MARSILIO, Roberto
 Distribuzione geografica
Continente #
EU - Europa 6.062
NA - Nord America 5.827
AS - Asia 766
AF - Africa 29
SA - Sud America 21
OC - Oceania 15
Continente sconosciuto - Info sul continente non disponibili 2
Totale 12.722
Nazione #
US - Stati Uniti d'America 5.797
IT - Italia 1.997
GB - Regno Unito 1.099
DE - Germania 872
FR - Francia 699
UA - Ucraina 494
CN - Cina 314
TR - Turchia 202
IE - Irlanda 173
SE - Svezia 155
RU - Federazione Russa 130
CH - Svizzera 111
KR - Corea 76
NL - Olanda 73
FI - Finlandia 72
AT - Austria 53
IN - India 50
BE - Belgio 41
JP - Giappone 29
MY - Malesia 27
HK - Hong Kong 23
CA - Canada 21
BG - Bulgaria 20
CI - Costa d'Avorio 17
AU - Australia 14
IR - Iran 11
TW - Taiwan 11
AP - ???statistics.table.value.countryCode.AP??? 10
VN - Vietnam 10
BR - Brasile 9
MX - Messico 9
CL - Cile 7
EU - Europa 7
JO - Giordania 7
RO - Romania 7
SG - Singapore 7
AE - Emirati Arabi Uniti 6
DK - Danimarca 4
HR - Croazia 4
KZ - Kazakistan 4
ZA - Sudafrica 4
BY - Bielorussia 3
DZ - Algeria 3
IL - Israele 3
BD - Bangladesh 2
CZ - Repubblica Ceca 2
ES - Italia 2
GR - Grecia 2
ID - Indonesia 2
LT - Lituania 2
LU - Lussemburgo 2
LV - Lettonia 2
PL - Polonia 2
PT - Portogallo 2
SN - Senegal 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
PE - Perù 1
PK - Pakistan 1
RS - Serbia 1
Totale 12.722
Città #
Ashburn 1.563
Southend 957
Seattle 574
Fairfield 451
Turin 444
Chandler 329
Princeton 271
Jacksonville 250
Woodbridge 208
Houston 201
Ann Arbor 186
Wilmington 175
Izmir 170
Dublin 164
Berlin 160
Milan 146
Chicago 144
San Ramon 139
Cambridge 135
Torino 121
Bern 111
Beijing 80
San Donato Milanese 69
Helsinki 67
Zhengzhou 66
Baltimore 63
Council Bluffs 62
Zaporozhye 59
Pennsylvania Furnace 56
Overberg 55
Monopoli 51
Shanghai 51
Vienna 50
Padua 49
Rome 47
San Francisco 42
Brussels 37
Bologna 36
Saint Petersburg 34
Des Moines 32
Boardman 31
Malatya 27
Redwood City 24
Buffalo 20
Sofia 19
London 18
Abidjan 17
Hangzhou 15
Hyderabad 15
Rivoli 15
San Diego 15
Norwalk 14
Fremont 13
Moscow 13
Redmond 13
Washington 13
Nanjing 12
Shenzhen 12
Asti 11
Falls Church 11
Naples 11
Villanova 11
Guagnano 10
Moncalieri 10
Mountain View 10
Seoul 10
Aosta 9
Cranfield 9
Florence 9
Genoa 9
Genova 9
Melfi 9
Varese 9
Atlanta 8
Austin 8
Bremen 8
Melbourne 8
New York 8
Ningbo 8
Toronto 8
Venaria Reale 8
Verona 8
Bardolino 7
Brescia 7
Changsha 7
Dalian 7
Guangzhou 7
Melun 7
Montréal 7
San Jose 7
Trieste 7
Andrate 6
Birmingham 6
Nichelino 6
San Antonio 6
Bresso 5
Dallas 5
Feltre 5
Frankfurt 5
Hong Kong 5
Totale 8.542
Nome #
A Computational Method for Combustion in High Speed Flows 402
A viscous inverse method for aerodynamic design 329
Numerical Simulation of Fluidic Thrust-Vectoring 323
Interazione tra onde d'urto e strato limite: generazione di strutture vorticose in configurazioni tipo 'corner' 309
A computational approach to the simulation of controlled flows by synthetic jets actuators 257
A computational method for combustion in supersonic flows 241
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 235
A Numerical Method for the Study of Fluidic Thrust-Vectoring 233
A Shock-Fitting Spectral Method for the Study of Shock-Vortex Interactions 231
A New Set of Boundary Conditions for Aerodynamic Design 230
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 223
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 221
Numerical Simulation of Fluidic Thrust-Vectoring 218
A Computational Method for Gas Turbine Engines 212
Shock-induced separated structures in symmetric corner flows 211
A Numerical Method for Solving the Three-DimensionalParabolized Navier-Stokes Equations 210
Numerical Simulation of Transient Operations in Aeroengines 205
Synthetic Jet Actuator Modeling for Flow Control Applications 205
A numerical method for solving the three­dimensional Parabolized Navier-Stokes equations 192
Shock-induced separated structures in symmetric corner flows 190
Euler Solver for 3D Inverse Problems 189
A CFD Method for Optimal Air-Intake Design 189
Asymmetric Vortical Solutions in Supersonic Corners:Steady 3D Space-marching Versus Time-Dependent Conical Results 185
A Vortex-In-Cell Method for the Simulation of Viscous Flows 185
Synthetic jet modeling for flow control applications 183
Numerical Simulations for Plug Nozzle Flowfields 177
Vortical Solutions in Supersonic Corner Flows 175
Frozen and Equilibrium Speeds of Sound in Non-equilibrium Flows 170
