PORTO @ Archivio Istituzionale della Ricerca

ICARDI, Ugo
 Distribuzione geografica
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Continente #
NA - Nord America 12.740
EU - Europa 11.395
AS - Asia 1.604
AF - Africa 30
SA - Sud America 25
OC - Oceania 12
Continente sconosciuto - Info sul continente non disponibili 4
Totale 25.810
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Nazione #
US - Stati Uniti d'America 12.678
GB - Regno Unito 2.283
IT - Italia 2.179
DE - Germania 2.023
FR - Francia 1.950
UA - Ucraina 1.125
CN - Cina 854
RU - Federazione Russa 426
TR - Turchia 346
IE - Irlanda 340
NL - Olanda 246
SE - Svezia 231
CH - Svizzera 182
FI - Finlandia 167
KR - Corea 115
AT - Austria 64
IN - India 64
CA - Canada 60
JO - Giordania 45
IR - Iran 42
JP - Giappone 35
SG - Singapore 31
AP - ???statistics.table.value.countryCode.AP??? 23
MY - Malesia 23
BE - Belgio 21
EU - Europa 21
RO - Romania 21
VN - Vietnam 16
GR - Grecia 12
HK - Hong Kong 12
IL - Israele 11
TW - Taiwan 11
ZA - Sudafrica 11
AU - Australia 10
ES - Italia 10
CL - Cile 9
BR - Brasile 8
BY - Bielorussia 8
PH - Filippine 8
PL - Polonia 6
PT - Portogallo 6
AR - Argentina 5
EG - Egitto 5
ID - Indonesia 5
BG - Bulgaria 4
DZ - Algeria 4
SN - Senegal 4
AE - Emirati Arabi Uniti 3
CZ - Repubblica Ceca 3
EE - Estonia 3
HR - Croazia 3
MA - Marocco 3
BD - Bangladesh 2
DK - Danimarca 2
KZ - Kazakistan 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
CI - Costa d'Avorio 1
CO - Colombia 1
GE - Georgia 1
GP - Guadalupe 1
HU - Ungheria 1
JM - Giamaica 1
LA - Repubblica Popolare Democratica del Laos 1
LU - Lussemburgo 1
LV - Lettonia 1
MD - Moldavia 1
SI - Slovenia 1
Totale 25.810
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Città #
Ashburn 3.609
Southend 2.072
Seattle 1.699
Fairfield 867
Jacksonville 551
Chandler 549
Princeton 494
Houston 474
San Ramon 437
Woodbridge 418
Turin 371
Ann Arbor 348
Dublin 332
Cambridge 330
Chicago 308
Wilmington 306
Berlin 295
Beijing 278
Izmir 267
Bern 175
Des Moines 166
San Donato Milanese 160
Helsinki 155
Torino 152
Bologna 147
Baltimore 138
Zhengzhou 131
Zaporozhye 130
Pennsylvania Furnace 128
Shanghai 124
Overberg 121
Saint Petersburg 93
Hangzhou 78
Milan 77
Boardman 71
Monopoli 69
Padua 68
Buffalo 67
San Francisco 62
Mountain View 55
Bremen 53
Vienna 48
Fremont 47
San Jose 46
San Diego 45
Moscow 41
Dearborn 39
Malatya 38
Redwood City 38
Atlanta 31
Frankfurt 28
Rome 28
Kiev 27
Hefei 26
Toronto 26
Washington 25
Las Vegas 23
Naples 23
Norwalk 23
Andover 22
Shenzhen 22
Amsterdam 21
Guangzhou 21
Melun 21
Paris 19
Singapore 18
Austin 17
Genova 17
Kocaeli 17
London 17
Brussels 16
Jinan 16
Verona 16
New York 15
Falls Church 14
Harbin 14
Novosibirsk 14
Ningbo 13
Rivoli 13
Galati 12
Indiana 12
Monza 12
Delhi 11
Lappeenranta 11
Nanjing 11
San Mateo 11
Shenyang 11
Yekaterinburg 11
Dalian 10
Florence 10
Frankfurt Am Main 10
Montréal 10
Pianezza 10
Samara 10
Skudai 10
Cupertino 9
Dallas 9
Fujian 9
Guangdong 9
Hamedan 9
Totale 17.587
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Nome #
Multilayered shell model with variable representation of displacements across the thickness 319
Layerwise mixed element with sublaminates approximation and 3D zig-zag field, for analysis of local effects in laminated and sandwich composites 315
Extension of the strain energy updating technique to a multilayered shell model with adaptive displacements and fixed DOF 309
Thermo-mechanical delamination analysis by a plate model with “adaptive” representation of displacements and temperature 306
RESPONSE OF SANDWICHES UNDERGOING STATIC AND BLAST PULSE LOADING WITH TAILORING OPTIMIZATION AND STITCHING 300
Variable kinematics layerwise model for analysis of bonded joints 300
Impact analysis of sandwich composites based on a refined plate element with strain energy updating 297
Assessment of recent theories for predicting failure of composite laminates 297
C0 Layerwise Model with Fixed Degrees of Freedom and Variable In- and Out-of-Plane Kinematics by Strain Energy Updating Technique 284
The nonlinear response of unsymmetric multilayered plates using smeared laminate and layerwise models 276
Indentation of Sandwiches Using a Refined Zig-Zag Model and a Mesoscale Damage Model 276
Aeronave radiocomandata di grandissime dimensioni 273
Layerwise zig-zag model with selective refinement across the thickness 261
Numerical assessment of the core deformability effect on the behavior of sandwich beams 259
