ICARDI, Ugo
 Distribuzione geografica
Continente #
NA - Nord America 14.279
EU - Europa 12.140
AS - Asia 4.629
SA - Sud America 541
AF - Africa 63
OC - Oceania 14
Continente sconosciuto - Info sul continente non disponibili 4
Totale 31.670
Nazione #
US - Stati Uniti d'America 14.166
GB - Regno Unito 2.321
IT - Italia 2.219
DE - Germania 2.083
FR - Francia 1.964
SG - Singapore 1.738
CN - Cina 1.551
UA - Ucraina 1.135
RU - Federazione Russa 566
NL - Olanda 547
BR - Brasile 461
TR - Turchia 390
IE - Irlanda 341
KR - Corea 292
SE - Svezia 235
CH - Svizzera 182
FI - Finlandia 174
HK - Hong Kong 171
AT - Austria 123
VN - Vietnam 115
IN - India 92
CA - Canada 81
IR - Iran 47
JO - Giordania 47
BG - Bulgaria 43
JP - Giappone 42
ID - Indonesia 34
AR - Argentina 30
BE - Belgio 27
ZA - Sudafrica 26
MY - Malesia 24
RO - Romania 24
AP - ???statistics.table.value.countryCode.AP??? 23
EU - Europa 21
BD - Bangladesh 20
EC - Ecuador 18
PL - Polonia 17
ES - Italia 14
IL - Israele 14
MX - Messico 14
AU - Australia 12
GR - Grecia 12
CL - Cile 11
TW - Taiwan 11
BY - Bielorussia 10
PH - Filippine 10
VE - Venezuela 10
IQ - Iraq 9
SN - Senegal 9
PK - Pakistan 8
EG - Egitto 7
PT - Portogallo 7
AE - Emirati Arabi Uniti 6
DZ - Algeria 6
SA - Arabia Saudita 6
UZ - Uzbekistan 6
CO - Colombia 5
HN - Honduras 5
KZ - Kazakistan 5
MA - Marocco 5
AZ - Azerbaigian 3
CZ - Repubblica Ceca 3
DK - Danimarca 3
DO - Repubblica Dominicana 3
EE - Estonia 3
HR - Croazia 3
JM - Giamaica 3
LB - Libano 3
NO - Norvegia 3
PY - Paraguay 3
AM - Armenia 2
BH - Bahrain 2
CR - Costa Rica 2
GE - Georgia 2
KG - Kirghizistan 2
LA - Repubblica Popolare Democratica del Laos 2
LT - Lituania 2
LV - Lettonia 2
MT - Malta 2
NG - Nigeria 2
NZ - Nuova Zelanda 2
PE - Perù 2
PS - Palestinian Territory 2
TH - Thailandia 2
BS - Bahamas 1
CG - Congo 1
CI - Costa d'Avorio 1
GA - Gabon 1
GP - Guadalupe 1
GT - Guatemala 1
HU - Ungheria 1
KE - Kenya 1
KW - Kuwait 1
LU - Lussemburgo 1
LY - Libia 1
MD - Moldavia 1
ML - Mali 1
MU - Mauritius 1
PA - Panama 1
PR - Porto Rico 1
Totale 31.666
Città #
Ashburn 3.744
Southend 2.072
Seattle 1.704
Singapore 904
Fairfield 867
Jacksonville 551
Chandler 549
Princeton 494
Houston 477
San Ramon 437
Woodbridge 418
Turin 382
Beijing 380
Ann Arbor 348
Dublin 333
Cambridge 330
Amsterdam 319
Chicago 318
Wilmington 306
Berlin 295
Izmir 271
Santa Clara 267
Boardman 217
Bern 175
Des Moines 166
San Donato Milanese 160
Hong Kong 159
Dallas 156
Helsinki 155
Torino 152
Bologna 147
Shanghai 141
Baltimore 139
Zhengzhou 134
Zaporozhye 130
Buffalo 129
Pennsylvania Furnace 128
Overberg 121
Saint Petersburg 93
Milan 80
Hangzhou 78
Los Angeles 73
Monopoli 69
Padua 68
San Francisco 66
Vienna 60
Council Bluffs 55
Mountain View 55
Bremen 53
New York 51
San Jose 48
Fremont 47
Moscow 47
San Diego 46
Columbus 41
Dearborn 39
Istanbul 39
The Dalles 39
Tongling 39
Guangzhou 38
Hefei 38
Malatya 38
Redwood City 38
Seoul 38
North Bergen 36
Atlanta 35
Ho Chi Minh City 35
Toronto 32
São Paulo 31
Piscataway 30
Rome 29
Frankfurt 28
Hanoi 27
Kiev 27
Munich 27
Washington 26
Las Vegas 23
London 23
Naples 23
Norwalk 23
Shenzhen 23
Andover 22
Brussels 22
Melun 21
Nuremberg 21
Yubileyny 21
Jakarta 20
Paris 20
Austin 17
Genova 17
Harbin 17
Jinan 17
Kocaeli 17
Verona 16
Dalian 14
Falls Church 14
Ningbo 14
Novosibirsk 14
Phoenix 14
Portsmouth 14
Totale 20.361
Nome #
Aeronave radiocomandata di grandissime dimensioni 593
Multilayered shell model with variable representation of displacements across the thickness 377
Variable kinematics layerwise model for analysis of bonded joints 357
Extension of the strain energy updating technique to a multilayered shell model with adaptive displacements and fixed DOF 357
Thermo-mechanical delamination analysis by a plate model with “adaptive” representation of displacements and temperature 351
Layerwise mixed element with sublaminates approximation and 3D zig-zag field, for analysis of local effects in laminated and sandwich composites 350
RESPONSE OF SANDWICHES UNDERGOING STATIC AND BLAST PULSE LOADING WITH TAILORING OPTIMIZATION AND STITCHING 347
Impact analysis of sandwich composites based on a refined plate element with strain energy updating 347
C0 Layerwise Model with Fixed Degrees of Freedom and Variable In- and Out-of-Plane Kinematics by Strain Energy Updating Technique 344
Assessment of recent theories for predicting failure of composite laminates 336
Indentation of Sandwiches Using a Refined Zig-Zag Model and a Mesoscale Damage Model 322
