PORTO @ Archivio Istituzionale della Ricerca

CESTINO, ENRICO
 Distribuzione geografica
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Continente #
EU - Europa 16.844
NA - Nord America 16.227
AS - Asia 15.027
SA - Sud America 924
AF - Africa 178
OC - Oceania 89
Continente sconosciuto - Info sul continente non disponibili 8
-- - ???statistics.table.value.continent.--??? 2
Totale 49.299
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Nazione #
US - Stati Uniti d'America 15.782
CN - Cina 6.618
IT - Italia 5.369
SG - Singapore 2.936
DE - Germania 2.700
GB - Regno Unito 2.683
VN - Vietnam 2.279
FR - Francia 1.640
RU - Federazione Russa 1.186
UA - Ucraina 825
KR - Corea 767
BR - Brasile 655
HK - Hong Kong 541
TR - Turchia 459
IN - India 419
NL - Olanda 410
CA - Canada 369
IE - Irlanda 332
SE - Svezia 314
CH - Svizzera 256
FI - Finlandia 233
BE - Belgio 185
JP - Giappone 152
AR - Argentina 143
AT - Austria 129
TH - Thailandia 102
MY - Malesia 96
ID - Indonesia 90
RO - Romania 88
PH - Filippine 84
AU - Australia 81
ES - Italia 80
IR - Iran 76
PL - Polonia 70
TW - Taiwan 65
BD - Bangladesh 64
IQ - Iraq 54
MX - Messico 52
PT - Portogallo 49
PK - Pakistan 46
BG - Bulgaria 36
CL - Cile 36
IL - Israele 36
RS - Serbia 32
ZA - Sudafrica 32
SA - Arabia Saudita 29
AP - ???statistics.table.value.countryCode.AP??? 28
EU - Europa 27
CZ - Repubblica Ceca 25
CO - Colombia 24
EG - Egitto 23
AE - Emirati Arabi Uniti 21
ET - Etiopia 21
JO - Giordania 21
EC - Ecuador 19
MA - Marocco 18
UZ - Uzbekistan 18
VE - Venezuela 17
SI - Slovenia 16
LT - Lituania 15
NG - Nigeria 15
NP - Nepal 15
DZ - Algeria 13
HR - Croazia 13
PE - Perù 12
TN - Tunisia 12
SY - Repubblica araba siriana 11
KZ - Kazakistan 10
AM - Armenia 8
BY - Bielorussia 8
DK - Danimarca 8
KE - Kenya 8
AL - Albania 7
CI - Costa d'Avorio 7
EE - Estonia 7
GR - Grecia 7
HU - Ungheria 7
MD - Moldavia 7
NZ - Nuova Zelanda 7
PY - Paraguay 7
LB - Libano 6
SN - Senegal 6
A2 - ???statistics.table.value.countryCode.A2??? 5
AZ - Azerbaigian 5
CR - Costa Rica 5
NO - Norvegia 5
UY - Uruguay 5
GE - Georgia 4
GH - Ghana 4
KH - Cambogia 4
KW - Kuwait 4
OM - Oman 4
QA - Qatar 4
SC - Seychelles 4
SK - Slovacchia (Repubblica Slovacca) 4
AO - Angola 3
BB - Barbados 3
BO - Bolivia 3
GA - Gabon 3
JM - Giamaica 3
Totale 49.246
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Città #
Zhengzhou 3.477
Ashburn 3.269
Southend 1.907
Singapore 1.731
Beijing 1.251
Turin 1.135
Chandler 1.020
Seattle 977
San Jose 853
Ho Chi Minh City 617
Council Bluffs 598
Hanoi 577
Des Moines 558
Fairfield 547
Princeton 491
Hong Kong 442
Santa Clara 417
Jacksonville 410
Munich 410
Seoul 336
Torino 324
Dublin 317
Berlin 316
Ann Arbor 314
Guangzhou 307
Houston 302
Milan 295
Woodbridge 272
San Ramon 266
Montréal 263
Boardman 260
Wilmington 254
Mcallen 253
Los Angeles 252
Izmir 251
Chicago 232
Shanghai 218
Cambridge 217
Bern 189
Lauterbourg 179
Dallas 177
Brussels 163
Rome 163
San Donato Milanese 151
Helsinki 149
Atlanta 134
Bologna 123
Hefei 118
Herkenbosch 116
Zaporozhye 106
Baltimore 102
Pennsylvania Furnace 94
Haiphong 93
Vienna 93
Saint Petersburg 89
Da Nang 86
New York 85
Buffalo 83
Fremont 81
Moscow 79
Overberg 77
Tokyo 75
Frankfurt am Main 69
Monopoli 68
Padua 67
Redwood City 63
Mountain View 60
São Paulo 60
Galati 59
Istanbul 59
London 59
Orem 59
Bangkok 57
Hangzhou 57
Tongling 57
Naples 56
Malatya 50
San Francisco 50
Paris 47
Amsterdam 44
Jakarta 44
Dearborn 43
Delft 42
Warsaw 40
Andover 38
Ankara 38
Chennai 37
Nanjing 36
Strambino 36
Lappeenranta 34
Sofia 34
Columbus 33
Frankfurt 32
Hải Dương 32
The Dalles 31
Turku 31
Alba 30
Genoa 30
Bari 28
Shenyang 28
Totale 30.479
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Nome #
ENFICA-FC: Design of transport aircraft powered by fuel cell & flight test of zero emission 2-seater aircraft powered by fuel cells fueled by hydrogen 1.733
HeliPlat: Design, Aerodynamic Structural Analysis of Long-Endurance Solar-Powered Stratospheric Platform 1.694
Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft 1.485
Analysis of slender thin-walled anisotropic box-beams including local stiffness and coupling effects 1.403
COSTRUZIONI AERONAUTICHE: Eserciziario minimo con soluzioni 1.084
Design and testing of a propeller for a two-seater aircraft powered by fuel cells 510
ALL ELECTRIC INTERCITY-AIRCRAFT DESIGN BASED ON FUEL CELL ENERGY SYSTEM 500
DESIGN AND OPTIMIZATION OF COMPOSITE VESSEL FOR HYDROGEN STORAGE SUBJECT TO INTERNAL PRESSURE & IN-FLIGHT LOADS 495
