PORTO @ Archivio Istituzionale della Ricerca

FRULLA, GIACOMO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 21.597
EU - Europa 18.092
AS - Asia 13.366
SA - Sud America 941
Continente sconosciuto - Info sul continente non disponibili 215
AF - Africa 151
OC - Oceania 51
-- - ???statistics.table.value.continent.--??? 1
Totale 54.414
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 21.314
IT - Italia 5.416
CN - Cina 4.944
SG - Singapore 3.100
GB - Regno Unito 2.982
DE - Germania 2.713
VN - Vietnam 2.158
FR - Francia 1.963
UA - Ucraina 1.242
RU - Federazione Russa 1.178
KR - Corea 757
BR - Brasile 691
TR - Turchia 555
NL - Olanda 440
IN - India 406
IE - Irlanda 382
HK - Hong Kong 380
SE - Svezia 364
FI - Finlandia 306
CH - Svizzera 299
BD - Bangladesh 243
AT - Austria 132
BE - Belgio 130
JP - Giappone 122
CA - Canada 117
AR - Argentina 85
RO - Romania 84
TH - Thailandia 81
CZ - Repubblica Ceca 74
IR - Iran 74
MY - Malesia 74
TW - Taiwan 70
MX - Messico 68
ID - Indonesia 66
PH - Filippine 66
AP - ???statistics.table.value.countryCode.AP??? 56
ES - Italia 48
IQ - Iraq 47
PL - Polonia 46
AU - Australia 45
PK - Pakistan 44
CO - Colombia 42
PT - Portogallo 40
IL - Israele 39
EC - Ecuador 38
CL - Cile 33
ZA - Sudafrica 31
SA - Arabia Saudita 27
JO - Giordania 26
RS - Serbia 24
EU - Europa 23
BG - Bulgaria 22
AE - Emirati Arabi Uniti 21
CR - Costa Rica 20
PE - Perù 20
UZ - Uzbekistan 20
DZ - Algeria 17
JM - Giamaica 17
NP - Nepal 16
HR - Croazia 15
EG - Egitto 13
VE - Venezuela 13
ET - Etiopia 11
GR - Grecia 11
HN - Honduras 11
KE - Kenya 11
LT - Lituania 11
NG - Nigeria 11
TT - Trinidad e Tobago 11
KZ - Kazakistan 10
MD - Moldavia 10
NI - Nicaragua 10
AM - Armenia 9
CI - Costa d'Avorio 9
DK - Danimarca 9
MA - Marocco 9
PY - Paraguay 9
TN - Tunisia 8
OM - Oman 7
SN - Senegal 7
SY - Repubblica araba siriana 7
AL - Albania 6
BY - Bielorussia 6
DO - Repubblica Dominicana 6
LB - Libano 6
NZ - Nuova Zelanda 6
GE - Georgia 5
PA - Panama 5
QA - Qatar 5
SI - Slovenia 5
GA - Gabon 4
GT - Guatemala 4
KG - Kirghizistan 4
KW - Kuwait 4
NO - Norvegia 4
PR - Porto Rico 4
SC - Seychelles 4
UY - Uruguay 4
A2 - ???statistics.table.value.countryCode.A2??? 3
AZ - Azerbaigian 3
Totale 54.148
Salva come PNG Salva come JPEG
Città #
Ashburn 4.265
Council Bluffs 2.884
Southend 2.559
Zhengzhou 2.492
Singapore 1.718
Seattle 1.403
San Jose 1.121
Des Moines 1.118
Turin 1.057
Chandler 939
Beijing 696
Fairfield 667
Jacksonville 632
Princeton 631
Ho Chi Minh City 606
Hanoi 505
Santa Clara 400
Berlin 391
San Ramon 375
Dublin 371
Ann Arbor 358
Chicago 349
Houston 338
Milan 337
Izmir 333
Boardman 317
Woodbridge 307
Seoul 296
Hong Kong 294
Wilmington 284
Torino 282
Bern 253
Helsinki 253
Cambridge 231
Los Angeles 228
San Donato Milanese 220
Shanghai 205
Lauterbourg 200
Guangzhou 190
Rome 170
Baltimore 148
Pennsylvania Furnace 140
Zaporozhye 140
Dallas 135
Herkenbosch 123
Overberg 123
Saint Petersburg 117
Moscow 113
Brussels 112
Monopoli 107
New York 105
Vienna 105
Padua 104
Buffalo 100
Haiphong 97
Fremont 91
Hangzhou 88
Da Nang 85
Hefei 81
Atlanta 77
Malatya 70
Redwood City 69
Frankfurt am Main 67
Galati 64
Munich 63
Alba 62
Bologna 61
Mountain View 58
Naples 58
Orem 55
Prague 55
São Paulo 54
Paris 52
Istanbul 50
Andover 48
Tokyo 47
London 46
Tongling 44
Amsterdam 43
Changsha 39
Ankara 37
Delft 37
Toronto 37
Norwalk 36
Washington 35
Bangkok 34
Nanjing 34
San Francisco 34
Verona 34
Dearborn 33
Valfenera 33
San Diego 32
Hải Dương 31
Bari 30
Columbus 29
Yubileyny 29
Falls Church 28
Florence 28
San Antonio 28
Palermo 27
Totale 34.217
Salva come PNG Salva come JPEG
