PORTO @ Archivio Istituzionale della Ricerca

PETROLO, MARCO
 Distribuzione geografica
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Continente #
NA - Nord America 28.869
EU - Europa 20.447
AS - Asia 12.170
SA - Sud America 1.279
AF - Africa 189
OC - Oceania 92
Continente sconosciuto - Info sul continente non disponibili 5
Totale 63.051
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Nazione #
US - Stati Uniti d'America 28.546
IT - Italia 6.914
SG - Singapore 4.356
CN - Cina 4.317
DE - Germania 3.397
GB - Regno Unito 2.728
FR - Francia 2.395
BR - Brasile 997
UA - Ucraina 943
KR - Corea 746
NL - Olanda 594
IE - Irlanda 587
TR - Turchia 531
RU - Federazione Russa 501
FI - Finlandia 408
HK - Hong Kong 396
VN - Vietnam 317
SE - Svezia 315
BE - Belgio 299
AT - Austria 296
IN - India 272
CA - Canada 235
CH - Svizzera 209
JP - Giappone 204
IL - Israele 188
IR - Iran 158
BG - Bulgaria 150
ID - Indonesia 146
PT - Portogallo 125
TW - Taiwan 110
ES - Italia 104
AU - Australia 85
PE - Perù 81
AR - Argentina 77
RO - Romania 76
AP - ???statistics.table.value.countryCode.AP??? 68
PL - Polonia 65
MY - Malesia 60
GR - Grecia 58
MX - Messico 58
ZA - Sudafrica 54
JO - Giordania 48
BD - Bangladesh 47
UZ - Uzbekistan 45
CZ - Repubblica Ceca 44
IQ - Iraq 42
LU - Lussemburgo 37
PK - Pakistan 35
AE - Emirati Arabi Uniti 31
DZ - Algeria 31
HR - Croazia 29
DK - Danimarca 27
CO - Colombia 26
EC - Ecuador 25
MA - Marocco 25
CL - Cile 24
EU - Europa 24
VE - Venezuela 21
SA - Arabia Saudita 20
KE - Kenya 14
TH - Thailandia 13
EG - Egitto 12
LT - Lituania 12
TN - Tunisia 12
UY - Uruguay 12
NG - Nigeria 10
PY - Paraguay 10
ET - Etiopia 9
HU - Ungheria 9
SI - Slovenia 9
AZ - Azerbaigian 8
EE - Estonia 8
NP - Nepal 8
RS - Serbia 8
LK - Sri Lanka 7
PH - Filippine 7
DO - Repubblica Dominicana 6
LV - Lettonia 6
NO - Norvegia 6
NZ - Nuova Zelanda 6
BY - Bielorussia 5
MD - Moldavia 5
TT - Trinidad e Tobago 5
AL - Albania 4
BN - Brunei Darussalam 4
JM - Giamaica 4
OM - Oman 4
SK - Slovacchia (Repubblica Slovacca) 4
SN - Senegal 4
AO - Angola 3
BH - Bahrain 3
BO - Bolivia 3
GA - Gabon 3
HN - Honduras 3
KG - Kirghizistan 3
KW - Kuwait 3
KZ - Kazakistan 3
LB - Libano 3
NI - Nicaragua 3
SY - Repubblica araba siriana 3
Totale 63.011
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Città #
Council Bluffs 6.735
Ashburn 4.388
Turin 2.502
Singapore 2.330
Southend 2.081
Beijing 1.436
Fairfield 1.423
Ann Arbor 1.334
Seattle 1.285
Torino 1.056
Chandler 977
Santa Clara 775
Dallas 753
Princeton 683
Houston 654
Woodbridge 621
Dublin 562
Des Moines 514
Wilmington 505
Cambridge 447
Jacksonville 431
Austin 424
Berlin 410
Hefei 394
Boardman 387
Milan 362
Seoul 322
San Ramon 308
Hong Kong 280
Izmir 266
Brussels 254
Herkenbosch 242
San Donato Milanese 212
Shanghai 212
New York 208
Buffalo 199
Helsinki 195
Lappeenranta 192
Frankfurt 186
Chicago 179
Bern 177
Zhengzhou 173
Los Angeles 169
Tel Aviv 164
North Bergen 159
Istanbul 155
San Francisco 155
Vienna 148
Guangzhou 147
Aachen 143
Tongling 140
Nuremberg 134
Borgosesia 124
Jakarta 124
Frankfurt am Main 112
Rome 104
Ho Chi Minh City 102
Redwood City 102
Amsterdam 101
San Diego 92
Genoa 91
Bari 90
Fremont 88
Baltimore 84
São Paulo 84
Tokyo 83
Dearborn 82
Hangzhou 81
Lauterbourg 79
Zaporozhye 79
Pennsylvania Furnace 74
San Jose 73
Atlanta 72
Lima 65
Shenzhen 65
Hanoi 64
Bristol 62
Mountain View 61
Overberg 57
Paris 57
Nanjing 56
Portsmouth 53
Norwalk 52
Munich 51
Monopoli 50
Redondo Beach 50
Saint Petersburg 50
Montréal 49
Bologna 48
London 48
Toronto 48
Melbourne 46
Phoenix 46
Chennai 45
Gilroy 45
Falls Church 43
Porto 43
Putian 43
Taipei 43
Yubileyny 43
Totale 41.892
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Nome #
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 612
Dynamic response of aerospace structures by means of refined beam theories 588
Buckling of composite thin walled beams by refined theory 575
Performance of CUF approach to analyze the structural behavior of slender bodies 556
Guidelines and Recommendations on the Use of Higher OrderFinite Elements for Bending Analysis of Plates 551
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 550
Refined Beam Elements with only Displacement Variables andPlate/Shell Capabilities 546
Classical, refined and component-wise analysis of reinforced-shell structures 527
