PORTO @ Archivio Istituzionale della Ricerca

PETROLO, MARCO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 28.103
EU - Europa 20.127
AS - Asia 10.498
SA - Sud America 1.132
AF - Africa 139
OC - Oceania 89
Continente sconosciuto - Info sul continente non disponibili 5
Totale 60.093
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 27.824
IT - Italia 6.801
CN - Cina 4.126
DE - Germania 3.365
SG - Singapore 3.285
GB - Regno Unito 2.698
FR - Francia 2.333
UA - Ucraina 940
BR - Brasile 904
KR - Corea 725
IE - Irlanda 585
NL - Olanda 584
TR - Turchia 524
RU - Federazione Russa 487
FI - Finlandia 404
HK - Hong Kong 325
SE - Svezia 309
BE - Belgio 294
AT - Austria 290
IN - India 256
CA - Canada 216
CH - Svizzera 209
IL - Israele 188
JP - Giappone 164
IR - Iran 152
BG - Bulgaria 150
VN - Vietnam 147
ID - Indonesia 130
PT - Portogallo 123
TW - Taiwan 105
ES - Italia 89
AU - Australia 82
PE - Perù 77
RO - Romania 75
AP - ???statistics.table.value.countryCode.AP??? 68
AR - Argentina 59
GR - Grecia 58
MY - Malesia 54
PL - Polonia 53
JO - Giordania 46
CZ - Repubblica Ceca 44
UZ - Uzbekistan 42
MX - Messico 39
LU - Lussemburgo 37
ZA - Sudafrica 37
BD - Bangladesh 35
PK - Pakistan 31
AE - Emirati Arabi Uniti 30
HR - Croazia 29
DZ - Algeria 28
DK - Danimarca 27
IQ - Iraq 26
EU - Europa 24
CO - Colombia 20
CL - Cile 19
EC - Ecuador 19
MA - Marocco 16
SA - Arabia Saudita 16
VE - Venezuela 14
TH - Thailandia 13
EG - Egitto 11
TN - Tunisia 11
NG - Nigeria 10
UY - Uruguay 10
HU - Ungheria 9
LT - Lituania 9
SI - Slovenia 9
EE - Estonia 8
KE - Kenya 8
PY - Paraguay 8
RS - Serbia 8
LK - Sri Lanka 7
NP - Nepal 7
DO - Repubblica Dominicana 6
LV - Lettonia 6
NO - Norvegia 6
NZ - Nuova Zelanda 6
PH - Filippine 6
AZ - Azerbaigian 5
BY - Bielorussia 5
MD - Moldavia 5
TT - Trinidad e Tobago 5
AL - Albania 4
BN - Brunei Darussalam 4
OM - Oman 4
SK - Slovacchia (Repubblica Slovacca) 4
BH - Bahrain 3
ET - Etiopia 3
HN - Honduras 3
JM - Giamaica 3
KG - Kirghizistan 3
LB - Libano 3
SN - Senegal 3
SY - Repubblica araba siriana 3
AO - Angola 2
BB - Barbados 2
BW - Botswana 2
CY - Cipro 2
GA - Gabon 2
KZ - Kazakistan 2
Totale 60.067
Salva come PNG Salva come JPEG
Città #
Council Bluffs 6.718
Ashburn 4.187
Turin 2.468
Southend 2.081
Singapore 1.935
Fairfield 1.423
Beijing 1.398
Ann Arbor 1.334
Seattle 1.285
Torino 1.056
Chandler 977
Santa Clara 755
Dallas 744
Princeton 683
Houston 649
Woodbridge 621
Dublin 560
Des Moines 514
Wilmington 505
Cambridge 447
Jacksonville 431
Austin 424
Berlin 410
Hefei 394
Boardman 386
Milan 344
San Ramon 308
Seoul 301
Izmir 265
Brussels 253
Herkenbosch 242
San Donato Milanese 212
Hong Kong 210
Shanghai 208
Helsinki 195
Lappeenranta 189
Frankfurt 186
Bern 177
New York 176
Chicago 173
Zhengzhou 172
Tel Aviv 164
Buffalo 163
San Francisco 155
Istanbul 154
Vienna 144
Aachen 143
Guangzhou 143
Tongling 140
Nuremberg 133
Los Angeles 127
Borgosesia 124
Jakarta 121
Redwood City 102
Amsterdam 98
Rome 97
San Diego 92
Genoa 91
Bari 89
Fremont 88
Baltimore 84
Frankfurt am Main 84
Dearborn 82
Hangzhou 80
Zaporozhye 79
Pennsylvania Furnace 74
São Paulo 71
Atlanta 69
Lima 64
Shenzhen 63
Bristol 62
Mountain View 61
Overberg 57
Paris 56
Nanjing 55
Portsmouth 53
Norwalk 52
Munich 51
Monopoli 50
Saint Petersburg 50
Montréal 49
Bologna 47
Lauterbourg 47
London 46
Gilroy 45
Melbourne 45
Tokyo 45
Falls Church 43
Ho Chi Minh City 43
Porto 43
Putian 43
Redondo Beach 43
Taipei 43
Toronto 43
Yubileyny 43
Chennai 41
Phoenix 39
San Antonio 39
Washington 39
Brooklyn 38
Totale 40.525
Salva come PNG Salva come JPEG
Nome #
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 595
Dynamic response of aerospace structures by means of refined beam theories 568
Buckling of composite thin walled beams by refined theory 563
Performance of CUF approach to analyze the structural behavior of slender bodies 550
Guidelines and Recommendations on the Use of Higher OrderFinite Elements for Bending Analysis of Plates 540
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 536
Refined Beam Elements with only Displacement Variables andPlate/Shell Capabilities 534
Classical, refined and component-wise analysis of reinforced-shell structures 513
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 498
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings 465
Accuracy of Refined Finite Elements for Laminated Plate Analysis 453
