ZAPPINO, ENRICO
 Distribuzione geografica
Continente #
NA - Nord America 16.132
EU - Europa 12.089
AS - Asia 7.384
SA - Sud America 832
AF - Africa 84
OC - Oceania 44
Continente sconosciuto - Info sul continente non disponibili 2
Totale 36.567
Nazione #
US - Stati Uniti d'America 15.924
IT - Italia 3.325
SG - Singapore 2.714
CN - Cina 2.524
DE - Germania 2.345
GB - Regno Unito 1.857
FR - Francia 1.715
BR - Brasile 697
UA - Ucraina 600
KR - Corea 475
TR - Turchia 385
IE - Irlanda 362
NL - Olanda 353
RU - Federazione Russa 293
HK - Hong Kong 276
VN - Vietnam 191
IN - India 189
AT - Austria 160
CA - Canada 152
CH - Svizzera 148
BE - Belgio 143
FI - Finlandia 143
SE - Svezia 128
JP - Giappone 125
IR - Iran 101
IL - Israele 98
ID - Indonesia 78
ES - Italia 77
BG - Bulgaria 74
TW - Taiwan 66
RO - Romania 62
PT - Portogallo 52
EE - Estonia 46
PL - Polonia 45
AR - Argentina 43
AU - Australia 42
MX - Messico 39
IQ - Iraq 27
JO - Giordania 27
AE - Emirati Arabi Uniti 26
CZ - Repubblica Ceca 23
HR - Croazia 22
UZ - Uzbekistan 22
ZA - Sudafrica 22
BD - Bangladesh 21
EC - Ecuador 18
GR - Grecia 18
CO - Colombia 17
MY - Malesia 16
PE - Perù 15
CL - Cile 14
VE - Venezuela 14
EG - Egitto 12
MA - Marocco 11
PK - Pakistan 11
EU - Europa 10
KE - Kenya 9
SA - Arabia Saudita 9
TN - Tunisia 9
AP - ???statistics.table.value.countryCode.AP??? 7
LU - Lussemburgo 7
DK - Danimarca 6
HU - Ungheria 6
PH - Filippine 6
PY - Paraguay 6
AZ - Azerbaigian 5
DZ - Algeria 5
ET - Etiopia 5
LT - Lituania 5
RS - Serbia 5
BY - Bielorussia 4
SN - Senegal 4
TT - Trinidad e Tobago 4
UY - Uruguay 4
DO - Repubblica Dominicana 3
GE - Georgia 3
KZ - Kazakistan 3
LK - Sri Lanka 3
NO - Norvegia 3
OM - Oman 3
BH - Bahrain 2
BO - Bolivia 2
CI - Costa d'Avorio 2
CY - Cipro 2
HN - Honduras 2
JM - Giamaica 2
LB - Libano 2
MD - Moldavia 2
NG - Nigeria 2
NP - Nepal 2
NZ - Nuova Zelanda 2
QA - Qatar 2
SK - Slovacchia (Repubblica Slovacca) 2
TH - Thailandia 2
A2 - ???statistics.table.value.countryCode.A2??? 1
AL - Albania 1
AO - Angola 1
BB - Barbados 1
BN - Brunei Darussalam 1
CR - Costa Rica 1
Totale 36.551
Città #
Council Bluffs 3.406
Ashburn 2.699
Southend 1.468
Singapore 1.418
Turin 1.103
Fairfield 750
Seattle 739
Chandler 712
Beijing 702
Ann Arbor 682
Torino 527
Dallas 464
Princeton 463
Santa Clara 435
Houston 386
Woodbridge 376
Dublin 343
Berlin 285
Jacksonville 284
Des Moines 260
Wilmington 259
Cambridge 247
Boardman 238
San Ramon 238
Izmir 219
Hefei 209
Hong Kong 206
Seoul 185
San Donato Milanese 168
Milan 149
Shanghai 145
Herkenbosch 139
Bern 138
Aachen 125
Paris 124
Frankfurt 123
Brussels 117
Buffalo 108
Helsinki 108
Zhengzhou 103
Chicago 92
New York 91
Tel Aviv 88
Istanbul 86
North Bergen 83
Tongling 76
Vienna 74
Rome 73
Los Angeles 72
Ho Chi Minh City 69
Austin 68
Guangzhou 67
São Paulo 66
Jakarta 65
Tokyo 61
Amsterdam 58
Frankfurt am Main 58
Hangzhou 58
San Francisco 57
Shenzhen 53
Nuremberg 52
Dearborn 50
Zaporozhye 49
Wenzhou 48
Baltimore 47
Saint Petersburg 47
Jinan 45
Borgosesia 44
Mountain View 43
Redwood City 43
Toronto 43
Fremont 42
Galati 42
Pennsylvania Furnace 42
San Diego 41
San Antonio 40
San Jose 40
Hanoi 36
Lauterbourg 36
Bari 33
London 33
Redondo Beach 32
Munich 31
Montreal 29
Bologna 28
Bristol 28
Cangzhou 28
Chennai 28
Lappeenranta 28
Montréal 28
Falls Church 27
Norwalk 27
Nürnberg 27
Redmond 27
Washington 27
Atlanta 26
Nanjing 26
Overberg 26
Portsmouth 26
Yubileyny 26
Totale 23.686
Nome #
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 586
Buckling of composite thin walled beams by refined theory 574
Performance of CUF approach to analyze the structural behavior of slender bodies 556
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 514
Finite element models with node-dependent kinematics for the analysis of composite beam structures 456
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 431
Recent developments on refined theories for beams with applications 431
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 415
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 395
Analysis of thin-walled structures with longitudinal and transversal stiffeners 391
Advanced models for static and dynamic analysis of wing and fuselage structures 380
