PORTO @ Archivio Istituzionale della Ricerca

ZAPPINO, ENRICO
 Distribuzione geografica
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Continente #
NA - Nord America 13.834
EU - Europa 10.421
AS - Asia 2.512
SA - Sud America 51
OC - Oceania 38
AF - Africa 23
Continente sconosciuto - Info sul continente non disponibili 2
Totale 26.881
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Nazione #
US - Stati Uniti d'America 13.708
IT - Italia 2.700
DE - Germania 2.195
GB - Regno Unito 1.779
FR - Francia 1.465
CN - Cina 1.215
UA - Ucraina 582
SG - Singapore 371
IE - Irlanda 351
NL - Olanda 308
TR - Turchia 282
KR - Corea 213
CH - Svizzera 148
RU - Federazione Russa 134
CA - Canada 119
SE - Svezia 119
FI - Finlandia 117
IN - India 106
BE - Belgio 104
BG - Bulgaria 73
HK - Hong Kong 64
RO - Romania 60
AT - Austria 59
JP - Giappone 58
IR - Iran 57
TW - Taiwan 53
AU - Australia 36
PT - Portogallo 34
IL - Israele 24
JO - Giordania 23
ES - Italia 22
BR - Brasile 21
CZ - Repubblica Ceca 21
VN - Vietnam 21
HR - Croazia 20
PL - Polonia 19
GR - Grecia 18
AE - Emirati Arabi Uniti 15
UZ - Uzbekistan 14
MY - Malesia 12
PE - Perù 11
CL - Cile 10
EU - Europa 10
EE - Estonia 8
AP - ???statistics.table.value.countryCode.AP??? 7
LU - Lussemburgo 7
MX - Messico 7
AR - Argentina 6
EG - Egitto 6
SA - Arabia Saudita 6
DK - Danimarca 5
HU - Ungheria 5
ZA - Sudafrica 5
BY - Bielorussia 4
IQ - Iraq 4
NO - Norvegia 3
SN - Senegal 3
CI - Costa d'Avorio 2
CY - Cipro 2
ET - Etiopia 2
GE - Georgia 2
LK - Sri Lanka 2
MD - Moldavia 2
NG - Nigeria 2
NZ - Nuova Zelanda 2
PK - Pakistan 2
A2 - ???statistics.table.value.countryCode.A2??? 1
BD - Bangladesh 1
CO - Colombia 1
DZ - Algeria 1
EC - Ecuador 1
FK - Isole Falkland (Malvinas) 1
ID - Indonesia 1
IM - Isola di Man 1
LT - Lituania 1
PH - Filippine 1
RS - Serbia 1
SC - Seychelles 1
SI - Slovenia 1
SK - Slovacchia (Repubblica Slovacca) 1
TH - Thailandia 1
TN - Tunisia 1
Totale 26.881
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Città #
Council Bluffs 3.345
Ashburn 2.257
Southend 1.468
Turin 798
Fairfield 750
Seattle 731
Chandler 712
Ann Arbor 681
Torino 527
Princeton 463
Beijing 448
Houston 382
Woodbridge 376
Dublin 333
Berlin 285
Jacksonville 282
Singapore 264
Des Moines 260
Wilmington 258
Cambridge 247
San Ramon 238
Boardman 233
Izmir 218
San Donato Milanese 168
Herkenbosch 139
Bern 138
Aachen 125
Frankfurt 123
Shanghai 120
Helsinki 104
Brussels 95
Milan 94
Zhengzhou 89
Chicago 70
New York 65
Seoul 60
Amsterdam 50
Dearborn 50
Hangzhou 50
San Francisco 50
Shenzhen 50
Vienna 49
Zaporozhye 49
Baltimore 47
Guangzhou 47
Saint Petersburg 47
Santa Clara 46
Wenzhou 46
Rome 45
Buffalo 43
Mountain View 43
Redwood City 43
Galati 42
Pennsylvania Furnace 42
Fremont 41
Jinan 41
San Diego 41
San Antonio 38
Toronto 36
Bristol 28
Montréal 28
Borgosesia 27
Falls Church 27
Norwalk 27
Nürnberg 27
Bari 26
Overberg 26
Washington 25
Monopoli 24
Nanjing 24
Redmond 24
Andover 23
Lake Forest 23
London 23
Bologna 22
Genoa 22
Malatya 22
Montreal 20
Taipei 19
Zagreb 18
Miami 17
Tel Aviv 17
Kayseri 16
Melbourne 16
Sofia 16
Studio City 16
Atlanta 15
Lansing 15
Palermo 15
Prague 15
Tokyo 15
Dong Ket 13
Kharagpur 13
Lappeenranta 13
Mcallen 13
Osaka 13
San Jose 13
San Mateo 13
Melun 12
Phoenix 12
Totale 18.775
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Nome #
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 529
Buckling of composite thin walled beams by refined theory 521
Performance of CUF approach to analyze the structural behavior of slender bodies 504
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 407
Finite element models with node-dependent kinematics for the analysis of composite beam structures 397
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 395
Recent developments on refined theories for beams with applications 390
Analysis of thin-walled structures with longitudinal and transversal stiffeners 363
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 352
Refined free vibration analysis of one-dimensional structures with compact and bridge-like cross-sections 332
Global-local analysis of laminated plates by node-dependent kinematic finite elements with variable ESL/LW capabilities 331
