PORTO @ Archivio Istituzionale della Ricerca

MAGGIORE, Paolo
 Distribuzione geografica
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Continente #
EU - Europa 20.649
NA - Nord America 18.662
AS - Asia 8.093
SA - Sud America 836
AF - Africa 199
OC - Oceania 96
Continente sconosciuto - Info sul continente non disponibili 12
Totale 48.547
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Nazione #
US - Stati Uniti d'America 18.306
IT - Italia 6.500
DE - Germania 3.386
GB - Regno Unito 3.277
CN - Cina 3.115
FR - Francia 2.505
SG - Singapore 2.151
UA - Ucraina 1.099
KR - Corea 741
RU - Federazione Russa 703
BR - Brasile 694
TR - Turchia 586
IE - Irlanda 540
NL - Olanda 439
SE - Svezia 393
AT - Austria 318
BE - Belgio 315
CA - Canada 281
CH - Svizzera 280
IN - India 274
FI - Finlandia 267
HK - Hong Kong 223
ID - Indonesia 151
MY - Malesia 137
IR - Iran 120
JP - Giappone 108
IL - Israele 90
VN - Vietnam 90
ES - Italia 87
EU - Europa 86
AU - Australia 74
PL - Polonia 66
RO - Romania 63
MX - Messico 51
EG - Egitto 47
AP - ???statistics.table.value.countryCode.AP??? 46
BG - Bulgaria 41
JO - Giordania 39
PH - Filippine 39
PK - Pakistan 37
GR - Grecia 36
IQ - Iraq 36
TW - Taiwan 36
ZA - Sudafrica 33
AR - Argentina 32
SN - Senegal 32
BD - Bangladesh 30
PE - Perù 26
CL - Cile 25
MA - Marocco 24
NO - Norvegia 24
PT - Portogallo 23
NZ - Nuova Zelanda 21
CO - Colombia 20
CZ - Repubblica Ceca 20
HR - Croazia 20
DK - Danimarca 19
AE - Emirati Arabi Uniti 17
EC - Ecuador 17
NG - Nigeria 14
SA - Arabia Saudita 14
UZ - Uzbekistan 14
AL - Albania 13
BY - Bielorussia 13
EE - Estonia 13
LT - Lituania 13
DZ - Algeria 11
TN - Tunisia 11
CI - Costa d'Avorio 9
HU - Ungheria 9
TH - Thailandia 9
LU - Lussemburgo 8
AZ - Azerbaigian 7
KZ - Kazakistan 7
LV - Lettonia 7
PY - Paraguay 7
VE - Venezuela 7
KE - Kenya 6
QA - Qatar 6
BH - Bahrain 5
BO - Bolivia 4
OM - Oman 4
PR - Porto Rico 4
PS - Palestinian Territory 4
UY - Uruguay 4
AO - Angola 3
CR - Costa Rica 3
CU - Cuba 3
GA - Gabon 3
IS - Islanda 3
JM - Giamaica 3
KH - Cambogia 3
KW - Kuwait 3
NI - Nicaragua 3
PA - Panama 3
RS - Serbia 3
SI - Slovenia 3
SK - Slovacchia (Repubblica Slovacca) 3
XK - ???statistics.table.value.countryCode.XK??? 3
CM - Camerun 2
Totale 48.523
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Città #
Ashburn 4.157
Southend 2.516
Turin 1.508
Chandler 1.248
Singapore 1.083
Seattle 1.076
Beijing 836
Fairfield 755
Santa Clara 735
Princeton 731
Ann Arbor 727
Jacksonville 534
Dublin 515
Torino 480
Houston 450
Berlin 447
Woodbridge 444
Boardman 406
Des Moines 400
San Ramon 393
Izmir 377
Milan 357
Wilmington 309
Brussels 295
Cambridge 274
Frankfurt 265
Council Bluffs 249
Shanghai 246
San Donato Milanese 242
Bern 233
Munich 207
Hefei 203
Zhengzhou 203
Vienna 199
Seoul 186
Helsinki 185
Guangzhou 159
Dearborn 157
Rome 155
Chicago 149
Montréal 144
Dallas 142
Zaporozhye 139
San Francisco 135
Hong Kong 128
Saint Petersburg 123
Jakarta 119
Baltimore 111
Amsterdam 109
Katy 108
Paris 107
Mcallen 106
Santa Cruz 98
Hangzhou 93
Pennsylvania Furnace 91
Mountain View 87
London 78
Istanbul 75
Redwood City 75
New York 74
Monopoli 72
The Dalles 69
Tel Aviv 65
Overberg 64
Buffalo 60
Falls Church 60
Genoa 60
Los Angeles 60
Herkenbosch 56
Fremont 55
Nuremberg 54
Padua 53
Shenzhen 53
São Paulo 51
Washington 51
Moscow 50
Toronto 49
San Diego 48
Nanjing 47
San Jose 47
Frankfurt am Main 46
Andover 44
Norwalk 43
Atlanta 42
Cairo 41
Columbus 41
Naples 38
San Antonio 38
Gilroy 35
Malatya 35
Dong Ket 34
Lappeenranta 34
Cupertino 32
Redmond 32
Cangzhou 30
Indiana 29
Jinan 29
Athens 28
Bremen 28
Delft 28
Totale 28.064
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Nome #
