PORTO @ Archivio Istituzionale della Ricerca

FRULLA, GIACOMO
 Distribuzione geografica
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Continente #
NA - Nord America 20.973
EU - Europa 17.985
AS - Asia 13.215
SA - Sud America 912
AF - Africa 149
OC - Oceania 51
Continente sconosciuto - Info sul continente non disponibili 8
-- - ???statistics.table.value.continent.--??? 1
Totale 53.294
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Nazione #
US - Stati Uniti d'America 20.768
IT - Italia 5.337
CN - Cina 4.940
SG - Singapore 3.054
GB - Regno Unito 2.978
DE - Germania 2.710
VN - Vietnam 2.153
FR - Francia 1.959
UA - Ucraina 1.239
RU - Federazione Russa 1.178
KR - Corea 757
BR - Brasile 680
TR - Turchia 550
NL - Olanda 436
IN - India 405
IE - Irlanda 382
HK - Hong Kong 377
SE - Svezia 364
FI - Finlandia 306
CH - Svizzera 299
BD - Bangladesh 167
AT - Austria 132
BE - Belgio 129
JP - Giappone 121
CA - Canada 102
AR - Argentina 85
RO - Romania 83
TH - Thailandia 81
IR - Iran 74
MY - Malesia 72
TW - Taiwan 70
CZ - Repubblica Ceca 69
PH - Filippine 66
ID - Indonesia 61
MX - Messico 61
AP - ???statistics.table.value.countryCode.AP??? 56
ES - Italia 46
IQ - Iraq 46
PL - Polonia 46
AU - Australia 45
PK - Pakistan 44
PT - Portogallo 40
IL - Israele 39
CO - Colombia 37
CL - Cile 33
EC - Ecuador 32
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
VE - Venezuela 10
AM - Armenia 9
CI - Costa d'Avorio 9
DK - Danimarca 9
MA - Marocco 9
MD - Moldavia 9
PY - Paraguay 9
CR - Costa Rica 8
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
JM - Giamaica 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
HN - Honduras 3
Totale 53.244
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Città #
Ashburn 4.181
Council Bluffs 2.776
Southend 2.559
Zhengzhou 2.492
Singapore 1.714
Seattle 1.401
Des Moines 1.118
San Jose 1.093
Turin 1.051
Chandler 938
Beijing 694
Fairfield 667
Jacksonville 631
Princeton 631
Ho Chi Minh City 604
Hanoi 505
Berlin 391
San Ramon 375
Dublin 371
Santa Clara 360
Ann Arbor 358
Chicago 346
Houston 336
Izmir 333
Milan 318
Boardman 317
Woodbridge 307
Seoul 296
Hong Kong 294
Torino 282
Wilmington 280
Bern 253
Helsinki 253
Cambridge 231
Los Angeles 225
San Donato Milanese 220
Shanghai 205
Lauterbourg 200
Guangzhou 190
Rome 162
Baltimore 148
Pennsylvania Furnace 140
Zaporozhye 140
Dallas 135
Herkenbosch 123
Overberg 123
Saint Petersburg 117
Moscow 113
Brussels 111
Monopoli 107
Vienna 105
Padua 103
Buffalo 99
Haiphong 96
New York 93
Fremont 91
Hangzhou 88
Da Nang 84
Hefei 81
Atlanta 75
Malatya 69
Redwood City 68
Frankfurt am Main 67
Galati 64
Munich 63
Alba 62
Bologna 61
Mountain View 58
Naples 57
Orem 55
São Paulo 54
Paris 52
Istanbul 50
Prague 50
Andover 48
Tokyo 47
London 45
Tongling 44
Amsterdam 43
Changsha 39
Ankara 37
Delft 37
Norwalk 36
Toronto 35
Bangkok 34
Nanjing 34
Washington 34
Dearborn 33
San Francisco 33
Valfenera 33
Verona 33
San Diego 32
Hải Dương 31
Columbus 29
Yubileyny 29
Falls Church 28
Florence 28
Palermo 26
San Antonio 26
Xian 26
Totale 33.860
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Nome #
HeliPlat: Design, Aerodynamic Structural Analysis of Long-Endurance Solar-Powered Stratospheric Platform 1.700
" Characterization of Several Advanced Composite Materials for CRV Space Program: Physical, chemical and mechanical properties; CME and CTE results" 1.662
" 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)". 1.586
Analysis of slender thin-walled anisotropic box-beams including local stiffness and coupling effects 1.410
COSTRUZIONI AERONAUTICHE: Eserciziario minimo con soluzioni 1.117
Delamination and fracture modeling techniques for shell composite structures in LS-DYNA 474
HELIPLAT: High altitude very-long endurance Solar Powered UAV for telecommunication and earth observation applications. 454
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 414
Structural Uncertainty Effect on Classical Wing Flutter Characteristics 407
"WindDesigner: An Open Tool for Analysis and Design of Wind Generators" 387
Development of an Aeroelastic Wing model with piezoelectric elements for gust load alleviation and Energy Harvesting 386
Wind Generator Innovative Blade Design: Variable Twist and Start-Up Control 383
Stability and Control of a High-Altitude-Long-Endurance UAV 366
