PORTO @ Archivio Istituzionale della Ricerca

PETROLO, MARCO
 Distribuzione geografica
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Continente #
NA - Nord America 23.989
EU - Europa 17.615
AS - Asia 3.961
SA - Sud America 117
OC - Oceania 74
AF - Africa 58
Continente sconosciuto - Info sul continente non disponibili 4
Totale 45.818
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Nazione #
US - Stati Uniti d'America 23.802
IT - Italia 5.648
DE - Germania 3.060
GB - Regno Unito 2.564
FR - Francia 2.199
CN - Cina 2.152
UA - Ucraina 921
IE - Irlanda 569
NL - Olanda 523
TR - Turchia 354
FI - Finlandia 345
SG - Singapore 301
SE - Svezia 300
KR - Corea 269
RU - Federazione Russa 242
BE - Belgio 235
CH - Svizzera 206
CA - Canada 167
IN - India 149
BG - Bulgaria 147
IR - Iran 117
AT - Austria 116
JP - Giappone 108
HK - Hong Kong 100
PT - Portogallo 99
TW - Taiwan 84
RO - Romania 73
AP - ???statistics.table.value.countryCode.AP??? 68
AU - Australia 68
IL - Israele 60
MY - Malesia 53
GR - Grecia 52
ES - Italia 47
BR - Brasile 44
JO - Giordania 43
CZ - Repubblica Ceca 38
VN - Vietnam 37
LU - Lussemburgo 35
UZ - Uzbekistan 34
PE - Perù 33
HR - Croazia 29
PL - Polonia 27
DK - Danimarca 25
EU - Europa 24
AE - Emirati Arabi Uniti 21
AR - Argentina 17
MX - Messico 17
ZA - Sudafrica 17
DZ - Algeria 16
CL - Cile 15
PK - Pakistan 11
TH - Thailandia 11
NG - Nigeria 10
EG - Egitto 9
SI - Slovenia 9
EE - Estonia 8
HU - Ungheria 8
CO - Colombia 7
LK - Sri Lanka 6
NZ - Nuova Zelanda 6
PH - Filippine 6
SA - Arabia Saudita 6
BY - Bielorussia 5
ID - Indonesia 5
MD - Moldavia 5
NO - Norvegia 3
RS - Serbia 3
SY - Repubblica araba siriana 3
CY - Cipro 2
IQ - Iraq 2
KZ - Kazakistan 2
LB - Libano 2
LT - Lituania 2
SN - Senegal 2
A2 - ???statistics.table.value.countryCode.A2??? 1
BD - Bangladesh 1
BZ - Belize 1
DO - Repubblica Dominicana 1
ET - Etiopia 1
GE - Georgia 1
GT - Guatemala 1
IM - Isola di Man 1
KH - Cambogia 1
LV - Lettonia 1
MA - Marocco 1
SC - Seychelles 1
SK - Slovacchia (Repubblica Slovacca) 1
TN - Tunisia 1
VE - Venezuela 1
Totale 45.818
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Città #
Council Bluffs 6.615
Ashburn 3.597
Southend 2.081
Turin 1.871
Fairfield 1.423
Ann Arbor 1.333
Seattle 1.271
Beijing 1.069
Torino 1.056
Chandler 977
Princeton 683
Houston 644
Woodbridge 621
Dublin 548
Des Moines 514
Wilmington 504
Cambridge 447
Jacksonville 428
Berlin 409
San Ramon 307
Izmir 264
Herkenbosch 242
San Donato Milanese 212
Brussels 208
Milan 196
Singapore 195
Helsinki 190
Frankfurt 186
Bern 177
Zhengzhou 159
Shanghai 157
Lappeenranta 147
Aachen 143
San Francisco 143
Chicago 140
New York 132
Boardman 117
Guangzhou 116
Buffalo 110
Redwood City 102
Seoul 93
San Diego 92
Amsterdam 89
Vienna 89
Fremont 88
Baltimore 84
Dearborn 82
Bari 80
Zaporozhye 79
Pennsylvania Furnace 74
Genoa 73
Hangzhou 72
Borgosesia 71
Rome 71
Mountain View 61
Shenzhen 59
Bristol 58
Overberg 57
Atlanta 56
Norwalk 52
Nanjing 51
Monopoli 50
Saint Petersburg 50
Montréal 49
Gilroy 45
Falls Church 43
Bologna 42
Paris 42
Porto 42
Putian 42
Toronto 38
Miami 37
Taipei 37
Tel Aviv 37
San Antonio 36
Washington 36
Melbourne 35
Galati 33
Las Vegas 33
Palermo 32
Fuzhou 31
Cupertino 30
London 30
Malatya 30
Dallas 29
Frankfurt am Main 29
Redmond 28
Sofia 27
Lake Forest 26
Nürnberg 26
Austin 25
Cadoneghe 25
Los Angeles 25
Naples 25
Moscow 24
Phoenix 24
Lowell 23
San Jose 23
Zagreb 23
Andover 22
Totale 32.549
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Nome #
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 545
Dynamic response of aerospace structures by means of refined beam theories 515
Buckling of composite thin walled beams by refined theory 515
Performance of CUF approach to analyze the structural behavior of slender bodies 499
Refined Beam Elements with only Displacement Variables andPlate/Shell Capabilities 486
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 478
Guidelines and Recommendations on the Use of Higher OrderFinite Elements for Bending Analysis of Plates 473
Classical, refined and component-wise analysis of reinforced-shell structures 464
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings 427
Best theory diagrams for cross-ply composite plates using polynomial, trigonometric and exponential thickness expansions 413
