PORTO @ Archivio Istituzionale della Ricerca

ICARDI, Ugo
 Distribuzione geografica
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Continente #
NA - Nord America 15.850
EU - Europa 12.851
AS - Asia 7.843
SA - Sud America 688
AF - Africa 113
OC - Oceania 14
Continente sconosciuto - Info sul continente non disponibili 4
Totale 37.363
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Nazione #
US - Stati Uniti d'America 15.687
SG - Singapore 2.346
GB - Regno Unito 2.345
IT - Italia 2.236
FR - Francia 2.112
DE - Germania 2.104
VN - Vietnam 1.766
CN - Cina 1.727
UA - Ucraina 1.139
RU - Federazione Russa 949
NL - Olanda 559
BR - Brasile 553
TR - Turchia 399
KR - Corea 368
IE - Irlanda 341
HK - Hong Kong 329
IN - India 277
SE - Svezia 237
FI - Finlandia 201
CH - Svizzera 183
AT - Austria 126
JP - Giappone 116
CA - Canada 94
IQ - Iraq 72
PH - Filippine 58
JO - Giordania 54
BD - Bangladesh 49
ID - Indonesia 47
IR - Iran 47
PT - Portogallo 47
BG - Bulgaria 44
AR - Argentina 43
TH - Thailandia 36
ZA - Sudafrica 36
TW - Taiwan 35
MX - Messico 30
MY - Malesia 29
RO - Romania 28
BE - Belgio 27
AP - ???statistics.table.value.countryCode.AP??? 23
EC - Ecuador 23
EU - Europa 21
PL - Polonia 21
VE - Venezuela 21
CL - Cile 20
ES - Italia 18
PK - Pakistan 18
IL - Israele 16
EG - Egitto 14
AU - Australia 12
BY - Bielorussia 12
CO - Colombia 12
GR - Grecia 12
SA - Arabia Saudita 12
SN - Senegal 11
TT - Trinidad e Tobago 10
KE - Kenya 9
MA - Marocco 9
PY - Paraguay 9
UZ - Uzbekistan 9
AE - Emirati Arabi Uniti 8
DZ - Algeria 8
HN - Honduras 8
KZ - Kazakistan 8
TN - Tunisia 7
AZ - Azerbaigian 6
AL - Albania 5
JM - Giamaica 5
KG - Kirghizistan 5
LB - Libano 5
OM - Oman 5
PE - Perù 5
QA - Qatar 5
CR - Costa Rica 4
DO - Repubblica Dominicana 4
ET - Etiopia 4
HR - Croazia 4
NG - Nigeria 4
NP - Nepal 4
RS - Serbia 4
CZ - Repubblica Ceca 3
DK - Danimarca 3
EE - Estonia 3
LT - Lituania 3
LV - Lettonia 3
NO - Norvegia 3
PS - Palestinian Territory 3
SY - Repubblica araba siriana 3
AM - Armenia 2
BH - Bahrain 2
CI - Costa d'Avorio 2
GE - Georgia 2
HU - Ungheria 2
KW - Kuwait 2
LA - Repubblica Popolare Democratica del Laos 2
LY - Libia 2
MN - Mongolia 2
MT - Malta 2
NZ - Nuova Zelanda 2
SI - Slovenia 2
Totale 37.344
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Città #
Ashburn 3.925
Southend 2.072
Seattle 1.706
Singapore 1.221
Fairfield 867
San Jose 779
Jacksonville 551
Chandler 549
Princeton 494
Houston 480
Ho Chi Minh City 460
Hanoi 448
San Ramon 437
Woodbridge 418
Beijing 387
Turin 384
Ann Arbor 348
Dublin 333
Cambridge 330
Amsterdam 324
Chicago 319
Wilmington 306
Berlin 295
Santa Clara 284
Izmir 271
Hong Kong 259
Boardman 217
Helsinki 182
Los Angeles 178
Bern 175
Dallas 166
Des Moines 166
San Donato Milanese 160
Torino 152
Bologna 148
Shanghai 145
Lauterbourg 144
Baltimore 139
Zhengzhou 135
Buffalo 131
Zaporozhye 130
Pennsylvania Furnace 128
Overberg 121
North Bergen 100
Saint Petersburg 93
Seoul 87
Council Bluffs 82
Milan 82
Da Nang 80
Hangzhou 80
New York 75
San Francisco 73
Monopoli 69
Moscow 68
Padua 68
Haiphong 66
Tokyo 65
Vienna 63
Mountain View 55
Bremen 53
Columbus 53
Fremont 47
San Diego 46
The Dalles 46
São Paulo 45
Atlanta 41
Guangzhou 41
Istanbul 41
Lisbon 40
Dearborn 39
Tongling 39
Hefei 38
Malatya 38
Redwood City 38
Orem 37
Baghdad 36
Piscataway 32
Toronto 32
Rome 30
Frankfurt 28
Kiev 27
Munich 27
Washington 26
London 25
Naples 24
Shenzhen 24
Las Vegas 23
Norwalk 23
Andover 22
Brussels 22
Frankfurt am Main 22
Jakarta 22
Nuremberg 22
Thái Nguyên 22
Melun 21
Paris 21
Yubileyny 21
Hải Dương 20
Chennai 19
Jinan 19
Totale 23.362
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Nome #
Aeronave radiocomandata di grandissime dimensioni 631
Multilayered shell model with variable representation of displacements across the thickness 433
Variable kinematics layerwise model for analysis of bonded joints 419
Layerwise mixed element with sublaminates approximation and 3D zig-zag field, for analysis of local effects in laminated and sandwich composites 391
Impact analysis of sandwich composites based on a refined plate element with strain energy updating 386
Extension of the strain energy updating technique to a multilayered shell model with adaptive displacements and fixed DOF 386
RESPONSE OF SANDWICHES UNDERGOING STATIC AND BLAST PULSE LOADING WITH TAILORING OPTIMIZATION AND STITCHING 384
Thermo-mechanical delamination analysis by a plate model with “adaptive” representation of displacements and temperature 381
C0 Layerwise Model with Fixed Degrees of Freedom and Variable In- and Out-of-Plane Kinematics by Strain Energy Updating Technique 377
