PORTO @ Archivio Istituzionale della Ricerca

FIORITI, MARCO
 Distribuzione geografica
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Continente #
EU - Europa 8.376
NA - Nord America 6.925
AS - Asia 1.907
AF - Africa 63
SA - Sud America 62
OC - Oceania 39
Continente sconosciuto - Info sul continente non disponibili 1
Totale 17.373
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Nazione #
US - Stati Uniti d'America 6.838
IT - Italia 2.500
DE - Germania 1.725
GB - Regno Unito 1.164
FR - Francia 1.025
CN - Cina 987
UA - Ucraina 632
SG - Singapore 244
IE - Irlanda 218
NL - Olanda 206
TR - Turchia 205
RU - Federazione Russa 198
KR - Corea 178
SE - Svezia 166
CH - Svizzera 116
CA - Canada 80
FI - Finlandia 72
AT - Austria 67
BE - Belgio 62
HK - Hong Kong 49
IN - India 49
JP - Giappone 43
ES - Italia 40
IR - Iran 34
ZA - Sudafrica 34
AU - Australia 33
BR - Brasile 31
TW - Taiwan 31
MY - Malesia 25
PL - Polonia 24
IL - Israele 16
GR - Grecia 15
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
ID - Indonesia 8
BD - Bangladesh 6
DZ - Algeria 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
LT - Lituania 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 17.373
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Città #
Ashburn 1.695
Southend 943
Turin 520
Fairfield 503
Seattle 475
Chandler 392
Princeton 280
Boardman 271
Beijing 247
Woodbridge 235
Houston 232
Dublin 207
Ann Arbor 206
Wilmington 200
Jacksonville 192
Hangzhou 191
Torino 191
Berlin 177
Cambridge 175
Singapore 175
San Ramon 151
Milan 139
Izmir 129
Shanghai 105
Bern 97
Buffalo 94
San Donato Milanese 86
Hamburg 73
Bologna 68
Rome 66
Helsinki 65
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
Council Bluffs 41
San Francisco 41
Luft 40
Putian 40
Moscow 38
Seoul 36
Baltimore 35
Fremont 35
Pennsylvania Furnace 31
Paris 30
Frankfurt am Main 29
Las Vegas 29
Monopoli 29
Munich 29
Xian 29
Padua 28
Delft 26
Des Moines 26
Santa Clara 26
Guangzhou 25
Kiev 25
Malatya 25
Amsterdam 24
Gilroy 24
Piscataway 24
Fuzhou 23
Naples 23
Shenzhen 22
Los Angeles 20
Mountain View 20
Nanjing 20
Ottawa 20
San Antonio 20
Aachen 19
Toronto 19
Venaria Reale 18
Cadoneghe 17
London 17
Overberg 17
San Diego 17
Genoa 16
Norwalk 16
Caserta 15
Denver 15
Hong Kong 15
Johannesburg 15
Madrid 15
Melbourne 15
Washington 15
Austin 14
Bremen 14
Dearborn 14
Istanbul 14
Schiedam 14
Verona 14
Cranfield 13
Dallas 13
Totale 10.523
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Nome #
ASTRID - AIRCRAFT ON BOARD SYSTEMS SIZING AND TRADE-OFF ANALYSIS IN INITIAL DESIGN 896
Functional Analysis in Systems Engineering: methodology and applications 752
ASTRID - aircraft on board systems sizing and trade-off analysis in initial design 720
Collaborative System of Systems Multidisciplinary Design Optimization for Civil Aircraft:AGILE EU project 452
A Computer Method to Develop and Validate on board Subsystem's Control Laws 437
Rational and affordable concepts of Landing Gear for small reentry vehicle demonstrators 431
Trade off studies of hybrid-electric aircraft by Fuzzy logic methodology 428
About Feasibility of a 5th generation Light Fighter Aircraft 422
Development and Validation of on-board systems control laws 411
Diesel Engine Application on AEW&C Turboprop Effectiveness-Cost Assessment 400
Automated Selection of the Optimal On-board Systems Architecture within MDO Collaborative Environment 391
UAV Logistic Support Definition 378
Hypothesis for Hypersonic Flight development 370
About Feasibility of 5th Generation Light Fighter Aircraft 319
An Alenia Aermacchi study and experience on MBSE application 314
Innovative solutions for light, very light and unmanned aircraft Preliminary design and Life Cycle Cost estimation 292
UAV BASED ADVANCED MONITORING SYSTEM: FLEET AND LOGISTIC SYSTEM SIZING BY OBJECT BASED MODEL AND MONTE-CARLO SIMULATION 283
STATUS AND PERSPECTIVES OF HYPERSONIC SYSTEMS AND TECHNOLOGIES WITH EMPHASIS ON THE ROLE OF SUB-ORBITAL FLIGHT 276
