PORTO @ Archivio Istituzionale della Ricerca

ZAPPINO, ENRICO
 Distribuzione geografica
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Continente #
NA - Nord America 15.605
EU - Europa 11.847
AS - Asia 5.774
SA - Sud America 683
AF - Africa 58
OC - Oceania 44
Continente sconosciuto - Info sul continente non disponibili 2
Totale 34.013
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Nazione #
US - Stati Uniti d'America 15.421
IT - Italia 3.213
DE - Germania 2.323
CN - Cina 2.274
GB - Regno Unito 1.845
FR - Francia 1.697
SG - Singapore 1.651
UA - Ucraina 597
BR - Brasile 587
KR - Corea 467
TR - Turchia 380
IE - Irlanda 360
NL - Olanda 346
RU - Federazione Russa 285
HK - Hong Kong 216
IN - India 175
AT - Austria 159
CH - Svizzera 148
CA - Canada 140
BE - Belgio 139
FI - Finlandia 137
SE - Svezia 124
JP - Giappone 99
IL - Israele 98
IR - Iran 75
BG - Bulgaria 74
VN - Vietnam 74
ID - Indonesia 69
TW - Taiwan 66
RO - Romania 61
ES - Italia 59
EE - Estonia 46
AU - Australia 42
PT - Portogallo 42
PL - Polonia 35
AR - Argentina 28
MX - Messico 28
JO - Giordania 26
AE - Emirati Arabi Uniti 25
CZ - Repubblica Ceca 23
HR - Croazia 22
UZ - Uzbekistan 21
BD - Bangladesh 18
GR - Grecia 18
IQ - Iraq 15
PE - Perù 14
MY - Malesia 13
CO - Colombia 12
EC - Ecuador 12
ZA - Sudafrica 12
CL - Cile 11
EG - Egitto 11
PK - Pakistan 11
EU - Europa 10
VE - Venezuela 9
MA - Marocco 8
AP - ???statistics.table.value.countryCode.AP??? 7
LU - Lussemburgo 7
SA - Arabia Saudita 7
TN - Tunisia 7
DK - Danimarca 6
HU - Ungheria 6
PY - Paraguay 6
BY - Bielorussia 4
KE - Kenya 4
PH - Filippine 4
RS - Serbia 4
TT - Trinidad e Tobago 4
AZ - Azerbaigian 3
DO - Repubblica Dominicana 3
DZ - Algeria 3
ET - Etiopia 3
LK - Sri Lanka 3
LT - Lituania 3
NO - Norvegia 3
SN - Senegal 3
BH - Bahrain 2
CI - Costa d'Avorio 2
CY - Cipro 2
GE - Georgia 2
HN - Honduras 2
JM - Giamaica 2
KZ - Kazakistan 2
MD - Moldavia 2
NG - Nigeria 2
NP - Nepal 2
NZ - Nuova Zelanda 2
OM - Oman 2
QA - Qatar 2
TH - Thailandia 2
UY - Uruguay 2
A2 - ???statistics.table.value.countryCode.A2??? 1
AL - Albania 1
AO - Angola 1
BB - Barbados 1
BN - Brunei Darussalam 1
BO - Bolivia 1
CR - Costa Rica 1
DJ - Gibuti 1
FK - Isole Falkland (Malvinas) 1
Totale 34.000
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Città #
Council Bluffs 3.404
Ashburn 2.546
Southend 1.468
Turin 1.054
Singapore 843
Fairfield 750
Seattle 737
Chandler 712
Ann Arbor 682
Beijing 632
Torino 527
Princeton 463
Dallas 453
Santa Clara 420
Houston 383
Woodbridge 376
Dublin 342
Berlin 285
Jacksonville 284
Des Moines 260
Wilmington 259
Cambridge 247
San Ramon 238
Boardman 237
Izmir 218
Hefei 209
Seoul 177
San Donato Milanese 168
Hong Kong 147
Shanghai 143
Herkenbosch 139
Bern 138
Milan 135
Aachen 125
Paris 124
Frankfurt 123
Brussels 117
Helsinki 107
Zhengzhou 101
Tel Aviv 88
Istanbul 85
Chicago 81
Buffalo 76
New York 76
Tongling 76
Vienna 74
Rome 70
Austin 68
Jakarta 65
Guangzhou 64
Amsterdam 57
San Francisco 57
Hangzhou 56
São Paulo 56
Shenzhen 53
Nuremberg 52
Dearborn 50
Los Angeles 50
Zaporozhye 49
Baltimore 47
Saint Petersburg 47
Wenzhou 46
Jinan 45
Borgosesia 44
Mountain View 43
Redwood City 43
Galati 42
Pennsylvania Furnace 42
Fremont 41
San Diego 41
Toronto 41
San Antonio 40
Tokyo 39
Frankfurt am Main 38
Bari 33
London 31
Munich 31
Bologna 28
Bristol 28
Cangzhou 28
Montréal 28
Falls Church 27
Norwalk 27
Nürnberg 27
Redmond 27
Washington 27
Chennai 26
Nanjing 26
Overberg 26
Portsmouth 26
Yubileyny 26
Genoa 25
Ho Chi Minh City 25
Lauterbourg 25
Atlanta 24
Monopoli 24
Montreal 24
Andover 23
Lake Forest 23
Lappeenranta 23
Totale 22.403
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Nome #
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 567
Buckling of composite thin walled beams by refined theory 561
Performance of CUF approach to analyze the structural behavior of slender bodies 548
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 471
Finite element models with node-dependent kinematics for the analysis of composite beam structures 444
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 423
Recent developments on refined theories for beams with applications 420
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 403
Analysis of thin-walled structures with longitudinal and transversal stiffeners 382