Nome #
HeliPlat: Design, Aerodynamic Structural Analysis of Long-Endurance Solar-Powered Stratospheric Platform 1.715
" Characterization of Several Advanced Composite Materials for CRV Space Program: Physical, chemical and mechanical properties; CME and CTE results" 1.688
" Qualification Activity of CFRP Tubes and Struts for the SAX Satellite Space Program; CME and CTE results (Attività di qualificazione di tubi e montanti in fibra di carbonio nell'ambito del programma SAX. Risultati delle prove di espansione igroscopica (CME) e Termica (CTE)". 1.607
Analysis of slender thin-walled anisotropic box-beams including local stiffness and coupling effects 1.414
COSTRUZIONI AERONAUTICHE: Eserciziario minimo con soluzioni 1.148
Delamination and fracture modeling techniques for shell composite structures in LS-DYNA 489
HELIPLAT: High altitude very-long endurance Solar Powered UAV for telecommunication and earth observation applications. 467
A Multi-objective Nonlinear Piezoaeroelastic Wing Solution for Energy Harvesting and Load Alleviation: Modeling and Simulation 454
Elica o rotore a passo variabile con svergolamento variabile di rendimento ottimo 436
Structural Uncertainty Effect on Classical Wing Flutter Characteristics 410
Wind Generator Innovative Blade Design: Variable Twist and Start-Up Control 389
Development of an Aeroelastic Wing model with piezoelectric elements for gust load alleviation and Energy Harvesting 388
"WindDesigner: An Open Tool for Analysis and Design of Wind Generators" 387
Stability and Control of a High-Altitude-Long-Endurance UAV 369
Innovative Aircraft Aeroelastic Modelling and Control 362
Design, manufacturing and testing of a HALE-UAV structural demonstrator 350
Energy harvesting from aeroelastic vibrations induced by discrete gust loads 348
HELIPLAT®: Detail Design & Manufacturing of a Scaled Prototype for High Altitude Very-Long Endurance Solar-Powered RPAS 340
Very-Long Endurance Solar Powered Autonomous Stratospheric (Vespas) Air Vehicles For Sea Border Surveillance; Anti-Illegal Immigration And Gmes Applications 338
Nonlinear Angle of Twist of Advanced Composite Wing Boxes under Pure Torsion 331
Experimental Slender Wing Model Design by the Application of Aeroelastic Scaling Laws 330
An Invariant-based Performance-Oriented Procedure for Preliminary Design of Composite Structures 323
Analisi strutturale di un'ala in materiale composito per un velivolo ad energia elettro-solare 321
Parametric analysis of a fluttering piezoelectric wing 320
Cicala's asymptotic approach to the linear shell theory 320
Environmental Friendly Inter-City Aircraft (ENFICA-FC) and Preliminary Analysis for 2-seat aircraft conversion into Fuel Cells Powered Innovative System 316
Topology Synthesis of Planar Ground Structures for Energy Harvesting Applications 314
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 312
Design, Analysis and Experimental Testing of a Morphing Wing 310
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 309
Critical Behaviour of Slender Wing Configurations 301
A variable twist blade concept for more effective wind generation: design and realization 298
Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems 297
Structural aerospace composite/metallic samples under fatigue loads: experimental activity on three case studies 296
Nonlinear LCO “amplitude-Frequency”Characteristics for Plates Fluttering at Supersonic Speeds 294
EQUIVALENT PLATE MODEL OF CURVILINEAR STIFFENED PANELS 294
Piezo-Aeroelastic modeling and flutter prediction of flexible composite wings 294