FUTURE SPACE EXPLORATION: FROM REFERENCE SCENARIO DEFINITION TO KEY TECHNOLOGIES ROADMAPS 573
A direct-drive solution for Hydrogen supplied all-electric airplane 514
A methodology for innovative technologies roadmaps assessment to support strategic decisions for future space exploration. 476
A methodology to support strategic decisions in future human space exploration: from scenario definition to building blocks assessment 466
Reusable space tug concept and mission 438
The Green Glider Project - actual and next future Evolutions 419
Analysis of a Moon outpost for Mars enabling technologies through a Virtual Reality environment 409
HUMAN EXPEDITION TO A NEAR EARTH ASTEROID: REFERENCE MISSION AND TECHNOLOGIES 407
Multidisciplinary Integrated Framework for the Optimal Design of a Jet Aircraft Wing 406
A Multi-Objective Design Optimization Approach for the Preliminary Design of High Speed Low Pressure Turbine Disks for Green Engine Architectures 396
Modelling of a safety relief valve through a MATLAB-Simulink and CFD based approach 382
A PEM fuel cell laminar and turbulent models comparison, aiming at identifying small-scale plate channel phenomena: a mesh independent configuration 381
Tensile and compression characterization of 3D printed ABS specimens for UAV applications 379
Additive Manufacturing Offers New Opportunities in UAV Research 370
A PEM fuel cell distributed parameters model aiming at studying the production of liquid water within the cell during its normal operation: model description, implementation and validation 349
Conjugate Heat Transfer Analysis of Integrated Brushless Generators for More Electric Engines 343
Aircraft Flap Control System: Proposal of a Simulink Test Bench for Evaluating Innovative Asymmetry Monitoring and Control Techniques 340
Development of an Environmental Control System Pack simulation model for a More Electric Aircraft 336
PEM fuel cell performance under pre-compression of electrode: a multidisciplinary, integrated and advanced calculus approach 336
Comparative analysis of a hydraulic servo-valve 334
A new CFD-Simulink based systems engineering approach applied to the modelling of a hydraulic safety relief valve 329
Conjugate Heat Transfer Analysis of Integrated Brushless Generators for More Electric Engines 321
Characterization of ABS specimens produced via the 3D printing technology for drone structural components 320
Multidisciplinary integrated design environment for aircraft wing sizing 318
Characterization and analysis of homogeneous and sandwich PLA/ABS specimens produced via the FDM printing process for UAV structural elements 317
Risk Analysis of the Future Implementation of a Safety Management System for Multiple RPAS Based on First Demonstration Flights 315
Evaluations on hydrogen fuel cells as a source of energy for specific operations category civil RPAS systems 314
Analysis of a Moon outpost for Mars enabling technologies through a Virtual Reality environment 311
Definition of parametric methods for fault analysis applied to an electromechanical servomechanism affected by multiple failures 311
H-due: Electric-Hydrogen Powered Personal Mobility Concept Vehicle 306
Innovative Hydrogen Storage Tank for Flying Fuel Cell Power System 306
HUMAN EXPLORATION MISSION TO A NEAR EARTH ASTEROID: MISSION DESCRIPTION AND KEY TECHNOLOGIES ASSESSMENT 302
Identification of Precursors of Servovalves Failures for Implementation of an Effective Prognostics 294
Electromechanical actuators affected by multiple failures: Prognostic method based on spectral analysis techniques 286
The double fuselage layout: a preliminary case study of a possible way of reducing the development costs for new high capacity aircraft 285