Adaptable conceptual aircraft design model 269
Preliminary Sub-Systems Design Integrated in a Multidisciplinary Design Optimization Framework 269
Zonal safety analysis in aircraft conceptual design: application to SAvE aircraft 264
Academic Course in Aircraft conceptual design and on-board systems preliminary design at Politecnico di Torino 256
Guided procedure for the Zonal Safety Analysis in aircraft preliminary design 249
Design of all electric secondary power system for future advanced MALE UAV 246
Methodology for an integrated definition of a system and its subsystems: the case-study of an airplane and its subsystems 240
CONTRIBUTIONS FROM EDUCATIONAL ACTIVITIES TO RESEARCHES ABOUT HYBRID PROPULSION OPPORTUNITIES FOR LIGHT AIRCAFT 231
SUPPORT AND MAINTENANCE STRATEGIES FOR FUTURE, INNOVATIVE AND LARGELY WIDESPREAD AIR PERSONAL TRANSPORTATION SYSTEMS 229
IMPACTS OF A PROGNOSTICS AND HEALTH MANAGEMENT SYSTEM ON AIRCRAFT FLEET OPERATING COST DURING CONCEPTUAL DESIGN PHASE BY USING PARAMETRIC ESTIMATION 224
Hybrid configuration – Advanced A.P.U. concept for future turboprop 222
Contribution To R.A.M.S estimation in early design phases of unmanned aerial vehicles - UAVs 221
Development of a new conceptual design methodology for parallel hybrid aircraft 221
Sulla previsione di costi, sicurezza, affidabilità e entità della manutenzione in avamprogetto 211
Virtual and flying models for aircraft development 211
Work-in-progress: European platform for innovation and collaboration between engineer students (EPICES) 209
All electric Secondary Power System for future advancedMALE UAV 208
The Effect of Sub-systems Design Parameters on Preliminary Aircraft Design in a Multidisciplinary Design Environment 202
Volo ipersonico per l’accesso allo Spazio: passato, presente e futuro 197
Future-oriented C4ISTAR applications. UAS versus manned aircraft. Merit analysis to consider performance/cost aspects 196
Cost-Estimating Model for Aircraft Maintenance 193
Ultra Light Aircraft: New concepts under study at Politecnico di Torino 186
Regional turboprop conversion for AEW&C purposes supposing auxiliary engine installation – Technical and economical analysis 185
Support and Maintenance Strategies for Future, Innovative and Largely Widespread Air Personal Transportation Systems 184
MALE UAV and its systems as basis of future definitions 183
Assessment of airframe-subsystems synergy on overall aircraft performance in a Collaborative Design 182
MARGARET: A PERSONAL TRANSPORTATION AIRCRAFT OF TOMORROW USED TODAY FOR COLLABORATION AMONG UNIVERSITIES 181
On-Board Systems Preliminary Sizing in an Overall Aircraft Design Environment 181
Possible hybrid propulsion configuration for transport jet aircraft 178
Methodology for the Safety and Reliability assessment of hypersonic transportation systems in conceptual design activities 178
The educational experience at Politecnico di Torino to develop and increase the capability in aircraft layout comprehension and definition 178
POSSIBLE HYBRID PROPULSION CONFIGURATION FOR TRANSPORT JET AIRCRAFT 174
PRELIMINARY DESIGN AND SIZING OF A CABIN ESCAPE SYSTEM FOR A SUBORBITAL VEHICLE AIMED AT PARABOLIC FLIGHTS 173
Collaborative systems driven aircraft configuration design optimization 170
A preliminary design study of maintenance and logistic infrastructure for MALE UAS 168
Una nuova applicazione per la simulazione in real-time 157
Preliminary design of a cabin escape system for a suborbital vehicle aimed at parabolic flights 157
INTEGRATED AEROSPACE SYSTEMS DESIGN COURSE: AN EDUCATIONAL EXPERIENCE AT POLITECNICO DI TORINO 124
A parametric cost model for estimating civil aircraft line and base maintenance 113
A virtual test bench of a parallel hybrid propulsion system for UAVs 102
AN EDUCATIONAL EXPERIENCE AT POLITECNICO DI TORINO TO STATE AND INCREASE CAPABILITY IN AIRCRAFT LAYOUT COMPREHENSION AND DEFINITION 97
A model-based rams estimation methodology for innovative aircraft on-board systems supporting mdo applications 89
