PORTO @ Archivio Istituzionale della Ricerca

PETROLO, MARCO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 25.005
EU - Europa 18.261
AS - Asia 5.098
SA - Sud America 129
OC - Oceania 74
AF - Africa 64
Continente sconosciuto - Info sul continente non disponibili 4
Totale 48.635
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 24.810
IT - Italia 5.911
DE - Germania 3.115
GB - Regno Unito 2.577
CN - Cina 2.323
FR - Francia 2.210
UA - Ucraina 922
SG - Singapore 903
IE - Irlanda 571
NL - Olanda 530
TR - Turchia 467
RU - Federazione Russa 458
FI - Finlandia 362
KR - Corea 355
SE - Svezia 300
BE - Belgio 275
CH - Svizzera 207
CA - Canada 169
IN - India 164
BG - Bulgaria 146
ID - Indonesia 123
IR - Iran 123
AT - Austria 120
HK - Hong Kong 113
JP - Giappone 109
PT - Portogallo 105
TW - Taiwan 90
RO - Romania 73
AP - ???statistics.table.value.countryCode.AP??? 68
AU - Australia 68
IL - Israele 60
MY - Malesia 53
BR - Brasile 52
GR - Grecia 52
ES - Italia 47
JO - Giordania 43
CZ - Repubblica Ceca 39
VN - Vietnam 38
LU - Lussemburgo 37
PE - Perù 37
UZ - Uzbekistan 34
HR - Croazia 29
PL - Polonia 27
DK - Danimarca 25
EU - Europa 24
AE - Emirati Arabi Uniti 21
MX - Messico 21
ZA - Sudafrica 19
AR - Argentina 17
DZ - Algeria 17
CL - Cile 15
PK - Pakistan 14
TH - Thailandia 12
NG - Nigeria 10
EG - Egitto 9
HU - Ungheria 9
SI - Slovenia 9
EE - Estonia 8
CO - Colombia 7
LK - Sri Lanka 6
NZ - Nuova Zelanda 6
PH - Filippine 6
SA - Arabia Saudita 6
BY - Bielorussia 5
LT - Lituania 5
MD - Moldavia 5
NO - Norvegia 4
RS - Serbia 4
DO - Repubblica Dominicana 3
IQ - Iraq 3
MA - Marocco 3
SK - Slovacchia (Repubblica Slovacca) 3
SY - Repubblica araba siriana 3
CY - Cipro 2
KZ - Kazakistan 2
LB - Libano 2
SC - Seychelles 2
SN - Senegal 2
A2 - ???statistics.table.value.countryCode.A2??? 1
BD - Bangladesh 1
BZ - Belize 1
ET - Etiopia 1
GE - Georgia 1
GT - Guatemala 1
IM - Isola di Man 1
KH - Cambogia 1
LV - Lettonia 1
TN - Tunisia 1
VE - Venezuela 1
Totale 48.635
Salva come PNG Salva come JPEG
Città #
Council Bluffs 6.617
Ashburn 3.652
Southend 2.081
Turin 1.986
Fairfield 1.423
Ann Arbor 1.333
Seattle 1.275
Beijing 1.080
Torino 1.056
Chandler 977
Singapore 703
Princeton 683
Houston 645
Woodbridge 621
Dublin 550
Des Moines 514
Wilmington 504
Cambridge 447
Jacksonville 428
Berlin 409
Boardman 372
Santa Clara 344
San Ramon 307
Izmir 264
Brussels 247
Herkenbosch 242
Milan 233
San Donato Milanese 212
Helsinki 194
Frankfurt 186
Bern 177
Shanghai 165
Lappeenranta 160
Zhengzhou 159
Aachen 143
San Francisco 143
Chicago 140
New York 133
Guangzhou 124
Istanbul 121
Jakarta 120
Buffalo 110
Borgosesia 109
Redwood City 102
Seoul 93
San Diego 92
Amsterdam 91
Vienna 91
Fremont 88
Baltimore 84
Dearborn 82
Bari 81
Zaporozhye 79
Rome 75
Pennsylvania Furnace 74
Genoa 73
Hangzhou 73
Frankfurt am Main 63
Bristol 62
Mountain View 61
Shenzhen 60
Overberg 57
Atlanta 56
Norwalk 52
Nanjing 51
Monopoli 50
Saint Petersburg 50
Montréal 49
Paris 48
Gilroy 45
Falls Church 43
Putian 43
Yubileyny 43
Bologna 42
Porto 42
Taipei 41
Toronto 39
Miami 37
Tel Aviv 37
San Antonio 36
Washington 36
Melbourne 35
London 34
Palermo 34
Galati 33
Las Vegas 33
Fuzhou 32
Dongguan 31
Cupertino 30
Dallas 30
Malatya 30
Redmond 30
Los Angeles 27
Naples 27
Sofia 27
Lake Forest 26
Lima 26
Nürnberg 26
Austin 25
Cadoneghe 25
Totale 34.271
Salva come PNG Salva come JPEG
Nome #
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 557
Buckling of composite thin walled beams by refined theory 526
Dynamic response of aerospace structures by means of refined beam theories 524
Performance of CUF approach to analyze the structural behavior of slender bodies 509
Refined Beam Elements with only Displacement Variables andPlate/Shell Capabilities 494
Guidelines and Recommendations on the Use of Higher OrderFinite Elements for Bending Analysis of Plates 486
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 486
Classical, refined and component-wise analysis of reinforced-shell structures 475
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings 434
Best theory diagrams for cross-ply composite plates using polynomial, trigonometric and exponential thickness expansions 420
