MARSILIO, Roberto
 Distribuzione geografica
Continente #
EU - Europa 6.533
NA - Nord America 6.225
AS - Asia 1.158
AF - Africa 31
SA - Sud America 23
OC - Oceania 15
Continente sconosciuto - Info sul continente non disponibili 2
Totale 13.987
Nazione #
US - Stati Uniti d'America 6.191
IT - Italia 2.300
GB - Regno Unito 1.099
DE - Germania 885
FR - Francia 702
UA - Ucraina 494
CN - Cina 356
SG - Singapore 242
TR - Turchia 225
RU - Federazione Russa 216
IE - Irlanda 173
SE - Svezia 155
KR - Corea 127
CH - Svizzera 112
NL - Olanda 92
FI - Finlandia 81
BE - Belgio 69
IN - India 58
AT - Austria 57
HK - Hong Kong 30
JP - Giappone 30
MY - Malesia 27
CA - Canada 24
BG - Bulgaria 23
ID - Indonesia 18
CI - Costa d'Avorio 17
AU - Australia 14
IR - Iran 12
BR - Brasile 11
TW - Taiwan 11
AP - ???statistics.table.value.countryCode.AP??? 10
IL - Israele 10
VN - Vietnam 10
MX - Messico 9
CL - Cile 7
EU - Europa 7
JO - Giordania 7
RO - Romania 7
AE - Emirati Arabi Uniti 6
CZ - Repubblica Ceca 4
DK - Danimarca 4
HR - Croazia 4
KZ - Kazakistan 4
ZA - Sudafrica 4
BY - Bielorussia 3
DZ - Algeria 3
BD - Bangladesh 2
ES - Italia 2
GR - Grecia 2
LT - Lituania 2
LU - Lussemburgo 2
LV - Lettonia 2
PL - Polonia 2
PT - Portogallo 2
SN - Senegal 2
TG - Togo 2
VE - Venezuela 2
AR - Argentina 1
CO - Colombia 1
EE - Estonia 1
EG - Egitto 1
ET - Etiopia 1
IQ - Iraq 1
MT - Malta 1
NG - Nigeria 1
NO - Norvegia 1
NZ - Nuova Zelanda 1
PA - Panama 1
PE - Perù 1
PK - Pakistan 1
QA - Qatar 1
RS - Serbia 1
Totale 13.987
Città #
Ashburn 1.579
Southend 957
Seattle 576
Turin 537
Fairfield 451
Chandler 329
Princeton 271
Jacksonville 250
Woodbridge 208
Houston 201
Singapore 197
Ann Arbor 186
Milan 182
Wilmington 175
Izmir 170
Dublin 164
Berlin 160
Chicago 144
San Ramon 139
Cambridge 135
Santa Clara 129
Boardman 123
Torino 121
Bern 111
Beijing 80
Helsinki 75
Council Bluffs 71
San Donato Milanese 69
Zhengzhou 66
Baltimore 63
Brussels 61
Zaporozhye 59
Pennsylvania Furnace 56
Overberg 55
Shanghai 54
Vienna 54
Monopoli 51
Padua 49
Rome 48
San Francisco 43
Bologna 41
Saint Petersburg 34
Borgosesia 33
Des Moines 32
Malatya 27
Redwood City 24
Istanbul 23
Buffalo 20
Sofia 19
London 18
Abidjan 17
Jakarta 17
Seoul 17
Washington 17
New York 16
Hangzhou 15
Hyderabad 15
Rivoli 15
San Diego 15
Norwalk 14
Fremont 13
Moscow 13
Naples 13
Redmond 13
Shenzhen 13
Hong Kong 12
Nanjing 12
Asti 11
Brescia 11
Falls Church 11
Florence 11
Gilroy 11
Villanova 11
Guagnano 10
Moncalieri 10
Mountain View 10
Varese 10
Aosta 9
Cranfield 9
Genoa 9
Genova 9
Melfi 9
Toronto 9
Atlanta 8
Austin 8
Bremen 8
Livorno Ferraris 8
Melbourne 8
Ningbo 8
Venaria Reale 8
Verona 8
Bardolino 7
Changsha 7
Dalian 7
Frankfurt am Main 7
Guangzhou 7
Melun 7
Montréal 7
San Jose 7
Tel Aviv 7
Totale 9.254
Nome #
A Computational Method for Combustion in High Speed Flows 421
A viscous inverse method for aerodynamic design 346
Numerical Simulation of Fluidic Thrust-Vectoring 328
Interazione tra onde d'urto e strato limite: generazione di strutture vorticose in configurazioni tipo 'corner' 327
A computational approach to the simulation of controlled flows by synthetic jets actuators 278
A Numerical Method for the Study of Fluidic Thrust-Vectoring 250
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 248
A computational method for combustion in supersonic flows 244
A New Set of Boundary Conditions for Aerodynamic Design 241
A Shock-Fitting Spectral Method for the Study of Shock-Vortex Interactions 238
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 232
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 226
Numerical Simulation of Fluidic Thrust-Vectoring 225
Shock-induced separated structures in symmetric corner flows 218
A Computational Method for Gas Turbine Engines 216
A Numerical Method for Solving the Three-DimensionalParabolized Navier-Stokes Equations 216
Synthetic Jet Actuator Modeling for Flow Control Applications 214
Numerical Simulation of Transient Operations in Aeroengines 212
A numerical method for solving the three­dimensional Parabolized Navier-Stokes equations 207
Shock-induced separated structures in symmetric corner flows 199
Euler Solver for 3D Inverse Problems 198
A CFD Method for Optimal Air-Intake Design 194
A Vortex-In-Cell Method for the Simulation of Viscous Flows 193
Asymmetric Vortical Solutions in Supersonic Corners:Steady 3D Space-marching Versus Time-Dependent Conical Results 189
Synthetic jet modeling for flow control applications 187
Numerical Simulations for Plug Nozzle Flowfields 183
Vortical Solutions in Supersonic Corner Flows 180
Frozen and Equilibrium Speeds of Sound in Non-equilibrium Flows 177
Shock-Fitting Method for Two-Dimensional Inviscid, Steady SupersonicFlows in Ducts 175
Shock-Fitting Technique for High Speed Flows 172
Inverse Problem for Advance Nozzle Design 165