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 379
Global-local analysis of laminated plates by node-dependent kinematic finite elements with variable ESL/LW capabilities 367
Advanced models for static and dynamic analysis of wing and fuselage structures 364
Refined free vibration analysis of one-dimensional structures with compact and bridge-like cross-sections 355
Free vibration analysis of rotating composite blades via Carrera Unified Formulation 345
Free Vibration Analysis of thin-walled cylinders reinforced with longitudinal and transversal stiffeners 339
Analysis of tapered composite structures using a refined beam theory 330
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 329
Analysis of Rotor Dynamic by One-Dimensional Variable Kinematic Theories 328
Free Vibration analysis of Reinforced Thin-Walled Plates and Shells through Various Finite Element Models 328
Accurate Free Vibration Analysis of Launcher Structures Using Refined 1D Models 328
Free-vibration analysis of space vehicle structures made by composite materials 321
A Component-Wise Approach in Structural Analysis 319
Analysis of piezoelectric actuators under mechanical and electrical loads 318
Numerical analyses of piezoceramic actuators for high temperature applications 316
Aeroelastic analysis of Versatile Thermal Insulation (VTI) panels with pinched boundary conditions 313
Component-wise vibration analysis of stiffened plates accounting for stiffener modes 312
A Variable Kinematic One-Dimensional Model for the Hygro-Mechanical Analysis of Composite Materials 312
Effect of Solid Mass consumption on the free-vibration analysis of launchers 306
Laminated Beam Analysis by Polynomial, rigonometric, Exponential and Zig-Zag Theories 305
One-dimensional finite element formulation with node-dependent kinematics 302
Aeroelastic analysis of pinched panels in a variable supersonic flow changing with altitude. 292
Static analysis of reinforced thin-walled plates and shells by means of finite element models 291
Full Aircraft Dynamic Response by Simplified Structural Models 289
Variable kinematic 1D, 2D and 3D Models for the Analysis of Aerospace Structures 281
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 280
Component-Wise Approach for Efficient and Accurate Analysis of Structures of Launchers 275
Buckling of thin walled beams by refined theory 274
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 273
An adaptable refinement approach for shell finite element models based on node-dependent kinematics 269
Structural Analysis of Launcher Structures by means of Refined Beam Models 264
Static and dynamic experimental analysis of a full composite VLA aircraft 264
Global-local plug-in for high-fidelity composite stress analysis in Femap/NX Nastran 257
Free Vibration Analysis of Rotating Structures By One-Dimensional, Variable Kinematic Theories 256
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 256
Aeroelastic design of Versatile Thermal Insulation (VTI) panels 253
Accurate Analysis of Launcher Structures by Means of Refined One Dimensional Model 250
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 248
Aeroelastic behavior of launcher thermal insulation panel, accounting for various aerodynamic and structural models 247
Application of the Unified Formulation to bending analysis of magnetostrictive unimorph microbeams 242
Aeroelastic Instabilities Analysis of Elastic and Viscoelastic Multi-Layered Panels 241
Refined one-dimensional models for the multi-field analysis of layered smart structures 239
The analysis of tapered structures using a component-wise approach based on refined one-dimensional models 237
A Componet-Wise Approach for the Failure of Complex Aeronautical Structures 237
Reissner's mixed variational theorem for layer-wise refined beam models based on the unified formulation 235
Use of higher-order Legendre polynomials for multilayered plate elements with node-dependent kinematics 234
Virtual design and manufacturing of composite structures using refined kinematic models 230
Static and dynamic testing of a full-composite VLA by using digital image correlation and output only ground vibration testing 229
BUCKLING OF COMPOSITE THIN WALLED BEAMS BY REFINED THEORY 226