Innovative Aircraft Aeroelastic Modelling and Control 356
Energy harvesting from aeroelastic vibrations induced by discrete gust loads 345
Design, manufacturing and testing of a HALE-UAV structural demonstrator 344
HELIPLAT®: Detail Design & Manufacturing of a Scaled Prototype for High Altitude Very-Long Endurance Solar-Powered RPAS 339
Very-Long Endurance Solar Powered Autonomous Stratospheric (Vespas) Air Vehicles For Sea Border Surveillance; Anti-Illegal Immigration And Gmes Applications 337
Experimental Slender Wing Model Design by the Application of Aeroelastic Scaling Laws 329
Nonlinear Angle of Twist of Advanced Composite Wing Boxes under Pure Torsion 326
Analisi strutturale di un'ala in materiale composito per un velivolo ad energia elettro-solare 318
An Invariant-based Performance-Oriented Procedure for Preliminary Design of Composite Structures 318
Parametric analysis of a fluttering piezoelectric wing 316
Environmental Friendly Inter-City Aircraft (ENFICA-FC) and Preliminary Analysis for 2-seat aircraft conversion into Fuel Cells Powered Innovative System 314
Topology Synthesis of Planar Ground Structures for Energy Harvesting Applications 312
Cicala's asymptotic approach to the linear shell theory 309
Design, Analysis and Experimental Testing of a Morphing Wing 308
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 308
A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings 307
Critical Behaviour of Slender Wing Configurations 299
A variable twist blade concept for more effective wind generation: design and realization 297
Structural aerospace composite/metallic samples under fatigue loads: experimental activity on three case studies 295
Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems 293
Piezo-Aeroelastic modeling and flutter prediction of flexible composite wings 292
Nonlinear LCO “amplitude-Frequency”Characteristics for Plates Fluttering at Supersonic Speeds 290
HELIPLAT®: a high altitude very-long endurance solar powered platform for border patrol and forest fire detection 289
Design of high-altitude long-endurance solar-powered unmanned air vehicle for multi-payload and operations 288
Innovative blade design for wind generator application 286
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 284
Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings 283
Second down selection test report for wing panels in AL-LI LASER welded 282
Indagine sullo stato dell'arte dei materiali innovativi nella realizzazione delle strutture dei sistemi produttivi 280
Nonlinear analysis of anisotropic plates with initial imperfections and various boundary conditions subjected to combined biaxial compression and shear loads 280
Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams 278
Attività di qualificazione di tubi e montanti in fibra di carbonio nell'ambito del programma SAX. Risultati delle prove meccaniche 278
Generalized topology for resonators having N commensurate harmonics 277
Determinazione delle caratteristiche igrotermiche di pannelli sandwich in grafite/epoxy nell'ambito del programma spaziale SOHO-UVCS 274
EQUIVALENT PLATE MODEL OF CURVILINEAR STIFFENED PANELS 274
A new test facility for measuring the coefficient of moisture expansion of advanced composite materials 274
Structural Aerospace Composite/Metallic Samples under Fatigue Loads: Experimental Activity on Three Case Studies 273
Constrained combinatorial optimization of multi-layered composite structures by means of Stud GA with proportionate selection and extinction 273
Considerations on beam-wise structural models used for aeroelastic analysis of slender wings 271
Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings 270
HELIPLAT: Aerodynamic and Structural Analysis of HAVE Solar Powered platform 268
Final Analytical Data of the Aerodynamics Performance of Wing Profiles and Propellers for Low Reynolds Numbers 267
Low weight advanced composite primary structure design of platform 265
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) 262
Postbuckling Behaviour of Graphite/Epoxy Stiffened Panels with initial Imperfections subjected to eccentric Biaxial Compression Loading 261
Analytical and experimental results of the coefficient of thermal expansion of high-modulus graphite/epoxy materials 261