Accuracy of Refined Finite Elements for Laminated Plate Analysis 410
Component-wise Method Applied to Vibration of Wing Structures 401
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 400
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 399
Recent developments on refined theories for beams with applications 385
Guidelines and Recommendations to Construct Theories for Metallic and composite plates 380
Refined One-Dimensional Formulations for LaminatedStructure Analysis 375
Multiobjective Best Theory Diagrams for cross-ply composite plates employing polynomial, zig-zag, trigonometric and exponential thickness expansions 371
Analysis of thin-walled structures with longitudinal and transversal stiffeners 362
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 362
Computationally efficient, high-fidelity micromechanics framework using refined 1D models 359
Best Theory Diagrams for multilayered plates considering multifield analysis 355
Component-Wise Analysis of Laminated Anisotropic Composites 354
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 352
Analysis of laminated composites and sandwich structures by trigonometric, exponential and miscellaneous polynomials and a MITC9 plate element 352
Variable kinematic shell elements for composite laminates accounting for hygrothermal effects 352
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 341
A thermal stress finite element analysis of beam structures by hierarchical modelling 337
Unified formulation applied to free vibrations finite element analysisof beams with arbitrary section 331
Variable kinematic beam elements for electro-mechanical analysis 331
Refined free vibration analysis of one-dimensional structures with compact and bridge-like cross-sections 330
Analysis of slender, thin walled, composite madestructures with refined 1D theories 328
Micromechanical progressive failure analysis of fiber-reinforced composite using refined beam models 328
On the Effectiveness of Higher-Order Terms in Refined Beam Theories 327
Advanced models for static and dynamic analysis of wing and fuselage structures 327
Refined beam elements with arbitrary cross-section geometries 327
Evaluation of energy and failure parameters in composite structures via a Component-Wise approach 325
Further results on the development of a novel VTOL aircraft, the Anuloid. Part I: Aerodynamics 323
An axiomatic/asymptotic evaluation of best theories for isotropic metallic and functionally graded plates employing non-polynomic functions 321
A Component-Wise Approach for the Failure Analysis of Composite Structures 320
A refined 1D element for the structural analysis of single and multiple fiber/matrix cells 313
Computations and Evaluations of Higher-Order Theories for Free Vibration Analysis of Beams 301
Flutter analysis by refined 1D dynamic stiffness elements and doublet lattice method 297
Evaluation of mixed theories for laminated plates through the axiomatic/asymptotic method 296
A Component-Wise Approach in Structural Analysis 295
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 292
Results on best theories for metallic and laminated shells including Layer-Wise models 289
Evaluation of Failure Parameters in Composite Structures by Component-Wise Approach 286
On the development of the Anuloid, a disk-shaped VTOL aircraft for urban areas 281
Static and dynamic analysis of aircraft structures by component-wise approach 279
1D component-wise models for failure analysis of composites 276
Micromechanical Progressive Failure Analysis of Fiber-Reinforced Composite Using Refined Beam Models 276
Refined beam elements for the multiscale analysis of fiber-reinforced composite structures 274
Flutter analysis of composite lifting surfaces by the 1D Carreraunified formulation and the doublet lattice method 274
Progressive damage analysis of composite structures using higher-order layer-wise elements 274
Advanced 1D structural models for flutter analysis of lifting surfaces 272
1D Higher-Order Finite Element Models with onlyDisplacement Variables for the Analysis of Fiber-Reinforced Composite Structures 272
Free vibration analysis of damaged beams via refined models 262
1D multi-line refined models for the analysis of aerospace and civil engineering structures 261
