PORTO @ Archivio Istituzionale della Ricerca

ZAPPINO, ENRICO
 Distribuzione geografica
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Continente #
NA - Nord America 14.083
EU - Europa 10.742
AS - Asia 2.914
SA - Sud America 56
OC - Oceania 38
AF - Africa 23
Continente sconosciuto - Info sul continente non disponibili 2
Totale 27.858
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Nazione #
US - Stati Uniti d'America 13.955
IT - Italia 2.762
DE - Germania 2.216
GB - Regno Unito 1.787
FR - Francia 1.520
CN - Cina 1.268
UA - Ucraina 583
SG - Singapore 523
IE - Irlanda 352
TR - Turchia 348
NL - Olanda 313
RU - Federazione Russa 267
KR - Corea 250
CH - Svizzera 148
BE - Belgio 125
IN - India 124
CA - Canada 121
FI - Finlandia 120
SE - Svezia 119
HK - Hong Kong 75
BG - Bulgaria 73
ID - Indonesia 64
AT - Austria 61
RO - Romania 60
IR - Iran 59
JP - Giappone 58
TW - Taiwan 53
PT - Portogallo 37
AU - Australia 36
BR - Brasile 26
IL - Israele 24
ES - Italia 23
JO - Giordania 23
CZ - Repubblica Ceca 22
HR - Croazia 22
VN - Vietnam 21
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
LT - Lituania 2
MD - Moldavia 2
NG - Nigeria 2
NZ - Nuova Zelanda 2
PK - Pakistan 2
RS - Serbia 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
IM - Isola di Man 1
PH - Filippine 1
SC - Seychelles 1
SI - Slovenia 1
SK - Slovacchia (Repubblica Slovacca) 1
TH - Thailandia 1
TN - Tunisia 1
Totale 27.858
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Città #
Council Bluffs 3.345
Ashburn 2.272
Southend 1.468
Turin 824
Fairfield 750
Seattle 734
Chandler 712
Ann Arbor 681
Torino 527
Princeton 463
Beijing 457
Singapore 385
Houston 382
Woodbridge 376
Dublin 334
Berlin 285
Jacksonville 282
Des Moines 260
Wilmington 258
Cambridge 247
San Ramon 238
Boardman 233
Izmir 218
Santa Clara 201
San Donato Milanese 168
Herkenbosch 139
Bern 138
Aachen 125
Shanghai 124
Frankfurt 123
Brussels 115
Helsinki 106
Milan 101
Zhengzhou 89
Chicago 70
Istanbul 69
New York 65
Jakarta 63
Seoul 60
Amsterdam 51
Dearborn 50
Hangzhou 50
San Francisco 50
Shenzhen 50
Vienna 50
Zaporozhye 49
Guangzhou 48
Baltimore 47
Rome 47
Saint Petersburg 47
Wenzhou 46
Buffalo 43
Mountain View 43
Redwood City 43
Galati 42
Pennsylvania Furnace 42
Fremont 41
Jinan 41
San Diego 41
San Antonio 38
Toronto 38
Borgosesia 33
Bristol 28
Montréal 28
Falls Church 27
Frankfurt am Main 27
Norwalk 27
Nürnberg 27
Bari 26
Overberg 26
Yubileyny 26
London 25
Washington 25
Monopoli 24
Nanjing 24
Redmond 24
Andover 23
Lake Forest 23
Paris 23
Bologna 22
Genoa 22
Malatya 22
Montreal 20
Taipei 19
Hong Kong 18
Zagreb 18
Miami 17
Palermo 17
Tel Aviv 17
Kayseri 16
Melbourne 16
Sofia 16
Studio City 16
Atlanta 15
Lansing 15
Prague 15
Tokyo 15
Lappeenranta 14
Dong Ket 13
Kharagpur 13
Totale 19.306
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Nome #
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 532
Buckling of composite thin walled beams by refined theory 526
Performance of CUF approach to analyze the structural behavior of slender bodies 509
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 414
Finite element models with node-dependent kinematics for the analysis of composite beam structures 405
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 397
Recent developments on refined theories for beams with applications 394
Analysis of thin-walled structures with longitudinal and transversal stiffeners 367
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 354
Global-local analysis of laminated plates by node-dependent kinematic finite elements with variable ESL/LW capabilities 337
Refined free vibration analysis of one-dimensional structures with compact and bridge-like cross-sections 333
Advanced models for static and dynamic analysis of wing and fuselage structures 332
Free vibration analysis of rotating composite blades via Carrera Unified Formulation 323
Free Vibration Analysis of thin-walled cylinders reinforced with longitudinal and transversal stiffeners 319