Optimization of multi-core sandwich composites undergoing impact loads 252
Holographic interferometry assessment of stress distribution in sandwich beams in bending 248
Cylindrical bending of laminated cylindrical shells using a modified zig-zag theory 246
Preliminary study of an adaptive wing with shape memory alloy torsion actuators 246
C0 plate element for delamination damage analysis, based on a zig-zag model and strain energy updating 246
Simple, efficient mixed solid element for accurate analysis of local effects in laminated and sandwich composites 245
An evaluation of the influence of geometry and material properties at free edges and at corners of composite laminates 232
Assessment of recent zig-zag theories for laminated and sandwich structures 231
Aeromobile a sostentazione aerostatica ad alta manovrabilità 229
Multilayered Plate Model with "Adaptive" Representation of Displacements and TemperatureAcross the Thickness and Fixed D.O.F. 229
Analysis of thick multilayered anisotropic plates by a higher order plate element 229
A Three-Dimensional Zig-Zag Theory for Analysis of Thick Laminated Beams 226
SMA actuated mechanism for an adaptive wing 226
Eight-noded zig-zag element for deflection and stress analysis of plates with general lay-up 224
Extension of a new tailoring optimisation technique to sandwich shells with laminated faces 224
Failure analysis of composite laminates under large deflection 222
RECOVERING CRITICAL STRESSES IN SANDWICHES USING THROUGH-THETHICKNESS REINFORCEMENT 221
Smart structures featuring imperfect bonding interfaces: Modeling and implications 220
Large deflection of adaptive multilayered Timoshenko beams 218
On modeling of global and local response of sandwich plates with laminated faces 216
DEVELOPMENT OF AN EFFICIENT ZIG-ZAG MODEL WITH VARIABLE REPRESENTATION OF DISPLACEMENTS ACROSS THE THICKNESS 211
Impact analysis of sandwich composites 209
Velivolo cargo di grandissime dimensioni: sviluppo del progetto e sperimentazione didattica 207
Free edge stress propagation in composite laminates 206
Discrete-layer models for multilayered shells accounting for interlayer continuity 206
Large-deflection and stress analysis of multilayered plates with induced-strain actuators 206
On modeling of global response behavior of sandwich plates with laminated faces 205
Analysis of Laminated and Sandwich Composites by a Zig-zag Plate Element with Variable Kinematics and Fixed Degrees of Freedom 205
Dynamic response of adaptive cross-ply cantilevers featuring interlaminar bonding imperfections 204
Laminated shell model with second-order expansion of the reciprocals of Lamé coefficients Hα, Hβ and interlayer continuities fulfilment 203
Velivolo cargo di grandissime dimensioni: sviluppo del progetto e sperimentazione didattica 202
Analysis Of Bonded Joints With Laminated Adherends By A Variable Kinematics Layerwise Model 201
Postbuckling of laminated composite and sandwich plates and shells: on the significance of the fulfillment of static interlayer continuity conditions 198
Layerwise zig-zag model with selective refinement across the thickness 198
Co plate element for global/local analysis of multilayered composites, based on a 3D zig-zag model and strain energy updating 197
Optimization of sandwich panels to blast pulse loading 197
Laminated and sandwich panels subject to blast pulse loading 194
A new tailoring optimization approach for improving structural response and energy absorption capability of laminated and sandwich composites 194
Optimization of Variable Stiffness Laminates and Sandwiches Undergoing Impulsive Dynamic Loading 194
Modeling assessment and optimization of impacted multi-core sandwich composites 193
Through-the-thickness displacements measurement in laminated composites using electronic speckle photography 189
Large bending actuator made with SMA contractile wires: theory, numerical simulation and experiments 189
Variable Singularity Power Wedge Element for Multilayered Composites 189
Riduzione della freccia di una trave composita mediante stratificazione, materiale e spessori variabili lungo l'asse 188
APPLICATION OF A NEW TAILORING OPTIMIZATION TECHNIQUE TO LAMINATED AND SANDWICH PLATES AND TO SANDWICH SPHERICAL PANELS 187
Application of a new tailoring optimization technique to laminated and sandwich plates and to spherical panels 187
Higher-order zig-zag model for analysis of thick composite beams with including transverse normal stress and sublaminates approximations 185
