FIORITI, MARCO
 Distribuzione geografica
Continente #
EU - Europa 10.537
NA - Nord America 10.401
AS - Asia 6.609
SA - Sud America 569
Continente sconosciuto - Info sul continente non disponibili 298
AF - Africa 148
OC - Oceania 86
Totale 28.648
Nazione #
US - Stati Uniti d'America 10.105
IT - Italia 3.128
DE - Germania 1.939
SG - Singapore 1.800
CN - Cina 1.710
FR - Francia 1.481
VN - Vietnam 1.303
GB - Regno Unito 1.253
UA - Ucraina 639
RU - Federazione Russa 605
BR - Brasile 426
KR - Corea 400
NL - Olanda 306
TR - Turchia 262
HK - Hong Kong 257
IE - Irlanda 232
CA - Canada 198
IN - India 189
SE - Svezia 178
BD - Bangladesh 150
CH - Svizzera 133
FI - Finlandia 119
AT - Austria 116
JP - Giappone 90
AU - Australia 78
BE - Belgio 71
ID - Indonesia 70
ZA - Sudafrica 65
ES - Italia 58
TW - Taiwan 56
PL - Polonia 53
PH - Filippine 47
TH - Thailandia 42
AR - Argentina 40
MY - Malesia 38
IR - Iran 36
IQ - Iraq 35
MX - Messico 31
GR - Grecia 23
UZ - Uzbekistan 23
IL - Israele 22
CL - Cile 21
EC - Ecuador 20
PK - Pakistan 19
PT - Portogallo 19
SA - Arabia Saudita 19
JO - Giordania 16
MA - Marocco 15
AE - Emirati Arabi Uniti 14
CR - Costa Rica 14
DZ - Algeria 14
PE - Perù 14
RO - Romania 14
CO - Colombia 12
HU - Ungheria 12
JM - Giamaica 12
LT - Lituania 12
LV - Lettonia 12
PY - Paraguay 12
BG - Bulgaria 11
EU - Europa 11
VE - Venezuela 11
BY - Bielorussia 10
LU - Lussemburgo 10
NO - Norvegia 10
CZ - Repubblica Ceca 9
NG - Nigeria 9
UY - Uruguay 9
NP - Nepal 8
EG - Egitto 7
HN - Honduras 7
KE - Kenya 7
NZ - Nuova Zelanda 7
TT - Trinidad e Tobago 7
AL - Albania 6
KW - Kuwait 6
AM - Armenia 5
CI - Costa d'Avorio 5
HR - Croazia 5
KZ - Kazakistan 5
NI - Nicaragua 5
RS - Serbia 5
AZ - Azerbaigian 4
EE - Estonia 4
ET - Etiopia 4
GT - Guatemala 4
PA - Panama 4
AP - ???statistics.table.value.countryCode.AP??? 3
BB - Barbados 3
BH - Bahrain 3
BO - Bolivia 3
DK - Danimarca 3
GE - Georgia 3
ME - Montenegro 3
OM - Oman 3
PR - Porto Rico 3
SC - Seychelles 3
SN - Senegal 3
SV - El Salvador 3
TN - Tunisia 3
Totale 28.312
Città #
Ashburn 2.353
Singapore 990
Southend 943
Turin 716
San Jose 673
Fairfield 504
Seattle 481
Chandler 392
Beijing 390
Ho Chi Minh City 364
Hanoi 321
Boardman 288
Princeton 280
Santa Clara 275
Dallas 235
Houston 235
Woodbridge 235
Dublin 220
Milan 219
Ann Arbor 210
Wilmington 201
Hangzhou 196
Jacksonville 193
Torino 191
Berlin 177
Cambridge 176
Hong Kong 168
Council Bluffs 165
Seoul 163
Los Angeles 157
San Ramon 151
Shanghai 136
Buffalo 131
Izmir 129
Lauterbourg 115
Frankfurt am Main 107
Rome 106
Chicago 99
Bern 97
Helsinki 90
San Donato Milanese 86
Munich 81
Bologna 76
Hamburg 75
Vienna 72
Zhengzhou 69
Frankfurt 62
Brussels 60
New York 60
San Francisco 60
Amsterdam 59
Falls Church 56
North Bergen 55
Saint Petersburg 55
Da Nang 54
Herkenbosch 51
Moscow 51
Zaporozhye 51
Boise 49
Haiphong 47
Tokyo 47
Paris 45
Katy 44
Montreal 44
Redwood City 43
Toronto 43
Putian 42
Jakarta 41
Luft 40
Istanbul 39
Baltimore 38
Fremont 36
Guangzhou 35
Naples 35
Las Vegas 34
Shenzhen 34
São Paulo 34
Des Moines 33
London 32
Padua 32
Pennsylvania Furnace 31
Phoenix 30
Arlington 29
Delft 29
Melbourne 29
Monopoli 29
Xian 29
Aachen 28
Nuremberg 26
Kiev 25
Malatya 25
Nanjing 25
Piscataway 25
Gilroy 24
Atlanta 23
Fuzhou 23
Genoa 23
Ottawa 23
San Antonio 23
Sydney 23
Totale 15.794
Nome #
ASTRID - AIRCRAFT ON BOARD SYSTEMS SIZING AND TRADE-OFF ANALYSIS IN INITIAL DESIGN 1.308
Functional Analysis in Systems Engineering: methodology and applications 1.289
ASTRID - aircraft on board systems sizing and trade-off analysis in initial design 810
Collaborative System of Systems Multidisciplinary Design Optimization for Civil Aircraft:AGILE EU project 592
About Feasibility of a 5th generation Light Fighter Aircraft 572
Rational and affordable concepts of Landing Gear for small reentry vehicle demonstrators 553
Development and Validation of on-board systems control laws 544
UAV Logistic Support Definition 541
Automated Selection of the Optimal On-board Systems Architecture within MDO Collaborative Environment 527
A Computer Method to Develop and Validate on board Subsystem's Control Laws 526
Trade off studies of hybrid-electric aircraft by Fuzzy logic methodology 518
Hypothesis for Hypersonic Flight development 513
Diesel Engine Application on AEW&C Turboprop Effectiveness-Cost Assessment 502
About Feasibility of 5th Generation Light Fighter Aircraft 425
