental investigation on the delamination onset and propagation in composite specimens subjected to compressive loads by using Digital Image Correlation 121
A fast numerical procedure for the simulation of inter-laminar damage growth in stiffened composite panels 120
Compressive behaviour of a damaged omega stiffened panel: Damage detection and numerical analysis 120
STRESS CONCENTRATION ANALYSIS OF COMPOSITE FUSELAGE SECTION INCLUDING PASSENGERS’ DOOR AND WINDOWS 120
Multifunctional Polypropylene Core for Aerospace Sandwich Composite Panels 118
Shape Memory Alloy Actuators for Controlled Movement of an Automotive Spoiler 117
Numerical investigation of the stringer termination debonding in composite stiffened panels 115
Damage evolution in fuselage stiffened composite panels under asymmetrical bending loading conditions 114
Influence of failure criteria and intralaminar damage progression numerical models on the prediction of the mechanical behavior of composite laminates 114
Shape Memory Alloys Applied to Automotive Adaptive Aerodynamics 113
On the mechanical behavior of laminated composite plates subjected to compression after impact tests 113
Advanced Material Thermomechanical Modelling of Shape Memory Alloys Applied to Automotive Design 112
The peculiar SMart-Time XB approach for delamination growth prediction and its evolution towards fatigue investigations 112
Analytical tool for the preliminary design of an adhesively bonded T joint 112
FE Analysis of an ablative Thermal Protection Systems for re-entry vehicles 112
Structural Evaluation of a Vertical Tail for a Supersonic Vehicle: Architecture, Boundary Conditions, and Material System Influence 111
A user defined material model for the simulation of impact induced damage in composite 110
Nanofillers’ effects on fracture energy in composite aerospace structures 109
On the Use of Digital Image Correlation to Assess the Damage Behavior of Composite Coupons Under Compression 108
Modeling Delamination Growth in Composite Panels subjected to Fatigue Load 107
HYBRID METAL/COMPOSITE LATTICE STRUCTURES: DESIGN FOR ADDITIVE MANUFACTURING 107
Influence of manufacturing defects on the mechanical behaviour of all-composite wing under service load conditions 106
Fibreglass wind turbine blades: Damage tolerant design and verification 106
A numerical assessment on the influences of material toughness on the crashworthiness of a composite fuselage barrel 105
A Numerical and Experimental Investigation on the Mechanical Response of Composite Specimens Subjected to Low Velocity Impacts 103
Numerical Study on the Compressive Behaviour of Repaired Composite Panels 103
Influence of Kinesiologic Tape on Post-operative Swelling After Orthognathic Surgery 103
On the crashworthiness behaviour of a composite fuselage Sub-floor component 103
Ultrasonic damage detection of impacted long and short fibre composite specimens 103
GLP-1 Receptor Agonists Are Associated with Reduced Ascending Aorta Dilatation in Patients with Type 2 Diabetes: A Prospective Study 102
Morphing Spoiler for Adaptive Aerodynamics by Shape Memory Alloys 102
Delamination Growth in Composite Plates Under Fatigue Loading Conditions 102
Modeling the Behavior of Shape Memory Alloys and Memory Alloy-Based Devices 102
Double-Double Laminate Composites for Unmanned Aerial Vehicles 101
Influence of Stitching on Skin Stringer Debonding in Stiffened Composite Panels 101
On the Compressive Behaviour of a Composite Stiffened Panel with Artificially Introduced Delamination 100
Characterisation of the impact induced damage in composites by cross-comparison among experimental non-destructive evaluation techniques and numerical simulations 100
Parametric investigation on the damage behavior of a CFRP omega reinforced panel subjected to asymmetrical flexural load conditions 100
Cross-influence between intra-laminar damages and fibre bridging at the skin-stringer interface in stiffened composite panels under compression 99
Crashworthiness of a Composite Wing Section: Numerical Investigation of the Bird Strike Phenomenon by Using a Coupled Eulerian–Lagrangian Approach 98
Numerical simulation of the mechanical behaviour of shape memory alloys based actuators 98
Intra-laminar progressive failure analysis of composite laminates with a large notch damage 97
Modeling low velocity impact phenomena on composite structures 95
Crashworthiness of a general aviation fuselage section: 3D FEM numerical modelling and validation 95
Parametric Investigation of Stiffened Panel Subjected to Compressive Loads: Influence of Initial Delamination Length on Damage Behaviour 94
Numerical investigation of a stiffened panel subjected to low velocity impacts 94
On the use of selective stitching in stiffened composite panels to prevent skin-stringer debonding 93
Totale 12.895
Categoria #
all - tutte 57.674
article - articoli 0
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 57.674


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202122 0 0 0 0 0 0 0 0 0 0 0 22
2021/2022664 10 7 10 16 210 16 14 25 38 13 46 259
2022/20231.383 159 65 45 90 72 80 15 41 761 16 20 19
2023/2024813 49 26 48 41 244 61 62 26 28 21 62 145
2024/20252.605 33 65 13 63 394 355 382 195 364 329 222 190
2025/20269.605 279 382 590 446 843 5.407 453 217 397 324 185 82
Totale 16.483