A Fuel Cell Based Propulsion System for General Aviation Aircraft: The ENFICA-FC Experience 490
Air Cooling of a Two-Seater Fuel Cells Powered Aircraft: Dynamic Modelling and Comparisons with Experiemtal Data 487
Engineering Method for Air-Cooling Design of Two-Seat Propeller-Driven Aircraft Powered by Fuel Cells 453
A Multi-objective Nonlinear Piezoaeroelastic Wing Solution for Energy Harvesting and Load Alleviation: Modeling and Simulation 449
Multi-objective optimization of the composite wing box of solar powered HALE UAV 447
Optimization of advanced composite wing box structures subjected to combined loads and impact 443
Delamination and fracture modeling techniques for shell composite structures in LS-DYNA 426
Modular Multifunctional Composite Structure for CubeSat Applications: Preliminary Design and Structural Analysis 422
Comparative Analysis of eVTOL, Drone, and Ground Transportation Systems for Emergency Delivery of Blood-Derived Medication 413
"A Review of UAV in the World. Design and Technology of Long Endurance UAV Powered by Solar Energy". Contract with Shenyang Aerospace University, China 410
Structural Uncertainty Effect on Classical Wing Flutter Characteristics 404
Development of an Aeroelastic Wing model with piezoelectric elements for gust load alleviation and Energy Harvesting 384
Design and Optimization of a Composite Vessel for Hydrogen Storage Subject to Internal Pressure and In-Flight Loads for UAVs 378
More/All electric aircraft based on fuel cell energy system: the ENFICA-FC experience 376
L_1 adaptive flutter suppression control strategy for highly flexible structure 375
"Preliminary Design of HALE-UAV Configuration for 6 Months Endurance by In-House Developed Software". Contract with Shenyang Aerospace University, China 371
A Fuel Cell Based Propulsion System for General Aviation Aircraft: The ENFICA-FC Experience 367
Stability and Control of a High-Altitude-Long-Endurance UAV 365
Design of inter-city transport aircraft powered by fuel cell & flight test of zero emission 2-seater aircraft powered by fuel cells 354
ℒ1 Adaptive Flutter Suppression Control Strategy for Highly Flexible Structure 353
Innovative Aircraft Aeroelastic Modelling and Control 352
Numerical/experimental evaluation of buckling behaviour and residual tensile strength of composite aerospace structures after low velocity impact 347
UAV ad Energia Solare per Sorveglianza del Territorio e per Telerilevamento 344
Impact of lift propeller drag on the performance of eVTOL lift+cruise aircraft 341
Energy harvesting from aeroelastic vibrations induced by discrete gust loads 340
Design, manufacturing and testing of a HALE-UAV structural demonstrator 339
HELIPLAT®: Detail Design & Manufacturing of a Scaled Prototype for High Altitude Very-Long Endurance Solar-Powered RPAS 337
Very-Long Endurance Solar Powered Autonomous Stratospheric (Vespas) Air Vehicles For Sea Border Surveillance; Anti-Illegal Immigration And Gmes Applications 336
Experimental Slender Wing Model Design by the Application of Aeroelastic Scaling Laws 328
A REDUCED ORDER MODEL TO ESTIMATING PROPELLER/WING INTERACTION IN SOLAR POWERED AIRCRAFT PRELIMINARY DESIGN 325
Velivolo Elettrico con Potenza da Celle a Combustibile ad Idrogeno ad Inquinamento Zero 320
Very-long endurance solar powered autonomous UAVS: role and constraints for GMES applications 319
Design of solar high altitude long endurance aircraft for multi payload & operations 318
Parametric analysis of a fluttering piezoelectric wing 313
Topology Synthesis of Planar Ground Structures for Energy Harvesting Applications 308
Team-Based Learning in Aerospace Engineering Education: Fostering Collaboration, Inclusivity, and long-term Knowledge Retention 306
Design, Analysis and Experimental Testing of a Morphing Wing 306
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 306
Environmental Friendly Inter-City Aircraft (ENFICA-FC) and Preliminary Analysis for 2-seat aircraft conversion into Fuel Cells Powered Innovative System 305
ENFICA-FC: Design of Transport Aircraft Powered by Fuel Cell & Flight Test of Zero Emission 2-Seater Aircraft Powered By Fuel Cells fuelled by Hydrogen 302
Improved Multibody Model of Flexible Wing 301
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 300
Critical Behaviour of Slender Wing Configurations 297
Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems 292