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 515
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings 478
Best theory diagrams for cross-ply composite plates using polynomial, trigonometric and exponential thickness expansions 461
Accuracy of Refined Finite Elements for Laminated Plate Analysis 461
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 455
Component-wise Method Applied to Vibration of Wing Structures 437
Recent developments on refined theories for beams with applications 433
Best Theory Diagrams for multilayered plates considering multifield analysis 428
Multiobjective Best Theory Diagrams for cross-ply composite plates employing polynomial, zig-zag, trigonometric and exponential thickness expansions 421
Guidelines and Recommendations to Construct Theories for Metallic and composite plates 418
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 417
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 416
Refined One-Dimensional Formulations for LaminatedStructure Analysis 409
Analysis of laminated composites and sandwich structures by trigonometric, exponential and miscellaneous polynomials and a MITC9 plate element 402
Computationally efficient, high-fidelity micromechanics framework using refined 1D models 402
Variable kinematic shell elements for composite laminates accounting for hygrothermal effects 402
Component-Wise Analysis of Laminated Anisotropic Composites 402
A thermal stress finite element analysis of beam structures by hierarchical modelling 399
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 395
Analysis of thin-walled structures with longitudinal and transversal stiffeners 392
Refined beam elements with arbitrary cross-section geometries 387
Evaluation of energy and failure parameters in composite structures via a Component-Wise approach 386
Advanced models for static and dynamic analysis of wing and fuselage structures 384
Variable kinematic beam elements for electro-mechanical analysis 382
Micromechanical progressive failure analysis of fiber-reinforced composite using refined beam models 381
Further results on the development of a novel VTOL aircraft, the Anuloid. Part I: Aerodynamics 380
Unified formulation applied to free vibrations finite element analysisof beams with arbitrary section 370
An axiomatic/asymptotic evaluation of best theories for isotropic metallic and functionally graded plates employing non-polynomic functions 368
Refined free vibration analysis of one-dimensional structures with compact and bridge-like cross-sections 365
A refined 1D element for the structural analysis of single and multiple fiber/matrix cells 362
On the Effectiveness of Higher-Order Terms in Refined Beam Theories 361
A Component-Wise Approach for the Failure Analysis of Composite Structures 360
Analysis of slender, thin walled, composite madestructures with refined 1D theories 358
Results on best theories for metallic and laminated shells including Layer-Wise models 355
Computations and Evaluations of Higher-Order Theories for Free Vibration Analysis of Beams 354
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 354
Progressive damage analysis of composite structures using higher-order layer-wise elements 353
Evaluation of mixed theories for laminated plates through the axiomatic/asymptotic method 350
Progressive delamination of laminated composites via 1D models 347
Micromechanical Progressive Failure Analysis of Fiber-Reinforced Composite Using Refined Beam Models 333
Nonlinear analysis of compact and thin-walled metallic structures including localized plasticity under contact conditions 329
Flutter analysis by refined 1D dynamic stiffness elements and doublet lattice method 328
A Component-Wise Approach in Structural Analysis 328
Evaluation of Failure Parameters in Composite Structures by Component-Wise Approach 324
On the development of the Anuloid, a disk-shaped VTOL aircraft for urban areas 323
Best theory diagram for metallic and laminated composite plates 323
1D Higher-Order Finite Element Models with onlyDisplacement Variables for the Analysis of Fiber-Reinforced Composite Structures 322
1D component-wise models for failure analysis of composites 319
Axiomatic/Asymptotic Analysis of Refined Layer-Wise Theories for Composite and Sandwich Plates 317
Static analysis of thin-walled beams accounting for nonlinearities 314
