PORTO @ Archivio Istituzionale della Ricerca

MARSILIO, Roberto
 Distribuzione geografica
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Continente #
EU - Europa 7.140
NA - Nord America 7.080
AS - Asia 3.035
SA - Sud America 407
AF - Africa 53
OC - Oceania 22
Continente sconosciuto - Info sul continente non disponibili 3
Totale 17.740
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Nazione #
US - Stati Uniti d'America 7.010
IT - Italia 2.611
SG - Singapore 1.227
GB - Regno Unito 1.120
DE - Germania 952
CN - Cina 875
FR - Francia 774
UA - Ucraina 501
BR - Brasile 346
KR - Corea 274
RU - Federazione Russa 241
TR - Turchia 235
IE - Irlanda 174
SE - Svezia 157
CH - Svizzera 112
NL - Olanda 107
FI - Finlandia 101
AT - Austria 96
HK - Hong Kong 90
IN - India 75
BE - Belgio 71
VN - Vietnam 68
JP - Giappone 39
CA - Canada 34
MY - Malesia 31
MX - Messico 27
AR - Argentina 26
BG - Bulgaria 23
ID - Indonesia 22
AU - Australia 20
CI - Costa d'Avorio 17
IQ - Iraq 16
IR - Iran 16
BD - Bangladesh 13
IL - Israele 12
ES - Italia 11
TW - Taiwan 11
ZA - Sudafrica 11
AP - ???statistics.table.value.countryCode.AP??? 10
PL - Polonia 10
RO - Romania 9
CL - Cile 8
CO - Colombia 8
VE - Venezuela 8
AE - Emirati Arabi Uniti 7
EU - Europa 7
JO - Giordania 7
KZ - Kazakistan 7
PK - Pakistan 7
UZ - Uzbekistan 7
DZ - Algeria 6
EC - Ecuador 5
MA - Marocco 5
CZ - Repubblica Ceca 4
DK - Danimarca 4
HR - Croazia 4
NP - Nepal 4
SN - Senegal 4
AZ - Azerbaigian 3
BY - Bielorussia 3
LT - Lituania 3
PE - Perù 3
TG - Togo 3
AL - Albania 2
EG - Egitto 2
GR - Grecia 2
KE - Kenya 2
KG - Kirghizistan 2
LU - Lussemburgo 2
LV - Lettonia 2
NZ - Nuova Zelanda 2
PT - Portogallo 2
PY - Paraguay 2
QA - Qatar 2
RS - Serbia 2
SA - Arabia Saudita 2
TT - Trinidad e Tobago 2
BB - Barbados 1
BO - Bolivia 1
DO - Repubblica Dominicana 1
EE - Estonia 1
ET - Etiopia 1
GA - Gabon 1
GD - Grenada 1
HN - Honduras 1
HT - Haiti 1
JM - Giamaica 1
KH - Cambogia 1
MD - Moldavia 1
MT - Malta 1
NG - Nigeria 1
NO - Norvegia 1
OM - Oman 1
PA - Panama 1
PH - Filippine 1
SK - Slovacchia (Repubblica Slovacca) 1
XK - ???statistics.table.value.countryCode.XK??? 1
Totale 17.740
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Città #
Ashburn 1.722
Southend 957
Turin 664
Singapore 640
Seattle 577
Fairfield 451
Chandler 329
Princeton 271
Jacksonville 250
Milan 222
Woodbridge 208
Houston 201
Ann Arbor 186
Dallas 178
Wilmington 175
Beijing 174
Izmir 170
Dublin 164
Berlin 162
Chicago 149
Santa Clara 142
San Ramon 139
Cambridge 135
Boardman 127
Torino 121
Seoul 120
Bern 111
Council Bluffs 95
Helsinki 76
Zhengzhou 74
Hefei 73
Hong Kong 71
Rome 71
San Donato Milanese 69
Baltimore 63
Vienna 62
Brussels 61
Shanghai 60
Zaporozhye 59
Buffalo 56
Pennsylvania Furnace 56
Overberg 55
Monopoli 51
Bologna 49
Los Angeles 49
Padua 49
San Francisco 47
Borgosesia 34
Saint Petersburg 34
Des Moines 32
Munich 32
North Bergen 29
New York 28
Malatya 27
Istanbul 24
Redwood City 24
London 23
Ho Chi Minh City 22
São Paulo 22
Frankfurt am Main 20
Guangzhou 20
San Jose 20
Sofia 19
Hanoi 18
Abidjan 17
Changsha 17
Hangzhou 17
Jakarta 17
Washington 17
Hyderabad 15
Moscow 15
Nanjing 15
Rivoli 15
San Diego 15
The Dalles 15
Naples 14
Norwalk 14
Nuremberg 14
Shenzhen 14
Florence 13
Fremont 13
Redmond 13
Redondo Beach 13
Lappeenranta 12
Turku 12
Asti 11
Brescia 11
Falls Church 11
Gilroy 11
Tokyo 11
Villanova 11
Atlanta 10
Belo Horizonte 10
Columbus 10
Genoa 10
Guagnano 10
Moncalieri 10
Mountain View 10
Tongling 10
Toronto 10
Totale 10.882
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Nome #