Parametric approach to operating costs estimation for an innovative regional aircraft 78
Towards a methodology for new technologies assessment in aircraft operating cost 76
Method for Estimation of Electrical Wiring Interconnection Systems in Preliminary Aircraft Design 73
New methodology for flight control system sizing and hinge moment estimation 72
Environmental & flight control system architecture optimization from a family concept design perspective 71
Effect of Progressive Integration of On-Board Systems Design Discipline in an MDA Framework for Aircraft Design with Different Level of Systems Electrification 69
Design of the strut braced wing aircraft in the agile collaborative MDO framework 68
Integration of on-board systems preliminary design discipline within a collaborative 3rd generation MDO framework 66
ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES 65
Comparative Study of Advanced Turboprop Aircraft with Wing and Rear Mounted Propulsion System in the Agile EU project 65
Studies on propulsion and on-board systems matching in agile project distributed collaborative MDO environment applying for advanced regional and medium haul jet 60
Multiphase Drives for Hybrid-Electric Propulsion in Light Aircrafts: A Viable Solution 58
Design of hybrid electric heavy fuel MALE ISR UAV enabling technologies for military operations 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 55
Propulsion System for BWB Configurations in the Agile project 53
A Design Model for Electric Environmental Control System in Aircraft Conceptual and Preliminary Design 51
Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project 51
Innovative concepts of electric system architectures and hybrid propulsion system for regional turboprop aircraft 48
Preliminary Study on OBS Electrification Efficiency for Advanced Supersonic Business and Medium Jet with Unified Engines 41
Propulsion and On-Board System Integration for Advanced Regional Jet with Different Level of Electrification in the AGILE project 40
Advanced turboprop multidisciplinary design and optimization within agile project 40
Multidisciplinary aircraft integration within a collaborative and distributed design framework using the AGILE paradigm 38
Methodology for the automated preliminary certification of on-board systems architectures through requirements analysis 37
MBSE Certification-Driven Design of a UAV MALE Configuration in the AGILE 4.0 Design Environment 26
Stream Life Cycle Assessment Model for Aircraft Preliminary Design 24
ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT 23
Model-Based Mission Assurance/Model-Based Reliability, Availability, Maintainability, and Safety (RAMS) 22
Performance and Reliability Evaluation of Innovative High-Lift Devices for Aircraft Using Electromechanical Actuators 21
Multidisciplinary design of a more electric regional aircraft including certification constraints 21
Automated evaluation of performance, certification and maintenance aspects of aircraft on-board system architectures during preliminary design stages 17
Multidisciplinary Design and Optimization of Regional Jet Retrofitting Activity 16
Assessing the Integration of Electrified On-Board Systems in an MDAO framework for a small transport aircraft 15
Collaborative Design of a Business Jet Family Using the AGILE 4.0 MBSE Environment 15
A parametric model for thermal management system for more electric and hybrid aircraft 15
Streamlining cross-organizational aircraft development: Results from the agile project 12
null 12
Totale 17.651
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Categoria #
all - tutte 40.763
article - articoli 13.651
book - libri 694
conference - conferenze 23.586
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.832
Totale 81.526
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.459 0 0 0 208 190 156 128 232 220 125 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
2024/2025647 76 384 178 9 0 0 0 0 0 0 0 0
Totale 17.651