PORTO @ Archivio Istituzionale della Ricerca

CESTINO, ENRICO
 Distribuzione geografica
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Continente #
EU - Europa 13.925
NA - Nord America 11.981
AS - Asia 6.457
SA - Sud America 129
OC - Oceania 64
AF - Africa 55
Continente sconosciuto - Info sul continente non disponibili 6
-- - ???statistics.table.value.continent.--??? 2
Totale 32.619
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Nazione #
US - Stati Uniti d'America 11.654
CN - Cina 5.345
IT - Italia 4.415
GB - Regno Unito 2.544
DE - Germania 2.470
FR - Francia 1.388
UA - Ucraina 806
TR - Turchia 354
NL - Olanda 326
IE - Irlanda 322
CA - Canada 318
RU - Federazione Russa 317
SE - Svezia 290
CH - Svizzera 236
KR - Corea 224
BE - Belgio 163
FI - Finlandia 141
IN - India 125
AT - Austria 100
MY - Malesia 85
RO - Romania 84
AR - Argentina 83
IR - Iran 70
JP - Giappone 68
AU - Australia 58
ES - Italia 41
PL - Polonia 36
BG - Bulgaria 35
HK - Hong Kong 32
AP - ???statistics.table.value.countryCode.AP??? 28
EU - Europa 27
TW - Taiwan 27
BR - Brasile 24
PK - Pakistan 24
RS - Serbia 23
IL - Israele 21
PT - Portogallo 20
SG - Singapore 17
SA - Arabia Saudita 15
NG - Nigeria 14
JO - Giordania 13
HR - Croazia 12
SI - Slovenia 12
AE - Emirati Arabi Uniti 11
CZ - Repubblica Ceca 11
CL - Cile 10
ET - Etiopia 10
ID - Indonesia 9
AM - Armenia 8
KZ - Kazakistan 8
TH - Thailandia 8
VN - Vietnam 8
CO - Colombia 7
EE - Estonia 7
MX - Messico 7
BY - Bielorussia 6
CI - Costa d'Avorio 6
DK - Danimarca 6
NZ - Nuova Zelanda 6
PH - Filippine 6
A2 - ???statistics.table.value.countryCode.A2??? 5
EG - Egitto 5
GR - Grecia 5
LT - Lituania 5
NO - Norvegia 5
BD - Bangladesh 4
GH - Ghana 4
SN - Senegal 4
LK - Sri Lanka 3
PE - Perù 3
SC - Seychelles 3
SY - Repubblica araba siriana 3
ZA - Sudafrica 3
DZ - Algeria 2
GE - Georgia 2
HU - Ungheria 2
LV - Lettonia 2
MD - Moldavia 2
MK - Macedonia 2
MV - Maldive 2
QA - Qatar 2
UZ - Uzbekistan 2
DO - Repubblica Dominicana 1
EC - Ecuador 1
MA - Marocco 1
NI - Nicaragua 1
SD - Sudan 1
TN - Tunisia 1
UG - Uganda 1
VE - Venezuela 1
Totale 32.619
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Città #
Zhengzhou 3.464
Ashburn 2.678
Southend 1.907
Beijing 1.036
Chandler 1.020
Seattle 965
Turin 884
Des Moines 556
Fairfield 547
Princeton 491
Jacksonville 409
Council Bluffs 327
Torino 324
Munich 315
Ann Arbor 314
Dublin 308
Berlin 307
Houston 291
Guangzhou 280
Woodbridge 272
San Ramon 266
Montréal 263
Wilmington 254
Mcallen 253
Izmir 251
Cambridge 216
Milan 201
Shanghai 190
Bern 189
Chicago 189
San Donato Milanese 151
Brussels 142
Helsinki 118
Atlanta 117
Herkenbosch 116
Bologna 108
Zaporozhye 106
Baltimore 100
Pennsylvania Furnace 94
Rome 93
Saint Petersburg 89
Fremont 81
Boardman 80
Vienna 79
Overberg 77
Monopoli 68
Redwood City 63
Mountain View 60
Padua 60
Galati 59
Seoul 58
Hangzhou 50
Malatya 50
Moscow 47
Dearborn 43
Andover 38
Delft 38
San Francisco 37
Sofia 34
Frankfurt 32
London 32
Paris 32
Alba 28
Amsterdam 28
Nanjing 27
Norwalk 27
Strambino 27
Ankara 26
Naples 26
Podenzano 25
Toulouse 25
Bangalore 24
Leinì 24
Genova 23
Verona 23
Redmond 22
San Antonio 22
Shenzhen 22
Novara 21
San Diego 21
Shenyang 21
Xian 21
Caserta 20
Falls Church 20
Ottawa 20
Cordoba 19
Tokyo 19
Buffalo 18
Guwahati 18
Melbourne 18
Perth 18
Toronto 18
Valfenera 18
Bari 17
Los Angeles 17
Palermo 17
Tel Aviv 17
Washington 17
Dallas 16
Lecce 16
Totale 22.125
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Nome #
HeliPlat: Design, Aerodynamic Structural Analysis of Long-Endurance Solar-Powered Stratospheric Platform 1.588
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 1.550
Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft 1.368
Analysis of slender thin-walled anisotropic box-beams including local stiffness and coupling effects 1.344
COSTRUZIONI AERONAUTICHE: Eserciziario minimo con soluzioni 743
A Fuel Cell Based Propulsion System for General Aviation Aircraft: The ENFICA-FC Experience 411
Air Cooling of a Two-Seater Fuel Cells Powered Aircraft: Dynamic Modelling and Comparisons with Experiemtal Data 395
Design and testing of a propeller for a two-seater aircraft powered by fuel cells 390
Engineering Method for Air-Cooling Design of Two-Seat Propeller-Driven Aircraft Powered by Fuel Cells 367