A Computational Method for Combustion in High Speed Flows 465
Divertor Tokamak Test facility project: status of design and implementation 385
A viscous inverse method for aerodynamic design 382
Numerical Simulation of Fluidic Thrust-Vectoring 349
Interazione tra onde d'urto e strato limite: generazione di strutture vorticose in configurazioni tipo 'corner' 346
A computational approach to the simulation of controlled flows by synthetic jets actuators 299
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 295
A Numerical Method for the Study of Fluidic Thrust-Vectoring 294
A computational method for combustion in supersonic flows 266
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 262
A New Set of Boundary Conditions for Aerodynamic Design 261
A Shock-Fitting Spectral Method for the Study of Shock-Vortex Interactions 258
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 256
Shock-induced separated structures in symmetric corner flows 251
Numerical Simulation of Fluidic Thrust-Vectoring 249
A Computational Method for Gas Turbine Engines 239
A Numerical Method for Solving the Three-DimensionalParabolized Navier-Stokes Equations 238
Numerical Simulation of Transient Operations in Aeroengines 234
Synthetic Jet Actuator Modeling for Flow Control Applications 234
A numerical method for solving the three­dimensional Parabolized Navier-Stokes equations 232
Synthetic jet modeling for flow control applications 227
Design of a large wind tunnel for risk assessment on-board Oil & Gas Platforms 223
Shock-induced separated structures in symmetric corner flows 222
A CFD Method for Optimal Air-Intake Design 219
Euler Solver for 3D Inverse Problems 217
A Vortex-In-Cell Method for the Simulation of Viscous Flows 217
Numerical Simulations for Plug Nozzle Flowfields 215
Asymmetric Vortical Solutions in Supersonic Corners:Steady 3D Space-marching Versus Time-Dependent Conical Results 210
Frozen and Equilibrium Speeds of Sound in Non-equilibrium Flows 200
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 198
Vortical Solutions in Supersonic Corner Flows 198
Experimental Characterization of a Linear Aerospike Nozzle Flow 193
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 193
Inverse Problem for Advance Nozzle Design 190
Shock-Fitting Method for Two-Dimensional Inviscid, Steady SupersonicFlows in Ducts 190
Shock-Fitting Technique for High Speed Flows 189
Numerical Design of Dual-Bell Nozzles 186
Computation of plug nozzle turbulent flowfields 186
An Eulerian-Lagrangian Method for Vortical Flow Simulations 184
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 183
Investigation of High Speed Flows over a Flat Plate 181
Numerical Approximation of Boundary Conditions for Initial-Boundary-Value Problems 180
Inverse Problems for Advanced Nozzle Design. 179
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 178
Simulation of Jet Engine Transient by a CFD Method 177
Innovative concepts in the DTT neutral beam injector 173
Two-Dimensional Shock-Fitting for Inviscid, Steady, Supersonic, InternalFlows 171
Aerodynamic Design by Inverse Method 171
Numerical Design of Dual-Bell Nozzle 169
A Methodology to Solve External Flowfields in Aero-Spike Engines 168
Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike 166
High velocity flows over symmetric and asymmetric intake-type configurations 165
An Upwind 3D Space-Marching Procedure 165
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector 164
Interaction of Homogeneous Turbulence with a 3-D Shock Wave 163
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 163