Global-local plug-in for high-fidelity composite stress analysis in ABAQUS 226
Thermo-Piezo-Elastic Analysis of Complex Structures Using a Node Dependent Kinematic One-Dimensional Model 224
Aeroelastic Instabilities of FGM Panels under Thermo-Mechanical Loads 224
Analysis of Tapered Structures by means of Refined 1D Models 223
Free vibration analysis of locally damaged aerospace tapered composite structures using component-wise models 218
Analysis of Composite Space Structures Subjected to Loading Factor  215
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 214
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES 214
Node-dependent kinematics, refined zig-zag and multi-line beam theories for the analysis of composite structures 213
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 212
Multidimensional Model for the Stress Analysis of Reinforced Shell Structures 208
Full field strain measurements of composite wing by digital image correlation 208
High-Fidelity One-Dimensional Models for Tapered Structures Analyses 207
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 206
Analysis of Composite Launcher with Non-Structural Masses Subjected to Loading Factor 204
Use of molecular dynamic analysis to build appropriate structural models for CNTs 203
Accurate Evaluation of Interlaminar Stresses in Composite Laminates via Mixed One-Dimensional Formulation 198
Static and Dynamic Analysis of Composite Beams by 1-D Variable Kinematic Theories 193
Process induced deformations and residual stresses in curved composite parts: a parametric analysis 193
OPTIMAL LAY-UPS TO MINIMIZE PROCESS-INDUCED DEFORMATIONS IN L-SHAPED CFRP PARTS 192
Free vibration analysis of thin-walled structures through 1D and 2D refined models 192
Finite elements with node dependent kinematics and scalable accuracy for the analysis of Stokes flows 192
Aeroelastic analysis of versatile thermal insulation panels for launchers applications 191
Analysis of Complex Structures Coupling Variable Kinematics One-Dimensional Models 191
Panel flutter analysis of composite panel with non classical configuration. 188
EFFECT OF FIBER ORIENTATION PATH ON THE BUCKLING, FREE VIBRATION, AND STATIC ANALYSES OF VARIABLE ANGLE TOW PANELS 188
Application of refined beam elements to the coupled-field analysis of magnetostrictive microbeams 186
Effect of Localized Damages on the Free Vibration Analysis of Civil Structures by Component-Wise Approach 184
Panel flutter analysis of curved panels for launcher applicatiions 182
A variable kinematic one-dimensional model for the hygro-mechanical analysis of composite materials 179
Experimental and numerical analysis of 3D printed open-hole plates reinforced with carbon fibers 179
Numerical Analysis of the Impact of Process Parameters on the Residual Stress of a Flat Composite Part 178
Advanced non-linear models for the design of deployable composite space structures 177
A component-wise approach to analyse a composite launcher structure subjected to loading factor 177
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): 177
Comparisons between 1D and 2D formulations for thin-walled structure analysis 175
Tapered composite beams analysis using refined 1-D models 167
Free Vibration Analysis of Beams with Piezo-Patches Using a One-Dimensional Model with Node-Dependent Kinematic 166
Assessment of classical, advanced, and layer-wise theories for the vibration of rotating composite anisotropic blades 166
On the role of structural theories on aeroelastic models 164
Representation, characterization and simulation of tool-part interaction and its effects on process-induced deformations in composites 163
Multiscale thermoelastic analyses of fibre-reinforced composites by high-order unified finite element models 161
Totale 26.422
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Categoria #
all - tutte 98.766
article - articoli 48.514
book - libri 1.076
conference - conferenze 44.664
curatela - curatele 0
other - altro 1.832
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.959
Totale 196.811
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.726 0 0 0 241 59 140 123 214 182 378 241 148
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
2025/20262.693 747 679 1.083 184 0 0 0 0 0 0 0 0
Totale 34.425