The nonlinear response of unsymmetric multilayered plates using smeared laminate and layerwise models 316
Optimization of multi-core sandwich composites undergoing impact loads 305
Numerical assessment of the core deformability effect on the behavior of sandwich beams 304
Layerwise zig-zag model with selective refinement across the thickness 302
Holographic interferometry assessment of stress distribution in sandwich beams in bending 299
Simple, efficient mixed solid element for accurate analysis of local effects in laminated and sandwich composites 290
Preliminary study of an adaptive wing with shape memory alloy torsion actuators 286
Cylindrical bending of laminated cylindrical shells using a modified zig-zag theory 285
Assessment of recent zig-zag theories for laminated and sandwich structures 284
An evaluation of the influence of geometry and material properties at free edges and at corners of composite laminates 278
C0 plate element for delamination damage analysis, based on a zig-zag model and strain energy updating 278
RECOVERING CRITICAL STRESSES IN SANDWICHES USING THROUGH-THETHICKNESS REINFORCEMENT 277
Multilayered Plate Model with "Adaptive" Representation of Displacements and TemperatureAcross the Thickness and Fixed D.O.F. 270
Failure analysis of composite laminates under large deflection 269
Aeromobile a sostentazione aerostatica ad alta manovrabilità 268
Eight-noded zig-zag element for deflection and stress analysis of plates with general lay-up 267
Analysis of thick multilayered anisotropic plates by a higher order plate element 265
Large deflection of adaptive multilayered Timoshenko beams 264
Analysis of Laminated and Sandwich Composites by a Zig-zag Plate Element with Variable Kinematics and Fixed Degrees of Freedom 261
Smart structures featuring imperfect bonding interfaces: Modeling and implications 260
SMA actuated mechanism for an adaptive wing 260
A Three-Dimensional Zig-Zag Theory for Analysis of Thick Laminated Beams 257
Velivolo cargo di grandissime dimensioni: sviluppo del progetto e sperimentazione didattica 254
On modeling of global and local response of sandwich plates with laminated faces 254
DEVELOPMENT OF AN EFFICIENT ZIG-ZAG MODEL WITH VARIABLE REPRESENTATION OF DISPLACEMENTS ACROSS THE THICKNESS 252
Dynamic response of adaptive cross-ply cantilevers featuring interlaminar bonding imperfections 251
Optimization of Variable Stiffness Laminates and Sandwiches Undergoing Impulsive Dynamic Loading 248
Laminated shell model with second-order expansion of the reciprocals of Lamé coefficients Hα, Hβ and interlayer continuities fulfilment 248
Analysis Of Bonded Joints With Laminated Adherends By A Variable Kinematics Layerwise Model 246
Discrete-layer models for multilayered shells accounting for interlayer continuity 243
Improving energy absorption and dissipation of composites through optimized tailoring 243
On modeling of global response behavior of sandwich plates with laminated faces 241
Velivolo cargo di grandissime dimensioni: sviluppo del progetto e sperimentazione didattica 240
Extension of a new tailoring optimisation technique to sandwich shells with laminated faces 240
Large-deflection and stress analysis of multilayered plates with induced-strain actuators 240
Impact analysis of sandwich composites 240
Laminated and sandwich panels subject to blast pulse loading 238
Free edge stress propagation in composite laminates 237
Co plate element for global/local analysis of multilayered composites, based on a 3D zig-zag model and strain energy updating 237
Application of a new tailoring optimization technique to laminated and sandwich plates and to spherical panels 235
Layerwise zig-zag model with selective refinement across the thickness 235
Large bending actuator made with SMA contractile wires: theory, numerical simulation and experiments 234
A new tailoring optimization approach for improving structural response and energy absorption capability of laminated and sandwich composites 234
Through-the-thickness displacements measurement in laminated composites using electronic speckle photography 233
Postbuckling of laminated composite and sandwich plates and shells: on the significance of the fulfillment of static interlayer continuity conditions 233
Riduzione della freccia di una trave composita mediante stratificazione, materiale e spessori variabili lungo l'asse 229
Optimization of sandwich panels to blast pulse loading 229
Variable Singularity Power Wedge Element for Multilayered Composites 229