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 165
Inverse Problems for Advanced Nozzle Design. 165
Investigation of High Speed Flows over a Flat Plate 161
An Eulerian-Lagrangian Method for Vortical Flow Simulations 159
Numerical Approximation of Boundary Conditions for Initial-Boundary-Value Problems 158
Numerical Design of Dual-Bell Nozzles 154
Aerodynamic Design by Inverse Method 153
Computation of plug nozzle turbulent flowfields 151
Numerical Design of Dual-Bell Nozzle 151
Two-Dimensional Shock-Fitting for Inviscid, Steady, Supersonic, InternalFlows 150
Simulation of Jet Engine Transient by a CFD Method 149
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 148
High velocity flows over symmetric and asymmetric intake-type configurations 144
Investigation of high speed flows over a flat plate 143
A Methodology to Solve External Flowfields in Aero-Spike Engines 139
Numerical Method for Designing 3D Turbomachinery Blade Rows 138
Studio Numerico dell'Interazione Tridimensionale Vortice-Urto 138
An Upwind 3D Space-Marching Procedure 138
Interaction of Homogeneous Turbulence with a 3-D Shock Wave 137
Turbulent Model Validation for Spike Nozzle External Flows 137
Implementation and Validation of the Spalart-AllmarasTurbulence Model for High Speed Flows 135
Soluzioni Vorticose nei Flussi Supersonici Conici 134
Non-equilibrium 3D Flows of Air Through Inlets 134
Design of a large wind tunnel for risk assessment on-board Oil & Gas Platforms 134
Experimental Characterization of a Linear Aerospike Nozzle Flow 133
Flussi Vorticosi Asimmetrici: Confronto tra due Metodi diCalcolo 130
A Study of the Stability of Vortical Structures in Supersonic Inlets 130
Three-dimensional Numerical Simulation of Shock-VortexInteraction 126
Inverse Problem for Spike Nozzle Design 125
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 124
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 124
High Velocity Flows over Symmetric and Asymmetric Intake-typeConfigurations 122
Fluid-Dynamic Model of a Supersonic Jet Expansion: Comparison withExperimental Results 118
Shock-Fitting in Three Space Dimensions 118
Una Metodologia Upwind per il calcolo di flussi Supersonici, Stazionari,Euleriani 116
AI Assisted Detection of Shock Motions Inside a Transonic Duct 116
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 115
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 106
Numerical Analysis of Supersonic Turbulent Flows over an Axisymmetric Afterbody 104
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 103
Numerical Analysis of the Supersonic Confluence Past a Jet-on Axisymmetric Afterbody 101
Divertor Tokamak Test facility project: status of design and implementation 98
Shock Vector Control Technique for Aerospike Nozzles 98
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 98
Numerical simulation of the unsteady flowfield in complete propulsion systems 89
Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike 84
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 84
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector 83
Cold Gas Measurement System for Linear Aerospike Nozzles 81
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 79
Numerical validation and analysis of supersonic retropropulsion test cases 76
Numerical Simulation of a Vectored Axisymmetric Nozzle 69
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 68
Numerical and Experimental Assessment of a Linear Aerospike 67
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 65
Influence of Hot Flow Conditions on Nozzle Performances 61
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 51
Technical summary of the injector for the CTT NBI system 49
Computational Investigation of Injection Effects on Shock Vector Control Performance 49
A Framework for Testing Differential Throttling in Linear Aerospike Nozzle 47
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 40
Passive Control of Vortices in the Wake of a Bluff Body 32
Numerical Study of the Flowfield in a Differentially-Throttled Linear Aerospike 31
Numerical simulations for plug nozzle flowfiels 27
Innovative concepts in the DTT neutral beam injector 17
Totale 14.168
Categoria #
all - tutte 43.998
article - articoli 8.811
book - libri 0
conference - conferenze 31.189
curatela - curatele 0
other - altro 2.076
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.922
Totale 87.996


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020648 0 0 0 0 0 0 102 193 168 113 41 31
2020/20211.117 156 135 40 146 78 131 44 104 40 126 82 35
2021/20221.136 50 49 103 94 17 121 41 45 91 89 191 245
2022/20231.406 122 244 43 127 136 191 122 62 134 20 70 135
2023/2024886 53 76 47 64 71 126 57 106 55 61 80 90
2024/20251.123 50 282 103 287 198 143 60 0 0 0 0 0
Totale 14.168