PORTO @ Archivio Istituzionale della Ricerca

FRULLA, GIACOMO
 Distribuzione geografica
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Continente #
NA - Nord America 20.397
EU - Europa 17.848
AS - Asia 13.028
SA - Sud America 905
AF - Africa 149
OC - Oceania 51
Continente sconosciuto - Info sul continente non disponibili 8
-- - ???statistics.table.value.continent.--??? 1
Totale 52.387
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Nazione #
US - Stati Uniti d'America 20.212
IT - Italia 5.211
CN - Cina 4.929
SG - Singapore 3.006
GB - Regno Unito 2.978
DE - Germania 2.710
VN - Vietnam 2.153
FR - Francia 1.958
UA - Ucraina 1.239
RU - Federazione Russa 1.178
KR - Corea 756
BR - Brasile 678
TR - Turchia 549
NL - Olanda 436
IN - India 401
IE - Irlanda 382
HK - Hong Kong 372
SE - Svezia 363
FI - Finlandia 306
CH - Svizzera 297
AT - Austria 132
BE - Belgio 129
JP - Giappone 119
CA - Canada 90
AR - Argentina 84
RO - Romania 83
TH - Thailandia 81
IR - Iran 74
MY - Malesia 70
TW - Taiwan 70
PH - Filippine 66
CZ - Repubblica Ceca 65
ID - Indonesia 60
MX - Messico 60
AP - ???statistics.table.value.countryCode.AP??? 56
BD - Bangladesh 56
ES - Italia 46
IQ - Iraq 46
AU - Australia 45
PK - Pakistan 44
PL - Polonia 44
PT - Portogallo 39
IL - Israele 38
CO - Colombia 36
EC - Ecuador 32
CL - Cile 31
ZA - Sudafrica 31
JO - Giordania 26
SA - Arabia Saudita 26
RS - Serbia 24
EU - Europa 23
BG - Bulgaria 22
AE - Emirati Arabi Uniti 21
UZ - Uzbekistan 19
PE - Perù 17
DZ - Algeria 16
NP - Nepal 16
HR - Croazia 15
EG - Egitto 13
ET - Etiopia 11
GR - Grecia 11
LT - Lituania 11
NG - Nigeria 11
KE - Kenya 10
KZ - Kazakistan 10
AM - Armenia 9
CI - Costa d'Avorio 9
DK - Danimarca 9
MA - Marocco 9
MD - Moldavia 9
PY - Paraguay 9
VE - Venezuela 9
TN - Tunisia 8
OM - Oman 7
SN - Senegal 7
SY - Repubblica araba siriana 7
AL - Albania 6
BY - Bielorussia 6
CR - Costa Rica 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
KG - Kirghizistan 4
KW - Kuwait 4
NI - Nicaragua 4
NO - Norvegia 4
SC - Seychelles 4
TT - Trinidad e Tobago 4
UY - Uruguay 4
A2 - ???statistics.table.value.countryCode.A2??? 3
AZ - Azerbaigian 3
CG - Congo 3
GH - Ghana 3
LK - Sri Lanka 3
MN - Mongolia 3
Totale 52.341
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Città #
Ashburn 4.119
Council Bluffs 2.753
Southend 2.559
Zhengzhou 2.492
Singapore 1.702
Seattle 1.401
Des Moines 1.118
Turin 1.043
Chandler 938
San Jose 902
Beijing 690
Fairfield 667
Princeton 631
Jacksonville 628
Ho Chi Minh City 604
Hanoi 505
Berlin 391
San Ramon 375
Dublin 370
Ann Arbor 358
Chicago 346
Houston 335
Izmir 333
Santa Clara 324
Boardman 312
Milan 310
Woodbridge 307
Seoul 296
Hong Kong 289
Torino 282
Wilmington 280
Bern 253
Helsinki 253
Cambridge 230
San Donato Milanese 220
Los Angeles 215
Shanghai 205
Lauterbourg 200
Guangzhou 190
Baltimore 146
Rome 145
Pennsylvania Furnace 140
Zaporozhye 140
Dallas 126
Herkenbosch 123
Overberg 123
Saint Petersburg 117
Moscow 113
Brussels 111
Monopoli 107
Vienna 105
Padua 103
Haiphong 96
Buffalo 95
Fremont 91
Hangzhou 88
Da Nang 84
Hefei 81
Atlanta 75
Malatya 69
Redwood City 68
Frankfurt am Main 67
Galati 64
Munich 63
New York 63
Alba 62
Bologna 59
Mountain View 58
São Paulo 54
Paris 52
Orem 51
Istanbul 50
Naples 50
Andover 48
Prague 46
Tokyo 46
London 45
Tongling 44
Amsterdam 43
Ankara 37
Changsha 37
Delft 37
Norwalk 36
Bangkok 34
Nanjing 34
Toronto 34
Dearborn 33
Valfenera 33
San Diego 32
San Francisco 32
Verona 32
Washington 32
Hải Dương 31
Columbus 29
Yubileyny 29
Falls Church 28
Florence 26
Xian 26
Frankfurt 25
San Antonio 25
Totale 33.399
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Nome #
HeliPlat: Design, Aerodynamic Structural Analysis of Long-Endurance Solar-Powered Stratospheric Platform 1.694
" Characterization of Several Advanced Composite Materials for CRV Space Program: Physical, chemical and mechanical properties; CME and CTE results" 1.640
" 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)". 1.573
Analysis of slender thin-walled anisotropic box-beams including local stiffness and coupling effects 1.403
