PORTO @ Archivio Istituzionale della Ricerca

ICARDI, Ugo
 Distribuzione geografica
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Continente #
NA - Nord America 13.581
EU - Europa 12.012
AS - Asia 2.831
SA - Sud America 176
AF - Africa 40
OC - Oceania 13
Continente sconosciuto - Info sul continente non disponibili 4
Totale 28.657
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Nazione #
US - Stati Uniti d'America 13.510
GB - Regno Unito 2.301
IT - Italia 2.208
DE - Germania 2.050
FR - Francia 1.961
UA - Ucraina 1.130
CN - Cina 1.040
SG - Singapore 888
RU - Federazione Russa 557
NL - Olanda 544
TR - Turchia 385
IE - Irlanda 340
SE - Svezia 233
KR - Corea 199
CH - Svizzera 182
FI - Finlandia 167
BR - Brasile 147
AT - Austria 111
IN - India 68
CA - Canada 63
JO - Giordania 46
IR - Iran 45
BG - Bulgaria 43
JP - Giappone 35
BE - Belgio 27
HK - Hong Kong 25
AP - ???statistics.table.value.countryCode.AP??? 23
ID - Indonesia 23
MY - Malesia 23
RO - Romania 23
EU - Europa 21
VN - Vietnam 16
ZA - Sudafrica 14
GR - Grecia 12
AU - Australia 11
CL - Cile 11
ES - Italia 11
IL - Israele 11
TW - Taiwan 11
AR - Argentina 10
BY - Bielorussia 8
PH - Filippine 8
EG - Egitto 6
PL - Polonia 6
PT - Portogallo 6
SN - Senegal 6
UZ - Uzbekistan 5
AE - Emirati Arabi Uniti 4
DZ - Algeria 4
MA - Marocco 4
PK - Pakistan 4
AZ - Azerbaigian 3
BD - Bangladesh 3
CZ - Repubblica Ceca 3
EE - Estonia 3
HR - Croazia 3
IQ - Iraq 3
KZ - Kazakistan 3
MX - Messico 3
VE - Venezuela 3
CO - Colombia 2
DK - Danimarca 2
GE - Georgia 2
LB - Libano 2
MT - Malta 2
NG - Nigeria 2
NO - Norvegia 2
NZ - Nuova Zelanda 2
PE - Perù 2
SA - Arabia Saudita 2
TH - Thailandia 2
AM - Armenia 1
BH - Bahrain 1
CG - Congo 1
CI - Costa d'Avorio 1
CR - Costa Rica 1
DO - Repubblica Dominicana 1
EC - Ecuador 1
GP - Guadalupe 1
HN - Honduras 1
HU - Ungheria 1
JM - Giamaica 1
KE - Kenya 1
KG - Kirghizistan 1
LA - Repubblica Popolare Democratica del Laos 1
LT - Lituania 1
LU - Lussemburgo 1
LV - Lettonia 1
MD - Moldavia 1
PS - Palestinian Territory 1
QA - Qatar 1
SI - Slovenia 1
TN - Tunisia 1
Totale 28.657
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Città #
Ashburn 3.664
Southend 2.072
Seattle 1.700
Fairfield 867
Jacksonville 551
Chandler 549
Princeton 494
Houston 474
San Ramon 437
Woodbridge 418
Turin 379
Singapore 365
Ann Arbor 348
Dublin 332
Cambridge 330
Amsterdam 317
Chicago 308
Wilmington 306
Berlin 295
Beijing 281
Izmir 271
Santa Clara 245
Boardman 217
Bern 175
Des Moines 166
San Donato Milanese 160
Helsinki 155
Torino 152
Bologna 147
Baltimore 138
Shanghai 134
Zhengzhou 131
Zaporozhye 130
Pennsylvania Furnace 128
Overberg 121
Saint Petersburg 93
Hangzhou 78
Milan 78
Monopoli 69
Padua 68
Buffalo 67
San Francisco 62
Vienna 58
Mountain View 55
Bremen 53
Council Bluffs 52
Fremont 47
Moscow 47
San Jose 46
San Diego 45
New York 41
Dearborn 39
Istanbul 38
Malatya 38
Redwood City 38
Atlanta 31
Piscataway 30
Frankfurt 28
Guangzhou 28
Rome 28
Toronto 28
Kiev 27
Hefei 26
Washington 25
Las Vegas 23
Naples 23
Norwalk 23
Andover 22
Brussels 22
Shenzhen 22
Melun 21
Yubileyny 21
London 20
Jakarta 19
Paris 19
Austin 17
Genova 17
Kocaeli 17
Nuremberg 17
Jinan 16
Verona 16
Falls Church 14
Harbin 14
Novosibirsk 14
Portsmouth 14
Hong Kong 13
Ningbo 13
Rivoli 13
Dalian 12
Galati 12
Indiana 12
Monza 12
São Paulo 12
Delhi 11
Lappeenranta 11
Nanjing 11
San Mateo 11
Shenyang 11
Yekaterinburg 11
Cermenate 10
Totale 18.886
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Nome #
Aeronave radiocomandata di grandissime dimensioni 578
Multilayered shell model with variable representation of displacements across the thickness 351
Thermo-mechanical delamination analysis by a plate model with “adaptive” representation of displacements and temperature 334
Layerwise mixed element with sublaminates approximation and 3D zig-zag field, for analysis of local effects in laminated and sandwich composites 332
Impact analysis of sandwich composites based on a refined plate element with strain energy updating 326
Variable kinematics layerwise model for analysis of bonded joints 324
Extension of the strain energy updating technique to a multilayered shell model with adaptive displacements and fixed DOF 321
RESPONSE OF SANDWICHES UNDERGOING STATIC AND BLAST PULSE LOADING WITH TAILORING OPTIMIZATION AND STITCHING 319
Assessment of recent theories for predicting failure of composite laminates 313
C0 Layerwise Model with Fixed Degrees of Freedom and Variable In- and Out-of-Plane Kinematics by Strain Energy Updating Technique 311
The nonlinear response of unsymmetric multilayered plates using smeared laminate and layerwise models 295