Advanced models for static and dynamic analysis of wing and fuselage structures 330
Free vibration analysis of rotating composite blades via Carrera Unified Formulation 319
Free Vibration Analysis of thin-walled cylinders reinforced with longitudinal and transversal stiffeners 316
Analysis of Rotor Dynamic by One-Dimensional Variable Kinematic Theories 310
Free Vibration analysis of Reinforced Thin-Walled Plates and Shells through Various Finite Element Models 299
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 298
A Component-Wise Approach in Structural Analysis 297
Accurate Free Vibration Analysis of Launcher Structures Using Refined 1D Models 297
Numerical analyses of piezoceramic actuators for high temperature applications 297
Analysis of piezoelectric actuators under mechanical and electrical loads 295
Aeroelastic analysis of Versatile Thermal Insulation (VTI) panels with pinched boundary conditions 293
Analysis of tapered composite structures using a refined beam theory 289
Free-vibration analysis of space vehicle structures made by composite materials 288
One-dimensional finite element formulation with node-dependent kinematics 284
Component-wise vibration analysis of stiffened plates accounting for stiffener modes 281
Laminated Beam Analysis by Polynomial, rigonometric, Exponential and Zig-Zag Theories 279
Full Aircraft Dynamic Response by Simplified Structural Models 278
Effect of Solid Mass consumption on the free-vibration analysis of launchers 273
A Variable Kinematic One-Dimensional Model for the Hygro-Mechanical Analysis of Composite Materials 272
Aeroelastic analysis of pinched panels in a variable supersonic flow changing with altitude. 269
Static analysis of reinforced thin-walled plates and shells by means of finite element models 267
Buckling of thin walled beams by refined theory 253
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 252
Variable kinematic 1D, 2D and 3D Models for the Analysis of Aerospace Structures 247
Component-Wise Approach for Efficient and Accurate Analysis of Structures of Launchers 246
Structural Analysis of Launcher Structures by means of Refined Beam Models 239
Aeroelastic design of Versatile Thermal Insulation (VTI) panels 238
Aeroelastic behavior of launcher thermal insulation panel, accounting for various aerodynamic and structural models 232
Free Vibration Analysis of Rotating Structures By One-Dimensional, Variable Kinematic Theories 231
Accurate Analysis of Launcher Structures by Means of Refined One Dimensional Model 227
Refined one-dimensional models for the multi-field analysis of layered smart structures 222
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 219
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 216
Application of the Unified Formulation to bending analysis of magnetostrictive unimorph microbeams 216
BUCKLING OF COMPOSITE THIN WALLED BEAMS BY REFINED THEORY 215
The analysis of tapered structures using a component-wise approach based on refined one-dimensional models 212
Static and dynamic experimental analysis of a full composite VLA aircraft 212
Reissner's mixed variational theorem for layer-wise refined beam models based on the unified formulation 211
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 208
A Componet-Wise Approach for the Failure of Complex Aeronautical Structures 206
Use of higher-order Legendre polynomials for multilayered plate elements with node-dependent kinematics 206
Node-dependent kinematics, refined zig-zag and multi-line beam theories for the analysis of composite structures 204
Analysis of Tapered Structures by means of Refined 1D Models 203
Thermo-Piezo-Elastic Analysis of Complex Structures Using a Node Dependent Kinematic One-Dimensional Model 203
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 201
An adaptable refinement approach for shell finite element models based on node-dependent kinematics 198
Aeroelastic Instabilities of FGM Panels under Thermo-Mechanical Loads 195
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 193
Analysis of Composite Space Structures Subjected to Loading Factor  193
