CINECA IRIS Institutional Research Information System

FANTERIA, DANIELE
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 3.536
EU - Europa 1.710
AS - Asia 1.056
SA - Sud America 121
AF - Africa 72
Continente sconosciuto - Info sul continente non disponibili 3
OC - Oceania 2
Totale 6.500
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 3.424
IT - Italia 736
CN - Cina 422
SG - Singapore 329
SE - Svezia 166
BG - Bulgaria 144
DE - Germania 143
BR - Brasile 111
HK - Hong Kong 105
CA - Canada 102
GB - Regno Unito 89
AT - Austria 83
TR - Turchia 76
FR - Francia 64
RU - Federazione Russa 63
CI - Costa d'Avorio 62
FI - Finlandia 62
UA - Ucraina 58
VN - Vietnam 54
NL - Olanda 25
CH - Svizzera 21
IR - Iran 21
BE - Belgio 17
IN - India 15
ES - Italia 13
GR - Grecia 7
PL - Polonia 7
MX - Messico 6
KR - Corea 5
BD - Bangladesh 4
IQ - Iraq 4
DK - Danimarca 3
EC - Ecuador 3
EU - Europa 3
MA - Marocco 3
PK - Pakistan 3
RO - Romania 3
AR - Argentina 2
AU - Australia 2
BJ - Benin 2
CO - Colombia 2
EG - Egitto 2
JP - Giappone 2
LT - Lituania 2
PH - Filippine 2
SV - El Salvador 2
TH - Thailandia 2
UZ - Uzbekistan 2
AE - Emirati Arabi Uniti 1
AZ - Azerbaigian 1
BN - Brunei Darussalam 1
BO - Bolivia 1
CL - Cile 1
DZ - Algeria 1
HR - Croazia 1
HU - Ungheria 1
IE - Irlanda 1
JM - Giamaica 1
KG - Kirghizistan 1
KH - Cambogia 1
LB - Libano 1
MY - Malesia 1
NI - Nicaragua 1
OM - Oman 1
PT - Portogallo 1
SA - Arabia Saudita 1
SN - Senegal 1
TN - Tunisia 1
TW - Taiwan 1
VE - Venezuela 1
Totale 6.500
Salva come PNG Salva come JPEG
Città #
Ashburn 372
Ann Arbor 364
Woodbridge 356
Santa Clara 323
Fairfield 293
Chandler 230
Houston 187
Singapore 160
Milan 151
Sofia 143
Shanghai 129
Beijing 128
Serra 126
Seattle 124
Wilmington 103
Hong Kong 99
New York 98
Cambridge 92
Ottawa 77
Jacksonville 74
Boardman 71
Vienna 70
Florence 69
Princeton 63
Abidjan 62
Lawrence 56
Munich 53
Nanjing 42
Medford 36
Istanbul 32
Boulder 28
Helsinki 27
Mcallen 27
Des Moines 25
Lancaster 24
Izmir 22
Bern 21
Dong Ket 20
Montréal 20
Pisa 18
Rome 18
San Diego 17
Los Angeles 16
Delft 15
Falkenstein 15
Pune 14
Shenyang 13
Council Bluffs 12
Dearborn 12
Redwood City 12
Brussels 11
Jüchen 11
Nanchang 11
Berlin 10
Guangzhou 10
Hebei 10
Kunming 10
Lucca 10
Marseille 10
Norwalk 10
São Paulo 10
Tehran 10
Hefei 9
Ankara 8
Changsha 8
Torino 8
Bologna 7
College Station 7
London 7
Paris 7
Pontedera 7
Auburn Hills 6
Siena 6
Curitiba 5
Naples 5
Ogden 5
Phoenix 5
Santa Croce sull'Arno 5
Villeurbanne 5
Bari 4
Bordeaux 4
Bristol 4
Düsseldorf 4
Jiaxing 4
Lauterbourg 4
San Nicola la Strada 4
Seoul 4
Tianjin 4
Valencia 4
Wroclaw 4
Athens 3
Belo Horizonte 3
Brescia 3
Eboli 3
Falls Church 3
Frankfurt am Main 3
Glasgow 3
Hangzhou 3
Hull 3
Indiana 3
Totale 4.866
Salva come PNG Salva come JPEG
Nome #
null 208
Finite-element-based assessment of analytical methods for the design of fuselage frames 201
Comportamento post-buckling di pannelli piani irrigiditi realizzati in carboresina soggetti a compressione monoassiale 172
Delaminations growth in compression after impact test simulations: influence of cohesive elements parameters on numerical results 171
A non-linear model of large radial tyres for the simulation of aircraft braking 170
Fatigue crack growth in pin-loaded cold-worked holes 161
Comportamento post-buckling di pannelli piani realizzati in carboresina soggetti a compressione monoassiale 157
Crack propagation in flat panels stiffened by bonded pads 156
Development of analytical methods for fuselage design: validation by means of Finite Element analyses 154
Damage initialization techniques for non-sequential FE propagation analysis of delaminations in composite aerospace structures 154
Post-buckling behaviour of flat stiffened composite panels: Experiments vs. analysis 149
A sensitivity study on cohesive elements parameters: Towards their effective use to predict delaminations in low-velocity impacts on composites 146
Analysis and Control of the Flexible Dynamics of Landing Gear in the Presence of Antiskid Control Systems 145
Experimental and analytical assessment of fatigue and crack propagation in cold worked open hole specimens 145
A non-linear shear damage model to reproduce permanent indentation caused by impacts in composite laminates 145
Improved methodology for the design of damage tolerant helicopter structures in composite materials 140
CO-INFUSED AND SECONDARY BONDED COMPOSITE STIFFENED PANELS LOADED IN COMPRESSION: NUMERICAL ANALYSES AND EXPERIMENTAL TESTS IN LINEAR AND POST-BUCKLING REGIMES 136
Numerical prediction of fatigue crack propagation in Cold-Expanded Holes 129
A non-linear model for in-plane shear damage and failure of composite laminates 125
Influence of turning parameters on the high-temperature fatigue performance of Inconel 718 superalloy 124
Influence of environment conditioning on the interlaminar fracture toughness of a graphite/epoxy unidirectional material 124
