PORTO @ Archivio Istituzionale della Ricerca

FRULLA, GIACOMO
 Distribuzione geografica
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Continente #
NA - Nord America 17.335
EU - Europa 15.826
AS - Asia 5.736
SA - Sud America 72
AF - Africa 53
OC - Oceania 48
Continente sconosciuto - Info sul continente non disponibili 4
-- - ???statistics.table.value.continent.--??? 1
Totale 39.075
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Nazione #
US - Stati Uniti d'America 17.259
IT - Italia 4.653
CN - Cina 3.806
GB - Regno Unito 2.866
DE - Germania 2.569
FR - Francia 1.717
UA - Ucraina 1.220
SG - Singapore 592
RU - Federazione Russa 588
TR - Turchia 514
NL - Olanda 386
IE - Irlanda 377
SE - Svezia 353
KR - Corea 327
CH - Svizzera 282
FI - Finlandia 190
BE - Belgio 126
IN - India 118
AT - Austria 113
RO - Romania 78
IR - Iran 72
MY - Malesia 63
AP - ???statistics.table.value.countryCode.AP??? 56
CA - Canada 55
JP - Giappone 50
TW - Taiwan 43
AU - Australia 42
IL - Israele 30
PT - Portogallo 30
ID - Indonesia 29
ES - Italia 27
AR - Argentina 23
EU - Europa 23
BG - Bulgaria 22
HK - Hong Kong 22
PL - Polonia 20
MX - Messico 19
CO - Colombia 18
JO - Giordania 17
RS - Serbia 17
PK - Pakistan 16
BR - Brasile 15
CZ - Repubblica Ceca 15
SA - Arabia Saudita 15
HR - Croazia 14
VN - Vietnam 14
AE - Emirati Arabi Uniti 11
DZ - Algeria 11
NG - Nigeria 10
AM - Armenia 9
CI - Costa d'Avorio 9
CL - Cile 8
KZ - Kazakistan 8
DK - Danimarca 7
GR - Grecia 7
PE - Perù 7
NZ - Nuova Zelanda 6
PH - Filippine 6
SN - Senegal 6
BY - Bielorussia 5
LT - Lituania 5
SI - Slovenia 5
BD - Bangladesh 4
EG - Egitto 4
NO - Norvegia 4
ZA - Sudafrica 4
A2 - ???statistics.table.value.countryCode.A2??? 3
GH - Ghana 3
MD - Moldavia 3
SC - Seychelles 3
TH - Thailandia 3
UZ - Uzbekistan 3
EE - Estonia 2
GE - Georgia 2
LV - Lettonia 2
MV - Maldive 2
QA - Qatar 2
DO - Repubblica Dominicana 1
EC - Ecuador 1
ET - Etiopia 1
LK - Sri Lanka 1
LY - Libia 1
MK - Macedonia 1
NI - Nicaragua 1
SY - Repubblica araba siriana 1
TJ - Tagikistan 1
UG - Uganda 1
Totale 39.075
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Città #
Ashburn 3.667
Council Bluffs 2.627
Southend 2.559
Zhengzhou 2.479
Seattle 1.392
Des Moines 1.116
Chandler 938
Turin 893
Fairfield 667
Princeton 631
Jacksonville 628
Beijing 501
Singapore 418
Berlin 385
San Ramon 375
Dublin 366
Ann Arbor 358
Izmir 333
Houston 328
Chicago 327
Boardman 309
Woodbridge 307
Torino 282
Wilmington 280
Milan 254
Bern 253
Cambridge 230
San Donato Milanese 220
Shanghai 188
Helsinki 169
Guangzhou 167
Baltimore 144
Pennsylvania Furnace 140
Zaporozhye 140
Herkenbosch 123
Overberg 123
Saint Petersburg 117
Brussels 108
Monopoli 107
Rome 106
Padua 100
Vienna 96
Fremont 91
Moscow 90
Hangzhou 83
Malatya 69
Atlanta 68
Redwood City 68
Santa Clara 67
Galati 64
Alba 62
Mountain View 58
Bologna 53
Andover 48
Paris 44
Istanbul 41
Delft 37
Naples 37
Seoul 37
Norwalk 36
Dearborn 33
Valfenera 33
San Diego 32
Amsterdam 31
Ankara 31
Washington 31
London 30
Verona 30
Yubileyny 29
Falls Church 28
Toronto 27
Changsha 26
New York 26
Xian 26
Frankfurt 25
Nanjing 25
San Antonio 24
San Francisco 24
Genova 23
Podenzano 23
Florence 22
Frankfurt am Main 22
San Mateo 22
Jakarta 21
Modena 21
Pisa 21
Melbourne 20
Palermo 20
Guwahati 19
Sofia 19
Strambino 19
Ningbo 18
Toulouse 18
Bangalore 17
Hamburg 17
Los Angeles 17
Novara 17
Bari 16
Buffalo 16
Liverpool 16
Totale 26.939
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Nome #
HeliPlat: Design, Aerodynamic Structural Analysis of Long-Endurance Solar-Powered Stratospheric Platform 1.617
" Characterization of Several Advanced Composite Materials for CRV Space Program: Physical, chemical and mechanical properties; CME and CTE results" 1.412
" 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)". 1.368
Analysis of slender thin-walled anisotropic box-beams including local stiffness and coupling effects 1.348
COSTRUZIONI AERONAUTICHE: Eserciziario minimo con soluzioni 811
A Multi-objective Nonlinear Piezoaeroelastic Wing Solution for Energy Harvesting and Load Alleviation: Modeling and Simulation 368
HELIPLAT: High altitude very-long endurance Solar Powered UAV for telecommunication and earth observation applications. 355
Elica o rotore a passo variabile con svergolamento variabile di rendimento ottimo 353
Structural Uncertainty Effect on Classical Wing Flutter Characteristics 344