Global-local analysis of laminated plates by node-dependent kinematic finite elements with variable ESL/LW capabilities 380
Refined free vibration analysis of one-dimensional structures with compact and bridge-like cross-sections 365
Free vibration analysis of rotating composite blades via Carrera Unified Formulation 358
Free Vibration Analysis of thin-walled cylinders reinforced with longitudinal and transversal stiffeners 354
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 354
Analysis of tapered composite structures using a refined beam theory 344
Accurate Free Vibration Analysis of Launcher Structures Using Refined 1D Models 338
Analysis of Rotor Dynamic by One-Dimensional Variable Kinematic Theories 337
Free Vibration analysis of Reinforced Thin-Walled Plates and Shells through Various Finite Element Models 337
Free-vibration analysis of space vehicle structures made by composite materials 330
Numerical analyses of piezoceramic actuators for high temperature applications 329
A Variable Kinematic One-Dimensional Model for the Hygro-Mechanical Analysis of Composite Materials 328
A Component-Wise Approach in Structural Analysis 327
Analysis of piezoelectric actuators under mechanical and electrical loads 326
Aeroelastic analysis of Versatile Thermal Insulation (VTI) panels with pinched boundary conditions 322
Component-wise vibration analysis of stiffened plates accounting for stiffener modes 322
Effect of Solid Mass consumption on the free-vibration analysis of launchers 320
Laminated Beam Analysis by Polynomial, rigonometric, Exponential and Zig-Zag Theories 316
One-dimensional finite element formulation with node-dependent kinematics 307
Aeroelastic analysis of pinched panels in a variable supersonic flow changing with altitude. 306
Static analysis of reinforced thin-walled plates and shells by means of finite element models 302
Variable kinematic 1D, 2D and 3D Models for the Analysis of Aerospace Structures 299
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 298
Full Aircraft Dynamic Response by Simplified Structural Models 298
Component-Wise Approach for Efficient and Accurate Analysis of Structures of Launchers 293
Global-local plug-in for high-fidelity composite stress analysis in Femap/NX Nastran 284
Static and dynamic experimental analysis of a full composite VLA aircraft 283
Buckling of thin walled beams by refined theory 282
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 281
An adaptable refinement approach for shell finite element models based on node-dependent kinematics 280
Free Vibration Analysis of Rotating Structures By One-Dimensional, Variable Kinematic Theories 273
Structural Analysis of Launcher Structures by means of Refined Beam Models 272
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 269
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 263
Aeroelastic design of Versatile Thermal Insulation (VTI) panels 258
Accurate Analysis of Launcher Structures by Means of Refined One Dimensional Model 258
Aeroelastic behavior of launcher thermal insulation panel, accounting for various aerodynamic and structural models 255
Aeroelastic Instabilities Analysis of Elastic and Viscoelastic Multi-Layered Panels 253
Global-local plug-in for high-fidelity composite stress analysis in ABAQUS 251
Refined one-dimensional models for the multi-field analysis of layered smart structures 249
Application of the Unified Formulation to bending analysis of magnetostrictive unimorph microbeams 249
A Componet-Wise Approach for the Failure of Complex Aeronautical Structures 248
Virtual design and manufacturing of composite structures using refined kinematic models 248
Use of higher-order Legendre polynomials for multilayered plate elements with node-dependent kinematics 244
The analysis of tapered structures using a component-wise approach based on refined one-dimensional models 243
Static and dynamic testing of a full-composite VLA by using digital image correlation and output only ground vibration testing 243
Thermo-Piezo-Elastic Analysis of Complex Structures Using a Node Dependent Kinematic One-Dimensional Model 241
Reissner's mixed variational theorem for layer-wise refined beam models based on the unified formulation 241
