CINECA IRIS Institutional Research Information System

FANTERIA, DANIELE
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 5.223
AS - Asia 2.457
EU - Europa 2.346
SA - Sud America 349
AF - Africa 135
OC - Oceania 7
Continente sconosciuto - Info sul continente non disponibili 4
Totale 10.521
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 5.022
IT - Italia 1.025
SG - Singapore 770
CN - Cina 643
HK - Hong Kong 375
BR - Brasile 265
DE - Germania 209
SE - Svezia 173
VN - Vietnam 169
FR - Francia 164
GB - Regno Unito 157
BG - Bulgaria 144
CA - Canada 139
TR - Turchia 95
AT - Austria 84
FI - Finlandia 81
IN - India 70
RU - Federazione Russa 68
UA - Ucraina 65
CI - Costa d'Avorio 63
KR - Corea 60
JP - Giappone 59
BD - Bangladesh 46
NL - Olanda 42
IQ - Iraq 31
MX - Messico 30
ES - Italia 24
CH - Svizzera 23
PL - Polonia 22
AR - Argentina 21
IR - Iran 21
BE - Belgio 20
PK - Pakistan 20
ZA - Sudafrica 17
SA - Arabia Saudita 14
VE - Venezuela 14
UZ - Uzbekistan 13
JM - Giamaica 12
PH - Filippine 12
EC - Ecuador 11
GR - Grecia 11
KE - Kenya 11
CL - Cile 10
CO - Colombia 10
IE - Irlanda 9
AU - Australia 7
MA - Marocco 7
TN - Tunisia 7
ID - Indonesia 6
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
DK - Danimarca 3
DZ - Algeria 3
EU - Europa 3
LB - Libano 3
LT - Lituania 3
NG - Nigeria 3
PS - Palestinian Territory 3
TT - Trinidad e Tobago 3
TW - Taiwan 3
BB - Barbados 2
BS - Bahamas 2
CG - Congo 2
CR - Costa Rica 2
GT - Guatemala 2
HU - Ungheria 2
LV - Lettonia 2
PA - Panama 2
PT - Portogallo 2
PY - Paraguay 2
SR - Suriname 2
SV - El Salvador 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
ET - Etiopia 1
GA - Gabon 1
HR - Croazia 1
KG - Kirghizistan 1
Totale 10.510
Salva come PNG Salva come JPEG
Città #
Dallas 703
Ashburn 533
Singapore 447
Hong Kong 365
Ann Arbor 364
Woodbridge 356
Santa Clara 335
Fairfield 293
San Jose 245
Chandler 230
Houston 192
Beijing 175
Milan 171
Sofia 143
Shanghai 130
Seattle 126
Serra 126
New York 117
Wilmington 103
Cambridge 92
Florence 91
Munich 89
Ottawa 77
Jacksonville 74
Los Angeles 74
Pisa 73
Boardman 71
Vienna 71
Princeton 64
Abidjan 63
Hefei 62
Lawrence 56
Lauterbourg 55
Tokyo 54
Seoul 53
Rome 50
Nanjing 42
Ho Chi Minh City 38
Buffalo 36
Istanbul 36
Medford 36
Helsinki 35
Paris 30
Boulder 28
Hanoi 28
Mcallen 27
São Paulo 27
Council Bluffs 26
Des Moines 25
Lancaster 24
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
Farmington Hills 16
Delft 15
Falkenstein 15
Ankara 14
London 14
San Giuliano Terme 14
Shenyang 14
Naples 13
Dearborn 12
Redwood City 12
Tashkent 12
Turin 12
Bologna 11
Brussels 11
Curitiba 11
Frankfurt am Main 11
Guangzhou 11
Jüchen 11
Manchester 11
Nanchang 11
Warsaw 11
Amsterdam 10
Berlin 10
Dhaka 10
Genoa 10
Hebei 10
Johannesburg 10
Kingston 10
Kunming 10
Montreal 10
Nairobi 10
Norwalk 10
Tehran 10
Atlanta 9
Changsha 9
Chennai 9
Dublin 9
Memphis 9
Da Nang 8
Totale 7.407
Salva come PNG Salva come JPEG
Nome #
Mode III interlaminar fracture toughness of advanced composite materials: experimental testing and numerical modelling 450
Experimental and numerical study of delamination in composite laminates with bending-twisting elastic couplings 437
Development of the EXCITE IOD/IOV mission 293
Finite-element-based assessment of analytical methods for the design of fuselage frames 246
Delaminations growth in compression after impact test simulations: influence of cohesive elements parameters on numerical results 220
CO-INFUSED AND SECONDARY BONDED COMPOSITE STIFFENED PANELS LOADED IN COMPRESSION: NUMERICAL ANALYSES AND EXPERIMENTAL TESTS IN LINEAR AND POST-BUCKLING REGIMES 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 213
Fatigue crack growth in pin-loaded cold-worked holes 213
Development of analytical methods for fuselage design: validation by means of Finite Element analyses 212
null 208
Influence of environment conditioning on the interlaminar fracture toughness of a graphite/epoxy unidirectional material 205
Crack propagation in flat panels stiffened by bonded pads 203
A sensitivity study on cohesive elements parameters: Towards their effective use to predict delaminations in low-velocity impacts on composites 194
Analysis and Control of the Flexible Dynamics of Landing Gear in the Presence of Antiskid Control Systems 192
Damage initialization techniques for non-sequential FE propagation analysis of delaminations in composite aerospace structures 192
Post-buckling behaviour of flat stiffened composite panels: Experiments vs. analysis 190
Improved methodology for the design of damage tolerant helicopter structures in composite materials 187
Experimental and analytical assessment of fatigue and crack propagation in cold worked open hole specimens 186
Comportamento post-buckling di pannelli piani realizzati in carboresina soggetti a compressione monoassiale 185