Analysis of environmental benefits resulting from use of hydrogen technology in handling operations at airports 284
Approximated models for aerodynamic coefficients estimation in a multidisciplinary design environment 284
Electromechanical actuators affected by multiple failures: a simulated-annealing-based fault identification algorithm 284
CAD based shape optimization for gas turbine component design 283
Fuel cell size and weight reduction due to innovative metallic bipolar plates: technical process details and improvements 281
Model based analysis of precursors of electromechanical servomechanisms failures using an artificial neural network 279
MBSE Modelling Environment and Multi-Objective Optimization of Thermal Control Strategies for Multifunctional Structures 275
Numerical modelling of sinusoidal brushless motor for aerospace actuator systems 274
IMPACT OF AN OPTIMIZED POWER TURBINE DISKS CAVITY ON GEARED OPEN ROTOR PERFORMANCE – A MULTIDISCIPLINARY APPROACH IN THE PRELIMINARY DESIGN 273
Development of the Electric Power Generation Control System for an Innovative Unmanned Airship 270
NEA robotic friend: an innovative and versatile vehicle to support human mobility around asteroids 269
Fluid dynamic analysis of pollutants’ dispersion behind an aircraft engine during idling 269
Sensitivity Analysis for a PEM Fuel Cell Model aimed to Optimization 269
New Prognostic Method Based on Spectral Analysis Techniques Dealing with Motor Static Eccentricity for Aerospace Electromechanical Actuators 268
A Comparison between 3D Printing and Milling Process for a Spar Cap Fitting (Wing-fuselage) of UAV Aircraft 268
Robust simulation model approach to evaluate innovative asymmetry monitoring and control techniques in critical flap failure and aircraft controllability 268
Incremental architectures for a permanent human lunar outpost with focus on isru technologies. 267
A New Prognostic Method Based on Simulated Annealing Algorithm to Deal with the Effects of Dry Friction on Electromechanical Actuators 267
PEM fuel cell performance under particular operating conditions causing the production of liquid water: a morphing on bipolar plate's channels approach 264
Variable fidelity aerodynamic analysis for multidisciplinary wing design 261
Light Simulator for Solar Power Systems 260
A Robust Multifunctional Sandwich Panel Design with Trabecular Structures by the Use of Additive Manufacturing Technology for a New De-Icing System 259
Virtual Reality to assist the engineering decision-making process: improving the Concurrent Design approach 258
Fattibilita' di conversione 'All Electric' per attuali velivoli da trasporto regionale 256
Route profitability for helicopters 256
Electromechanical servomechanisms affected by motor static eccentricity: Proposal of fault evaluation algorithm based on spectral analysis techniques 256
Development of a multifunctional panel for aerospace use through SLM Additive Manufacturing 256
Proposal of Multidisciplinary Design Optimization Approach for a Proton Exchange Membrane Fuel Cell Performance Estimate 255
System Modeling Framework and MDO Tool Integration: MBSE Methodologies Applied to Design and Analysis of Space System 254
Linear Electromechanical Actuators Affected by Mechanical Backlash: a Fault Identification Method Based on Simulated Annealing Algorithm 252
AEROMOBILE DOTATO DI SISTEMA ANTIGHIACCIO STRUTTURALMENTE INTEGRATO 252
Risk Assessment and Failure Analysis for an Innovative Remotely-Piloted Airship 251
Multi-objective Optimization of Thermal Control Strategies for Multifunctional Structures 249
Enabling technologies to support human life in permanent lunar base 249