An Alenia Aermacchi study and experience on MBSE application 407
IMPACTS OF A PROGNOSTICS AND HEALTH MANAGEMENT SYSTEM ON AIRCRAFT FLEET OPERATING COST DURING CONCEPTUAL DESIGN PHASE BY USING PARAMETRIC ESTIMATION 383
UAV BASED ADVANCED MONITORING SYSTEM: FLEET AND LOGISTIC SYSTEM SIZING BY OBJECT BASED MODEL AND MONTE-CARLO SIMULATION 381
Innovative solutions for light, very light and unmanned aircraft Preliminary design and Life Cycle Cost estimation 369
STATUS AND PERSPECTIVES OF HYPERSONIC SYSTEMS AND TECHNOLOGIES WITH EMPHASIS ON THE ROLE OF SUB-ORBITAL FLIGHT 355
Hybrid configuration – Advanced A.P.U. concept for future turboprop 344
Adaptable conceptual aircraft design model 341
Cost-Estimating Model for Aircraft Maintenance 335
Preliminary Sub-Systems Design Integrated in a Multidisciplinary Design Optimization Framework 330
Guided procedure for the Zonal Safety Analysis in aircraft preliminary design 328
Academic Course in Aircraft conceptual design and on-board systems preliminary design at Politecnico di Torino 325
Contribution To R.A.M.S estimation in early design phases of unmanned aerial vehicles - UAVs 324
Development of a new conceptual design methodology for parallel hybrid aircraft 320
Methodology for an integrated definition of a system and its subsystems: the case-study of an airplane and its subsystems 319
Zonal safety analysis in aircraft conceptual design: application to SAvE aircraft 314
CONTRIBUTIONS FROM EDUCATIONAL ACTIVITIES TO RESEARCHES ABOUT HYBRID PROPULSION OPPORTUNITIES FOR LIGHT AIRCAFT 314
SUPPORT AND MAINTENANCE STRATEGIES FOR FUTURE, INNOVATIVE AND LARGELY WIDESPREAD AIR PERSONAL TRANSPORTATION SYSTEMS 314
Design of all electric secondary power system for future advanced MALE UAV 309
The Effect of Sub-systems Design Parameters on Preliminary Aircraft Design in a Multidisciplinary Design Environment 300
Volo ipersonico per l’accesso allo Spazio: passato, presente e futuro 283
Future-oriented C4ISTAR applications. UAS versus manned aircraft. Merit analysis to consider performance/cost aspects 283
All electric Secondary Power System for future advancedMALE UAV 280
Collaborative systems driven aircraft configuration design optimization 278
MALE UAV and its systems as basis of future definitions 275
Virtual and flying models for aircraft development 274
A parametric cost model for estimating civil aircraft line and base maintenance 274
Possible hybrid propulsion configuration for transport jet aircraft 271
PRELIMINARY DESIGN AND SIZING OF A CABIN ESCAPE SYSTEM FOR A SUBORBITAL VEHICLE AIMED AT PARABOLIC FLIGHTS 270
Support and Maintenance Strategies for Future, Innovative and Largely Widespread Air Personal Transportation Systems 268
Sulla previsione di costi, sicurezza, affidabilità e entità della manutenzione in avamprogetto 267
MARGARET: A PERSONAL TRANSPORTATION AIRCRAFT OF TOMORROW USED TODAY FOR COLLABORATION AMONG UNIVERSITIES 265
Methodology for the Safety and Reliability assessment of hypersonic transportation systems in conceptual design activities 265
On-Board Systems Preliminary Sizing in an Overall Aircraft Design Environment 263
POSSIBLE HYBRID PROPULSION CONFIGURATION FOR TRANSPORT JET AIRCRAFT 262
Regional turboprop conversion for AEW&C purposes supposing auxiliary engine installation – Technical and economical analysis 261
Work-in-progress: European platform for innovation and collaboration between engineer students (EPICES) 260
Assessment of airframe-subsystems synergy on overall aircraft performance in a Collaborative Design 256
A preliminary design study of maintenance and logistic infrastructure for MALE UAS 249
The educational experience at Politecnico di Torino to develop and increase the capability in aircraft layout comprehension and definition 247
Ultra Light Aircraft: New concepts under study at Politecnico di Torino 241
Effect of Progressive Integration of On-Board Systems Design Discipline in an MDA Framework for Aircraft Design with Different Level of Systems Electrification 237
Preliminary design of a cabin escape system for a suborbital vehicle aimed at parabolic flights 236
Comparative Analysis of Machine Learning Algorithms for Heat Exchangers Diagnosis in Electrified Aircraft 231
ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES 229
A model-based rams estimation methodology for innovative aircraft on-board systems supporting mdo applications 216
