PORTO @ Archivio Istituzionale della Ricerca

CESTINO, ENRICO
 Distribuzione geografica
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Continente #
EU - Europa 14.472
NA - Nord America 12.949
AS - Asia 7.447
SA - Sud America 134
OC - Oceania 73
AF - Africa 60
Continente sconosciuto - Info sul continente non disponibili 6
-- - ???statistics.table.value.continent.--??? 2
Totale 35.143
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Nazione #
US - Stati Uniti d'America 12.615
CN - Cina 5.503
IT - Italia 4.657
GB - Regno Unito 2.558
DE - Germania 2.509
FR - Francia 1.407
UA - Ucraina 806
SG - Singapore 617
RU - Federazione Russa 480
TR - Turchia 414
NL - Olanda 337
KR - Corea 335
IE - Irlanda 326
CA - Canada 325
SE - Svezia 294
CH - Svizzera 241
BE - Belgio 181
FI - Finlandia 148
IN - India 146
AT - Austria 102
AR - Argentina 86
MY - Malesia 85
RO - Romania 84
IR - Iran 70
JP - Giappone 69
AU - Australia 67
ES - Italia 43
ID - Indonesia 39
BG - Bulgaria 36
PL - Polonia 36
HK - Hong Kong 35
PT - Portogallo 31
AP - ???statistics.table.value.countryCode.AP??? 28
TW - Taiwan 28
EU - Europa 27
PK - Pakistan 25
BR - Brasile 24
RS - Serbia 23
IL - Israele 22
CZ - Repubblica Ceca 15
SA - Arabia Saudita 15
NG - Nigeria 14
JO - Giordania 13
CL - Cile 12
HR - Croazia 12
SI - Slovenia 12
AE - Emirati Arabi Uniti 11
ET - Etiopia 10
PH - Filippine 9
AM - Armenia 8
KZ - Kazakistan 8
TH - Thailandia 8
VN - Vietnam 8
CO - Colombia 7
EE - Estonia 7
EG - Egitto 7
MX - Messico 7
BY - Bielorussia 6
CI - Costa d'Avorio 6
DK - Danimarca 6
LT - Lituania 6
NZ - Nuova Zelanda 6
A2 - ???statistics.table.value.countryCode.A2??? 5
GR - Grecia 5
NO - Norvegia 5
ZA - Sudafrica 5
BD - Bangladesh 4
GH - Ghana 4
SN - Senegal 4
DZ - Algeria 3
LK - Sri Lanka 3
PE - Perù 3
SC - Seychelles 3
SY - Repubblica araba siriana 3
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 35.143
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Città #
Zhengzhou 3.466
Ashburn 2.768
Southend 1.907
Beijing 1.046
Chandler 1.020
Seattle 965
Turin 948
Des Moines 556
Fairfield 547
Princeton 491
Singapore 461
Jacksonville 409
Santa Clara 375
Council Bluffs 346
Torino 324
Munich 315
Ann Arbor 314
Dublin 312
Berlin 311
Houston 291
Guangzhou 284
Woodbridge 272
San Ramon 266
Montréal 263
Boardman 257
Wilmington 254
Mcallen 253
Izmir 251
Milan 224
Cambridge 216
Chicago 208
Shanghai 197
Bern 189
Brussels 160
San Donato Milanese 151
Atlanta 119
Helsinki 118
Herkenbosch 116
Bologna 115
Zaporozhye 106
Baltimore 100
Rome 100
Pennsylvania Furnace 94
Saint Petersburg 89
Fremont 81
Vienna 81
Overberg 77
Monopoli 68
Redwood City 63
Mountain View 60
Padua 60
Galati 59
Seoul 59
Moscow 56
Hangzhou 52
Malatya 50
Istanbul 49
Dearborn 43
Andover 38
Delft 38
San Francisco 38
Naples 37
London 36
Strambino 36
Paris 35
Sofia 34
Frankfurt 32
New York 31
Alba 30
Jakarta 30
Amsterdam 28
Nanjing 27
Norwalk 27
Ankara 26
Podenzano 25
Toulouse 25
Yubileyny 25
Bangalore 24
Frankfurt am Main 24
Leinì 24
Shenzhen 24
Genova 23
Verona 23
Genoa 22
Redmond 22
San Antonio 22
Bari 21
Caserta 21
Lappeenranta 21
Melbourne 21
Novara 21
San Diego 21
Shenyang 21
Xian 21
Buffalo 20
Falls Church 20
Ottawa 20
Tokyo 20
Toronto 20
Cordoba 19
Totale 23.525
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Nome #
HeliPlat: Design, Aerodynamic Structural Analysis of Long-Endurance Solar-Powered Stratospheric Platform 1.619
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 1.593
Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft 1.391
Analysis of slender thin-walled anisotropic box-beams including local stiffness and coupling effects 1.348
COSTRUZIONI AERONAUTICHE: Eserciziario minimo con soluzioni 822
A Fuel Cell Based Propulsion System for General Aviation Aircraft: The ENFICA-FC Experience 421
Air Cooling of a Two-Seater Fuel Cells Powered Aircraft: Dynamic Modelling and Comparisons with Experiemtal Data 410
Design and testing of a propeller for a two-seater aircraft powered by fuel cells 403
Engineering Method for Air-Cooling Design of Two-Seat Propeller-Driven Aircraft Powered by Fuel Cells 386
DESIGN AND OPTIMIZATION OF COMPOSITE VESSEL FOR HYDROGEN STORAGE SUBJECT TO INTERNAL PRESSURE & IN-FLIGHT LOADS 377