Indentation of Sandwiches Using a Refined Zig-Zag Model and a Mesoscale Damage Model 294
Layerwise zig-zag model with selective refinement across the thickness 282
Numerical assessment of the core deformability effect on the behavior of sandwich beams 278
Preliminary study of an adaptive wing with shape memory alloy torsion actuators 268
Optimization of multi-core sandwich composites undergoing impact loads 266
Holographic interferometry assessment of stress distribution in sandwich beams in bending 264
C0 plate element for delamination damage analysis, based on a zig-zag model and strain energy updating 263
Cylindrical bending of laminated cylindrical shells using a modified zig-zag theory 262
Assessment of recent zig-zag theories for laminated and sandwich structures 262
Simple, efficient mixed solid element for accurate analysis of local effects in laminated and sandwich composites 256
An evaluation of the influence of geometry and material properties at free edges and at corners of composite laminates 250
Aeromobile a sostentazione aerostatica ad alta manovrabilità 249
Multilayered Plate Model with "Adaptive" Representation of Displacements and TemperatureAcross the Thickness and Fixed D.O.F. 248
RECOVERING CRITICAL STRESSES IN SANDWICHES USING THROUGH-THETHICKNESS REINFORCEMENT 247
Analysis of thick multilayered anisotropic plates by a higher order plate element 247
A Three-Dimensional Zig-Zag Theory for Analysis of Thick Laminated Beams 242
Failure analysis of composite laminates under large deflection 242
Eight-noded zig-zag element for deflection and stress analysis of plates with general lay-up 241
SMA actuated mechanism for an adaptive wing 238
Large deflection of adaptive multilayered Timoshenko beams 236
Analysis of Laminated and Sandwich Composites by a Zig-zag Plate Element with Variable Kinematics and Fixed Degrees of Freedom 235
On modeling of global and local response of sandwich plates with laminated faces 235
Smart structures featuring imperfect bonding interfaces: Modeling and implications 234
DEVELOPMENT OF AN EFFICIENT ZIG-ZAG MODEL WITH VARIABLE REPRESENTATION OF DISPLACEMENTS ACROSS THE THICKNESS 232
Extension of a new tailoring optimisation technique to sandwich shells with laminated faces 231
Velivolo cargo di grandissime dimensioni: sviluppo del progetto e sperimentazione didattica 230
Discrete-layer models for multilayered shells accounting for interlayer continuity 229
Laminated shell model with second-order expansion of the reciprocals of Lamé coefficients Hα, Hβ and interlayer continuities fulfilment 225
Impact analysis of sandwich composites 224
Dynamic response of adaptive cross-ply cantilevers featuring interlaminar bonding imperfections 222
Analysis Of Bonded Joints With Laminated Adherends By A Variable Kinematics Layerwise Model 221
On modeling of global response behavior of sandwich plates with laminated faces 220
Velivolo cargo di grandissime dimensioni: sviluppo del progetto e sperimentazione didattica 220
Large-deflection and stress analysis of multilayered plates with induced-strain actuators 219
Application of a new tailoring optimization technique to laminated and sandwich plates and to spherical panels 218
Free edge stress propagation in composite laminates 217
Laminated and sandwich panels subject to blast pulse loading 217
Layerwise zig-zag model with selective refinement across the thickness 216
Optimization of Variable Stiffness Laminates and Sandwiches Undergoing Impulsive Dynamic Loading 216
Postbuckling of laminated composite and sandwich plates and shells: on the significance of the fulfillment of static interlayer continuity conditions 215
A new tailoring optimization approach for improving structural response and energy absorption capability of laminated and sandwich composites 215
Co plate element for global/local analysis of multilayered composites, based on a 3D zig-zag model and strain energy updating 212
Large bending actuator made with SMA contractile wires: theory, numerical simulation and experiments 208
Optimization of sandwich panels to blast pulse loading 208
Through-the-thickness displacements measurement in laminated composites using electronic speckle photography 207
Variable Singularity Power Wedge Element for Multilayered Composites 207
Modeling assessment and optimization of impacted multi-core sandwich composites 207
Riduzione della freccia di una trave composita mediante stratificazione, materiale e spessori variabili lungo l'asse 205
APPLICATION OF A NEW TAILORING OPTIMIZATION TECHNIQUE TO LAMINATED AND SANDWICH PLATES AND TO SANDWICH SPHERICAL PANELS 203