Nonlinear LCO “amplitude-Frequency”Characteristics for Plates Fluttering at Supersonic Speeds 289
Piezo-Aeroelastic modeling and flutter prediction of flexible composite wings 287
HELIPLAT®: a high altitude very-long endurance solar powered platform for border patrol and forest fire detection 287
Design of high-altitude long-endurance solar-powered unmanned air vehicle for multi-payload and operations 282
Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams 276
Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings 274
ENFICA-FC: Environmental Friendly Inter-City Aircraft and 2-seat aircraft powered by Fuel Cells electric propulsion 273
Generalized topology for resonators having N commensurate harmonics 273
Constrained combinatorial optimization of multi-layered composite structures by means of Stud GA with proportionate selection and extinction 271
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 270
Hydrogen and Fuel Cell Project 268
Considerations on beam-wise structural models used for aeroelastic analysis of slender wings 268
EQUIVALENT PLATE MODEL OF CURVILINEAR STIFFENED PANELS 266
Design of a multifunctional composite structure for modular CubeSat applications 266
Final Analytical Data of the Aerodynamics Performance of Wing Profiles and Propellers for Low Reynolds Numbers 264
Low weight advanced composite primary structure design of platform 263
When fuel cells fly 259
Scaled size prototype assembling 248
A Possible Adaptive Wing Apparatus for New UAV Configurations 246
SHAMPO: Solar HALE aircraft for multi-payload & operations 245
RAPID200-FC, Flight Test of First All Electric Propulsion Aeroplane Powered by Fuel Cells 242
The Influence of Supersonic Stream on the Dependence “Amplitude-Frequency” of Nonlinear Vibrations of Flexible Plate 239
Safety Assessment of Pharmaceutical Distribution in a Hospital Environment 237
"The use of Vsaero CFD tool in the UAV Aero-dynamic project". 236
Aeroelastic scaling laws with considerations to the design of an experimental slender wing model 234
ENFICA-FC: All-electric aircraft Powered by Fuel Cells 233
“Virtual Design of UAV-VESPA for Mediterranean Sea Border Surveillance” 233
Experimental Data of High Efficiency Wing Profiles and Propellers for Low Reynolds Numbers 233
Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings 233
Configuration and Estimation Cost of the flying platform HeliPlat® 232
Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs 232
“Airfoil Geometry of Optimal Propeller for the Rapid 200-FC” 231
"HALE UAV Solar Configuration: Reliability, Maintainability and Safety" 226
Experimental buckling behavior of composite aerospace structures after low velocity impact 225
Analysis of slender thin-walled composite box-beams including local stiffness and coupling effects 225
"HALE UAV Modular Configuration: Reliability and Safety" 224
Critical Aeroelastic Behaviour of Slender Composite Wings in an Incompressible Flow 224
HALE UAV Modular Configuration: Structure Analysis (FEM). Final Report 223
Progetto S55 Replica 223
Graph-based element removal method for topology synthesis of beam based ground structures 220
"CAPECON HALE UAV: Solar, Modular Configuration design " 220
Una storia moderna 217
Coupled thermo-mechanical numerical modelling of carbon fibre reinforced composites impacted with different projectile configurations 216
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 215
Modular Multifunctional Composite Structure for CubeSat Applications: Embedded Battery Prototype Thermal Analysis 212
A Nonlinear Beam Finite Element with Bending–Torsion Coupling Formulation for Dynamic Analysis with Geometric Nonlinearities 212
HELIPLAT: Manufacturing and Structural Design of HAVE-UAV Scaled Prototype 212
“Status of Conversion” 212
Totale 36.449
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Categoria #
all - tutte 121.652
article - articoli 43.380
book - libri 1.779
conference - conferenze 58.210
curatela - curatele 0
other - altro 15.401
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.882
Totale 243.304
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021240 0 0 0 0 0 0 0 0 0 0 170 70
2021/20222.143 89 104 25 100 112 126 84 109 127 161 462 644
2022/20233.881 365 588 160 269 287 419 753 172 320 82 170 296
2023/20241.933 79 336 144 166 143 157 118 163 124 77 191 235
2024/20254.649 104 574 271 629 365 305 279 288 642 235 356 601
2025/202611.766 892 647 656 1.012 907 891 1.875 958 2.600 1.320 8 0
Totale 49.633