PORTO @ Archivio Istituzionale della Ricerca

FIORITI, MARCO
 Distribuzione geografica
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Continente #
EU - Europa 8.536
NA - Nord America 6.977
AS - Asia 2.120
SA - Sud America 68
AF - Africa 65
OC - Oceania 39
Continente sconosciuto - Info sul continente non disponibili 1
Totale 17.806
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Nazione #
US - Stati Uniti d'America 6.872
IT - Italia 2.531
DE - Germania 1.734
GB - Regno Unito 1.171
CN - Cina 1.058
FR - Francia 1.033
UA - Ucraina 632
SG - Singapore 312
RU - Federazione Russa 274
TR - Turchia 226
IE - Irlanda 218
NL - Olanda 215
KR - Corea 195
SE - Svezia 166
CH - Svizzera 127
CA - Canada 98
FI - Finlandia 76
AT - Austria 67
BE - Belgio 62
IN - India 52
HK - Hong Kong 50
JP - Giappone 43
ES - Italia 40
BR - Brasile 37
ID - Indonesia 37
IR - Iran 35
ZA - Sudafrica 34
AU - Australia 33
TW - Taiwan 31
MY - Malesia 26
PL - Polonia 24
GR - Grecia 17
IL - Israele 17
VN - Vietnam 14
UZ - Uzbekistan 12
EU - Europa 11
RO - Romania 11
BY - Bielorussia 10
JO - Giordania 10
LV - Lettonia 10
BG - Bulgaria 9
LU - Lussemburgo 9
PT - Portogallo 9
SA - Arabia Saudita 9
AR - Argentina 8
CL - Cile 8
DZ - Algeria 8
BD - Bangladesh 6
LT - Lituania 6
NZ - Nuova Zelanda 6
PE - Perù 6
AE - Emirati Arabi Uniti 5
HR - Croazia 5
KZ - Kazakistan 5
NG - Nigeria 5
CZ - Repubblica Ceca 4
IQ - Iraq 4
MX - Messico 4
NO - Norvegia 4
AL - Albania 3
AP - ???statistics.table.value.countryCode.AP??? 3
EE - Estonia 3
EG - Egitto 3
KW - Kuwait 3
ME - Montenegro 3
UY - Uruguay 3
VE - Venezuela 3
BW - Botswana 2
CI - Costa d'Avorio 2
CO - Colombia 2
DK - Danimarca 2
HU - Ungheria 2
LK - Sri Lanka 2
MA - Marocco 2
MD - Moldavia 2
NP - Nepal 2
PA - Panama 2
PH - Filippine 2
RS - Serbia 2
SN - Senegal 2
TH - Thailandia 2
AM - Armenia 1
CD - Congo 1
CR - Costa Rica 1
EC - Ecuador 1
ET - Etiopia 1
KE - Kenya 1
OM - Oman 1
PK - Pakistan 1
SC - Seychelles 1
SO - Somalia 1
TJ - Tagikistan 1
TN - Tunisia 1
TZ - Tanzania 1
Totale 17.806
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Città #
Ashburn 1.709
Southend 943
Turin 529
Fairfield 503
Seattle 475
Chandler 392
Princeton 280
Boardman 271
Beijing 247
Singapore 235
Woodbridge 235
Houston 232
Dublin 207
Ann Arbor 206
Wilmington 200
Jacksonville 192
Hangzhou 191
Torino 191
Berlin 177
Cambridge 175
San Ramon 151
Milan 145
Izmir 129
Shanghai 106
Bern 97
Buffalo 94
San Donato Milanese 86
Hamburg 73
Rome 72
Helsinki 69
Bologna 68
Frankfurt 62
Zhengzhou 62
Vienna 61
Brussels 56
Falls Church 56
Saint Petersburg 55
Herkenbosch 51
Zaporozhye 51
Boise 49
Chicago 49
Katy 44
Redwood City 43
Putian 42
Council Bluffs 41
San Francisco 41
Luft 40
Moscow 38
Santa Clara 36
Seoul 36
Baltimore 35
Frankfurt am Main 35
Fremont 35
Istanbul 33
Jakarta 33
Paris 32
Pennsylvania Furnace 31
Las Vegas 29
Monopoli 29
Munich 29
Xian 29
Padua 28
Toronto 28
Amsterdam 26
Delft 26
Des Moines 26
Guangzhou 25
Kiev 25
Malatya 25
Gilroy 24
Piscataway 24
Fuzhou 23
Naples 23
Ottawa 22
Shenzhen 22
Aachen 21
London 20
Los Angeles 20
Mountain View 20
Nanjing 20
San Antonio 20
Venaria Reale 18
Cadoneghe 17
Overberg 17
San Diego 17
Genoa 16
Hong Kong 16
Norwalk 16
Caserta 15
Denver 15
Johannesburg 15
Madrid 15
Melbourne 15
Washington 15
Austin 14
Bremen 14
Dearborn 14
Schiedam 14
Verona 14
Cranfield 13
Totale 10.701
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Nome #
ASTRID - AIRCRAFT ON BOARD SYSTEMS SIZING AND TRADE-OFF ANALYSIS IN INITIAL DESIGN 917
Functional Analysis in Systems Engineering: methodology and applications 764
ASTRID - aircraft on board systems sizing and trade-off analysis in initial design 724
Collaborative System of Systems Multidisciplinary Design Optimization for Civil Aircraft:AGILE EU project 456
A Computer Method to Develop and Validate on board Subsystem's Control Laws 439
Rational and affordable concepts of Landing Gear for small reentry vehicle demonstrators 438
Trade off studies of hybrid-electric aircraft by Fuzzy logic methodology 431
About Feasibility of a 5th generation Light Fighter Aircraft 424
Development and Validation of on-board systems control laws 419
Diesel Engine Application on AEW&C Turboprop Effectiveness-Cost Assessment 406
Automated Selection of the Optimal On-board Systems Architecture within MDO Collaborative Environment 397
UAV Logistic Support Definition 390
Hypothesis for Hypersonic Flight development 374