Analysis of Rotor Dynamic by One-Dimensional Variable Kinematic Theories 313
Free Vibration analysis of Reinforced Thin-Walled Plates and Shells through Various Finite Element Models 304
Accurate Free Vibration Analysis of Launcher Structures Using Refined 1D Models 303
A Component-Wise Approach in Structural Analysis 301
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 301
Numerical analyses of piezoceramic actuators for high temperature applications 300
Analysis of piezoelectric actuators under mechanical and electrical loads 298
Aeroelastic analysis of Versatile Thermal Insulation (VTI) panels with pinched boundary conditions 294
Analysis of tapered composite structures using a refined beam theory 294
Free-vibration analysis of space vehicle structures made by composite materials 294
Component-wise vibration analysis of stiffened plates accounting for stiffener modes 286
One-dimensional finite element formulation with node-dependent kinematics 286
Laminated Beam Analysis by Polynomial, rigonometric, Exponential and Zig-Zag Theories 280
Full Aircraft Dynamic Response by Simplified Structural Models 279
Effect of Solid Mass consumption on the free-vibration analysis of launchers 277
A Variable Kinematic One-Dimensional Model for the Hygro-Mechanical Analysis of Composite Materials 277
Aeroelastic analysis of pinched panels in a variable supersonic flow changing with altitude. 271
Static analysis of reinforced thin-walled plates and shells by means of finite element models 270
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 256
Buckling of thin walled beams by refined theory 256
Component-Wise Approach for Efficient and Accurate Analysis of Structures of Launchers 250
Variable kinematic 1D, 2D and 3D Models for the Analysis of Aerospace Structures 249
Structural Analysis of Launcher Structures by means of Refined Beam Models 244
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 242
Aeroelastic design of Versatile Thermal Insulation (VTI) panels 241
Aeroelastic behavior of launcher thermal insulation panel, accounting for various aerodynamic and structural models 234
Free Vibration Analysis of Rotating Structures By One-Dimensional, Variable Kinematic Theories 233
Accurate Analysis of Launcher Structures by Means of Refined One Dimensional Model 230
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 230
Refined one-dimensional models for the multi-field analysis of layered smart structures 226
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 225
Application of the Unified Formulation to bending analysis of magnetostrictive unimorph microbeams 219
Static and dynamic experimental analysis of a full composite VLA aircraft 218
An adaptable refinement approach for shell finite element models based on node-dependent kinematics 217
BUCKLING OF COMPOSITE THIN WALLED BEAMS BY REFINED THEORY 216
The analysis of tapered structures using a component-wise approach based on refined one-dimensional models 216
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 216
Reissner's mixed variational theorem for layer-wise refined beam models based on the unified formulation 212
Use of higher-order Legendre polynomials for multilayered plate elements with node-dependent kinematics 211
A Componet-Wise Approach for the Failure of Complex Aeronautical Structures 210
Thermo-Piezo-Elastic Analysis of Complex Structures Using a Node Dependent Kinematic One-Dimensional Model 207
Analysis of Tapered Structures by means of Refined 1D Models 205
Node-dependent kinematics, refined zig-zag and multi-line beam theories for the analysis of composite structures 205
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 202
Aeroelastic Instabilities of FGM Panels under Thermo-Mechanical Loads 198
Analysis of Composite Space Structures Subjected to Loading Factor  196
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 194
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 191
High-Fidelity One-Dimensional Models for Tapered Structures Analyses 190