Improving energy absorption and dissipation of composites through optimized tailoring 185
Impact analysis of laminated and sandwich composites using a plate finite element with strain energy updating 183
On modeling of laminated composite structures featuring interlaminae imperfections 183
Applications of zig-zag theories to sandwich beams 183
Impact and blast pulse: improving energy absorption of fibre-reinforced composites through optimized tailoring 182
Failure analysis of composite laminates under large deflection 182
Optimisation of sandwich panels with functionally graded core and faces 181
A comparison among several recent criteria for the failure analysis of composites 179
Assessment and optimization of multiple core sandwich composites 176
Free vibration of composite beams featuring interlaminar bonding imperfections and exposed to thermomechanical loading 176
INDENTATION OF SANDWICHES USING A PLATE MODEL WITH VARIABLE KINEMATICS AND FIXED DEGREES OF FREEDOM 173
Numerical assessment of the core deformability effect on the behavior of sandwich beams 171
Sul danneggiamento per delaminazione dei compositi multistrato 168
Using artificial intelligence in structural design. 168
INDENTATION OF SANDWICHES USING A LAYERWISE MODEL WITH FIXED DEGREES OF FREEDOM 167
Dimensionamento e studio degli effetti locali nelle strutture a nido d'ape (Nota Scientifica 211bis DIASP Politecnico di Torino) 165
Minimization of interlaminar stresses in sandwich composites by a new tailoring optimization concept 165
Finite element analysis of composite plates with induced-strain actuators: an evaluation of smeared-laminate and discrete-layer models 165
Multilayered Model with Variable Kinematics and Fixed D.O.F. for Analysis of Bonded Joints 165
Uno studio sull’assorbimento energetico ottimizzato dei compositi multistrato 164
Impact Damage Analysis with Stress Continuity Constraints Fulfilment at Damaged-Undamaged Regions and at Layer Interfaces 162
Effects of interfacial damage on the global and local static response of cross-ply laminates 160
C0 plate element based on strain energy updating and spline interpolation, for analysis of impact damage in laminated composites 157
C0 FIXED DEGREES OF FREEDOM ZIG-ZAG MODEL WITH VARIABLE IN-PLANE AND OUT-OF-PLANE KINEMATICS AND QUADRILATERAL PLATE ELEMENT 156
Analysis and testing of composite stiffened panels with impact induced delamination 156
Multiple core sandwich composites optimization for improving the impact behavior 155
Modeling techniques assessment and optimization of laminated and sandwich composites undergoing impact loads 155
A study of energy absorption in fiber-reinforced composites: transfer form bending to shear 155
An Assessment of Techniques for predicting Delamination: A Comparison among Stress based Criteria, Fracture Mechanics and Interface Models 155
Low velocity impact induced delamination on composite stiffened panels: fem simulation and c-scan detection 153
Divergence and Flutter of Adaptive Laminated Composite Aircraft Wings Featuring Damaged Bonding Interfaces 150
C0 MIXED LAYERWISE QUADRILATERAL PLATE ELEMENT WITH VARIABLE IN AND OUT-OF-PLANE KINEMATICS AND FIXED D.O.F 150
Structures Featuring Imperfect Bonding Interfaces: Modeling and Implications 149
Sulla modellizzazione del comportamento strutturale di elementi in materiale composito 147
Sandwich shell model with continuous transverse shear and normal stresses and thickness deformation. Nota Scientifica 284 DIASP-Politecnico di Torino,Ottobre 2009 147
Modellizzazione dei pannelli sandwich mediante un coside fem commerciale 147
EM SULLA MODELLIZZAZIONE DEL COMPORTAMENTO STRUTTURALE DI ELEMENTI IN MATERIALE COMPOSITO 146
A geometrically nonlinear theory of composite plates with induced-strain actuators 146
Some considerations concerning the edge-stress problem of laminates by finite elements 144
Totale 20.417
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Categoria #
all - tutte 73.903
article - articoli 39.648
book - libri 0
conference - conferenze 23.205
curatela - curatele 0
other - altro 9.826
patent - brevetti 1.224
selected - selezionate 0
volume - volumi 0
Totale 147.806
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/20191.079 0 0 0 0 0 0 0 0 0 0 609 470
2019/20203.116 261 187 164 391 400 347 223 439 398 174 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
2023/2024400 39 34 8 72 74 78 8 37 10 9 31 0
Totale 25.892