FIORITI, MARCO
 Distribuzione geografica
Continente #
EU - Europa 9.224
NA - Nord America 7.907
AS - Asia 3.316
SA - Sud America 390
AF - Africa 97
OC - Oceania 74
Continente sconosciuto - Info sul continente non disponibili 2
Totale 21.010
Nazione #
US - Stati Uniti d'America 7.776
IT - Italia 2.770
DE - Germania 1.845
CN - Cina 1.437
GB - Regno Unito 1.195
FR - Francia 1.136
SG - Singapore 814
UA - Ucraina 636
BR - Brasile 320
RU - Federazione Russa 297
KR - Corea 283
NL - Olanda 252
TR - Turchia 244
IE - Irlanda 219
SE - Svezia 172
CH - Svizzera 130
CA - Canada 117
AT - Austria 114
FI - Finlandia 99
HK - Hong Kong 98
IN - India 69
AU - Australia 68
BE - Belgio 67
VN - Vietnam 62
JP - Giappone 53
ID - Indonesia 51
ES - Italia 47
PL - Polonia 47
ZA - Sudafrica 47
IR - Iran 36
TW - Taiwan 33
MY - Malesia 27
GR - Grecia 23
IL - Israele 22
BD - Bangladesh 17
SA - Arabia Saudita 16
UZ - Uzbekistan 16
AR - Argentina 15
IQ - Iraq 13
RO - Romania 12
CL - Cile 11
EC - Ecuador 11
EU - Europa 11
JO - Giordania 11
PT - Portogallo 11
BG - Bulgaria 10
BY - Bielorussia 10
LV - Lettonia 10
DZ - Algeria 9
HU - Ungheria 9
LT - Lituania 9
LU - Lussemburgo 9
NG - Nigeria 9
PE - Perù 9
PK - Pakistan 9
CZ - Repubblica Ceca 8
MA - Marocco 8
MX - Messico 8
AE - Emirati Arabi Uniti 7
CO - Colombia 7
NO - Norvegia 7
PY - Paraguay 7
NZ - Nuova Zelanda 6
PH - Filippine 6
TH - Thailandia 6
HR - Croazia 5
KZ - Kazakistan 5
RS - Serbia 5
VE - Venezuela 5
AL - Albania 4
CI - Costa d'Avorio 4
EG - Egitto 4
KW - Kuwait 4
NP - Nepal 4
UY - Uruguay 4
AM - Armenia 3
AP - ???statistics.table.value.countryCode.AP??? 3
EE - Estonia 3
ET - Etiopia 3
ME - Montenegro 3
PA - Panama 3
BW - Botswana 2
DK - Danimarca 2
KE - Kenya 2
LK - Sri Lanka 2
MD - Moldavia 2
NA - Namibia 2
SN - Senegal 2
TJ - Tagikistan 2
BH - Bahrain 1
BN - Brunei Darussalam 1
BO - Bolivia 1
CD - Congo 1
CR - Costa Rica 1
DO - Repubblica Dominicana 1
GT - Guatemala 1
KG - Kirghizistan 1
KH - Cambogia 1
OM - Oman 1
PS - Palestinian Territory 1
Totale 21.002
Città #
Ashburn 1.874
Southend 943
Turin 619
Fairfield 504
Seattle 477
Singapore 394
Chandler 392
Beijing 344
Princeton 280
Boardman 276
Woodbridge 235
Houston 232
Santa Clara 213
Ann Arbor 210
Dublin 208
Dallas 206
Wilmington 200
Jacksonville 192
Hangzhou 191
Torino 191
Berlin 177
Cambridge 175
Milan 173
San Ramon 151
Izmir 129
Shanghai 125
Buffalo 115
Bern 97
Rome 87
San Donato Milanese 86
Helsinki 77
Council Bluffs 75
Munich 75
Seoul 75
Hamburg 73
Bologna 71
Vienna 70
Zhengzhou 67
Frankfurt 62
Brussels 60
Hong Kong 60
Frankfurt am Main 57
Falls Church 56
Saint Petersburg 55
Chicago 54
Los Angeles 54
Herkenbosch 51
Zaporozhye 51
Boise 49
Amsterdam 45
Katy 44
San Francisco 44
Redwood City 43
Putian 42
Moscow 41
Luft 40
Jakarta 39
Baltimore 35
Fremont 35
Istanbul 35
Paris 35
Guangzhou 32
Las Vegas 31
Pennsylvania Furnace 31
Ho Chi Minh City 29
Monopoli 29
Toronto 29
Xian 29
Aachen 28
Melbourne 28
Padua 28
Delft 27
Des Moines 26
Naples 26
Kiev 25
Malatya 25
Gilroy 24
Piscataway 24
Shenzhen 24
Fuzhou 23
Montreal 23
New York 23
Ottawa 23
São Paulo 23
Tokyo 23
Hefei 22
London 22
Nanjing 22
Nuremberg 21
Mountain View 20
San Antonio 20
Ankara 19
Johannesburg 19
The Dalles 18
Venaria Reale 18
Atlanta 17
Cadoneghe 17
Columbus 17
Denver 17
Genoa 17
Totale 12.085
Nome #
ASTRID - AIRCRAFT ON BOARD SYSTEMS SIZING AND TRADE-OFF ANALYSIS IN INITIAL DESIGN 1.099
Functional Analysis in Systems Engineering: methodology and applications 1.016
ASTRID - aircraft on board systems sizing and trade-off analysis in initial design 750
Collaborative System of Systems Multidisciplinary Design Optimization for Civil Aircraft:AGILE EU project 496
Rational and affordable concepts of Landing Gear for small reentry vehicle demonstrators 478
UAV Logistic Support Definition 472
About Feasibility of a 5th generation Light Fighter Aircraft 464
A Computer Method to Develop and Validate on board Subsystem's Control Laws 464
Development and Validation of on-board systems control laws 454
Trade off studies of hybrid-electric aircraft by Fuzzy logic methodology 454
Diesel Engine Application on AEW&C Turboprop Effectiveness-Cost Assessment 436
Automated Selection of the Optimal On-board Systems Architecture within MDO Collaborative Environment 435
Hypothesis for Hypersonic Flight development 409
About Feasibility of 5th Generation Light Fighter Aircraft 362