About Feasibility of 5th Generation Light Fighter Aircraft 331
An Alenia Aermacchi study and experience on MBSE application 317
Innovative solutions for light, very light and unmanned aircraft Preliminary design and Life Cycle Cost estimation 296
UAV BASED ADVANCED MONITORING SYSTEM: FLEET AND LOGISTIC SYSTEM SIZING BY OBJECT BASED MODEL AND MONTE-CARLO SIMULATION 286
STATUS AND PERSPECTIVES OF HYPERSONIC SYSTEMS AND TECHNOLOGIES WITH EMPHASIS ON THE ROLE OF SUB-ORBITAL FLIGHT 279
Preliminary Sub-Systems Design Integrated in a Multidisciplinary Design Optimization Framework 276
Adaptable conceptual aircraft design model 272
Zonal safety analysis in aircraft conceptual design: application to SAvE aircraft 265
Academic Course in Aircraft conceptual design and on-board systems preliminary design at Politecnico di Torino 258
Guided procedure for the Zonal Safety Analysis in aircraft preliminary design 252
Design of all electric secondary power system for future advanced MALE UAV 248
IMPACTS OF A PROGNOSTICS AND HEALTH MANAGEMENT SYSTEM ON AIRCRAFT FLEET OPERATING COST DURING CONCEPTUAL DESIGN PHASE BY USING PARAMETRIC ESTIMATION 245
Methodology for an integrated definition of a system and its subsystems: the case-study of an airplane and its subsystems 241
CONTRIBUTIONS FROM EDUCATIONAL ACTIVITIES TO RESEARCHES ABOUT HYBRID PROPULSION OPPORTUNITIES FOR LIGHT AIRCAFT 238
SUPPORT AND MAINTENANCE STRATEGIES FOR FUTURE, INNOVATIVE AND LARGELY WIDESPREAD AIR PERSONAL TRANSPORTATION SYSTEMS 234
Development of a new conceptual design methodology for parallel hybrid aircraft 226
Hybrid configuration – Advanced A.P.U. concept for future turboprop 225
Contribution To R.A.M.S estimation in early design phases of unmanned aerial vehicles - UAVs 223
Virtual and flying models for aircraft development 213
Sulla previsione di costi, sicurezza, affidabilità e entità della manutenzione in avamprogetto 212
All electric Secondary Power System for future advancedMALE UAV 210
Work-in-progress: European platform for innovation and collaboration between engineer students (EPICES) 210
The Effect of Sub-systems Design Parameters on Preliminary Aircraft Design in a Multidisciplinary Design Environment 206
Future-oriented C4ISTAR applications. UAS versus manned aircraft. Merit analysis to consider performance/cost aspects 203
Volo ipersonico per l’accesso allo Spazio: passato, presente e futuro 200
Cost-Estimating Model for Aircraft Maintenance 195
Regional turboprop conversion for AEW&C purposes supposing auxiliary engine installation – Technical and economical analysis 189
Support and Maintenance Strategies for Future, Innovative and Largely Widespread Air Personal Transportation Systems 187
MARGARET: A PERSONAL TRANSPORTATION AIRCRAFT OF TOMORROW USED TODAY FOR COLLABORATION AMONG UNIVERSITIES 186
Ultra Light Aircraft: New concepts under study at Politecnico di Torino 186
MALE UAV and its systems as basis of future definitions 185
Methodology for the Safety and Reliability assessment of hypersonic transportation systems in conceptual design activities 185
On-Board Systems Preliminary Sizing in an Overall Aircraft Design Environment 185
Assessment of airframe-subsystems synergy on overall aircraft performance in a Collaborative Design 185
The educational experience at Politecnico di Torino to develop and increase the capability in aircraft layout comprehension and definition 181
Possible hybrid propulsion configuration for transport jet aircraft 180
PRELIMINARY DESIGN AND SIZING OF A CABIN ESCAPE SYSTEM FOR A SUBORBITAL VEHICLE AIMED AT PARABOLIC FLIGHTS 180
POSSIBLE HYBRID PROPULSION CONFIGURATION FOR TRANSPORT JET AIRCRAFT 177
Collaborative systems driven aircraft configuration design optimization 174
A preliminary design study of maintenance and logistic infrastructure for MALE UAS 169
Preliminary design of a cabin escape system for a suborbital vehicle aimed at parabolic flights 161
Una nuova applicazione per la simulazione in real-time 158
INTEGRATED AEROSPACE SYSTEMS DESIGN COURSE: AN EDUCATIONAL EXPERIENCE AT POLITECNICO DI TORINO 125
A parametric cost model for estimating civil aircraft line and base maintenance 117
A virtual test bench of a parallel hybrid propulsion system for UAVs 106
AN EDUCATIONAL EXPERIENCE AT POLITECNICO DI TORINO TO STATE AND INCREASE CAPABILITY IN AIRCRAFT LAYOUT COMPREHENSION AND DEFINITION 100