Shock-Fitting Method for Two-Dimensional Inviscid, Steady SupersonicFlows in Ducts 169
Shock-Fitting Technique for High Speed Flows 165
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 161
Inverse Problem for Advance Nozzle Design 160
Inverse Problems for Advanced Nozzle Design. 159
Investigation of High Speed Flows over a Flat Plate 157
An Eulerian-Lagrangian Method for Vortical Flow Simulations 153
Numerical Approximation of Boundary Conditions for Initial-Boundary-Value Problems 151
Numerical Design of Dual-Bell Nozzles 148
Two-Dimensional Shock-Fitting for Inviscid, Steady, Supersonic, InternalFlows 146
Computation of plug nozzle turbulent flowfields 146
Numerical Design of Dual-Bell Nozzle 146
Aerodynamic Design by Inverse Method 145
Simulation of Jet Engine Transient by a CFD Method 143
Investigation of high speed flows over a flat plate 137
High velocity flows over symmetric and asymmetric intake-type configurations 135
Turbulent Model Validation for Spike Nozzle External Flows 134
Studio Numerico dell'Interazione Tridimensionale Vortice-Urto 133
A Methodology to Solve External Flowfields in Aero-Spike Engines 133
An Upwind 3D Space-Marching Procedure 132
Numerical Method for Designing 3D Turbomachinery Blade Rows 131
Interaction of Homogeneous Turbulence with a 3-D Shock Wave 131
Implementation and Validation of the Spalart-AllmarasTurbulence Model for High Speed Flows 131
Soluzioni Vorticose nei Flussi Supersonici Conici 130
A Study of the Stability of Vortical Structures in Supersonic Inlets 128
Non-equilibrium 3D Flows of Air Through Inlets 128
Flussi Vorticosi Asimmetrici: Confronto tra due Metodi diCalcolo 125
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 125
Three-dimensional Numerical Simulation of Shock-VortexInteraction 122
Inverse Problem for Spike Nozzle Design 120
High Velocity Flows over Symmetric and Asymmetric Intake-typeConfigurations 116
Una Metodologia Upwind per il calcolo di flussi Supersonici, Stazionari,Euleriani 113
Shock-Fitting in Three Space Dimensions 112
Fluid-Dynamic Model of a Supersonic Jet Expansion: Comparison withExperimental Results 111
Numerical Analysis of Supersonic Turbulent Flows over an Axisymmetric Afterbody 100
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 100
AI Assisted Detection of Shock Motions Inside a Transonic Duct 99
Numerical Analysis of the Supersonic Confluence Past a Jet-on Axisymmetric Afterbody 97
Experimental Characterization of a Linear Aerospike Nozzle Flow 95
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 91
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 91
Shock Vector Control Technique for Aerospike Nozzles 89
Design of a large wind tunnel for risk assessment on-board Oil & Gas Platforms 87
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 83
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 82
Numerical simulation of the unsteady flowfield in complete propulsion systems 80
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 77
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 72
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 69
Numerical validation and analysis of supersonic retropropulsion test cases 67
Cold Gas Measurement System for Linear Aerospike Nozzles 64
Numerical Simulation of a Vectored Axisymmetric Nozzle 58
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector 57
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 50
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 45
Computational Investigation of Injection Effects on Shock Vector Control Performance 43
Influence of Hot Flow Conditions on Nozzle Performances 42
Numerical and Experimental Assessment of a Linear Aerospike 36
Technical summary of the injector for the CTT NBI system 32
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 28
Numerical simulations for plug nozzle flowfiels 23
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 15
Totale 12.878
Categoria #
all - tutte 37.078
article - articoli 6.991
book - libri 0
conference - conferenze 26.570
curatela - curatele 0
other - altro 1.805
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.712
Totale 74.156


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019532 0 0 0 0 0 0 0 0 0 0 324 208
2019/20201.349 154 60 48 167 150 122 102 193 168 113 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
2023/2024719 53 76 47 64 71 126 57 106 55 61 3 0
Totale 12.878