An Alenia Aermacchi study and experience on MBSE application 331
Innovative solutions for light, very light and unmanned aircraft Preliminary design and Life Cycle Cost estimation 317
IMPACTS OF A PROGNOSTICS AND HEALTH MANAGEMENT SYSTEM ON AIRCRAFT FLEET OPERATING COST DURING CONCEPTUAL DESIGN PHASE BY USING PARAMETRIC ESTIMATION 317
UAV BASED ADVANCED MONITORING SYSTEM: FLEET AND LOGISTIC SYSTEM SIZING BY OBJECT BASED MODEL AND MONTE-CARLO SIMULATION 310
STATUS AND PERSPECTIVES OF HYPERSONIC SYSTEMS AND TECHNOLOGIES WITH EMPHASIS ON THE ROLE OF SUB-ORBITAL FLIGHT 305
Adaptable conceptual aircraft design model 289
Preliminary Sub-Systems Design Integrated in a Multidisciplinary Design Optimization Framework 289
Guided procedure for the Zonal Safety Analysis in aircraft preliminary design 288
Zonal safety analysis in aircraft conceptual design: application to SAvE aircraft 280
Academic Course in Aircraft conceptual design and on-board systems preliminary design at Politecnico di Torino 274
Design of all electric secondary power system for future advanced MALE UAV 266
Methodology for an integrated definition of a system and its subsystems: the case-study of an airplane and its subsystems 265
CONTRIBUTIONS FROM EDUCATIONAL ACTIVITIES TO RESEARCHES ABOUT HYBRID PROPULSION OPPORTUNITIES FOR LIGHT AIRCAFT 258
SUPPORT AND MAINTENANCE STRATEGIES FOR FUTURE, INNOVATIVE AND LARGELY WIDESPREAD AIR PERSONAL TRANSPORTATION SYSTEMS 258
Contribution To R.A.M.S estimation in early design phases of unmanned aerial vehicles - UAVs 254
Development of a new conceptual design methodology for parallel hybrid aircraft 248
Hybrid configuration – Advanced A.P.U. concept for future turboprop 246
The Effect of Sub-systems Design Parameters on Preliminary Aircraft Design in a Multidisciplinary Design Environment 242
Sulla previsione di costi, sicurezza, affidabilità e entità della manutenzione in avamprogetto 229
Virtual and flying models for aircraft development 229
Volo ipersonico per l’accesso allo Spazio: passato, presente e futuro 229
Future-oriented C4ISTAR applications. UAS versus manned aircraft. Merit analysis to consider performance/cost aspects 229
All electric Secondary Power System for future advancedMALE UAV 227
Cost-Estimating Model for Aircraft Maintenance 222
MALE UAV and its systems as basis of future definitions 221
Support and Maintenance Strategies for Future, Innovative and Largely Widespread Air Personal Transportation Systems 217
Work-in-progress: European platform for innovation and collaboration between engineer students (EPICES) 216
Regional turboprop conversion for AEW&C purposes supposing auxiliary engine installation – Technical and economical analysis 210
MARGARET: A PERSONAL TRANSPORTATION AIRCRAFT OF TOMORROW USED TODAY FOR COLLABORATION AMONG UNIVERSITIES 209
Possible hybrid propulsion configuration for transport jet aircraft 209
Methodology for the Safety and Reliability assessment of hypersonic transportation systems in conceptual design activities 208
The educational experience at Politecnico di Torino to develop and increase the capability in aircraft layout comprehension and definition 201
POSSIBLE HYBRID PROPULSION CONFIGURATION FOR TRANSPORT JET AIRCRAFT 200
Ultra Light Aircraft: New concepts under study at Politecnico di Torino 199
PRELIMINARY DESIGN AND SIZING OF A CABIN ESCAPE SYSTEM FOR A SUBORBITAL VEHICLE AIMED AT PARABOLIC FLIGHTS 199
Assessment of airframe-subsystems synergy on overall aircraft performance in a Collaborative Design 198
On-Board Systems Preliminary Sizing in an Overall Aircraft Design Environment 196
A preliminary design study of maintenance and logistic infrastructure for MALE UAS 189
Collaborative systems driven aircraft configuration design optimization 188
Preliminary design of a cabin escape system for a suborbital vehicle aimed at parabolic flights 182
A parametric cost model for estimating civil aircraft line and base maintenance 178
Una nuova applicazione per la simulazione in real-time 175
INTEGRATED AEROSPACE SYSTEMS DESIGN COURSE: AN EDUCATIONAL EXPERIENCE AT POLITECNICO DI TORINO 137
A virtual test bench of a parallel hybrid propulsion system for UAVs 132
A model-based rams estimation methodology for innovative aircraft on-board systems supporting mdo applications 124