Development of an Aeroelastic Wing model with piezoelectric elements for gust load alleviation and Energy Harvesting 332
"WindDesigner: An Open Tool for Analysis and Design of Wind Generators" 295
Stability and Control of a High-Altitude-Long-Endurance UAV 287
Analisi strutturale di un'ala in materiale composito per un velivolo ad energia elettro-solare 286
Experimental Slender Wing Model Design by the Application of Aeroelastic Scaling Laws 277
Design, manufacturing and testing of a HALE-UAV structural demonstrator 276
Very-Long Endurance Solar Powered Autonomous Stratospheric (Vespas) Air Vehicles For Sea Border Surveillance; Anti-Illegal Immigration And Gmes Applications 274
Innovative Aircraft Aeroelastic Modelling and Control 269
Cicala's asymptotic approach to the linear shell theory 268
Wind Generator Innovative Blade Design: Variable Twist and Start-Up Control 261
HELIPLAT®: Detail Design & Manufacturing of a Scaled Prototype for High Altitude Very-Long Endurance Solar-Powered RPAS 256
Critical Behaviour of Slender Wing Configurations 255
Energy harvesting from aeroelastic vibrations induced by discrete gust loads 253
Environmental Friendly Inter-City Aircraft (ENFICA-FC) and Preliminary Analysis for 2-seat aircraft conversion into Fuel Cells Powered Innovative System 250
Parametric analysis of a fluttering piezoelectric wing 243
Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems 243
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 240
Design of high-altitude long-endurance solar-powered unmanned air vehicle for multi-payload and operations 239
Design, Analysis and Experimental Testing of a Morphing Wing 238
Nonlinear Angle of Twist of Advanced Composite Wing Boxes under Pure Torsion 237
Topology Synthesis of Planar Ground Structures for Energy Harvesting Applications 230
HELIPLAT: Aerodynamic and Structural Analysis of HAVE Solar Powered platform 230
A new test facility for measuring the coefficient of moisture expansion of advanced composite materials 229
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 228
HELIPLAT®: a high altitude very-long endurance solar powered platform for border patrol and forest fire detection 227
An Invariant-based Performance-Oriented Procedure for Preliminary Design of Composite Structures 226
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 225
Structural aerospace composite/metallic samples under fatigue loads: experimental activity on three case studies 223
Nonlinear LCO “amplitude-Frequency”Characteristics for Plates Fluttering at Supersonic Speeds 221
Constrained combinatorial optimization of multi-layered composite structures by means of Stud GA with proportionate selection and extinction 221
Analytical and experimental results of the coefficient of thermal expansion of high-modulus graphite/epoxy materials 218
Considerations on beam-wise structural models used for aeroelastic analysis of slender wings 217
A variable twist blade concept for more effective wind generation: design and realization 217
Stretched exponential structural relaxation of composite materials induced by impurities desorption in vacuum 217
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 214
Determinazione delle caratteristiche igrotermiche di pannelli sandwich in grafite/epoxy nell'ambito del programma spaziale SOHO-UVCS 213
Piezo-Aeroelastic modeling and flutter prediction of flexible composite wings 212
Indagine sullo stato dell'arte dei materiali innovativi nella realizzazione delle strutture dei sistemi produttivi 211
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) 211
Preliminary evaluation of the fatigue behaviour of aluminium alloy in corrosive environment 211
Nonlinear analysis of anisotropic plates with initial imperfections and various boundary conditions subjected to combined biaxial compression and shear loads 209
Preliminary Reliability Design of a Solar Powered high-altitude very long endurance unmanned air vehicle 209
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 208
Risultati sperimentali sull'incollaggio di strutture in grafite/epoxy 207
Innovative blade design for wind generator application 207
Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings 206
Attività di qualificazione di tubi e montanti in fibra di carbonio nell'ambito del programma SAX. Risultati delle prove meccaniche 206
A Possible Adaptive Wing Apparatus for New UAV Configurations 204
Low weight advanced composite primary structure design of platform 203