Assessment of recent theories for predicting failure of composite laminates 372
Numerical assessment of the core deformability effect on the behavior of sandwich beams 363
Indentation of Sandwiches Using a Refined Zig-Zag Model and a Mesoscale Damage Model 360
Holographic interferometry assessment of stress distribution in sandwich beams in bending 353
The nonlinear response of unsymmetric multilayered plates using smeared laminate and layerwise models 343
Simple, efficient mixed solid element for accurate analysis of local effects in laminated and sandwich composites 335
Optimization of multi-core sandwich composites undergoing impact loads 331
C0 plate element for delamination damage analysis, based on a zig-zag model and strain energy updating 328
Layerwise zig-zag model with selective refinement across the thickness 327
Preliminary study of an adaptive wing with shape memory alloy torsion actuators 326
Analysis of Laminated and Sandwich Composites by a Zig-zag Plate Element with Variable Kinematics and Fixed Degrees of Freedom 325
Large deflection of adaptive multilayered Timoshenko beams 323
Assessment of recent zig-zag theories for laminated and sandwich structures 323
Failure analysis of composite laminates under large deflection 319
Analysis of thick multilayered anisotropic plates by a higher order plate element 319
Cylindrical bending of laminated cylindrical shells using a modified zig-zag theory 317
RECOVERING CRITICAL STRESSES IN SANDWICHES USING THROUGH-THETHICKNESS REINFORCEMENT 317
SMA actuated mechanism for an adaptive wing 316
Velivolo cargo di grandissime dimensioni: sviluppo del progetto e sperimentazione didattica 315
An evaluation of the influence of geometry and material properties at free edges and at corners of composite laminates 309
On modeling of global and local response of sandwich plates with laminated faces 307
Eight-noded zig-zag element for deflection and stress analysis of plates with general lay-up 304
Dynamic response of adaptive cross-ply cantilevers featuring interlaminar bonding imperfections 300
Multilayered Plate Model with "Adaptive" Representation of Displacements and TemperatureAcross the Thickness and Fixed D.O.F. 299
Aeromobile a sostentazione aerostatica ad alta manovrabilità 297
Discrete-layer models for multilayered shells accounting for interlayer continuity 297
Smart structures featuring imperfect bonding interfaces: Modeling and implications 295
INDENTATION OF SANDWICHES USING A PLATE MODEL WITH VARIABLE KINEMATICS AND FIXED DEGREES OF FREEDOM 295
Layerwise zig-zag model with selective refinement across the thickness 294
On modeling of global response behavior of sandwich plates with laminated faces 291
DEVELOPMENT OF AN EFFICIENT ZIG-ZAG MODEL WITH VARIABLE REPRESENTATION OF DISPLACEMENTS ACROSS THE THICKNESS 287
A Three-Dimensional Zig-Zag Theory for Analysis of Thick Laminated Beams 285
Effects of interfacial damage on the global and local static response of cross-ply laminates 285
Velivolo cargo di grandissime dimensioni: sviluppo del progetto e sperimentazione didattica 284
Application of a new tailoring optimization technique to laminated and sandwich plates and to spherical panels 283
On modeling of laminated composite structures featuring interlaminae imperfections 281
Optimization of Variable Stiffness Laminates and Sandwiches Undergoing Impulsive Dynamic Loading 280
Large-deflection and stress analysis of multilayered plates with induced-strain actuators 279
Impact analysis of laminated and sandwich composites using a plate finite element with strain energy updating 277
Analysis Of Bonded Joints With Laminated Adherends By A Variable Kinematics Layerwise Model 277
Impact analysis of sandwich composites 277
Laminated shell model with second-order expansion of the reciprocals of Lamé coefficients Hα, Hβ and interlayer continuities fulfilment 276
Improving energy absorption and dissipation of composites through optimized tailoring 276
Large bending actuator made with SMA contractile wires: theory, numerical simulation and experiments 275
Postbuckling of laminated composite and sandwich plates and shells: on the significance of the fulfillment of static interlayer continuity conditions 274
Laminated and sandwich panels subject to blast pulse loading 273
Free edge stress propagation in composite laminates 272
Co plate element for global/local analysis of multilayered composites, based on a 3D zig-zag model and strain energy updating 270
Riduzione della freccia di una trave composita mediante stratificazione, materiale e spessori variabili lungo l'asse 269
