CINECA IRIS Institutional Research Information System

FANTERIA, DANIELE
 Distribuzione geografica
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Continente #
NA - Nord America 5.312
EU - Europa 2.481
AS - Asia 2.465
SA - Sud America 356
Continente sconosciuto - Info sul continente non disponibili 139
AF - Africa 135
OC - Oceania 7
Totale 10.895
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Nazione #
US - Stati Uniti d'America 5.102
IT - Italia 1.137
SG - Singapore 771
CN - Cina 643
HK - Hong Kong 376
BR - Brasile 269
DE - Germania 209
SE - Svezia 193
VN - Vietnam 169
FR - Francia 164
GB - Regno Unito 158
BG - Bulgaria 144
CA - Canada 144
TR - Turchia 95
AT - Austria 84
FI - Finlandia 81
IN - India 70
RU - Federazione Russa 68
UA - Ucraina 65
CI - Costa d'Avorio 63
JP - Giappone 62
KR - Corea 62
BD - Bangladesh 46
NL - Olanda 42
IQ - Iraq 31
MX - Messico 30
ES - Italia 24
CH - Svizzera 23
PL - Polonia 23
AR - Argentina 22
IR - Iran 21
BE - Belgio 20
PK - Pakistan 20
ZA - Sudafrica 17
SA - Arabia Saudita 14
VE - Venezuela 14
JM - Giamaica 13
UZ - Uzbekistan 13
EC - Ecuador 12
PH - Filippine 12
CO - Colombia 11
GR - Grecia 11
KE - Kenya 11
CL - Cile 10
IE - Irlanda 9
AU - Australia 7
ID - Indonesia 7
MA - Marocco 7
TN - Tunisia 7
IL - Israele 6
MY - Malesia 6
UY - Uruguay 6
AE - Emirati Arabi Uniti 5
EG - Egitto 5
NP - Nepal 5
PE - Perù 5
AZ - Azerbaigian 4
JO - Giordania 4
MK - Macedonia 4
OM - Oman 4
RO - Romania 4
SN - Senegal 4
AL - Albania 3
BJ - Benin 3
BO - Bolivia 3
CR - Costa Rica 3
DK - Danimarca 3
DZ - Algeria 3
EU - Europa 3
LB - Libano 3
LT - Lituania 3
NG - Nigeria 3
PS - Palestinian Territory 3
SV - El Salvador 3
TT - Trinidad e Tobago 3
TW - Taiwan 3
BB - Barbados 2
BS - Bahamas 2
CG - Congo 2
GT - Guatemala 2
HU - Ungheria 2
LV - Lettonia 2
PA - Panama 2
PT - Portogallo 2
PY - Paraguay 2
SR - Suriname 2
TG - Togo 2
TH - Thailandia 2
UG - Uganda 2
AM - Armenia 1
AO - Angola 1
BN - Brunei Darussalam 1
BZ - Belize 1
CM - Camerun 1
CW - ???statistics.table.value.countryCode.CW??? 1
CY - Cipro 1
CZ - Repubblica Ceca 1
ET - Etiopia 1
GA - Gabon 1
HN - Honduras 1
Totale 10.747
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Città #
Dallas 704
Ashburn 553
Singapore 447
Hong Kong 366
Ann Arbor 364
Woodbridge 356
Santa Clara 337
Fairfield 293
San Jose 256
Chandler 230
Houston 192
Milan 187
Beijing 175
Sofia 143
Shanghai 130
Seattle 126
Serra 126
New York 118
Wilmington 103
Florence 96
Cambridge 92
Munich 89
Pisa 89
Ottawa 77
Jacksonville 75
Los Angeles 74
Boardman 71
Vienna 71
Rome 65
Princeton 64
Abidjan 63
Hefei 62
Lawrence 56
Lauterbourg 55
Tokyo 55
Seoul 53
Nanjing 42
Council Bluffs 39
Ho Chi Minh City 38
Buffalo 36
Istanbul 36
Medford 36
Helsinki 35
Paris 30
Boulder 28
Hanoi 28
São Paulo 28
Mcallen 27
Des Moines 25
Lancaster 25
Izmir 22
Bern 21
Dong Ket 20
Lucca 20
Montréal 20
Orem 20
Baghdad 19
San Diego 18
Marseille 17
Pune 17
Redondo Beach 17
Bologna 16
Farmington Hills 16
Naples 16
Delft 15
Falkenstein 15
Turin 15
Ankara 14
London 14
San Giuliano Terme 14
Shenyang 14
Atlanta 12
Dearborn 12
Redwood City 12
Tashkent 12
Brussels 11
Curitiba 11
Frankfurt am Main 11
Genoa 11
Guangzhou 11
Jüchen 11
Kingston 11
Manchester 11
Nanchang 11
Warsaw 11
Amsterdam 10
Berlin 10
Dhaka 10
Hebei 10
Johannesburg 10
Kunming 10
Memphis 10
Montreal 10
Nairobi 10
Norwalk 10
Tehran 10
Changsha 9
Chennai 9
Dublin 9
Toronto 9
Totale 7.530
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Nome #
Mode III interlaminar fracture toughness of advanced composite materials: experimental testing and numerical modelling 456