Risultati sperimentali sull'incollaggio di strutture in grafite/epoxy 257
Preliminary Reliability Design of a Solar Powered high-altitude very long endurance unmanned air vehicle 255
Some considerations about the concepts of asymptotic approach 254
Scaled size prototype assembling 252
HELIPLAT: A Solar Powered HAVE-UAV for Telecommunication Applications. Design & Parametric Results. Analysis, Manufacturing & Testing of Advanced Composite Structures 251
A Possible Adaptive Wing Apparatus for New UAV Configurations 250
Stretched exponential structural relaxation of composite materials induced by impurities desorption in vacuum 249
Nonlinear Analysis of Graphite/Epoxy Wing Boxes under Pure Bending Including Lateral Pressure 248
SHAMPO: Solar HALE aircraft for multi-payload & operations 248
Structural Reliability Aspects for advanced Composite material Applications 246
Numerical/experimental structural characterization of composite advanced joints for HALE-UAV platforms 244
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 244
UVCS-SPA Joint tension and shear capability - Jointed panel buckling 241
The Influence of Supersonic Stream on the Dependence “Amplitude-Frequency” of Nonlinear Vibrations of Flexible Plate 241
Preliminary evaluation of the fatigue behaviour of aluminium alloy in corrosive environment 241
Materiali compositi grafite/epoxy per strutture ad alta stabilità dimensionale impiegati in programmi spaziali. Determinazione delle caratteristiche fisio-meccaniche del materiale M55J/M18 239
Safety Assessment of Pharmaceutical Distribution in a Hospital Environment 238
"The use of Vsaero CFD tool in the UAV Aero-dynamic project". 238
ENFICA-FC: All-electric aircraft Powered by Fuel Cells 236
Experimental Data of High Efficiency Wing Profiles and Propellers for Low Reynolds Numbers 236
Aeroelastic scaling laws with considerations to the design of an experimental slender wing model 236
“Virtual Design of UAV-VESPA for Mediterranean Sea Border Surveillance” 234
Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings 234
A Practical Engineering Approach to the Design and Manufacturing of a mini kW BladeWind Turbine: Definition, optimization and CFD Analysis 234
The Cicala’s asymptotic approach to the linear shell theory, Modern Trend in the Foundation of the Theory of Shell and Plates 233
Configuration and Estimation Cost of the flying platform HeliPlat® 233
Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs 233
A Nonlinear Beam Finite Element with Bending–Torsion Coupling Formulation for Dynamic Analysis with Geometric Nonlinearities 232
HELIPLAT: Design of High altitude very-long endurance Solar Powered platform for telecommunication and earth observation applications 231
"HALE UAV Solar Configuration: Reliability, Maintainability and Safety" 230
HELIPLAT:High Altitude very-long endurance Solar Powered UAV for telecommunication Applications. FEM analysis manufacturing and testing of 21m long CFRP wing box 229
Progetto S55 Replica 229
Experimental buckling behavior of composite aerospace structures after low velocity impact 228
Analytical and experimental comparison of composite panels under combined biaxial compression and shear loads 227
Preliminary design of anisotropic plate in critical and post-critical regime by extended Trace procedure 226
Critical Aeroelastic Behaviour of Slender Composite Wings in an Incompressible Flow 226
Analysis of slender thin-walled composite box-beams including local stiffness and coupling effects 226
HALE UAV Modular Configuration: Structure Analysis (FEM). Final Report 225
"CAPECON HALE UAV: Solar, Modular Configuration design " 222
Bearing Strength of bolted Joints in CFRP Wing Fittings 221
Totale 34.247
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Categoria #
all - tutte 142.472
article - articoli 45.166
book - libri 1.835
conference - conferenze 62.900
curatela - curatele 0
other - altro 28.148
patent - brevetti 1.042
selected - selezionate 0
volume - volumi 3.381
Totale 284.944
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202163 0 0 0 0 0 0 0 0 0 0 0 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
2025/202611.746 751 628 623 1.021 692 767 1.720 856 2.463 1.360 387 478
Totale 53.501