Best theory diagrams for cross-ply composite plates using polynomial, trigonometric and exponential thickness expansions 450
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 445
Component-wise Method Applied to Vibration of Wing Structures 427
Recent developments on refined theories for beams with applications 422
Best Theory Diagrams for multilayered plates considering multifield analysis 413
Guidelines and Recommendations to Construct Theories for Metallic and composite plates 408
Multiobjective Best Theory Diagrams for cross-ply composite plates employing polynomial, zig-zag, trigonometric and exponential thickness expansions 407
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 407
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 405
Refined One-Dimensional Formulations for LaminatedStructure Analysis 401
Variable kinematic shell elements for composite laminates accounting for hygrothermal effects 394
Analysis of laminated composites and sandwich structures by trigonometric, exponential and miscellaneous polynomials and a MITC9 plate element 393
Computationally efficient, high-fidelity micromechanics framework using refined 1D models 393
Component-Wise Analysis of Laminated Anisotropic Composites 390
A thermal stress finite element analysis of beam structures by hierarchical modelling 389
Analysis of thin-walled structures with longitudinal and transversal stiffeners 384
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 382
Refined beam elements with arbitrary cross-section geometries 377
Evaluation of energy and failure parameters in composite structures via a Component-Wise approach 375
Variable kinematic beam elements for electro-mechanical analysis 373
Micromechanical progressive failure analysis of fiber-reinforced composite using refined beam models 368
Advanced models for static and dynamic analysis of wing and fuselage structures 367
Further results on the development of a novel VTOL aircraft, the Anuloid. Part I: Aerodynamics 366
An axiomatic/asymptotic evaluation of best theories for isotropic metallic and functionally graded plates employing non-polynomic functions 360
Unified formulation applied to free vibrations finite element analysisof beams with arbitrary section 359
Refined free vibration analysis of one-dimensional structures with compact and bridge-like cross-sections 357
On the Effectiveness of Higher-Order Terms in Refined Beam Theories 355
Analysis of slender, thin walled, composite madestructures with refined 1D theories 355
A refined 1D element for the structural analysis of single and multiple fiber/matrix cells 351
A Component-Wise Approach for the Failure Analysis of Composite Structures 350
Progressive damage analysis of composite structures using higher-order layer-wise elements 345
Computations and Evaluations of Higher-Order Theories for Free Vibration Analysis of Beams 344
Results on best theories for metallic and laminated shells including Layer-Wise models 338
Evaluation of mixed theories for laminated plates through the axiomatic/asymptotic method 338
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 332
Progressive delamination of laminated composites via 1D models 330
Micromechanical Progressive Failure Analysis of Fiber-Reinforced Composite Using Refined Beam Models 322
Flutter analysis by refined 1D dynamic stiffness elements and doublet lattice method 321
A Component-Wise Approach in Structural Analysis 321
Nonlinear analysis of compact and thin-walled metallic structures including localized plasticity under contact conditions 321
On the development of the Anuloid, a disk-shaped VTOL aircraft for urban areas 315
Evaluation of Failure Parameters in Composite Structures by Component-Wise Approach 314
1D Higher-Order Finite Element Models with onlyDisplacement Variables for the Analysis of Fiber-Reinforced Composite Structures 313
Best theory diagram for metallic and laminated composite plates 309
1D component-wise models for failure analysis of composites 308
Refined beam elements for the multiscale analysis of fiber-reinforced composite structures 303
Axiomatic/Asymptotic Analysis of Refined Layer-Wise Theories for Composite and Sandwich Plates 303
Flutter analysis of composite lifting surfaces by the 1D Carreraunified formulation and the doublet lattice method 303