Australasian research on Applied Mechanics and Aerospace - Preface 260
Static analysis of functionally graded plates using new nonpolynomial displacement fields via Carrera Unified Formulation 259
Accurate evaluation of failure indices of composite layered structures via various FE models 259
Axiomatic/Asymptotic Analysis of Refined Layer-Wise Theories for Composite and Sandwich Plates 254
Nonlinear analysis of compact and thin-walled metallic structures including localized plasticity under contact conditions 253
SMART’13: Smart Materials and Structures 252
Best theory diagram for metallic and laminated composite plates 252
Buckling of thin walled beams by refined theory 251
On the effectiveness of higher-order terms in layer-wise shell models 242
Progressive delamination of laminated composites via 1D models 241
Beam Structures: Classical and Advanced Theories 239
Refined 1D finite elements for the analysis of secondary, primary and complete civil engineering structure 237
Refined Beam Models for Static and Dynamic Analysis of Wingsand Rotor Blades 235
High-Fidelity and Computationally Efficient Component-Wise Structural Models: an Overview of Applications and Perspectives 235
Dynamic response of laminated and sandwich composite structures via 1D models based on Chebyshev polynomials 231
A Modern and Compact Way to Formulate Classical and Advanced Beam Theories 230
A Best Theory Diagram for Metallic and Laminated Shells 229
A beam formulation with shell capabilities 229
Guidelines and Recommendations to Construct Refinementsof Classical Theories for Metallic and Composite Plates- Extended Form - 228
Advanced aeroelastic models for the analysis of lifting surfaces made of composite materials 228
Further Results on the Development of a Novel VTOL Aircraft, the Anuloid: Part II: Flight Mechanics 226
Methods and guidelines for the choice of shell theories 224
Elastoplastic and progressive failure analysis of fiber-reinforced composites via an efficient nonlinear microscale model 223
Evaluation of the influence of voids on 3D representative volume elements of fiber-reinforced polymer composites using CUF micromechanics 223
Three-dimensional stress analysis for beam-like structures using Serendipity Lagrange shape functions 217
A Best Theory Diagram for Metallic andLaminated Shells 216
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 216
Progressive damage analysis of composite laminates subjected to low-velocity impact using 2D layer-wise structural models 216
Who needs refined structural theories? 213
BUCKLING OF COMPOSITE THIN WALLED BEAMS BY REFINED THEORY 212
Computationally Efficient Concurrent Multiscale Framework for the Nonlinear Analysis of Composite Structures 211
Contact analysis of laminated structures including transverse shear and stretching 210
Vibration analysis of metallic and composite damaged structures by Component-Wise models 209
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 204
Multi-line-beam with variable kinematic models for the analysis of composite structures 204
Refined 1D finite elements for thin-walled curved structures 203
Elastoplastic analysis of compact and thin-walled structures using classical and refined beam finite element models 203
Variable Kinematics and Component-Wise Models for Failure Analysis of Composite Structures 201
Multibody models with flexible components for inflatable space structures 201
Computationally Efficient Concurrent Multiscale Framework for the Linear Analysis of Composite Structures 199
Comparison of dynamic stiffness and finite element methods in dynamics and aeroelastic response 197
Totale 30.022
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Categoria #
all - tutte 129.306
article - articoli 66.102
book - libri 1.427
conference - conferenze 54.259
curatela - curatele 1.228
other - altro 1.057
patent - brevetti 710
selected - selezionate 0
volume - volumi 3.542
Totale 257.631
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20204.432 0 249 193 529 629 423 389 585 620 318 341 156
2020/20213.864 420 395 158 359 143 337 218 346 366 499 373 250
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
2023/20243.044 235 229 277 269 342 269 181 187 73 288 365 329
2024/2025333 256 77 0 0 0 0 0 0 0 0 0 0
Totale 46.559