PORTO @ Archivio Istituzionale della Ricerca

ZAPPINO, ENRICO
 Distribuzione geografica
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Continente #
NA - Nord America 18.621
EU - Europa 15.699
AS - Asia 12.407
SA - Sud America 1.021
AF - Africa 174
OC - Oceania 49
Continente sconosciuto - Info sul continente non disponibili 3
Totale 47.974
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Nazione #
US - Stati Uniti d'America 18.312
IT - Italia 3.771
SG - Singapore 3.331
VN - Vietnam 2.762
CN - Cina 2.689
NL - Olanda 2.407
DE - Germania 2.388
FR - Francia 1.931
GB - Regno Unito 1.930
RU - Federazione Russa 893
BR - Brasile 825
HK - Hong Kong 723
KR - Corea 696
UA - Ucraina 607
IN - India 442
TR - Turchia 395
IE - Irlanda 374
JP - Giappone 274
BD - Bangladesh 227
FI - Finlandia 205
CA - Canada 202
AT - Austria 169
CH - Svizzera 160
BE - Belgio 147
SE - Svezia 128
TW - Taiwan 124
ES - Italia 106
PH - Filippine 104
IL - Israele 102
IR - Iran 101
IQ - Iraq 94
ID - Indonesia 90
BG - Bulgaria 77
RO - Romania 67
AR - Argentina 65
TH - Thailandia 64
MX - Messico 63
PT - Portogallo 56
PL - Polonia 49
AU - Australia 47
EE - Estonia 47
ZA - Sudafrica 40
JO - Giordania 33
AE - Emirati Arabi Uniti 32
UZ - Uzbekistan 30
CO - Colombia 27
CZ - Repubblica Ceca 26
EC - Ecuador 25
PK - Pakistan 25
HR - Croazia 24
MY - Malesia 24
EG - Egitto 21
MA - Marocco 21
VE - Venezuela 20
KE - Kenya 19
PE - Perù 19
CL - Cile 18
GR - Grecia 18
SA - Arabia Saudita 15
TN - Tunisia 15
DZ - Algeria 13
ET - Etiopia 11
EU - Europa 10
PY - Paraguay 10
HU - Ungheria 9
JM - Giamaica 9
NP - Nepal 9
OM - Oman 9
SN - Senegal 9
AZ - Azerbaigian 8
LT - Lituania 8
AO - Angola 7
AP - ???statistics.table.value.countryCode.AP??? 7
DK - Danimarca 7
LU - Lussemburgo 7
RS - Serbia 7
TT - Trinidad e Tobago 7
HN - Honduras 6
KZ - Kazakistan 6
BY - Bielorussia 5
LB - Libano 5
UY - Uruguay 5
BH - Bahrain 4
BO - Bolivia 4
CI - Costa d'Avorio 4
DO - Repubblica Dominicana 4
GE - Georgia 4
NI - Nicaragua 4
PS - Palestinian Territory 4
SK - Slovacchia (Repubblica Slovacca) 4
CR - Costa Rica 3
KH - Cambogia 3
LK - Sri Lanka 3
LV - Lettonia 3
MD - Moldavia 3
MT - Malta 3
NG - Nigeria 3
NO - Norvegia 3
QA - Qatar 3
SY - Repubblica araba siriana 3
Totale 47.932
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Città #
Council Bluffs 3.502
Ashburn 3.070
Amsterdam 2.025
Singapore 1.847
Southend 1.468
Turin 1.209
San Jose 1.082
Fairfield 750
Seattle 745
Ho Chi Minh City 722
Chandler 713
Beijing 712
Ann Arbor 682
Hanoi 638
Hong Kong 576
Torino 527
Dallas 481
Santa Clara 473
Princeton 463
Houston 396
Woodbridge 376
Dublin 355
Seoul 354
Jacksonville 287
Berlin 285
Des Moines 260
Wilmington 259
Cambridge 247
Boardman 246
Los Angeles 241
San Ramon 238
Milan 223
Izmir 221
Hefei 211
Lauterbourg 201
San Donato Milanese 168
Tokyo 168
Shanghai 150
New York 146
Helsinki 142
Herkenbosch 139
Bern 138
Buffalo 131
Paris 130
Aachen 125
Frankfurt 123
Brussels 121
Haiphong 121
Da Nang 114
Rome 104
Zhengzhou 103
Chicago 97
North Bergen 92
Istanbul 89
Tel Aviv 88
São Paulo 86
Vienna 82
Frankfurt am Main 81
Groningen 78
Tongling 76
Hangzhou 73
Guangzhou 71
Austin 69
Jakarta 67
San Francisco 62
Shenzhen 61
Toronto 58
Nuremberg 55
Dearborn 50
Baltimore 49
Bari 49
Zaporozhye 49
Wenzhou 48
Saint Petersburg 47
Moscow 46
Jinan 45
London 45
Montreal 45
Borgosesia 44
Chennai 44
San Diego 44
Mountain View 43
Redwood City 43
Fremont 42
Galati 42
Pennsylvania Furnace 42
San Antonio 41
Baghdad 38
Bologna 38
Lappeenranta 36
Munich 36
Orem 36
Can Tho 35
Columbus 35
Hải Dương 35
Atlanta 32
Redondo Beach 32
Biên Hòa 30
Basingstoke 29
Genoa 29
Totale 30.792
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Nome #
CUF Multifield Models for Virtual Manufacturing of Composites 1.147
Variable kinematics models for the analysis of thermal stresses in metallic and composite laminates 1.087
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 663
Buckling of composite thin walled beams by refined theory 615
Performance of CUF approach to analyze the structural behavior of slender bodies 599
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 587
Finite element models with node-dependent kinematics for the analysis of composite beam structures 501
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 496
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 488
Recent developments on refined theories for beams with applications 461
Advanced models for static and dynamic analysis of wing and fuselage structures 433
Global-local analysis of laminated plates by node-dependent kinematic finite elements with variable ESL/LW capabilities 418