Accuracy of Refined Finite Elements for Laminated Plate Analysis 417
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 416
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 414
Component-wise Method Applied to Vibration of Wing Structures 407
Recent developments on refined theories for beams with applications 394
Guidelines and Recommendations to Construct Theories for Metallic and composite plates 388
Refined One-Dimensional Formulations for LaminatedStructure Analysis 381
Multiobjective Best Theory Diagrams for cross-ply composite plates employing polynomial, zig-zag, trigonometric and exponential thickness expansions 379
Best Theory Diagrams for multilayered plates considering multifield analysis 373
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 372
Computationally efficient, high-fidelity micromechanics framework using refined 1D models 367
Analysis of thin-walled structures with longitudinal and transversal stiffeners 367
Variable kinematic shell elements for composite laminates accounting for hygrothermal effects 365
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 362
Analysis of laminated composites and sandwich structures by trigonometric, exponential and miscellaneous polynomials and a MITC9 plate element 361
Component-Wise Analysis of Laminated Anisotropic Composites 361
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 352
A thermal stress finite element analysis of beam structures by hierarchical modelling 345
Variable kinematic beam elements for electro-mechanical analysis 341
Micromechanical progressive failure analysis of fiber-reinforced composite using refined beam models 340
Unified formulation applied to free vibrations finite element analysisof beams with arbitrary section 335
Evaluation of energy and failure parameters in composite structures via a Component-Wise approach 334
Refined beam elements with arbitrary cross-section geometries 334
On the Effectiveness of Higher-Order Terms in Refined Beam Theories 333
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
An axiomatic/asymptotic evaluation of best theories for isotropic metallic and functionally graded plates employing non-polynomic functions 332
Further results on the development of a novel VTOL aircraft, the Anuloid. Part I: Aerodynamics 332
Analysis of slender, thin walled, composite madestructures with refined 1D theories 331
A Component-Wise Approach for the Failure Analysis of Composite Structures 326
A refined 1D element for the structural analysis of single and multiple fiber/matrix cells 320
Evaluation of mixed theories for laminated plates through the axiomatic/asymptotic method 310
Computations and Evaluations of Higher-Order Theories for Free Vibration Analysis of Beams 308
Flutter analysis by refined 1D dynamic stiffness elements and doublet lattice method 303
A Component-Wise Approach in Structural Analysis 301
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 301
Results on best theories for metallic and laminated shells including Layer-Wise models 300
Evaluation of Failure Parameters in Composite Structures by Component-Wise Approach 293
On the development of the Anuloid, a disk-shaped VTOL aircraft for urban areas 291
Progressive damage analysis of composite structures using higher-order layer-wise elements 286
1D component-wise models for failure analysis of composites 285
Micromechanical Progressive Failure Analysis of Fiber-Reinforced Composite Using Refined Beam Models 285
Flutter analysis of composite lifting surfaces by the 1D Carreraunified formulation and the doublet lattice method 284
Static and dynamic analysis of aircraft structures by component-wise approach 282
1D Higher-Order Finite Element Models with onlyDisplacement Variables for the Analysis of Fiber-Reinforced Composite Structures 282
Refined beam elements for the multiscale analysis of fiber-reinforced composite structures 280
Advanced 1D structural models for flutter analysis of lifting surfaces 274
Progressive delamination of laminated composites via 1D models 272
Axiomatic/Asymptotic Analysis of Refined Layer-Wise Theories for Composite and Sandwich Plates 269