A model-based rams estimation methodology for innovative aircraft on-board systems supporting mdo applications 93
Parametric approach to operating costs estimation for an innovative regional aircraft 82
Towards a methodology for new technologies assessment in aircraft operating cost 78
New methodology for flight control system sizing and hinge moment estimation 78
Method for Estimation of Electrical Wiring Interconnection Systems in Preliminary Aircraft Design 77
Environmental & flight control system architecture optimization from a family concept design perspective 76
Effect of Progressive Integration of On-Board Systems Design Discipline in an MDA Framework for Aircraft Design with Different Level of Systems Electrification 73
ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES 72
Integration of on-board systems preliminary design discipline within a collaborative 3rd generation MDO framework 72
Design of the strut braced wing aircraft in the agile collaborative MDO framework 70
Comparative Study of Advanced Turboprop Aircraft with Wing and Rear Mounted Propulsion System in the Agile EU project 69
Studies on propulsion and on-board systems matching in agile project distributed collaborative MDO environment applying for advanced regional and medium haul jet 65
Multiphase Drives for Hybrid-Electric Propulsion in Light Aircrafts: A Viable Solution 62
Design of hybrid electric heavy fuel MALE ISR UAV enabling technologies for military operations 62
A Design Model for Electric Environmental Control System in Aircraft Conceptual and Preliminary Design 58
Propulsion System for BWB Configurations in the Agile project 57
Applying a distributed collaborative MDAO environment to study the power matching of the propulsion system and the on-board electrified systems for advanced regional and short- to medium-range jetliners 56
Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project 53
Innovative concepts of electric system architectures and hybrid propulsion system for regional turboprop aircraft 49
Preliminary Study on OBS Electrification Efficiency for Advanced Supersonic Business and Medium Jet with Unified Engines 45
Multidisciplinary aircraft integration within a collaborative and distributed design framework using the AGILE paradigm 45
Propulsion and On-Board System Integration for Advanced Regional Jet with Different Level of Electrification in the AGILE project 44
Methodology for the automated preliminary certification of on-board systems architectures through requirements analysis 42
Advanced turboprop multidisciplinary design and optimization within agile project 41
ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT 32
MBSE Certification-Driven Design of a UAV MALE Configuration in the AGILE 4.0 Design Environment 31
Stream Life Cycle Assessment Model for Aircraft Preliminary Design 31
Performance and Reliability Evaluation of Innovative High-Lift Devices for Aircraft Using Electromechanical Actuators 28
Model-Based Mission Assurance/Model-Based Reliability, Availability, Maintainability, and Safety (RAMS) 26
Automated evaluation of performance, certification and maintenance aspects of aircraft on-board system architectures during preliminary design stages 26
Multidisciplinary design of a more electric regional aircraft including certification constraints 26
Assessing the Integration of Electrified On-Board Systems in an MDAO framework for a small transport aircraft 22
Multidisciplinary Design and Optimization of Regional Jet Retrofitting Activity 21
Collaborative Design of a Business Jet Family Using the AGILE 4.0 MBSE Environment 20
A parametric model for thermal management system for more electric and hybrid aircraft 20
Streamlining cross-organizational aircraft development: Results from the agile project 14
null 12
Totale 18.084
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Categoria #
all - tutte 42.154
article - articoli 14.128
book - libri 702
conference - conferenze 24.425
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.899
Totale 84.308
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.251 0 0 0 0 190 156 128 232 220 125 62 138
2020/20211.654 181 157 112 231 158 206 114 108 48 195 93 51
2021/20221.073 46 68 17 84 57 105 68 42 87 66 153 280
2022/20231.711 118 258 43 127 181 225 116 115 212 39 135 142
2023/20241.223 55 71 29 94 126 87 105 112 72 184 126 162
2024/20251.080 76 384 178 302 140 0 0 0 0 0 0 0
Totale 18.084