HELIPLAT®: a high altitude very-long endurance solar powered platform for border patrol and forest fire detection 293
Design of high-altitude long-endurance solar-powered unmanned air vehicle for multi-payload and operations 291
Materiali compositi grafite/epoxy per strutture ad alta stabilità dimensionale impiegati nel programma spaziale SOHO-UVCS. Prove di flessione di ovalizzazione e del coefficiente di espansione igroscopica (CME)del materiale M55J/M18 290
Innovative blade design for wind generator application 288
Nonlinear analysis of anisotropic plates with initial imperfections and various boundary conditions subjected to combined biaxial compression and shear loads 285
Second down selection test report for wing panels in AL-LI LASER welded 285
Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings 284
Indagine sullo stato dell'arte dei materiali innovativi nella realizzazione delle strutture dei sistemi produttivi 283
Attività di qualificazione di tubi e montanti in fibra di carbonio nell'ambito del programma SAX. Risultati delle prove meccaniche 283
Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams 280
Generalized topology for resonators having N commensurate harmonics 280
Structural Aerospace Composite/Metallic Samples under Fatigue Loads: Experimental Activity on Three Case Studies 277
Determinazione delle caratteristiche igrotermiche di pannelli sandwich in grafite/epoxy nell'ambito del programma spaziale SOHO-UVCS 276
A new test facility for measuring the coefficient of moisture expansion of advanced composite materials 276
Constrained combinatorial optimization of multi-layered composite structures by means of Stud GA with proportionate selection and extinction 275
HELIPLAT: Aerodynamic and Structural Analysis of HAVE Solar Powered platform 273
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 272
Final Analytical Data of the Aerodynamics Performance of Wing Profiles and Propellers for Low Reynolds Numbers 271
Considerations on beam-wise structural models used for aeroelastic analysis of slender wings 271
Low weight advanced composite primary structure design of platform 266
Attività di qualificazione di tubi e montanti in fibra di carbonio nell'ambito del programma SAX. Risultati delle prove di espansione igroscopica (CME) e termica (CTE) 266
Analytical and experimental results of the coefficient of thermal expansion of high-modulus graphite/epoxy materials 266
Postbuckling Behaviour of Graphite/Epoxy Stiffened Panels with initial Imperfections subjected to eccentric Biaxial Compression Loading 265
Preliminary Reliability Design of a Solar Powered high-altitude very long endurance unmanned air vehicle 260
Risultati sperimentali sull'incollaggio di strutture in grafite/epoxy 259
Scaled size prototype assembling 257
Some considerations about the concepts of asymptotic approach 256
HELIPLAT: A Solar Powered HAVE-UAV for Telecommunication Applications. Design & Parametric Results. Analysis, Manufacturing & Testing of Advanced Composite Structures 254
A Possible Adaptive Wing Apparatus for New UAV Configurations 252
A Nonlinear Beam Finite Element with Bending–Torsion Coupling Formulation for Dynamic Analysis with Geometric Nonlinearities 251
On determination of aerodynamic properties of morphing wing by numerical simulations 250
UVCS-SPA Joint tension and shear capability - Jointed panel buckling 250
Nonlinear Analysis of Graphite/Epoxy Wing Boxes under Pure Bending Including Lateral Pressure 250
Stretched exponential structural relaxation of composite materials induced by impurities desorption in vacuum 250