A Multi-objective Nonlinear Piezoaeroelastic Wing Solution for Energy Harvesting and Load Alleviation: Modeling and Simulation 364
DESIGN AND OPTIMIZATION OF COMPOSITE VESSEL FOR HYDROGEN STORAGE SUBJECT TO INTERNAL PRESSURE & IN-FLIGHT LOADS 357
Multi-objective optimization of the composite wing box of solar powered HALE UAV 354
Optimization of advanced composite wing box structures subjected to combined loads and impact 337
Structural Uncertainty Effect on Classical Wing Flutter Characteristics 332
Development of an Aeroelastic Wing model with piezoelectric elements for gust load alleviation and Energy Harvesting 325
ALL ELECTRIC INTERCITY-AIRCRAFT DESIGN BASED ON FUEL CELL ENERGY SYSTEM 310
A Fuel Cell Based Propulsion System for General Aviation Aircraft: The ENFICA-FC Experience 288
More/All electric aircraft based on fuel cell energy system: the ENFICA-FC experience 284
Stability and Control of a High-Altitude-Long-Endurance UAV 282
Experimental Slender Wing Model Design by the Application of Aeroelastic Scaling Laws 271
Design, manufacturing and testing of a HALE-UAV structural demonstrator 270
Very-Long Endurance Solar Powered Autonomous Stratospheric (Vespas) Air Vehicles For Sea Border Surveillance; Anti-Illegal Immigration And Gmes Applications 269
Design and Optimization of a Composite Vessel for Hydrogen Storage Subject to Internal Pressure and In-Flight Loads for UAVs 267
L_1 adaptive flutter suppression control strategy for highly flexible structure 263
Velivolo Elettrico con Potenza da Celle a Combustibile ad Idrogeno ad Inquinamento Zero 262
Innovative Aircraft Aeroelastic Modelling and Control 260
UAV ad Energia Solare per Sorveglianza del Territorio e per Telerilevamento 252
"A Review of UAV in the World. Design and Technology of Long Endurance UAV Powered by Solar Energy". Contract with Shenyang Aerospace University, China 252
Critical Behaviour of Slender Wing Configurations 249
Design of solar high altitude long endurance aircraft for multi payload & operations 249
ℒ1 Adaptive Flutter Suppression Control Strategy for Highly Flexible Structure 246
Numerical/experimental evaluation of buckling behaviour and residual tensile strength of composite aerospace structures after low velocity impact 246
HELIPLAT®: Detail Design & Manufacturing of a Scaled Prototype for High Altitude Very-Long Endurance Solar-Powered RPAS 245
Energy harvesting from aeroelastic vibrations induced by discrete gust loads 243
Environmental Friendly Inter-City Aircraft (ENFICA-FC) and Preliminary Analysis for 2-seat aircraft conversion into Fuel Cells Powered Innovative System 240
Very-long endurance solar powered autonomous UAVS: role and constraints for GMES applications 238
Parametric analysis of a fluttering piezoelectric wing 238
Design of high-altitude long-endurance solar-powered unmanned air vehicle for multi-payload and operations 236
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 235
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 234
Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems 234
"Preliminary Design of HALE-UAV Configuration for 6 Months Endurance by In-House Developed Software". Contract with Shenyang Aerospace University, China 232
Design of inter-city transport aircraft powered by fuel cell & flight test of zero emission 2-seater aircraft powered by fuel cells 231
Modular Multifunctional Composite Structure for CubeSat Applications: Preliminary Design and Structural Analysis 229
Design, Analysis and Experimental Testing of a Morphing Wing 228
ENFICA-FC: Environmental Friendly Inter-City Aircraft and 2-seat aircraft powered by Fuel Cells electric propulsion 228
Improved Multibody Model of Flexible Wing 224
HELIPLAT®: a high altitude very-long endurance solar powered platform for border patrol and forest fire detection 221
Topology Synthesis of Planar Ground Structures for Energy Harvesting Applications 219
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 218
Hydrogen and Fuel Cell Project 216
Nonlinear LCO “amplitude-Frequency”Characteristics for Plates Fluttering at Supersonic Speeds 214
Constrained combinatorial optimization of multi-layered composite structures by means of Stud GA with proportionate selection and extinction 212