COSTRUZIONI AERONAUTICHE: Eserciziario minimo con soluzioni 1.084
HELIPLAT: High altitude very-long endurance Solar Powered UAV for telecommunication and earth observation applications. 450
A Multi-objective Nonlinear Piezoaeroelastic Wing Solution for Energy Harvesting and Load Alleviation: Modeling and Simulation 448
Delamination and fracture modeling techniques for shell composite structures in LS-DYNA 425
Elica o rotore a passo variabile con svergolamento variabile di rendimento ottimo 407
Structural Uncertainty Effect on Classical Wing Flutter Characteristics 403
Development of an Aeroelastic Wing model with piezoelectric elements for gust load alleviation and Energy Harvesting 384
"WindDesigner: An Open Tool for Analysis and Design of Wind Generators" 384
Stability and Control of a High-Altitude-Long-Endurance UAV 365
Wind Generator Innovative Blade Design: Variable Twist and Start-Up Control 359
Innovative Aircraft Aeroelastic Modelling and Control 352
Energy harvesting from aeroelastic vibrations induced by discrete gust loads 340
Design, manufacturing and testing of a HALE-UAV structural demonstrator 338
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 326
Analisi strutturale di un'ala in materiale composito per un velivolo ad energia elettro-solare 317
Nonlinear Angle of Twist of Advanced Composite Wing Boxes under Pure Torsion 315
An Invariant-based Performance-Oriented Procedure for Preliminary Design of Composite Structures 313
Parametric analysis of a fluttering piezoelectric wing 311
Topology Synthesis of Planar Ground Structures for Energy Harvesting Applications 308
Design, Analysis and Experimental Testing of a Morphing Wing 306
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 306
Cicala's asymptotic approach to the linear shell theory 305
Environmental Friendly Inter-City Aircraft (ENFICA-FC) and Preliminary Analysis for 2-seat aircraft conversion into Fuel Cells Powered Innovative System 305
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 300
Critical Behaviour of Slender Wing Configurations 297
A variable twist blade concept for more effective wind generation: design and realization 296
Structural aerospace composite/metallic samples under fatigue loads: experimental activity on three case studies 291
Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems 291
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
Innovative blade design for wind generator application 284
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 282
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
Attività di qualificazione di tubi e montanti in fibra di carbonio nell'ambito del programma SAX. Risultati delle prove meccaniche 276
Indagine sullo stato dell'arte dei materiali innovativi nella realizzazione delle strutture dei sistemi produttivi 275
Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings 274
Determinazione delle caratteristiche igrotermiche di pannelli sandwich in grafite/epoxy nell'ambito del programma spaziale SOHO-UVCS 273
A new test facility for measuring the coefficient of moisture expansion of advanced composite materials 272
Generalized topology for resonators having N commensurate harmonics 272
Second down selection test report for wing panels in AL-LI LASER welded 271
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
Structural Aerospace Composite/Metallic Samples under Fatigue Loads: Experimental Activity on Three Case Studies 268
Considerations on beam-wise structural models used for aeroelastic analysis of slender wings 268
EQUIVALENT PLATE MODEL OF CURVILINEAR STIFFENED PANELS 266
HELIPLAT: Aerodynamic and Structural Analysis of HAVE Solar Powered platform 264
Low weight advanced composite primary structure design of platform 263
Final Analytical Data of the Aerodynamics Performance of Wing Profiles and Propellers for Low Reynolds Numbers 263
Analytical and experimental results of the coefficient of thermal expansion of high-modulus graphite/epoxy materials 260
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) 258