Failure rate evaluation method for HW architecture derived from functional safety standards (ISO 19014, ISO 25119, IEC 61508) 249
Human life support in permanent lunar base architectures 248
Proposal of a model based fault identification neural technique for more-electric aircraft flight control EM actuators 247
Multi-objective Optimization of a Multifunctional Structure through a MOGA and SOM based Methodology 246
Human exploration of the Moon: multi-stage lunar dust removal system 245
Fluid dynamic analysis of pollutants’ dispersion behind an aircraft engine during idling 244
Comparative Analysis of Spacecraft Anomalies using Complexity Indexes: a Top-Down Approach 242
Future Human Space Exploration: key technologies assessment and applicability analysis 242
UML-Based System-Level specifications for integrated systems 242
Risk Analysis: Sample Application To a Totally New Aircraft Design 235
Application of dust removal technologies for future lunar exploration 235
Proton Exchange Membrane Fuel Cell Performance Estimate through a Multidisciplinary Design Optimization approach 232
Multi-material sandwich panel produced with desktop 3D printer 230
LuNaDrone: nano drone for Lunar Exploration 229
The double-fuselage layout: a possible way to reduce development costs for new high capacity aircraft 227
Light flight management system: specifica base per velivoli ultraleggeri 224
Onboard Electromechanical Actuators Affected by Motor Static Eccentricity: a New Prognostic Method based on Spectral Analysis Techniques 224
Compression tests of ABS specimens for UAV components produced via the FDM technique 223
Proposal of a Fast Model-Based Prognostic Paradigm for Electrohydraulic Actuators affected by Multiple Failures 222
Proposal of prognostic parametric method applied to an electrohydraulic servomechanism affected by multiple failures 221
Effects of Dry Friction on Linear Electromechanical Actuators: A New Prognostic Method based on Simulated Annealing Algorithm 219
Special Issue on “Additive Manufacturing Technologies and Applications” 215
Dry friction acting on hydraulic motors and control valves: dynamic behaviour of flight controls 214
Optimized design of a multiphase induction machine for an open rotor aero-engine shaft-line-embedded starter/generatorIECON 2013 - 39th Annual Conference of the IEEE Industrial Electronics Society 210
A multifidelity approach to aerodynamic analysis in an integrated design environment 210
Design and Development of an Electromechanical Actuator Test Bench for Validation of Health Monitoring Models 210
Sandwich panel with lattice core for aircraft anti-ice system made by Selective Laser Melting 209
Parametric CAD modelling for shape optimization 208
Neural Network Design for Incipient Failure Detection on Aircraft EM Actuator 208
Comparison of Environmental Test Approaches Trough MAT€D AIV Data and Reference to ECSS 207
Performance estimate for a Proton Exchange Membrane Fuel Cell: Sensitivity Analysis aimed to Optimization 207
Totale 28.733
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Categoria #
all - tutte 137.225
article - articoli 44.230
book - libri 1.031
conference - conferenze 87.183
curatela - curatele 398
other - altro 2.379
patent - brevetti 911
selected - selezionate 0
volume - volumi 1.093
Totale 274.450
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20212.448 0 0 235 370 172 336 134 209 164 510 199 119
2021/20222.972 287 264 59 108 123 193 113 100 219 166 618 722
2022/20235.044 461 737 137 400 482 642 645 275 519 106 291 349
2023/20242.591 102 233 112 228 282 277 131 204 185 210 266 361
2024/20258.066 234 1.128 602 779 748 586 413 522 1.072 480 637 865
2025/20262.225 1.073 1.009 143 0 0 0 0 0 0 0 0 0
Totale 49.222