ZAPPINO, ENRICO
 Distribuzione geografica
Continente #
NA - Nord America 18.058
EU - Europa 15.440
AS - Asia 12.197
SA - Sud America 1.020
AF - Africa 173
OC - Oceania 48
Continente sconosciuto - Info sul continente non disponibili 3
Totale 46.939
Nazione #
US - Stati Uniti d'America 17.788
IT - Italia 3.543
SG - Singapore 3.294
VN - Vietnam 2.762
CN - Cina 2.671
NL - Olanda 2.402
DE - Germania 2.388
GB - Regno Unito 1.929
FR - Francia 1.923
RU - Federazione Russa 893
BR - Brasile 824
HK - Hong Kong 723
KR - Corea 696
UA - Ucraina 607
IN - India 439
TR - Turchia 394
IE - Irlanda 374
JP - Giappone 270
FI - Finlandia 197
CA - Canada 176
AT - Austria 169
CH - Svizzera 154
BE - Belgio 147
SE - Svezia 128
ES - Italia 105
PH - Filippine 104
TW - Taiwan 104
IL - Israele 102
BD - Bangladesh 101
IR - Iran 101
IQ - Iraq 94
ID - Indonesia 90
BG - Bulgaria 77
RO - Romania 67
AR - Argentina 65
TH - Thailandia 64
MX - Messico 62
PT - Portogallo 56
PL - Polonia 48
EE - Estonia 47
AU - Australia 46
ZA - Sudafrica 40
JO - Giordania 33
AE - Emirati Arabi Uniti 32
UZ - Uzbekistan 30
CO - Colombia 27
CZ - Repubblica Ceca 26
EC - Ecuador 25
HR - Croazia 24
MY - Malesia 24
PK - Pakistan 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 12
ET - Etiopia 11
EU - Europa 10
PY - Paraguay 10
HU - Ungheria 9
NP - Nepal 9
OM - Oman 9
SN - Senegal 9
AZ - Azerbaigian 8
AO - Angola 7
AP - ???statistics.table.value.countryCode.AP??? 7
DK - Danimarca 7
LT - Lituania 7
LU - Lussemburgo 7
RS - Serbia 7
JM - Giamaica 6
KZ - Kazakistan 6
BY - Bielorussia 5
LB - Libano 5
TT - Trinidad e Tobago 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
HN - Honduras 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
AL - Albania 2
Totale 46.900
Città #
Council Bluffs 3.450
Ashburn 3.026
Amsterdam 2.025
Singapore 1.843
Southend 1.468
Turin 1.167
San Jose 921
Fairfield 750
Seattle 744
Ho Chi Minh City 722
Chandler 713
Beijing 712
Ann Arbor 682
Hanoi 638
Hong Kong 576
Torino 527
Dallas 476
Princeton 463
Santa Clara 462
Houston 392
Woodbridge 376
Dublin 355
Seoul 354
Jacksonville 286
Berlin 285
Des Moines 260
Wilmington 259
Cambridge 247
Boardman 242
San Ramon 238
Izmir 221
Los Angeles 214
Hefei 211
Lauterbourg 201
Milan 178
San Donato Milanese 168
Tokyo 164
Shanghai 149
Helsinki 142
Herkenbosch 139
Bern 138
New York 129
Paris 128
Aachen 125
Frankfurt 123
Brussels 121
Haiphong 121
Buffalo 116
Da Nang 114
Zhengzhou 103
Chicago 95
North Bergen 92
Istanbul 88
Tel Aviv 88
São Paulo 86
Rome 82
Vienna 82
Frankfurt am Main 81
Groningen 78
Tongling 76
Guangzhou 71
Austin 68
Jakarta 67
Hangzhou 65
San Francisco 60
Shenzhen 60
Nuremberg 55
Dearborn 50
Zaporozhye 49
Baltimore 48
Toronto 48
Wenzhou 48
Saint Petersburg 47
Moscow 46
Jinan 45
London 45
Bari 44
Borgosesia 44
Chennai 44
Mountain View 43
Redwood City 43
San Diego 43
Fremont 42
Galati 42
Pennsylvania Furnace 42
San Antonio 41
Montreal 39
Baghdad 38
Lappeenranta 36
Munich 36
Orem 36
Can Tho 35
Hải Dương 35
Columbus 33
Redondo Beach 32
Atlanta 31
Bologna 31
Biên Hòa 30
Basingstoke 29
Nanjing 29
Totale 30.282
Nome #
CUF Multifield Models for Virtual Manufacturing of Composites 1.142
Variable kinematics models for the analysis of thermal stresses in metallic and composite laminates 1.076
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 643
Buckling of composite thin walled beams by refined theory 609
Performance of CUF approach to analyze the structural behavior of slender bodies 597
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 579
Finite element models with node-dependent kinematics for the analysis of composite beam structures 497
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 493
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 486
Recent developments on refined theories for beams with applications 458
Advanced models for static and dynamic analysis of wing and fuselage structures 429
Global-local analysis of laminated plates by node-dependent kinematic finite elements with variable ESL/LW capabilities 415
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 413