SHAMPO: Solar HALE aircraft for multi-payload & operations 250
Comportamento di travi e pannelli in grafite/epoxy soggetti a trazione, compressione e flessione. Confronto fra analisi teorica, rilevazioni estensimetriche e per mezzo di sensori a fibre ottiche 249
Structural Reliability Aspects for advanced Composite material Applications 247
Numerical/experimental structural characterization of composite advanced joints for HALE-UAV platforms 245
The Influence of Supersonic Stream on the Dependence “Amplitude-Frequency” of Nonlinear Vibrations of Flexible Plate 243
Materiali compositi grafite/epoxy per strutture ad alta stabilità dimensionale impiegati in programmi spaziali. Determinazione delle caratteristiche fisio-meccaniche del materiale M55J/M18 242
Preliminary evaluation of the fatigue behaviour of aluminium alloy in corrosive environment 242
"The use of Vsaero CFD tool in the UAV Aero-dynamic project". 242
Aeroelastic scaling laws with considerations to the design of an experimental slender wing model 242
ENFICA-FC: All-electric aircraft Powered by Fuel Cells 240
Experimental Data of High Efficiency Wing Profiles and Propellers for Low Reynolds Numbers 238
Safety Assessment of Pharmaceutical Distribution in a Hospital Environment 238
A Practical Engineering Approach to the Design and Manufacturing of a mini kW BladeWind Turbine: Definition, optimization and CFD Analysis 238
“Virtual Design of UAV-VESPA for Mediterranean Sea Border Surveillance” 237
Configuration and Estimation Cost of the flying platform HeliPlat® 237
The Cicala’s asymptotic approach to the linear shell theory, Modern Trend in the Foundation of the Theory of Shell and Plates 234
Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs 234
Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings 234
HELIPLAT: Design of High altitude very-long endurance Solar Powered platform for telecommunication and earth observation applications 234
Buckling and postbuckling Behavior of Anisotropic Rectangular panels under linearly Varying Combined Loads 233
Progetto S55 Replica 233
"HALE UAV Solar Configuration: Reliability, Maintainability and Safety" 232
HELIPLAT:High Altitude very-long endurance Solar Powered UAV for telecommunication Applications. FEM analysis manufacturing and testing of 21m long CFRP wing box 232
Experimental buckling behavior of composite aerospace structures after low velocity impact 231
Critical Aeroelastic Behaviour of Slender Composite Wings in an Incompressible Flow 230
Analytical and experimental comparison of composite panels under combined biaxial compression and shear loads 229
HALE UAV Modular Configuration: Structure Analysis (FEM). Final Report 228
Analysis of slender thin-walled composite box-beams including local stiffness and coupling effects 227
Investigation of different morph wing configurations for the rolling maneuver 226
Totale 34.731
Salva come PNG Salva come JPEG
Categoria #
all - tutte 147.037
article - articoli 46.736
book - libri 1.893
conference - conferenze 64.923
curatela - curatele 0
other - altro 28.902
patent - brevetti 1.082
selected - selezionate 0
volume - volumi 3.501
Totale 294.074
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20222.005 0 156 20 96 96 89 91 102 98 157 422 678
2022/20236.556 381 599 127 234 318 485 1.320 178 337 67 234 2.276
2023/20241.972 167 438 227 122 156 128 108 92 78 66 162 228
2024/20254.111 118 587 260 544 305 185 222 267 628 213 266 516
2025/202611.799 751 628 623 1.021 692 767 1.720 856 2.463 1.360 387 531
2026/2027860 489 371 0 0 0 0 0 0 0 0 0 0
Totale 54.414