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 416
Analysis of thin-walled structures with longitudinal and transversal stiffeners 409
Accurate Free Vibration Analysis of Launcher Structures Using Refined 1D Models 401
Free Vibration analysis of Reinforced Thin-Walled Plates and Shells through Various Finite Element Models 389
Free vibration analysis of rotating composite blades via Carrera Unified Formulation 388
A Variable Kinematic One-Dimensional Model for the Hygro-Mechanical Analysis of Composite Materials 386
Refined free vibration analysis of one-dimensional structures with compact and bridge-like cross-sections 382
Analysis of piezoelectric actuators under mechanical and electrical loads 382
Analysis of tapered composite structures using a refined beam theory 382
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 380
Analysis of Rotor Dynamic by One-Dimensional Variable Kinematic Theories 367
Free-vibration analysis of space vehicle structures made by composite materials 367
Free Vibration Analysis of thin-walled cylinders reinforced with longitudinal and transversal stiffeners 367
Component-wise vibration analysis of stiffened plates accounting for stiffener modes 364
A Component-Wise Approach in Structural Analysis 360
Numerical analyses of piezoceramic actuators for high temperature applications 358
Laminated Beam Analysis by Polynomial, rigonometric, Exponential and Zig-Zag Theories 357
Aeroelastic analysis of Versatile Thermal Insulation (VTI) panels with pinched boundary conditions 356
Variable kinematic 1D, 2D and 3D Models for the Analysis of Aerospace Structures 354
Effect of Solid Mass consumption on the free-vibration analysis of launchers 349
Global-local plug-in for high-fidelity composite stress analysis in Femap/NX Nastran 349
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 348
An adaptable refinement approach for shell finite element models based on node-dependent kinematics 340
Static and dynamic experimental analysis of a full composite VLA aircraft 335
Component-Wise Approach for Efficient and Accurate Analysis of Structures of Launchers 333
Aeroelastic analysis of pinched panels in a variable supersonic flow changing with altitude. 330
Static analysis of reinforced thin-walled plates and shells by means of finite element models 330
One-dimensional finite element formulation with node-dependent kinematics 328
Full Aircraft Dynamic Response by Simplified Structural Models 324
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 323
Analysis of Composite Space Structures Subjected to Loading Factor  322
Global-local plug-in for high-fidelity composite stress analysis in ABAQUS 317
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 314
Virtual design and manufacturing of composite structures using refined kinematic models 311
Buckling of thin walled beams by refined theory 307
Numerical Analysis of the Impact of Process Parameters on the Residual Stress of a Flat Composite Part 303
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 303
Free Vibration Analysis of Rotating Structures By One-Dimensional, Variable Kinematic Theories 299
Use of higher-order Legendre polynomials for multilayered plate elements with node-dependent kinematics 299
Structural Analysis of Launcher Structures by means of Refined Beam Models 298
Static and dynamic testing of a full-composite VLA by using digital image correlation and output only ground vibration testing 295
Application of the Unified Formulation to bending analysis of magnetostrictive unimorph microbeams 292
Aeroelastic Instabilities Analysis of Elastic and Viscoelastic Multi-Layered Panels 290
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES 290
Accurate Analysis of Launcher Structures by Means of Refined One Dimensional Model 289
Aeroelastic behavior of launcher thermal insulation panel, accounting for various aerodynamic and structural models 284
A Componet-Wise Approach for the Failure of Complex Aeronautical Structures 284
Thermo-Piezo-Elastic Analysis of Complex Structures Using a Node Dependent Kinematic One-Dimensional Model 279
Refined one-dimensional models for the multi-field analysis of layered smart structures 279
Aeroelastic design of Versatile Thermal Insulation (VTI) panels 278
Free vibration analysis of locally damaged aerospace tapered composite structures using component-wise models 277
Aeroelastic Instabilities of FGM Panels under Thermo-Mechanical Loads 275
Reissner's mixed variational theorem for layer-wise refined beam models based on the unified formulation 274