Nonlinear analysis of anisotropic plates with initial imperfections and various boundary conditions subjected to combined biaxial compression and shear loads 252
Preliminary Reliability Design of a Solar Powered high-altitude very long endurance unmanned air vehicle 252
Some considerations about the concepts of asymptotic approach 252
Risultati sperimentali sull'incollaggio di strutture in grafite/epoxy 251
Scaled size prototype assembling 248
HELIPLAT: A Solar Powered HAVE-UAV for Telecommunication Applications. Design & Parametric Results. Analysis, Manufacturing & Testing of Advanced Composite Structures 247
A Possible Adaptive Wing Apparatus for New UAV Configurations 246
SHAMPO: Solar HALE aircraft for multi-payload & operations 245
Stretched exponential structural relaxation of composite materials induced by impurities desorption in vacuum 244
Nonlinear Analysis of Graphite/Epoxy Wing Boxes under Pure Bending Including Lateral Pressure 243
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 243
Postbuckling Behaviour of Graphite/Epoxy Stiffened Panels with initial Imperfections subjected to eccentric Biaxial Compression Loading 241
Preliminary evaluation of the fatigue behaviour of aluminium alloy in corrosive environment 241
UVCS-SPA Joint tension and shear capability - Jointed panel buckling 240
Numerical/experimental structural characterization of composite advanced joints for HALE-UAV platforms 240
Structural Reliability Aspects for advanced Composite material Applications 240
Materiali compositi grafite/epoxy per strutture ad alta stabilità dimensionale impiegati in programmi spaziali. Determinazione delle caratteristiche fisio-meccaniche del materiale M55J/M18 239
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
Experimental Data of High Efficiency Wing Profiles and Propellers for Low Reynolds Numbers 233
Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings 233
ENFICA-FC: All-electric aircraft Powered by Fuel Cells 232
“Virtual Design of UAV-VESPA for Mediterranean Sea Border Surveillance” 232
Configuration and Estimation Cost of the flying platform HeliPlat® 232
Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs 232
The Cicala’s asymptotic approach to the linear shell theory, Modern Trend in the Foundation of the Theory of Shell and Plates 230
HELIPLAT: Design of High altitude very-long endurance Solar Powered platform for telecommunication and earth observation applications 230
HELIPLAT:High Altitude very-long endurance Solar Powered UAV for telecommunication Applications. FEM analysis manufacturing and testing of 21m long CFRP wing box 227
"HALE UAV Solar Configuration: Reliability, Maintainability and Safety" 225
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
Critical Aeroelastic Behaviour of Slender Composite Wings in an Incompressible Flow 224
HALE UAV Modular Configuration: Structure Analysis (FEM). Final Report 223
Preliminary design of anisotropic plate in critical and post-critical regime by extended Trace procedure 223
Progetto S55 Replica 223
Bearing Strength of bolted Joints in CFRP Wing Fittings 221
Static/fatigue Structural Behaviour of Damaged Stiffened Composite Plates for UAS Applications 221
Analytical and experimental comparison of composite panels under combined biaxial compression and shear loads 221
Graph-based element removal method for topology synthesis of beam based ground structures 220
"CAPECON HALE UAV: Solar, Modular Configuration design " 220
Totale 33.722
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Categoria #
all - tutte 137.467
article - articoli 43.418
book - libri 1.778
conference - conferenze 60.630
curatela - curatele 0
other - altro 27.349
patent - brevetti 1.022
selected - selezionate 0
volume - volumi 3.270
Totale 274.934
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021476 0 0 0 0 0 0 0 0 0 218 195 63
2021/20222.094 89 156 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
2025/202610.839 751 628 623 1.021 692 767 1.720 856 2.463 1.318 0 0
Totale 52.594