A new tailoring optimization approach for improving structural response and energy absorption capability of laminated and sandwich composites 268
Variable Singularity Power Wedge Element for Multilayered Composites 264
A comparison among several recent criteria for the failure analysis of composites 261
Optimization of sandwich panels to blast pulse loading 260
Multilayered Model with Variable Kinematics and Fixed D.O.F. for Analysis of Bonded Joints 260
INDENTATION OF SANDWICHES USING A LAYERWISE MODEL WITH FIXED DEGREES OF FREEDOM 258
Impact Damage Analysis with Stress Continuity Constraints Fulfilment at Damaged-Undamaged Regions and at Layer Interfaces 258
Through-the-thickness displacements measurement in laminated composites using electronic speckle photography 257
Failure analysis of composite laminates under large deflection 257
Modeling assessment and optimization of impacted multi-core sandwich composites 256
C0 MIXED LAYERWISE QUADRILATERAL PLATE ELEMENT WITH VARIABLE IN AND OUT-OF-PLANE KINEMATICS AND FIXED D.O.F 256
Extension of a new tailoring optimisation technique to sandwich shells with laminated faces 255
Higher-order zig-zag model for analysis of thick composite beams with including transverse normal stress and sublaminates approximations 255
Dimensionamento e studio degli effetti locali nelle strutture a nido d'ape (Nota Scientifica 211bis DIASP Politecnico di Torino) 253
APPLICATION OF A NEW TAILORING OPTIMIZATION TECHNIQUE TO LAMINATED AND SANDWICH PLATES AND TO SANDWICH SPHERICAL PANELS 252
Finite element analysis of composite plates with induced-strain actuators: an evaluation of smeared-laminate and discrete-layer models 252
Assessment and optimization of multiple core sandwich composites 251
Numerical assessment of the core deformability effect on the behavior of sandwich beams 251
Applications of zig-zag theories to sandwich beams 251
Optimisation of sandwich panels with functionally graded core and faces 247
Minimization of interlaminar stresses in sandwich composites by a new tailoring optimization concept 246
An Assessment of Techniques for predicting Delamination: A Comparison among Stress based Criteria, Fracture Mechanics and Interface Models 239
Using artificial intelligence in structural design. 236
Zig-zag theories differently accounting for layerwise effects of multilayered composites 235
C0 FIXED DEGREES OF FREEDOM ZIG-ZAG MODEL WITH VARIABLE IN-PLANE AND OUT-OF-PLANE KINEMATICS AND QUADRILATERAL PLATE ELEMENT 234
Modeling techniques assessment and optimization of laminated and sandwich composites undergoing impact loads 233
Impact and blast pulse: improving energy absorption of fibre-reinforced composites through optimized tailoring 233
On the buckling analysis of imperfect laminated stiffened conical shells 231
EM SULLA MODELLIZZAZIONE DEL COMPORTAMENTO STRUTTURALE DI ELEMENTI IN MATERIALE COMPOSITO 230
Sulla modellizzazione del comportamento strutturale di elementi in materiale composito 229
Uno studio sull’assorbimento energetico ottimizzato dei compositi multistrato 228
Free vibration of composite beams featuring interlaminar bonding imperfections and exposed to thermomechanical loading 227
Sul danneggiamento per delaminazione dei compositi multistrato 226
A geometrically nonlinear theory of composite plates with induced-strain actuators 225
Divergence and Flutter of Adaptive Laminated Composite Aircraft Wings Featuring Damaged Bonding Interfaces 223
Numerical studies on bending, free vibration and buckling of multilayered anysotropic plates 223
Analysis and testing of composite stiffened panels with impact induced delamination 223
Structures Featuring Imperfect Bonding Interfaces: Modeling and Implications 222
C0 plate element based on strain energy updating and spline interpolation, for analysis of impact damage in laminated composites 219
Effects of the interlayer continuities fulfilment and Lame' coefficients expansion in laminated cylindrical shells 219
A study of energy absorption in fiber-reinforced composites: transfer form bending to shear 218
Low velocity impact induced delamination on composite stiffened panels: fem simulation and c-scan detection 217
Totale 28.806
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Categoria #
all - tutte 106.620
article - articoli 57.668
book - libri 0
conference - conferenze 33.209
curatela - curatele 0
other - altro 13.809
patent - brevetti 1.934
selected - selezionate 0
volume - volumi 0
Totale 213.240
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021214 0 0 0 0 0 0 0 0 0 0 162 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
2025/20268.090 387 347 596 630 646 546 1.411 587 1.735 1.092 113 0
Totale 37.448