ALL ELECTRIC INTERCITY-AIRCRAFT DESIGN BASED ON FUEL CELL ENERGY SYSTEM 377
A Multi-objective Nonlinear Piezoaeroelastic Wing Solution for Energy Harvesting and Load Alleviation: Modeling and Simulation 370
Multi-objective optimization of the composite wing box of solar powered HALE UAV 367
Optimization of advanced composite wing box structures subjected to combined loads and impact 352
Structural Uncertainty Effect on Classical Wing Flutter Characteristics 347
Development of an Aeroelastic Wing model with piezoelectric elements for gust load alleviation and Energy Harvesting 334
A Fuel Cell Based Propulsion System for General Aviation Aircraft: The ENFICA-FC Experience 303
More/All electric aircraft based on fuel cell energy system: the ENFICA-FC experience 298
Design and Optimization of a Composite Vessel for Hydrogen Storage Subject to Internal Pressure and In-Flight Loads for UAVs 289
Stability and Control of a High-Altitude-Long-Endurance UAV 288
Very-Long Endurance Solar Powered Autonomous Stratospheric (Vespas) Air Vehicles For Sea Border Surveillance; Anti-Illegal Immigration And Gmes Applications 278
Experimental Slender Wing Model Design by the Application of Aeroelastic Scaling Laws 278
Design, manufacturing and testing of a HALE-UAV structural demonstrator 277
L_1 adaptive flutter suppression control strategy for highly flexible structure 275
Velivolo Elettrico con Potenza da Celle a Combustibile ad Idrogeno ad Inquinamento Zero 275
"A Review of UAV in the World. Design and Technology of Long Endurance UAV Powered by Solar Energy". Contract with Shenyang Aerospace University, China 273
Innovative Aircraft Aeroelastic Modelling and Control 269
UAV ad Energia Solare per Sorveglianza del Territorio e per Telerilevamento 269
Numerical/experimental evaluation of buckling behaviour and residual tensile strength of composite aerospace structures after low velocity impact 264
HELIPLAT®: Detail Design & Manufacturing of a Scaled Prototype for High Altitude Very-Long Endurance Solar-Powered RPAS 261
Design of solar high altitude long endurance aircraft for multi payload & operations 260
ℒ1 Adaptive Flutter Suppression Control Strategy for Highly Flexible Structure 257
Critical Behaviour of Slender Wing Configurations 255
Energy harvesting from aeroelastic vibrations induced by discrete gust loads 255
Environmental Friendly Inter-City Aircraft (ENFICA-FC) and Preliminary Analysis for 2-seat aircraft conversion into Fuel Cells Powered Innovative System 253
"Preliminary Design of HALE-UAV Configuration for 6 Months Endurance by In-House Developed Software". Contract with Shenyang Aerospace University, China 250
Very-long endurance solar powered autonomous UAVS: role and constraints for GMES applications 248
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 246
Modular Multifunctional Composite Structure for CubeSat Applications: Preliminary Design and Structural Analysis 246
Parametric analysis of a fluttering piezoelectric wing 245
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 243
Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems 243
Design of inter-city transport aircraft powered by fuel cell & flight test of zero emission 2-seater aircraft powered by fuel cells 241
Design of high-altitude long-endurance solar-powered unmanned air vehicle for multi-payload and operations 240
Design, Analysis and Experimental Testing of a Morphing Wing 240
ENFICA-FC: Environmental Friendly Inter-City Aircraft and 2-seat aircraft powered by Fuel Cells electric propulsion 240
Improved Multibody Model of Flexible Wing 233
Topology Synthesis of Planar Ground Structures for Energy Harvesting Applications 232
HELIPLAT®: a high altitude very-long endurance solar powered platform for border patrol and forest fire detection 230
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 229
Hydrogen and Fuel Cell Project 227
Nonlinear LCO “amplitude-Frequency”Characteristics for Plates Fluttering at Supersonic Speeds 224
Constrained combinatorial optimization of multi-layered composite structures by means of Stud GA with proportionate selection and extinction 223