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 190
High-Fidelity One-Dimensional Models for Tapered Structures Analyses 188
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 187
Global-local plug-in for high-fidelity composite stress analysis in Femap/NX Nastran 183
Free vibration analysis of thin-walled structures through 1D and 2D refined models 181
Static and Dynamic Analysis of Composite Beams by 1-D Variable Kinematic Theories 180
Aeroelastic Instabilities Analysis of Elastic and Viscoelastic Multi-Layered Panels 179
Free vibration analysis of locally damaged aerospace tapered composite structures using component-wise models 179
Aeroelastic analysis of versatile thermal insulation panels for launchers applications 178
Analysis of Composite Launcher with Non-Structural Masses Subjected to Loading Factor 178
Accurate Evaluation of Interlaminar Stresses in Composite Laminates via Mixed One-Dimensional Formulation 178
Panel flutter analysis of composite panel with non classical configuration. 175
Global-local plug-in for high-fidelity composite stress analysis in ABAQUS 174
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES 172
Use of molecular dynamic analysis to build appropriate structural models for CNTs 172
Analysis of Complex Structures Coupling Variable Kinematics One-Dimensional Models 170
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): 169
Multidimensional Model for the Stress Analysis of Reinforced Shell Structures 169
Comparisons between 1D and 2D formulations for thin-walled structure analysis 168
Panel flutter analysis of curved panels for launcher applicatiions 166
Application of refined beam elements to the coupled-field analysis of magnetostrictive microbeams 166
Full field strain measurements of composite wing by digital image correlation 163
Process induced deformations and residual stresses in curved composite parts: a parametric analysis 159
Static and dynamic testing of a full-composite VLA by using digital image correlation and output only ground vibration testing 157
Effect of Localized Damages on the Free Vibration Analysis of Civil Structures by Component-Wise Approach 153
Finite elements with node dependent kinematics and scalable accuracy for the analysis of Stokes flows 153
On the use of refined 1D structural models for reinforced cylinders with ends sealed 150
A variable kinematic one-dimensional model for the hygro-mechanical analysis of composite materials 150
A component-wise approach to analyse a composite launcher structure subjected to loading factor 149
Experimental and numerical analysis of 3D printed open-hole plates reinforced with carbon fibers 149
Tapered composite beams analysis using refined 1-D models 146
OPTIMAL LAY-UPS TO MINIMIZE PROCESS-INDUCED DEFORMATIONS IN L-SHAPED CFRP PARTS 140
Assessment of classical, advanced, and layer-wise theories for the vibration of rotating composite anisotropic blades 139
EFFECT OF FIBER ORIENTATION PATH ON THE BUCKLING, FREE VIBRATION, AND STATIC ANALYSES OF VARIABLE ANGLE TOW PANELS 138
Virtual design and manufacturing of composite structures using refined kinematic models 134
Advanced non-linear models for the design of deployable composite space structures 132
On the role of structural theories on aeroelastic models 132
Representation, characterization and simulation of tool-part interaction and its effects on process-induced deformations in composites 132
Free Vibration Analysis of Beams with Piezo-Patches Using a One-Dimensional Model with Node-Dependent Kinematic 131
Node-Dependent Kinematic One-dimensional FEM Models for the Analysis of Beams with Piezo-patches 130
Totale 23.189
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Categoria #
all - tutte 71.091
article - articoli 35.828
book - libri 891
conference - conferenze 30.611
curatela - curatele 0
other - altro 1.609
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.562
Totale 141.592
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20202.073 0 0 0 302 292 211 177 392 315 133 182 69
2020/20212.225 255 197 47 241 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
2024/2025872 135 518 204 15 0 0 0 0 0 0 0 0
Totale 27.227