AN EDUCATIONAL EXPERIENCE AT POLITECNICO DI TORINO TO STATE AND INCREASE CAPABILITY IN AIRCRAFT LAYOUT COMPREHENSION AND DEFINITION 123
ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES 122
New methodology for flight control system sizing and hinge moment estimation 119
Towards a methodology for new technologies assessment in aircraft operating cost 116
Comparative Analysis of Machine Learning Algorithms for Heat Exchangers Diagnosis in Electrified Aircraft 115
Environmental & flight control system architecture optimization from a family concept design perspective 110
Parametric approach to operating costs estimation for an innovative regional aircraft 109
Method for Estimation of Electrical Wiring Interconnection Systems in Preliminary Aircraft Design 105
Effect of Progressive Integration of On-Board Systems Design Discipline in an MDA Framework for Aircraft Design with Different Level of Systems Electrification 104
Integration of on-board systems preliminary design discipline within a collaborative 3rd generation MDO framework 94
Performance and Reliability Evaluation of Innovative High-Lift Devices for Aircraft Using Electromechanical Actuators 92
Design of the strut braced wing aircraft in the agile collaborative MDO framework 90
A Design Model for Electric Environmental Control System in Aircraft Conceptual and Preliminary Design 88
Studies on propulsion and on-board systems matching in agile project distributed collaborative MDO environment applying for advanced regional and medium haul jet 87
Comparative Study of Advanced Turboprop Aircraft with Wing and Rear Mounted Propulsion System in the Agile EU project 87
Multidisciplinary aircraft integration within a collaborative and distributed design framework using the AGILE paradigm 86
Methodology for the automated preliminary certification of on-board systems architectures through requirements analysis 83
Design of hybrid electric heavy fuel MALE ISR UAV enabling technologies for military operations 82
Multiphase Drives for Hybrid-Electric Propulsion in Light Aircrafts: A Viable Solution 81
ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT 78
Innovative concepts of electric system architectures and hybrid propulsion system for regional turboprop aircraft 78
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 78
Stream Life Cycle Assessment Model for Aircraft Preliminary Design 77
A parametric model for thermal management system for more electric and hybrid aircraft 77
Automated evaluation of performance, certification and maintenance aspects of aircraft on-board system architectures during preliminary design stages 76
Propulsion System for BWB Configurations in the Agile project 75
Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project 70
MBSE Certification-Driven Design of a UAV MALE Configuration in the AGILE 4.0 Design Environment 68
Preliminary Study on OBS Electrification Efficiency for Advanced Supersonic Business and Medium Jet with Unified Engines 68
Advanced turboprop multidisciplinary design and optimization within agile project 65
Propulsion and On-Board System Integration for Advanced Regional Jet with Different Level of Electrification in the AGILE project 61
Assessing the Integration of Electrified On-Board Systems in an MDAO framework for a small transport aircraft 58
Multidisciplinary design of a more electric regional aircraft including certification constraints 58
Collaborative Design of a Business Jet Family Using the AGILE 4.0 MBSE Environment 57
Model-Based Mission Assurance/Model-Based Reliability, Availability, Maintainability, and Safety (RAMS) 57
Automated generation of aircraft on-board system architectures and filtering through certification specification requirements 47
Multidisciplinary Design and Optimization of Regional Jet Retrofitting Activity 45
Streamlining cross-organizational aircraft development: Results from the agile project 33
Totale 21.298
Categoria #
all - tutte 53.458
article - articoli 17.904
book - libri 766
conference - conferenze 31.052
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 3.736
Totale 106.916


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.204 0 0 0 231 158 206 114 108 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
2024/20252.965 76 384 178 302 272 237 140 161 513 174 236 292
2025/20261.329 452 366 454 57 0 0 0 0 0 0 0 0
Totale 21.298