A non-linear shear damage model to reproduce permanent indentation caused by impacts in composite laminates 185
Numerical prediction of fatigue crack propagation in Cold-Expanded Holes 174
Influence of turning parameters on the high-temperature fatigue performance of Inconel 718 superalloy 172
Towards the development of a numerical code for the simulation of aircraft braking 171
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
Brake and tyre influence on the longitudinal stability of aircraft landing gear 154
Research Activities on Buckling of Composite Structures in Italy 154
A NON-LINEAR MODEL FOR IN-PLANE SHEAR DAMAGE AND FAILURE OF COMPOSITE LAMINATES 153
EXPERIMENTAL STUDY OF THE EFFECTS OF LAYERS ORIENTATION ON MODE I INTERLAMINAR FRACTURE TOUGHNESS USING FULLY UNCOUPLED MULTIDIRECTIONAL SPECIMENS 152
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 148
A numerical micro-mechanical study on damage induced by the curing process in carbon/epoxy unidirectional material 148
Comportamento post-buckling di pannelli piani realizzati in carboresina soggetti a compressione monoassiale 147
Low-velocity impact tests on carbon/epoxy composite laminates: A benchmark study 144
Methods for design and health monitoring of damage tolerant helicopter structures in fiber-reinforced polymer composites 142
Experimental characterization of the interlaminar fracture toughness of a woven and a unidirectional carbon/epoxy composite 142
Numerical simulation of fatigue crack growth in an open-hole specimen 138
Simulazione della dinamica dei carrelli e valutazione delle sollecitazioni in ambiente ADAMS 135
Effects of different models of tire and brake on the longitudinal dynamics of aircraft landing gear 130
Design and finite element assessment of fully uncoupled multi-directional layups for delamination tests 130
A Multi-step Crack Closure Technique for the Energetically Orthogonal Partitioning of the Energy Release Rate 129
Models of Wheel Contact Dynamics: an analytical study on the in-plane transient responses of a brush model 126
Assessment of a numerical strategy for fatigue growth and shape evolution of a corner crack from a pin-loaded hole 126
Least-weight composite plates with unconventional stacking sequences: Design, analysis and experiments 125
Buckling and post-buckling response of curved, composite, stiffened panels under combined loads including pressurization 124
Models and methods for the study of the in-plane transient responses of tyres 122
SENSITIVITY OF MATRIX-DOMINATED FAILURE MODES TO CARBON/EPOXY CONSTITUENT PROPERTIES VIA COMPUTATIONAL MICROMECHANICS 119
A three-dimensional damage model to simulate the progressive failure of composite structures 118
Modelli e metodi per lo studio della dinamica longitudinale del pneumatico 115
Quasi-trivial stacking sequences for the design of thick laminates 115
A numerical micro-mechanical study of the influence of fiber–matrix interphase failure on carbon/epoxy material properties 114
Experimental assessment of Fully-Uncoupled Multi-Directional specimens for mode I delamination tests 113
Multi-scale Least-Weight Design of a Wing-Box Through a Global/Local Modelling Approach 111
A consistent energy-based cohesive zone model to simulate delamination between differently oriented plies 111
Co-infused and secondary bonded composite stiffened panels in compression: Numerical and experimental strength assessment combined with NDI and guided waves based SHM 110
Quasi-trivial solutions for uncoupled, homogeneous and quasi-homogeneous laminates with high number of plies 109
Effects of hybridization and ply thickness on the strength and toughness of composite laminates 109
DEVELOPMENT AND FINITE ELEMENTS ASSESSMENT OF STACKING SEQUENCES FOR INTERLAMINAR FRACTURE TOUGHNESS TESTING OF ANGLE-PLY INTERFACES 108
Least-weight design of composite structures: an unconventional and general approach 107
Multi-scale optimisation of thin-walled structures by considering a global/local modelling approach 107
Quasi-trivial solutions for uncoupled, homogeneous and quasi-homogeneous laminates with high number of plies 99
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 73
Preface 68
DAMAGE TOLERANCE OF A CURVED COMPOSITE STIFFENED PANEL FABRICATED BY AN OUT OF AUTOCLAVE – LIQUID RESIN INFUSION PROCESS 22
Standard specimen geometries do not always lead to consistent fatigue results for epoxy adhesives 21
A non-linear model for in-plane shear damage and failure of composite laminates 5
Totale 10.656
Salva come PNG Salva come JPEG
Categoria #
all - tutte 28.086
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 28.086
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202171 0 0 0 0 0 0 0 0 0 0 0 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
2024/20252.330 6 86 32 78 275 290 128 127 205 248 276 579
2025/20263.217 182 447 548 224 352 241 477 113 200 285 110 38
Totale 10.656