Considerations on beam-wise structural models used for aeroelastic analysis of slender wings 219
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 214
Piezo-Aeroelastic modeling and flutter prediction of flexible composite wings 213
RAPID200-FC, Flight Test of First All Electric Propulsion Aeroplane Powered by Fuel Cells 209
Delamination and fracture modeling techniques for shell composite structures in LS-DYNA 209
Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings 208
ENFICA-FC: All-electric aircraft Powered by Fuel Cells 207
Low weight advanced composite primary structure design of platform 206
A REDUCED ORDER MODEL TO ESTIMATING PROPELLER/WING INTERACTION IN SOLAR POWERED AIRCRAFT PRELIMINARY DESIGN 205
A Possible Adaptive Wing Apparatus for New UAV Configurations 204
"The use of Vsaero CFD tool in the UAV Aero-dynamic project". 203
Safety Assessment of Pharmaceutical Distribution in a Hospital Environment 202
Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings 202
When fuel cells fly 201
SHAMPO: Solar HALE aircraft for multi-payload & operations 200
Impact of lift propeller drag on the performance of eVTOL lift+cruise aircraft 200
EQUIVALENT PLATE MODEL OF CURVILINEAR STIFFENED PANELS 196
“Airfoil Geometry of Optimal Propeller for the Rapid 200-FC” 195
The Influence of Supersonic Stream on the Dependence “Amplitude-Frequency” of Nonlinear Vibrations of Flexible Plate 195
Final Analytical Data of the Aerodynamics Performance of Wing Profiles and Propellers for Low Reynolds Numbers 194
“Virtual Design of UAV-VESPA for Mediterranean Sea Border Surveillance” 193
Generalized topology for resonators having N commensurate harmonics 193
Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams 191
Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs 190
Configuration and Estimation Cost of the flying platform HeliPlat® 188
Scaled size prototype assembling 187
Experimental Data of High Efficiency Wing Profiles and Propellers for Low Reynolds Numbers 187
Analysis of slender thin-walled composite box-beams including local stiffness and coupling effects 186
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 183
"CAPECON HALE UAV: Solar, Modular Configuration design " 178
Aeroelastic scaling laws with considerations to the design of an experimental slender wing model 178
HELIPLAT: Manufacturing and Structural Design of HAVE-UAV Scaled Prototype 177
Safety assessment of pharmaceutical distribution in a hospital environment 176
"HALE UAV Solar Configuration: Reliability, Maintainability and Safety" 172
ENFICA-FC Environmental Friendly Inter-City Aircraft and 2-seat aircraft powered by Fuel Cells electric propulsion 172
Design of high altitude long endurance solar powered unmanned air vehicle for multi payload and operations- SHAMPO 170
HALE UAV Modular Configuration: Structure Analysis (FEM). Final Report 169
HELIPLAT®: Manufacturing and Structural Design of UAV Scaled Prototype 168
"HALE UAV Modular Configuration: Reliability and Safety" 167
“Status of Conversion” 166
HELIPLAT: A high altitude very-long endurance solar powered platform for border patrol and forest fire detection 166
Critical Aeroelastic Behaviour of Slender Composite Wings in an Incompressible Flow 164
Graph-based element removal method for topology synthesis of beam based ground structures 162
Design of Solar powered UAV for Border Surveillance and Risk Management 160
Eccentricity Effect on the Critical Aeroelastic Condition of Slender Wings 155
Experimental buckling behavior of composite aerospace structures after low velocity impact 154
Failure Mode and Effects Analysis to improve safety in pharmaceutical distribution 152
Totale 29.160
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Categoria #
all - tutte 87.563
article - articoli 31.277
book - libri 1.303
conference - conferenze 40.612
curatela - curatele 0
other - altro 11.963
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.408
Totale 175.126
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.940 0 0 0 0 0 270 196 436 462 223 177 176
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
2023/20241.933 79 336 144 166 143 157 118 163 124 77 191 235
2024/20252.215 104 574 271 629 365 272 0 0 0 0 0 0
Totale 35.433