Analysis of thin-walled structures with longitudinal and transversal stiffeners 407
Accurate Free Vibration Analysis of Launcher Structures Using Refined 1D Models 399
Free Vibration analysis of Reinforced Thin-Walled Plates and Shells through Various Finite Element Models 386
Free vibration analysis of rotating composite blades via Carrera Unified Formulation 384
A Variable Kinematic One-Dimensional Model for the Hygro-Mechanical Analysis of Composite Materials 383
Analysis of piezoelectric actuators under mechanical and electrical loads 381
Refined free vibration analysis of one-dimensional structures with compact and bridge-like cross-sections 380
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 377
Analysis of tapered composite structures using a refined beam theory 376
Free Vibration Analysis of thin-walled cylinders reinforced with longitudinal and transversal stiffeners 366
Analysis of Rotor Dynamic by One-Dimensional Variable Kinematic Theories 364
Component-wise vibration analysis of stiffened plates accounting for stiffener modes 363
Free-vibration analysis of space vehicle structures made by composite materials 362
A Component-Wise Approach in Structural Analysis 358
Numerical analyses of piezoceramic actuators for high temperature applications 356
Aeroelastic analysis of Versatile Thermal Insulation (VTI) panels with pinched boundary conditions 354
Laminated Beam Analysis by Polynomial, rigonometric, Exponential and Zig-Zag Theories 352
Effect of Solid Mass consumption on the free-vibration analysis of launchers 347
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 347
Global-local plug-in for high-fidelity composite stress analysis in Femap/NX Nastran 346
Variable kinematic 1D, 2D and 3D Models for the Analysis of Aerospace Structures 342
An adaptable refinement approach for shell finite element models based on node-dependent kinematics 338
Static and dynamic experimental analysis of a full composite VLA aircraft 334
Static analysis of reinforced thin-walled plates and shells by means of finite element models 329
Component-Wise Approach for Efficient and Accurate Analysis of Structures of Launchers 328
Aeroelastic analysis of pinched panels in a variable supersonic flow changing with altitude. 327
One-dimensional finite element formulation with node-dependent kinematics 326
Full Aircraft Dynamic Response by Simplified Structural Models 323
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 322
Global-local plug-in for high-fidelity composite stress analysis in ABAQUS 315
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 312
Buckling of thin walled beams by refined theory 305
Virtual design and manufacturing of composite structures using refined kinematic models 302
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 301
Structural Analysis of Launcher Structures by means of Refined Beam Models 297
Free Vibration Analysis of Rotating Structures By One-Dimensional, Variable Kinematic Theories 296
Use of higher-order Legendre polynomials for multilayered plate elements with node-dependent kinematics 296
Static and dynamic testing of a full-composite VLA by using digital image correlation and output only ground vibration testing 293
Analysis of Composite Space Structures Subjected to Loading Factor  292
Application of the Unified Formulation to bending analysis of magnetostrictive unimorph microbeams 290
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES 289
Aeroelastic Instabilities Analysis of Elastic and Viscoelastic Multi-Layered Panels 287
Accurate Analysis of Launcher Structures by Means of Refined One Dimensional Model 285
Aeroelastic behavior of launcher thermal insulation panel, accounting for various aerodynamic and structural models 281
A Componet-Wise Approach for the Failure of Complex Aeronautical Structures 281
Refined one-dimensional models for the multi-field analysis of layered smart structures 278
Numerical Analysis of the Impact of Process Parameters on the Residual Stress of a Flat Composite Part 277
Aeroelastic design of Versatile Thermal Insulation (VTI) panels 277