Static analysis of functionally graded plates using new nonpolynomial displacement fields via Carrera Unified Formulation 267
Australasian research on Applied Mechanics and Aerospace - Preface 267
Accurate evaluation of failure indices of composite layered structures via various FE models 267
1D multi-line refined models for the analysis of aerospace and civil engineering structures 266
Free vibration analysis of damaged beams via refined models 266
Best theory diagram for metallic and laminated composite plates 265
Nonlinear analysis of compact and thin-walled metallic structures including localized plasticity under contact conditions 265
SMART’13: Smart Materials and Structures 264
Buckling of thin walled beams by refined theory 256
On the effectiveness of higher-order terms in layer-wise shell models 251
Beam Structures: Classical and Advanced Theories 248
High-Fidelity and Computationally Efficient Component-Wise Structural Models: an Overview of Applications and Perspectives 241
Refined 1D finite elements for the analysis of secondary, primary and complete civil engineering structure 241
Refined Beam Models for Static and Dynamic Analysis of Wingsand Rotor Blades 240
Evaluation of the influence of voids on 3D representative volume elements of fiber-reinforced polymer composites using CUF micromechanics 239
Dynamic response of laminated and sandwich composite structures via 1D models based on Chebyshev polynomials 238
Guidelines and Recommendations to Construct Refinementsof Classical Theories for Metallic and Composite Plates- Extended Form - 237
A Modern and Compact Way to Formulate Classical and Advanced Beam Theories 236
Methods and guidelines for the choice of shell theories 234
A Best Theory Diagram for Metallic and Laminated Shells 233
Advanced aeroelastic models for the analysis of lifting surfaces made of composite materials 233
Further Results on the Development of a Novel VTOL Aircraft, the Anuloid: Part II: Flight Mechanics 233
A beam formulation with shell capabilities 232
Elastoplastic and progressive failure analysis of fiber-reinforced composites via an efficient nonlinear microscale model 232
Analysis of process-induced deformations and residual stresses in curved composite parts considering transverse shear stress and thickness stretching 230
Progressive damage analysis of composite laminates subjected to low-velocity impact using 2D layer-wise structural models 227
Computationally Efficient Concurrent Multiscale Framework for the Nonlinear Analysis of Composite Structures 226
Three-dimensional stress analysis for beam-like structures using Serendipity Lagrange shape functions 225
Contact analysis of laminated structures including transverse shear and stretching 225
Who needs refined structural theories? 225
A Best Theory Diagram for Metallic andLaminated Shells 221
Vibration analysis of metallic and composite damaged structures by Component-Wise models 217
BUCKLING OF COMPOSITE THIN WALLED BEAMS BY REFINED THEORY 216
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 216
Computationally Efficient Concurrent Multiscale Framework for the Linear Analysis of Composite Structures 216
Refined 1D finite elements for thin-walled curved structures 213
Variable Kinematics and Component-Wise Models for Failure Analysis of Composite Structures 212
Elastoplastic analysis of compact and thin-walled structures using classical and refined beam finite element models 210
Multibody models with flexible components for inflatable space structures 210
Multi-line-beam with variable kinematic models for the analysis of composite structures 207
The MAMS J.N. Reddy Medal at the 1st and 2nd ICMAMS 206
Totale 30.914
Salva come PNG Salva come JPEG
Categoria #
all - tutte 143.078
article - articoli 72.300
book - libri 1.514
conference - conferenze 61.052
curatela - curatele 1.492
other - altro 1.104
patent - brevetti 750
selected - selezionate 0
volume - volumi 3.839
Totale 285.129
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20203.461 0 0 0 0 629 423 389 585 620 318 341 156
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
2023/20243.036 235 229 277 269 342 269 181 187 73 288 365 321
2024/20253.181 251 885 421 993 631 0 0 0 0 0 0 0
Totale 49.399