A comparison among several recent criteria for the failure analysis of composites 224
INDENTATION OF SANDWICHES USING A LAYERWISE MODEL WITH FIXED DEGREES OF FREEDOM 224
Modeling assessment and optimization of impacted multi-core sandwich composites 224
APPLICATION OF A NEW TAILORING OPTIMIZATION TECHNIQUE TO LAMINATED AND SANDWICH PLATES AND TO SANDWICH SPHERICAL PANELS 223
INDENTATION OF SANDWICHES USING A PLATE MODEL WITH VARIABLE KINEMATICS AND FIXED DEGREES OF FREEDOM 223
Higher-order zig-zag model for analysis of thick composite beams with including transverse normal stress and sublaminates approximations 222
On modeling of laminated composite structures featuring interlaminae imperfections 221
Impact analysis of laminated and sandwich composites using a plate finite element with strain energy updating 220
Effects of interfacial damage on the global and local static response of cross-ply laminates 220
Multilayered Model with Variable Kinematics and Fixed D.O.F. for Analysis of Bonded Joints 219
Assessment and optimization of multiple core sandwich composites 218
Optimisation of sandwich panels with functionally graded core and faces 216
Failure analysis of composite laminates under large deflection 213
Impact Damage Analysis with Stress Continuity Constraints Fulfilment at Damaged-Undamaged Regions and at Layer Interfaces 213
Applications of zig-zag theories to sandwich beams 211
Minimization of interlaminar stresses in sandwich composites by a new tailoring optimization concept 206
Impact and blast pulse: improving energy absorption of fibre-reinforced composites through optimized tailoring 205
Finite element analysis of composite plates with induced-strain actuators: an evaluation of smeared-laminate and discrete-layer models 205
Numerical assessment of the core deformability effect on the behavior of sandwich beams 204
Sul danneggiamento per delaminazione dei compositi multistrato 202
Free vibration of composite beams featuring interlaminar bonding imperfections and exposed to thermomechanical loading 202
C0 MIXED LAYERWISE QUADRILATERAL PLATE ELEMENT WITH VARIABLE IN AND OUT-OF-PLANE KINEMATICS AND FIXED D.O.F 199
Dimensionamento e studio degli effetti locali nelle strutture a nido d'ape (Nota Scientifica 211bis DIASP Politecnico di Torino) 198
C0 FIXED DEGREES OF FREEDOM ZIG-ZAG MODEL WITH VARIABLE IN-PLANE AND OUT-OF-PLANE KINEMATICS AND QUADRILATERAL PLATE ELEMENT 197
Analysis and testing of composite stiffened panels with impact induced delamination 197
Uno studio sull’assorbimento energetico ottimizzato dei compositi multistrato 196
An Assessment of Techniques for predicting Delamination: A Comparison among Stress based Criteria, Fracture Mechanics and Interface Models 195
Using artificial intelligence in structural design. 194
Modeling techniques assessment and optimization of laminated and sandwich composites undergoing impact loads 193
A study of energy absorption in fiber-reinforced composites: transfer form bending to shear 190
C0 plate element based on strain energy updating and spline interpolation, for analysis of impact damage in laminated composites 188
Sulla modellizzazione del comportamento strutturale di elementi in materiale composito 187
Zig-zag theories differently accounting for layerwise effects of multilayered composites 185
Multiple core sandwich composites optimization for improving the impact behavior 184
Divergence and Flutter of Adaptive Laminated Composite Aircraft Wings Featuring Damaged Bonding Interfaces 183
A geometrically nonlinear theory of composite plates with induced-strain actuators 183
Low velocity impact induced delamination on composite stiffened panels: fem simulation and c-scan detection 182
Structures Featuring Imperfect Bonding Interfaces: Modeling and Implications 180
Some considerations concerning the edge-stress problem of laminates by finite elements 179
Elementi singolari per la Meccanica della Frattura 178
On the buckling analysis of imperfect laminated stiffened conical shells 177
Totale 24.749
Categoria #
all - tutte 97.201
article - articoli 52.592
book - libri 0
conference - conferenze 30.126
curatela - curatele 0
other - altro 12.660
patent - brevetti 1.823
selected - selezionate 0
volume - volumi 0
Totale 194.402


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021974 0 0 0 0 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
2024/20253.275 75 601 129 350 270 84 110 149 506 491 167 343
2025/20262.397 387 347 596 630 437 0 0 0 0 0 0 0
Totale 31.755