Thermo-Piezo-Elastic Analysis of Complex Structures Using a Node Dependent Kinematic One-Dimensional Model 277
Free vibration analysis of locally damaged aerospace tapered composite structures using component-wise models 275
Aeroelastic Instabilities of FGM Panels under Thermo-Mechanical Loads 274
Reissner's mixed variational theorem for layer-wise refined beam models based on the unified formulation 273
The analysis of tapered structures using a component-wise approach based on refined one-dimensional models 268
Process induced deformations and residual stresses in curved composite parts: a parametric analysis 268
High-Fidelity One-Dimensional Models for Tapered Structures Analyses 264
OPTIMAL LAY-UPS TO MINIMIZE PROCESS-INDUCED DEFORMATIONS IN L-SHAPED CFRP PARTS 263
Full field strain measurements of composite wing by digital image correlation 262
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 258
BUCKLING OF COMPOSITE THIN WALLED BEAMS BY REFINED THEORY 255
Analysis of Tapered Structures by means of Refined 1D Models 255
Finite elements with node dependent kinematics and scalable accuracy for the analysis of Stokes flows 255
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 250
Advanced non-linear models for the design of deployable composite space structures 248
Analysis of Composite Launcher with Non-Structural Masses Subjected to Loading Factor 248
Use of molecular dynamic analysis to build appropriate structural models for CNTs 248
Experimental and numerical analysis of 3D printed open-hole plates reinforced with carbon fibers 247
EFFECT OF FIBER ORIENTATION PATH ON THE BUCKLING, FREE VIBRATION, AND STATIC ANALYSES OF VARIABLE ANGLE TOW PANELS 246
A variable kinematic one-dimensional model for the hygro-mechanical analysis of composite materials 243
Multidimensional Model for the Stress Analysis of Reinforced Shell Structures 240
Tapered composite beams analysis using refined 1-D models 238
Thermal stress analysis of variable angle tow composite plates through high-order structural models 235
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 235
Node-dependent kinematics, refined zig-zag and multi-line beam theories for the analysis of composite structures 234
Free vibration analysis of thin-walled structures through 1D and 2D refined models 231
Dynamic characterization of 3D printed lightweight structures 231
Multiscale thermoelastic analyses of fibre-reinforced composites by high-order unified finite element models 229
Effect of Localized Damages on the Free Vibration Analysis of Civil Structures by Component-Wise Approach 229
Analysis of Complex Structures Coupling Variable Kinematics One-Dimensional Models 228
A theory-guided probabilistic machine learning framework for accelerated prediction of process-induced deformations in advanced composites 227
Accurate Evaluation of Interlaminar Stresses in Composite Laminates via Mixed One-Dimensional Formulation 227
A second-generation finite element method for the analysis of multifunctional composite structures 226
Post-buckling and nonlinear thermal stress of laminated composite by CUF 225
Computationally efficient multi-field simulation of the curing process of thick composite parts 225
Application of refined beam elements to the coupled-field analysis of magnetostrictive microbeams 225
Finite element models with node-dependent kinematics adopting Legendre polynomial expansions for the analysis of laminated plates 223
On the role of structural theories on aeroelastic models 223
Representation, characterization and simulation of tool-part interaction and its effects on process-induced deformations in composites 223
Totale 33.279
Categoria #
all - tutte 120.395
article - articoli 57.260
book - libri 1.266
conference - conferenze 56.688
curatela - curatele 0
other - altro 2.028
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.290
Totale 239.927


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021389 0 0 0 0 0 0 0 0 0 0 241 148
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
2025/202615.674 747 679 1.083 1.248 1.024 815 2.071 941 5.240 1.666 160 0
Totale 47.406