On modeling of laminated composite structures featuring interlaminae imperfections 203
Improving energy absorption and dissipation of composites through optimized tailoring 202
Higher-order zig-zag model for analysis of thick composite beams with including transverse normal stress and sublaminates approximations 201
A comparison among several recent criteria for the failure analysis of composites 201
Applications of zig-zag theories to sandwich beams 201
Impact analysis of laminated and sandwich composites using a plate finite element with strain energy updating 199
Assessment and optimization of multiple core sandwich composites 197
INDENTATION OF SANDWICHES USING A PLATE MODEL WITH VARIABLE KINEMATICS AND FIXED DEGREES OF FREEDOM 197
Failure analysis of composite laminates under large deflection 197
Optimisation of sandwich panels with functionally graded core and faces 196
Impact and blast pulse: improving energy absorption of fibre-reinforced composites through optimized tailoring 195
INDENTATION OF SANDWICHES USING A LAYERWISE MODEL WITH FIXED DEGREES OF FREEDOM 194
Multilayered Model with Variable Kinematics and Fixed D.O.F. for Analysis of Bonded Joints 192
Impact Damage Analysis with Stress Continuity Constraints Fulfilment at Damaged-Undamaged Regions and at Layer Interfaces 191
Free vibration of composite beams featuring interlaminar bonding imperfections and exposed to thermomechanical loading 188
Numerical assessment of the core deformability effect on the behavior of sandwich beams 186
Effects of interfacial damage on the global and local static response of cross-ply laminates 185
Finite element analysis of composite plates with induced-strain actuators: an evaluation of smeared-laminate and discrete-layer models 184
Dimensionamento e studio degli effetti locali nelle strutture a nido d'ape (Nota Scientifica 211bis DIASP Politecnico di Torino) 183
Minimization of interlaminar stresses in sandwich composites by a new tailoring optimization concept 183
Sul danneggiamento per delaminazione dei compositi multistrato 182
Using artificial intelligence in structural design. 181
Uno studio sull’assorbimento energetico ottimizzato dei compositi multistrato 178
Modeling techniques assessment and optimization of laminated and sandwich composites undergoing impact loads 177
A study of energy absorption in fiber-reinforced composites: transfer form bending to shear 177
C0 FIXED DEGREES OF FREEDOM ZIG-ZAG MODEL WITH VARIABLE IN-PLANE AND OUT-OF-PLANE KINEMATICS AND QUADRILATERAL PLATE ELEMENT 177
An Assessment of Techniques for predicting Delamination: A Comparison among Stress based Criteria, Fracture Mechanics and Interface Models 175
C0 MIXED LAYERWISE QUADRILATERAL PLATE ELEMENT WITH VARIABLE IN AND OUT-OF-PLANE KINEMATICS AND FIXED D.O.F 172
Multiple core sandwich composites optimization for improving the impact behavior 169
C0 plate element based on strain energy updating and spline interpolation, for analysis of impact damage in laminated composites 168
Zig-zag theories differently accounting for layerwise effects of multilayered composites 168
Analysis and testing of composite stiffened panels with impact induced delamination 166
Low velocity impact induced delamination on composite stiffened panels: fem simulation and c-scan detection 165
Divergence and Flutter of Adaptive Laminated Composite Aircraft Wings Featuring Damaged Bonding Interfaces 164
Sulla modellizzazione del comportamento strutturale di elementi in materiale composito 163
Structures Featuring Imperfect Bonding Interfaces: Modeling and Implications 161
EM SULLA MODELLIZZAZIONE DEL COMPORTAMENTO STRUTTURALE DI ELEMENTI IN MATERIALE COMPOSITO 160
A geometrically nonlinear theory of composite plates with induced-strain actuators 160
Optimization of energy absorption and dissipation of composites 159
Some considerations concerning the edge-stress problem of laminates by finite elements 159
Totale 22.543
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Categoria #
all - tutte 86.700
article - articoli 46.744
book - libri 0
conference - conferenze 26.855
curatela - curatele 0
other - altro 11.410
patent - brevetti 1.691
selected - selezionate 0
volume - volumi 0
Totale 173.400
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020306 0 0 0 0 0 0 0 0 0 174 78 54
2020/20211.960 330 309 71 276 59 208 45 175 71 202 162 52
2021/20221.206 80 94 13 29 29 105 45 44 55 73 237 402
2022/20232.310 212 402 48 128 251 323 287 116 232 6 80 225
2023/2024591 39 34 8 72 74 78 8 37 10 9 72 150
2024/20252.659 75 601 129 350 270 84 110 149 506 385 0 0
Totale 28.742