Global-local plug-in for high-fidelity composite stress analysis in Femap/NX Nastran 189
Aeroelastic Instabilities Analysis of Elastic and Viscoelastic Multi-Layered Panels 186
Free vibration analysis of locally damaged aerospace tapered composite structures using component-wise models 185
Free vibration analysis of thin-walled structures through 1D and 2D refined models 183
Analysis of Composite Launcher with Non-Structural Masses Subjected to Loading Factor 182
Static and Dynamic Analysis of Composite Beams by 1-D Variable Kinematic Theories 181
Accurate Evaluation of Interlaminar Stresses in Composite Laminates via Mixed One-Dimensional Formulation 181
Global-local plug-in for high-fidelity composite stress analysis in ABAQUS 180
Aeroelastic analysis of versatile thermal insulation panels for launchers applications 179
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES 179
Panel flutter analysis of composite panel with non classical configuration. 177
Multidimensional Model for the Stress Analysis of Reinforced Shell Structures 176
Use of molecular dynamic analysis to build appropriate structural models for CNTs 175
Analysis of Complex Structures Coupling Variable Kinematics One-Dimensional Models 174
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): 172
Comparisons between 1D and 2D formulations for thin-walled structure analysis 169
Full field strain measurements of composite wing by digital image correlation 168
Panel flutter analysis of curved panels for launcher applicatiions 167
Application of refined beam elements to the coupled-field analysis of magnetostrictive microbeams 166
Process induced deformations and residual stresses in curved composite parts: a parametric analysis 165
Static and dynamic testing of a full-composite VLA by using digital image correlation and output only ground vibration testing 164
Effect of Localized Damages on the Free Vibration Analysis of Civil Structures by Component-Wise Approach 161
Finite elements with node dependent kinematics and scalable accuracy for the analysis of Stokes flows 160
A component-wise approach to analyse a composite launcher structure subjected to loading factor 156
A variable kinematic one-dimensional model for the hygro-mechanical analysis of composite materials 155
Experimental and numerical analysis of 3D printed open-hole plates reinforced with carbon fibers 155
On the use of refined 1D structural models for reinforced cylinders with ends sealed 152
Tapered composite beams analysis using refined 1-D models 150
OPTIMAL LAY-UPS TO MINIMIZE PROCESS-INDUCED DEFORMATIONS IN L-SHAPED CFRP PARTS 146
Assessment of classical, advanced, and layer-wise theories for the vibration of rotating composite anisotropic blades 144
EFFECT OF FIBER ORIENTATION PATH ON THE BUCKLING, FREE VIBRATION, AND STATIC ANALYSES OF VARIABLE ANGLE TOW PANELS 143
Virtual design and manufacturing of composite structures using refined kinematic models 142
Representation, characterization and simulation of tool-part interaction and its effects on process-induced deformations in composites 140
Free Vibration Analysis of Beams with Piezo-Patches Using a One-Dimensional Model with Node-Dependent Kinematic 139
Node-Dependent Kinematic One-dimensional FEM Models for the Analysis of Beams with Piezo-patches 138
Advanced non-linear models for the design of deployable composite space structures 137
On the role of structural theories on aeroelastic models 136
Totale 23.661
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Categoria #
all - tutte 75.626
article - articoli 37.433
book - libri 908
conference - conferenze 33.426
curatela - curatele 0
other - altro 1.639
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.617
Totale 150.649
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.771 0 0 0 0 292 211 177 392 315 133 182 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
2024/20251.858 135 518 204 565 436 0 0 0 0 0 0 0
Totale 28.213