Considerations on beam-wise structural models used for aeroelastic analysis of slender wings 209
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 207
Piezo-Aeroelastic modeling and flutter prediction of flexible composite wings 205
Safety Assessment of Pharmaceutical Distribution in a Hospital Environment 198
ENFICA-FC: All-electric aircraft Powered by Fuel Cells 197
RAPID200-FC, Flight Test of First All Electric Propulsion Aeroplane Powered by Fuel Cells 197
Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings 197
A Possible Adaptive Wing Apparatus for New UAV Configurations 197
"The use of Vsaero CFD tool in the UAV Aero-dynamic project". 197
Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings 197
Low weight advanced composite primary structure design of platform 193
SHAMPO: Solar HALE aircraft for multi-payload & operations 193
The Influence of Supersonic Stream on the Dependence “Amplitude-Frequency” of Nonlinear Vibrations of Flexible Plate 192
“Airfoil Geometry of Optimal Propeller for the Rapid 200-FC” 189
A REDUCED ORDER MODEL TO ESTIMATING PROPELLER/WING INTERACTION IN SOLAR POWERED AIRCRAFT PRELIMINARY DESIGN 189
“Virtual Design of UAV-VESPA for Mediterranean Sea Border Surveillance” 188
When fuel cells fly 187
Final Analytical Data of the Aerodynamics Performance of Wing Profiles and Propellers for Low Reynolds Numbers 184
Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs 183
EQUIVALENT PLATE MODEL OF CURVILINEAR STIFFENED PANELS 182
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 180
Analysis of slender thin-walled composite box-beams including local stiffness and coupling effects 179
Scaled size prototype assembling 178
Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams 178
Generalized topology for resonators having N commensurate harmonics 178
Configuration and Estimation Cost of the flying platform HeliPlat® 177
Experimental Data of High Efficiency Wing Profiles and Propellers for Low Reynolds Numbers 177
Aeroelastic scaling laws with considerations to the design of an experimental slender wing model 173
Safety assessment of pharmaceutical distribution in a hospital environment 172
Impact of lift propeller drag on the performance of eVTOL lift+cruise aircraft 171
"CAPECON HALE UAV: Solar, Modular Configuration design " 169
HELIPLAT: Manufacturing and Structural Design of HAVE-UAV Scaled Prototype 167
ENFICA-FC Environmental Friendly Inter-City Aircraft and 2-seat aircraft powered by Fuel Cells electric propulsion 167
Design of high altitude long endurance solar powered unmanned air vehicle for multi payload and operations- SHAMPO 162
HELIPLAT®: Manufacturing and Structural Design of UAV Scaled Prototype 161
"HALE UAV Solar Configuration: Reliability, Maintainability and Safety" 161
HELIPLAT: A high altitude very-long endurance solar powered platform for border patrol and forest fire detection 159
HALE UAV Modular Configuration: Structure Analysis (FEM). Final Report 158
“Status of Conversion” 156
"HALE UAV Modular Configuration: Reliability and Safety" 156
Design of Solar powered UAV for Border Surveillance and Risk Management 152
Eccentricity Effect on the Critical Aeroelastic Condition of Slender Wings 149
Failure Mode and Effects Analysis to improve safety in pharmaceutical distribution 148
Graph-based element removal method for topology synthesis of beam based ground structures 148
Critical Aeroelastic Behaviour of Slender Composite Wings in an Incompressible Flow 146
Flutter Analysis Of A High Aspect Ratio Composite Wing Test-Model 144
HALE UAV Solar Configuration: Aerodynamic and structure Analysis. 2nd iteration. Final Report-1st Issue 141
Totale 27.848
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Categoria #
all - tutte 75.825
article - articoli 27.303
book - libri 1.087
conference - conferenze 34.649
curatela - curatele 0
other - altro 10.746
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.040
Totale 151.650
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019927 0 0 0 0 0 0 0 0 0 0 550 377
2019/20203.004 203 135 79 365 282 270 196 436 462 223 177 176
2020/20212.584 348 389 142 232 156 336 135 148 169 289 170 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
2023/20241.621 79 336 144 166 143 157 118 163 124 77 114 0
Totale 32.906