Numerical Method for Designing 3D Turbomachinery Blade Rows 161
Investigation of high speed flows over a flat plate 158
Studio Numerico dell'Interazione Tridimensionale Vortice-Urto 157
Implementation and Validation of the Spalart-AllmarasTurbulence Model for High Speed Flows 157
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 157
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 155
Soluzioni Vorticose nei Flussi Supersonici Conici 154
Flussi Vorticosi Asimmetrici: Confronto tra due Metodi diCalcolo 153
AI Assisted Detection of Shock Motions Inside a Transonic Duct 153
A Study of the Stability of Vortical Structures in Supersonic Inlets 152
Turbulent Model Validation for Spike Nozzle External Flows 147
Three-dimensional Numerical Simulation of Shock-VortexInteraction 145
Inverse Problem for Spike Nozzle Design 145
Non-equilibrium 3D Flows of Air Through Inlets 145
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 144
Shock-Fitting in Three Space Dimensions 137
High Velocity Flows over Symmetric and Asymmetric Intake-typeConfigurations 136
Fluid-Dynamic Model of a Supersonic Jet Expansion: Comparison withExperimental Results 135
Una Metodologia Upwind per il calcolo di flussi Supersonici, Stazionari,Euleriani 133
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 133
Cold Gas Measurement System for Linear Aerospike Nozzles 132
Numerical and Experimental Assessment of a Linear Aerospike 128
Innovative Concepts in the Design of DTT Neutral Beam Injector. 123
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 123
Shock Vector Control Technique for Aerospike Nozzles 119
Numerical simulation of the unsteady flowfield in complete propulsion systems 118
Numerical Analysis of the Supersonic Confluence Past a Jet-on Axisymmetric Afterbody 115
Numerical Analysis of Supersonic Turbulent Flows over an Axisymmetric Afterbody 115
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 110
Influence of Hot Flow Conditions on Nozzle Performances 109
Numerical Study of the Flowfield in a Differentially-Throttled Linear Aerospike 105
A Framework for Testing Differential Throttling in Linear Aerospike Nozzle 104
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 103
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 101
Technical summary of the injector for the CTT NBI system 96
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 96
Numerical Simulation of a Vectored Axisymmetric Nozzle 95
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector. 93
Numerical validation and analysis of supersonic retropropulsion test cases 93
Passive Control of Vortices in the Wake of a Bluff Body 78
Computational Investigation of Injection Effects on Shock Vector Control Performance 66
A Two-Dimensional Analysis of the Flowfield and Performances of Linear Aerospikes During Differential Throttling 64
Numerical simulations for plug nozzle flowfiels 47
Differential Throttling in Linear Aerospike: A Combined Experimental and Numerical Study 45
Totale 17.903
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Categoria #
all - tutte 56.322
article - articoli 12.044
book - libri 0
conference - conferenze 39.605
curatela - curatele 0
other - altro 2.477
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.196
Totale 112.644
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021562 0 0 0 0 0 131 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
2024/20252.634 50 282 103 287 198 143 246 156 374 260 253 282
2025/20262.267 405 338 468 475 305 276 0 0 0 0 0 0
Totale 17.946