High-Fidelity One-Dimensional Models for Tapered Structures Analyses 271
Process induced deformations and residual stresses in curved composite parts: a parametric analysis 270
The analysis of tapered structures using a component-wise approach based on refined one-dimensional models 269
OPTIMAL LAY-UPS TO MINIMIZE PROCESS-INDUCED DEFORMATIONS IN L-SHAPED CFRP PARTS 267
Advanced non-linear models for the design of deployable composite space structures 265
Full field strain measurements of composite wing by digital image correlation 263
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 261
BUCKLING OF COMPOSITE THIN WALLED BEAMS BY REFINED THEORY 257
Analysis of Tapered Structures by means of Refined 1D Models 257
Experimental and numerical analysis of 3D printed open-hole plates reinforced with carbon fibers 257
Finite elements with node dependent kinematics and scalable accuracy for the analysis of Stokes flows 256
Analysis of Composite Launcher with Non-Structural Masses Subjected to Loading Factor 253
DOCUMENTO FINALE ATTIVITA' PANNELLO VTI (LIVELLO-1): Literature overview of panel flutter phenomena for the simply-supported (SS) cylindrical panels and analysis of the critical conditions of VTI-panels in case of SS-BCs.RESEARCH CONTRACT: THALES ALENIA SPACE ITALIA S.p.A N. 861/2010 (VS. N.571051570090): ”VERSATILE THERMAL INSULATION (VTI) FLUTTER ANALYSIS” RESP. PROF. E. CARRERA 251
Use of molecular dynamic analysis to build appropriate structural models for CNTs 249
EFFECT OF FIBER ORIENTATION PATH ON THE BUCKLING, FREE VIBRATION, AND STATIC ANALYSES OF VARIABLE ANGLE TOW PANELS 249
Computationally efficient multi-field simulation of the curing process of thick composite parts 248
A second-generation finite element method for the analysis of multifunctional composite structures 246
Tapered composite beams analysis using refined 1-D models 246
Thermal stress analysis of variable angle tow composite plates through high-order structural models 245
A variable kinematic one-dimensional model for the hygro-mechanical analysis of composite materials 244
Multidimensional Model for the Stress Analysis of Reinforced Shell Structures 241
Node-dependent kinematics, refined zig-zag and multi-line beam theories for the analysis of composite structures 238
DOCUMENTO FINALE ATTIVITA' PANNELLO VTI (LIVELLO-2): Development of a FE model suitable for Piston Theory (Supersonic Flow) analysis of VTI-panels with real BCs, 4/6 points pinched case. Calculation of critical Mach number. RESEARCH CONTRACT: THALES ALENIA SPACE ITALIA S.p.A N. 861/2010 (VS. N.571051570090): ”VERSATILE THERMAL INSULATION (VTI) FLUTTER ANALYSIS” RESP. PROF. E. CARRERA 236
Dynamic characterization of 3D printed lightweight structures 235
Free vibration analysis of thin-walled structures through 1D and 2D refined models 234
Multiscale thermoelastic analyses of fibre-reinforced composites by high-order unified finite element models 233
Post-buckling and nonlinear thermal stress of laminated composite by CUF 233
A theory-guided probabilistic machine learning framework for accelerated prediction of process-induced deformations in advanced composites 232
Analysis of Complex Structures Coupling Variable Kinematics One-Dimensional Models 230
Effect of Localized Damages on the Free Vibration Analysis of Civil Structures by Component-Wise Approach 230
Finite element models with node-dependent kinematics adopting Legendre polynomial expansions for the analysis of laminated plates 229
Accurate Evaluation of Interlaminar Stresses in Composite Laminates via Mixed One-Dimensional Formulation 229
Representation, characterization and simulation of tool-part interaction and its effects on process-induced deformations in composites 228
Vibro-acoustic analysis of composite plate-cavity systems via CUF finite elements 226
Application of refined beam elements to the coupled-field analysis of magnetostrictive microbeams 226
Totale 33.712
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Categoria #
all - tutte 124.905
article - articoli 59.058
book - libri 1.296
conference - conferenze 59.226
curatela - curatele 0
other - altro 2.082
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.342
Totale 248.909
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021148 0 0 0 0 0 0 0 0 0 0 0 148
2021/20222.071 99 139 121 83 145 145 96 83 91 205 276 588
2022/20236.552 266 447 71 221 255 354 417 171 241 114 318 3.677
2023/20241.253 65 90 112 127 133 128 53 111 39 55 170 170
2024/20255.377 135 518 204 565 535 434 389 500 756 267 423 651
2025/202616.709 747 679 1.083 1.248 1.024 815 2.071 941 5.240 1.666 581 614
Totale 48.441