Experimental and numerical study of delamination in composite laminates with bending-twisting elastic couplings 449
Development of the EXCITE IOD/IOV mission 334
Finite-element-based assessment of analytical methods for the design of fuselage frames 251
Delaminations growth in compression after impact test simulations: influence of cohesive elements parameters on numerical results 221
CO-INFUSED AND SECONDARY BONDED COMPOSITE STIFFENED PANELS LOADED IN COMPRESSION: NUMERICAL ANALYSES AND EXPERIMENTAL TESTS IN LINEAR AND POST-BUCKLING REGIMES 221
Fatigue crack growth in pin-loaded cold-worked holes 219
Comportamento post-buckling di pannelli piani irrigiditi realizzati in carboresina soggetti a compressione monoassiale 217
A non-linear model of large radial tyres for the simulation of aircraft braking 216
Development of analytical methods for fuselage design: validation by means of Finite Element analyses 214
null 208
Influence of environment conditioning on the interlaminar fracture toughness of a graphite/epoxy unidirectional material 207
Crack propagation in flat panels stiffened by bonded pads 206
A sensitivity study on cohesive elements parameters: Towards their effective use to predict delaminations in low-velocity impacts on composites 196
Damage initialization techniques for non-sequential FE propagation analysis of delaminations in composite aerospace structures 194
Post-buckling behaviour of flat stiffened composite panels: Experiments vs. analysis 193
Analysis and Control of the Flexible Dynamics of Landing Gear in the Presence of Antiskid Control Systems 192
Improved methodology for the design of damage tolerant helicopter structures in composite materials 192
A non-linear shear damage model to reproduce permanent indentation caused by impacts in composite laminates 188
Comportamento post-buckling di pannelli piani realizzati in carboresina soggetti a compressione monoassiale 187
Experimental and analytical assessment of fatigue and crack propagation in cold worked open hole specimens 186
Numerical prediction of fatigue crack propagation in Cold-Expanded Holes 175
Influence of turning parameters on the high-temperature fatigue performance of Inconel 718 superalloy 173
Towards the development of a numerical code for the simulation of aircraft braking 172
A non-linear model for in-plane shear damage and failure of composite laminates 170
Comportamento Post-Buckling di Pannelli Irrigiditi In Composito, Realizzati con Diverse Tecnologie, Soggetti a Compressione 162
EXPERIMENTAL STUDY OF THE EFFECTS OF LAYERS ORIENTATION ON MODE I INTERLAMINAR FRACTURE TOUGHNESS USING FULLY UNCOUPLED MULTIDIRECTIONAL SPECIMENS 156
Research Activities on Buckling of Composite Structures in Italy 155
Brake and tyre influence on the longitudinal stability of aircraft landing gear 154
A NON-LINEAR MODEL FOR IN-PLANE SHEAR DAMAGE AND FAILURE OF COMPOSITE LAMINATES 154
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. 150
Simulation of delaminations induced by low velocity impacts in composites: a sensitivity study to guide an effective use of cohesive elements 150
Comportamento post-buckling di pannelli piani realizzati in carboresina soggetti a compressione monoassiale 149
A numerical micro-mechanical study on damage induced by the curing process in carbon/epoxy unidirectional material 149
Numerical simulation of fatigue crack growth in an open-hole specimen 146
Low-velocity impact tests on carbon/epoxy composite laminates: A benchmark study 145
Experimental characterization of the interlaminar fracture toughness of a woven and a unidirectional carbon/epoxy composite 144