CARATTERIZZAZIONE SPERIMENTALE DELLE ZONE DI RINFORZO INTORNO A GRANDI APERTURE DI FUSOLIERA" Collaborazione di ricerca fra il Dipartimento di Ingegneria Aerospaziale e la Alenia Aeronautica. 123
Towards the development of a numerical code for the simulation of aircraft braking 115
Comportamento post-buckling di pannelli piani realizzati in carboresina soggetti a compressione monoassiale 109
A NON-LINEAR MODEL FOR IN-PLANE SHEAR DAMAGE AND FAILURE OF COMPOSITE LAMINATES 108
Comportamento Post-Buckling di Pannelli Irrigiditi In Composito, Realizzati con Diverse Tecnologie, Soggetti a Compressione 107
Brake and tyre influence on the longitudinal stability of aircraft landing gear 106
Methods for design and health monitoring of damage tolerant helicopter structures in fiber-reinforced polymer composites 106
Research Activities on Buckling of Composite Structures in Italy 105
Simulation of delaminations induced by low velocity impacts in composites: a sensitivity study to guide an effective use of cohesive elements 105
Effects of different models of tire and brake on the longitudinal dynamics of aircraft landing gear 104
Low-velocity impact tests on carbon/epoxy composite laminates: A benchmark study 103
Models of Wheel Contact Dynamics: an analytical study on the in-plane transient responses of a brush model 98
EXPERIMENTAL STUDY OF THE EFFECTS OF LAYERS ORIENTATION ON MODE I INTERLAMINAR FRACTURE TOUGHNESS USING FULLY UNCOUPLED MULTIDIRECTIONAL SPECIMENS 94
Models and methods for the study of the in-plane transient responses of tyres 92
Least-weight composite plates with unconventional stacking sequences: Design, analysis and experiments 91
null 91
Mode III interlaminar fracture toughness of advanced composite materials: experimental testing and numerical modelling 89
Simulazione della dinamica dei carrelli e valutazione delle sollecitazioni in ambiente ADAMS 89
A three-dimensional damage model to simulate the progressive failure of composite structures 88
Modelli e metodi per lo studio della dinamica longitudinale del pneumatico 85
Design and finite element assessment of fully uncoupled multi-directional layups for delamination tests 85
A numerical micro-mechanical study on damage induced by the curing process in carbon/epoxy unidirectional material 82
Experimental and numerical study of delamination in composite laminates with bending-twisting elastic couplings 76
SENSITIVITY OF MATRIX-DOMINATED FAILURE MODES TO CARBON/EPOXY CONSTITUENT PROPERTIES VIA COMPUTATIONAL MICROMECHANICS 76
Numerical simulation of fatigue crack growth in an open-hole specimen 76
Quasi-trivial stacking sequences for the design of thick laminates 71
Experimental characterization of the interlaminar fracture toughness of a woven and a unidirectional carbon/epoxy composite 68
Quasi-trivial solutions for uncoupled, homogeneous and quasi-homogeneous laminates with high number of plies 66
Buckling and post-buckling response of curved, composite, stiffened panels under combined loads including pressurization 66
Experimental assessment of Fully-Uncoupled Multi-Directional specimens for mode I delamination tests 65
Least-weight design of composite structures: an unconventional and general approach 64
Co-infused and secondary bonded composite stiffened panels in compression: Numerical and experimental strength assessment combined with NDI and guided waves based SHM 63
A consistent energy-based cohesive zone model to simulate delamination between differently oriented plies 61
Assessment of a numerical strategy for fatigue growth and shape evolution of a corner crack from a pin-loaded hole 60
Multi-scale Least-Weight Design of a Wing-Box Through a Global/Local Modelling Approach 57
An experimental validation of the effectiveness of quasi-trivial solutions for composite laminates 56
DEVELOPMENT AND FINITE ELEMENTS ASSESSMENT OF STACKING SEQUENCES FOR INTERLAMINAR FRACTURE TOUGHNESS TESTING OF ANGLE-PLY INTERFACES 56
Quasi-trivial solutions for uncoupled, homogeneous and quasi-homogeneous laminates with high number of plies 49
Effects of hybridization and ply thickness on the strength and toughness of composite laminates 49
Multi-scale optimisation of thin-walled structures by considering a global/local modelling approach 48
A numerical micro-mechanical study of the influence of fiber–matrix interphase failure on carbon/epoxy material properties 45
Delamination onset in composite materials due to fatigue loading 30
A multi-step crack closure technique for the energetically orthogonal partitioning of the energy release rate 21
Preface 18
Totale 6.628
Salva come PNG Salva come JPEG
Categoria #
all - tutte 19.005
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 19.005
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020104 0 0 0 0 0 0 0 0 0 0 82 22
2020/2021454 33 28 27 19 34 25 47 55 41 37 37 71
2021/2022603 15 42 21 23 109 86 52 25 46 11 37 136
2022/2023811 81 93 88 54 85 106 1 53 158 6 75 11
2023/2024790 88 68 98 32 87 154 41 47 23 25 56 71
2024/20251.519 6 86 32 78 275 290 128 127 205 248 44 0
Totale 6.628