Static analysis of thin-walled beams accounting for nonlinearities 303
Australasian research on Applied Mechanics and Aerospace - Preface 298
Static and dynamic analysis of aircraft structures by component-wise approach 297
SMART’13: Smart Materials and Structures 295
Advanced 1D structural models for flutter analysis of lifting surfaces 292
Accurate evaluation of failure indices of composite layered structures via various FE models 290
Beam Structures: Classical and Advanced Theories 289
Who needs refined structural theories? 289
Free vibration analysis of damaged beams via refined models 287
Static analysis of functionally graded plates using new nonpolynomial displacement fields via Carrera Unified Formulation 285
Advanced aeroelastic models for the analysis of lifting surfaces made of composite materials 284
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 283
Progressive damage analysis of composite laminates subjected to low-velocity impact using 2D layer-wise structural models 278
On the effectiveness of higher-order terms in layer-wise shell models 277
1D multi-line refined models for the analysis of aerospace and civil engineering structures 277
Buckling of thin walled beams by refined theory 276
A critical assessment of design tools for stress analysis of adhesively bonded double lap joints 274
Classical, Refined, Zig-Zag, Layer-Wise Models and Best Theory Diagrams for Laminated Structures 272
Evaluation of the influence of voids on 3D representative volume elements of fiber-reinforced polymer composites using CUF micromechanics 271
Advanced finite elements and neural networks for scaled models 271
A Modern and Compact Way to Formulate Classical and Advanced Beam Theories 268
Refined 1D finite elements for the analysis of secondary, primary and complete civil engineering structure 265
Methods and guidelines for the choice of shell theories 265
Dynamic response of laminated and sandwich composite structures via 1D models based on Chebyshev polynomials 264
Contact analysis of laminated structures including transverse shear and stretching 264
Global-local plug-in for high-fidelity composite stress analysis in Femap/NX Nastran 264
Computationally Efficient Concurrent Multiscale Framework for the Nonlinear Analysis of Composite Structures 263
Elastoplastic Micromechanical Analysis of Fiber‑Reinforced Composites with Defects 263
High-Fidelity and Computationally Efficient Component-Wise Structural Models: an Overview of Applications and Perspectives 262
Classical, refined and component-wise analysis of reinforced-shell structures 258
Further Results on the Development of a Novel VTOL Aircraft, the Anuloid: Part II: Flight Mechanics 256
Refined Beam Models for Static and Dynamic Analysis of Wingsand Rotor Blades 254
Elastoplastic and progressive failure analysis of fiber-reinforced composites via an efficient nonlinear microscale model 253
Computationally Efficient Concurrent Multiscale Framework for the Linear Analysis of Composite Structures 252
Compressive damage modeling of fiber-reinforced composite laminates using 2D higher-order layer-wise models 252
Global/local capabilities of MUL2 for the nonlinear analysis of composite structures 252
Guidelines and Recommendations to Construct Refinementsof Classical Theories for Metallic and Composite Plates- Extended Form - 250
A Best Theory Diagram for Metallic and Laminated Shells 249
A beam formulation with shell capabilities 248
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 246
Three-dimensional stress analysis for beam-like structures using Serendipity Lagrange shape functions 245
Totale 34.299
Salva come PNG Salva come JPEG
Categoria #
all - tutte 190.551
article - articoli 93.156
book - libri 1.859
conference - conferenze 85.074
curatela - curatele 2.311
other - altro 1.247
patent - brevetti 890
selected - selezionate 0
volume - volumi 4.766
Totale 379.854
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20212.891 0 0 0 359 143 337 218 346 366 499 373 250
2021/20223.843 162 224 241 179 297 290 165 121 254 329 599 982
2022/202312.057 373 667 96 331 409 561 793 270 400 331 631 7.195
2023/20243.036 235 229 277 269 342 269 181 187 73 288 365 321
2024/20259.245 251 885 421 993 803 762 425 893 1.330 545 779 1.158
2025/20265.473 1.318 1.064 1.697 1.394 0 0 0 0 0 0 0 0
Totale 60.936