Methods for design and health monitoring of damage tolerant helicopter structures in fiber-reinforced polymer composites 143
A Multi-step Crack Closure Technique for the Energetically Orthogonal Partitioning of the Energy Release Rate 142
Simulazione della dinamica dei carrelli e valutazione delle sollecitazioni in ambiente ADAMS 136
Buckling and post-buckling response of curved, composite, stiffened panels under combined loads including pressurization 133
Effects of different models of tire and brake on the longitudinal dynamics of aircraft landing gear 132
Design and finite element assessment of fully uncoupled multi-directional layups for delamination tests 131
Assessment of a numerical strategy for fatigue growth and shape evolution of a corner crack from a pin-loaded hole 130
Models of Wheel Contact Dynamics: an analytical study on the in-plane transient responses of a brush model 126
Least-weight composite plates with unconventional stacking sequences: Design, analysis and experiments 125
Models and methods for the study of the in-plane transient responses of tyres 123
SENSITIVITY OF MATRIX-DOMINATED FAILURE MODES TO CARBON/EPOXY CONSTITUENT PROPERTIES VIA COMPUTATIONAL MICROMECHANICS 123
Effects of hybridization and ply thickness on the strength and toughness of composite laminates 120
A three-dimensional damage model to simulate the progressive failure of composite structures 119
A consistent energy-based cohesive zone model to simulate delamination between differently oriented plies 118
Modelli e metodi per lo studio della dinamica longitudinale del pneumatico 116
Co-infused and secondary bonded composite stiffened panels in compression: Numerical and experimental strength assessment combined with NDI and guided waves based SHM 116
A numerical micro-mechanical study of the influence of fiber–matrix interphase failure on carbon/epoxy material properties 116
Quasi-trivial stacking sequences for the design of thick laminates 115
Multi-scale optimisation of thin-walled structures by considering a global/local modelling approach 114
Experimental assessment of Fully-Uncoupled Multi-Directional specimens for mode I delamination tests 114
Multi-scale Least-Weight Design of a Wing-Box Through a Global/Local Modelling Approach 112
Quasi-trivial solutions for uncoupled, homogeneous and quasi-homogeneous laminates with high number of plies 109
DEVELOPMENT AND FINITE ELEMENTS ASSESSMENT OF STACKING SEQUENCES FOR INTERLAMINAR FRACTURE TOUGHNESS TESTING OF ANGLE-PLY INTERFACES 109
Least-weight design of composite structures: an unconventional and general approach 107
Quasi-trivial solutions for uncoupled, homogeneous and quasi-homogeneous laminates with high number of plies 101
An experimental validation of the effectiveness of quasi-trivial solutions for composite laminates 96
null 91
Delamination onset in composite materials due to fatigue loading 89
Preface 72
Standard specimen geometries do not always lead to consistent fatigue results for epoxy adhesives 31
DAMAGE TOLERANCE OF A CURVED COMPOSITE STIFFENED PANEL FABRICATED BY AN OUT OF AUTOCLAVE – LIQUID RESIN INFUSION PROCESS 30
A non-linear model for in-plane shear damage and failure of composite laminates 5
Totale 10.895
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Categoria #
all - tutte 29.557
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 29.557
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022588 0 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
2024/20252.330 6 86 32 78 275 290 128 127 205 248 276 579
2025/20263.311 182 447 548 224 352 241 477 113 200 285 110 132
2026/2027145 106 39 0 0 0 0 0 0 0 0 0 0
Totale 10.895