ENFICA-FC: All-electric aircraft Powered by Fuel Cells 203
Some considerations about the concepts of asymptotic approach 202
"The use of Vsaero CFD tool in the UAV Aero-dynamic project". 202
Safety Assessment of Pharmaceutical Distribution in a Hospital Environment 201
Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings 201
Delamination and fracture modeling techniques for shell composite structures in LS-DYNA 201
Nonlinear Analysis of Graphite/Epoxy Wing Boxes under Pure Bending Including Lateral Pressure 200
HELIPLAT: A Solar Powered HAVE-UAV for Telecommunication Applications. Design & Parametric Results. Analysis, Manufacturing & Testing of Advanced Composite Structures 200
SHAMPO: Solar HALE aircraft for multi-payload & operations 199
Materiali compositi grafite/epoxy per strutture ad alta stabilità dimensionale impiegati in programmi spaziali. Determinazione delle caratteristiche fisio-meccaniche del materiale M55J/M18 197
Numerical/experimental structural characterization of composite advanced joints for HALE-UAV platforms 195
The Influence of Supersonic Stream on the Dependence “Amplitude-Frequency” of Nonlinear Vibrations of Flexible Plate 195
Postbuckling Behaviour of Graphite/Epoxy Stiffened Panels with initial Imperfections subjected to eccentric Biaxial Compression Loading 194
Structural Reliability Aspects for advanced Composite material Applications 194
EQUIVALENT PLATE MODEL OF CURVILINEAR STIFFENED PANELS 194
null 194
Final Analytical Data of the Aerodynamics Performance of Wing Profiles and Propellers for Low Reynolds Numbers 192
“Virtual Design of UAV-VESPA for Mediterranean Sea Border Surveillance” 192
Analytical and experimental comparison of composite panels under combined biaxial compression and shear loads 191
Aeroelastic behavior of solar powered high altitude very long endurance unmanned air vehicle slender wing 191
Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams 189
Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs 189
Generalized topology for resonators having N commensurate harmonics 188
Scaled size prototype assembling 186
Second down selection test report for wing panels in AL-LI LASER welded 186
Analysis of slender thin-walled composite box-beams including local stiffness and coupling effects 186
Configuration and Estimation Cost of the flying platform HeliPlat® 185
Experimental Data of High Efficiency Wing Profiles and Propellers for Low Reynolds Numbers 185
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 183
Bearing Strength of bolted Joints in CFRP Wing Fittings 182
UVCS-SPA Joint tension and shear capability - Jointed panel buckling 181
Graphite/epoxy Materials for Structures with High Dimensional Stability used in the space project SOHO-UVCS. 4-point Bending, Bearing and CME tests of the M55J/M18 material = 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 179
The Cicala’s asymptotic approach to the linear shell theory, Modern Trend in the Foundation of the Theory of Shell and Plates 178
"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
HELIPLAT: Design of High altitude very-long endurance Solar Powered platform for telecommunication and earth observation applications 177
Safety assessment of pharmaceutical distribution in a hospital environment 176
Determinazione delle caratteristiche fisico-maccaniche del materiale composito GY70/M18 ed adesivo epossidico nell'ambito del programma spaziale SOHO-UVCS. Caratteristiche meccaniche. Determinazione dei coefficienti di espansione termica(CTE) ed igroscopico (CME). Tensione di ovalizzazione di giunzioni forate. 176
Structural Aerospace Composite/Metallic Samples under Fatigue Loads: Experimental Activity on Three Case Studies 172
"HALE UAV Solar Configuration: Reliability, Maintainability and Safety" 170
Experimental Behavior of composite advanced joint under cyclic loads 170
Totale 27.424
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Categoria #
all - tutte 102.728
article - articoli 32.039
book - libri 1.272
conference - conferenze 44.108
curatela - curatele 0
other - altro 21.705
patent - brevetti 879
selected - selezionate 0
volume - volumi 2.725
Totale 205.456
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.959 0 0 0 0 306 292 173 424 431 209 68 56
2020/20212.265 371 339 97 250 63 308 66 158 137 218 195 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
2024/20251.618 118 587 260 544 109 0 0 0 0 0 0 0
Totale 39.262