Free vibration analysis of locally damaged aerospace tapered composite structures using component-wise models 236
Analysis of Composite Space Structures Subjected to Loading Factor  234
BUCKLING OF COMPOSITE THIN WALLED BEAMS BY REFINED THEORY 233
Analysis of Tapered Structures by means of Refined 1D Models 231
Aeroelastic Instabilities of FGM Panels under Thermo-Mechanical Loads 231
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES 230
Use of molecular dynamic analysis to build appropriate structural models for CNTs 224
Full field strain measurements of composite wing by digital image correlation 224
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 222
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 220
High-Fidelity One-Dimensional Models for Tapered Structures Analyses 219
Node-dependent kinematics, refined zig-zag and multi-line beam theories for the analysis of composite structures 218
Multidimensional Model for the Stress Analysis of Reinforced Shell Structures 216
Analysis of Composite Launcher with Non-Structural Masses Subjected to Loading Factor 213
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 213
Process induced deformations and residual stresses in curved composite parts: a parametric analysis 207
Accurate Evaluation of Interlaminar Stresses in Composite Laminates via Mixed One-Dimensional Formulation 205
OPTIMAL LAY-UPS TO MINIMIZE PROCESS-INDUCED DEFORMATIONS IN L-SHAPED CFRP PARTS 204
Application of refined beam elements to the coupled-field analysis of magnetostrictive microbeams 204
Numerical Analysis of the Impact of Process Parameters on the Residual Stress of a Flat Composite Part 203
Analysis of Complex Structures Coupling Variable Kinematics One-Dimensional Models 203
Finite elements with node dependent kinematics and scalable accuracy for the analysis of Stokes flows 202
Free vibration analysis of thin-walled structures through 1D and 2D refined models 201
Aeroelastic analysis of versatile thermal insulation panels for launchers applications 199
EFFECT OF FIBER ORIENTATION PATH ON THE BUCKLING, FREE VIBRATION, AND STATIC ANALYSES OF VARIABLE ANGLE TOW PANELS 198
Static and Dynamic Analysis of Composite Beams by 1-D Variable Kinematic Theories 197
Panel flutter analysis of composite panel with non classical configuration. 196
Experimental and numerical analysis of 3D printed open-hole plates reinforced with carbon fibers 194
Effect of Localized Damages on the Free Vibration Analysis of Civil Structures by Component-Wise Approach 193
Advanced non-linear models for the design of deployable composite space structures 189
Panel flutter analysis of curved panels for launcher applicatiions 188
A component-wise approach to analyse a composite launcher structure subjected to loading factor 188
A variable kinematic one-dimensional model for the hygro-mechanical analysis of composite materials 188
Comparisons between 1D and 2D formulations for thin-walled structure analysis 182
DOCUMENTO FINALE ATTIVITA' PANNELLO VTI (LIVELLO-3): VTI real panel Guidelines and Results Summary Report. RESEARCH CONTRACT: THALES ALENIA SPACE ITALIA S.p.A N. 861/2010 (VS. N.571051570090): 182
Free Vibration Analysis of Beams with Piezo-Patches Using a One-Dimensional Model with Node-Dependent Kinematic 181
Tapered composite beams analysis using refined 1-D models 181
Assessment of classical, advanced, and layer-wise theories for the vibration of rotating composite anisotropic blades 179
Representation, characterization and simulation of tool-part interaction and its effects on process-induced deformations in composites 179
On the role of structural theories on aeroelastic models 178
Thermal stress analysis of variable angle tow composite plates through high-order structural models 174
Totale 27.646
Categoria #
all - tutte 105.020
article - articoli 51.321
book - libri 1.165
conference - conferenze 47.803
curatela - curatele 0
other - altro 1.904
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.056
Totale 209.269


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.426 0 0 0 0 0 140 123 214 182 378 241 148
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
2025/20265.260 747 679 1.083 1.248 1.024 479 0 0 0 0 0 0
Totale 36.992