Refined beam elements for the multiscale analysis of fiber-reinforced composite structures 313
Advanced aeroelastic models for the analysis of lifting surfaces made of composite materials 312
Flutter analysis of composite lifting surfaces by the 1D Carreraunified formulation and the doublet lattice method 307
Australasian research on Applied Mechanics and Aerospace - Preface 307
Static and dynamic analysis of aircraft structures by component-wise approach 302
SMART’13: Smart Materials and Structures 300
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 300
Advanced 1D structural models for flutter analysis of lifting surfaces 299
Accurate evaluation of failure indices of composite layered structures via various FE models 297
Beam Structures: Classical and Advanced Theories 296
Who needs refined structural theories? 296
Free vibration analysis of damaged beams via refined models 294
Static analysis of functionally graded plates using new nonpolynomial displacement fields via Carrera Unified Formulation 289
Progressive damage analysis of composite laminates subjected to low-velocity impact using 2D layer-wise structural models 289
Classical, Refined, Zig-Zag, Layer-Wise Models and Best Theory Diagrams for Laminated Structures 286
A critical assessment of design tools for stress analysis of adhesively bonded double lap joints 286
Global-local plug-in for high-fidelity composite stress analysis in Femap/NX Nastran 286
1D multi-line refined models for the analysis of aerospace and civil engineering structures 285
On the effectiveness of higher-order terms in layer-wise shell models 283
Buckling of thin walled beams by refined theory 283
Evaluation of the influence of voids on 3D representative volume elements of fiber-reinforced polymer composites using CUF micromechanics 282
Advanced finite elements and neural networks for scaled models 281
Contact analysis of laminated structures including transverse shear and stretching 277
A Modern and Compact Way to Formulate Classical and Advanced Beam Theories 276
Computationally Efficient Concurrent Multiscale Framework for the Nonlinear Analysis of Composite Structures 274
Classical, refined and component-wise analysis of reinforced-shell structures 272
Refined 1D finite elements for the analysis of secondary, primary and complete civil engineering structure 272
Compressive damage modeling of fiber-reinforced composite laminates using 2D higher-order layer-wise models 272
Elastoplastic Micromechanical Analysis of Fiber‑Reinforced Composites with Defects 272
Dynamic response of laminated and sandwich composite structures via 1D models based on Chebyshev polynomials 271
Methods and guidelines for the choice of shell theories 270
Global/local capabilities of MUL2 for the nonlinear analysis of composite structures 270
Further Results on the Development of a Novel VTOL Aircraft, the Anuloid: Part II: Flight Mechanics 268
Computationally Efficient Concurrent Multiscale Framework for the Linear Analysis of Composite Structures 268
Elastoplastic and progressive failure analysis of fiber-reinforced composites via an efficient nonlinear microscale model 267
High-Fidelity and Computationally Efficient Component-Wise Structural Models: an Overview of Applications and Perspectives 266
Guidelines and Recommendations to Construct Refinementsof Classical Theories for Metallic and Composite Plates- Extended Form - 259
Refined Beam Models for Static and Dynamic Analysis of Wingsand Rotor Blades 258
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 257
Refined 1D finite elements for thin-walled curved structures 257
Numerical analysis of disbonding in sandwich structures using 1D finite elements 254
A Best Theory Diagram for Metallic and Laminated Shells 253
Totale 35.371
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Categoria #
all - tutte 197.829
article - articoli 96.309
book - libri 1.931
conference - conferenze 88.674
curatela - curatele 2.425
other - altro 1.292
patent - brevetti 925
selected - selezionate 0
volume - volumi 4.956
Totale 394.341
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20212.389 0 0 0 0 0 337 218 346 366 499 373 250
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
2025/20268.447 1.318 1.064 1.697 1.896 1.437 1.035 0 0 0 0 0 0
Totale 63.910