Multidisciplinary aircraft integration within a collaborative and distributed design framework using the AGILE paradigm 215
Una nuova applicazione per la simulazione in real-time 211
AN EDUCATIONAL EXPERIENCE AT POLITECNICO DI TORINO TO STATE AND INCREASE CAPABILITY IN AIRCRAFT LAYOUT COMPREHENSION AND DEFINITION 209
Automated evaluation of performance, certification and maintenance aspects of aircraft on-board system architectures during preliminary design stages 199
New methodology for flight control system sizing and hinge moment estimation 196
Parametric approach to operating costs estimation for an innovative regional aircraft 194
Environmental & flight control system architecture optimization from a family concept design perspective 194
Methodology for the automated preliminary certification of on-board systems architectures through requirements analysis 193
INTEGRATED AEROSPACE SYSTEMS DESIGN COURSE: AN EDUCATIONAL EXPERIENCE AT POLITECNICO DI TORINO 193
Design of hybrid electric heavy fuel MALE ISR UAV enabling technologies for military operations 193
Performance and Reliability Evaluation of Innovative High-Lift Devices for Aircraft Using Electromechanical Actuators 185
Studies on propulsion and on-board systems matching in agile project distributed collaborative MDO environment applying for advanced regional and medium haul jet 185
A virtual test bench of a parallel hybrid propulsion system for UAVs 185
Towards a methodology for new technologies assessment in aircraft operating cost 183
Method for Estimation of Electrical Wiring Interconnection Systems in Preliminary Aircraft Design 177
Stream Life Cycle Assessment Model for Aircraft Preliminary Design 172
Integration of on-board systems preliminary design discipline within a collaborative 3rd generation MDO framework 172
Comparative Study of Advanced Turboprop Aircraft with Wing and Rear Mounted Propulsion System in the Agile EU project 165
A parametric model for thermal management system for more electric and hybrid aircraft 165
Design of the strut braced wing aircraft in the agile collaborative MDO framework 150
ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT 147
Propulsion System for BWB Configurations in the Agile project 146
Assessing the Integration of Electrified On-Board Systems in an MDAO framework for a small transport aircraft 144
A Design Model for Electric Environmental Control System in Aircraft Conceptual and Preliminary Design 144
MBSE Certification-Driven Design of a UAV MALE Configuration in the AGILE 4.0 Design Environment 140
Advanced turboprop multidisciplinary design and optimization within agile project 139
Collaborative Design of a Business Jet Family Using the AGILE 4.0 MBSE Environment 136
Multiphase Drives for Hybrid-Electric Propulsion in Light Aircrafts: A Viable Solution 135
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 134
Streamlining cross-organizational aircraft development: Results from the agile project 129
Model-Based Mission Assurance/Model-Based Reliability, Availability, Maintainability, and Safety (RAMS) 127
Preliminary Study on OBS Electrification Efficiency for Advanced Supersonic Business and Medium Jet with Unified Engines 127
Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project 121
Propulsion and On-Board System Integration for Advanced Regional Jet with Different Level of Electrification in the AGILE project 119
Multidisciplinary design of a more electric regional aircraft including certification constraints 119
Multidisciplinary Design and Optimization of Regional Jet Retrofitting Activity 118
Innovative concepts of electric system architectures and hybrid propulsion system for regional turboprop aircraft 117
Automated generation of aircraft on-board system architectures and filtering through certification specification requirements 111
Modulization and Simulation of Thermal Management System Based on Pumped Two-Phase Loop for Hybrid-Electric Aircraft 95
A SysML-based framework towards EASA CS-23 digitalization: An MBSE approach 91
Totale 28.648
Categoria #
all - tutte 70.704
article - articoli 23.994
book - libri 889
conference - conferenze 41.086
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 4.735
Totale 141.408


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022942 0 0 0 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
2025/20267.334 452 366 454 508 522 526 1.015 557 1.557 736 309 332
2026/20271.345 241 323 553 228 0 0 0 0 0 0 0 0
Totale 28.648