PORTO @ Archivio Istituzionale della Ricerca

MARSILIO, Roberto
 Distribuzione geografica
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Continente #
NA - Nord America 7.873
EU - Europa 7.804
AS - Asia 5.046
SA - Sud America 460
AF - Africa 75
OC - Oceania 25
Continente sconosciuto - Info sul continente non disponibili 3
Totale 21.286
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Nazione #
US - Stati Uniti d'America 7.792
IT - Italia 2.712
SG - Singapore 1.461
VN - Vietnam 1.316
GB - Regno Unito 1.135
DE - Germania 967
CN - Cina 922
FR - Francia 875
RU - Federazione Russa 617
UA - Ucraina 498
BR - Brasile 378
KR - Corea 341
TR - Turchia 239
HK - Hong Kong 206
IN - India 198
IE - Irlanda 178
SE - Svezia 159
FI - Finlandia 118
CH - Svizzera 113
NL - Olanda 111
AT - Austria 97
BE - Belgio 72
JP - Giappone 63
CA - Canada 37
TH - Thailandia 36
TW - Taiwan 34
IQ - Iraq 33
MY - Malesia 33
AR - Argentina 32
MX - Messico 31
ID - Indonesia 27
BD - Bangladesh 25
ES - Italia 25
BG - Bulgaria 24
PH - Filippine 23
AU - Australia 22
CI - Costa d'Avorio 18
ZA - Sudafrica 17
IR - Iran 16
PK - Pakistan 13
IL - Israele 12
CL - Cile 11
MA - Marocco 11
PL - Polonia 11
RO - Romania 11
UZ - Uzbekistan 11
VE - Venezuela 11
AP - ???statistics.table.value.countryCode.AP??? 10
CO - Colombia 10
JO - Giordania 10
KZ - Kazakistan 10
EC - Ecuador 9
AE - Emirati Arabi Uniti 7
DZ - Algeria 7
EU - Europa 7
NP - Nepal 7
SA - Arabia Saudita 7
CZ - Repubblica Ceca 5
HR - Croazia 5
OM - Oman 5
PT - Portogallo 5
SN - Senegal 5
DK - Danimarca 4
EG - Egitto 4
LT - Lituania 4
LV - Lettonia 4
PY - Paraguay 4
AL - Albania 3
AZ - Azerbaigian 3
BY - Bielorussia 3
KE - Kenya 3
PE - Perù 3
TG - Togo 3
TT - Trinidad e Tobago 3
DO - Repubblica Dominicana 2
GR - Grecia 2
HU - Ungheria 2
JM - Giamaica 2
KG - Kirghizistan 2
LU - Lussemburgo 2
NZ - Nuova Zelanda 2
QA - Qatar 2
RS - Serbia 2
TN - Tunisia 2
AO - Angola 1
BB - Barbados 1
BH - Bahrain 1
BO - Bolivia 1
EE - Estonia 1
ET - Etiopia 1
FJ - Figi 1
GA - Gabon 1
GD - Grenada 1
GE - Georgia 1
GT - Guatemala 1
GY - Guiana 1
HN - Honduras 1
HT - Haiti 1
KH - Cambogia 1
MD - Moldavia 1
Totale 21.278
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Città #
Ashburn 1.776
Southend 956
Singapore 818
Turin 707
Seattle 577
San Jose 493
Fairfield 449
Ho Chi Minh City 327
Chandler 325
Hanoi 306
Princeton 267
Jacksonville 250
Milan 231
Woodbridge 208
Houston 202
Ann Arbor 186
Dallas 181
Beijing 179
Wilmington 174
Izmir 170
Seoul 170
Dublin 168
Berlin 160
Hong Kong 156
Chicago 153
Santa Clara 152
San Ramon 139
Cambridge 134
Boardman 124
Torino 117
Bern 111
Los Angeles 107
Council Bluffs 106
Helsinki 92
Lauterbourg 87
Rome 75
Zhengzhou 74
Hefei 72
Da Nang 70
San Donato Milanese 69
Baltimore 63
Vienna 63
Brussels 62
Shanghai 61
Buffalo 59
Zaporozhye 59
Pennsylvania Furnace 56
Overberg 55
Monopoli 51
Padua 51
Haiphong 50
San Francisco 49
Bologna 45
New York 43
Moscow 42
Munich 34
Saint Petersburg 34
Borgosesia 33
Des Moines 32
North Bergen 29
Frankfurt am Main 27
Malatya 27
Istanbul 26
Redwood City 24
São Paulo 24
London 23
Tokyo 23
Guangzhou 21
Orem 20
Hải Dương 19
Sofia 19
The Dalles 19
Abidjan 18
Hangzhou 18
Jakarta 18
Washington 18
Changsha 17
Hyderabad 17
Atlanta 15
Columbus 15
Nanjing 15
Naples 15
Nuremberg 15
Rivoli 15
San Diego 15
Bangkok 14
Can Tho 14
Norwalk 14
Shenzhen 14
Florence 13
Fremont 13
Lappeenranta 13
Redmond 13
Redondo Beach 13
Thái Nguyên 13
Bremen 12
Bến Tre 12
Genoa 12
Turku 12
Asti 11
Totale 12.765
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Nome #
Divertor Tokamak Test facility project: status of design and implementation 512
A Computational Method for Combustion in High Speed Flows 488
A viscous inverse method for aerodynamic design 408
Numerical Simulation of Fluidic Thrust-Vectoring 373
Interazione tra onde d'urto e strato limite: generazione di strutture vorticose in configurazioni tipo 'corner' 366
A Numerical Method for the Study of Fluidic Thrust-Vectoring 321
A computational approach to the simulation of controlled flows by synthetic jets actuators 320
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 308
A computational method for combustion in supersonic flows 294
A New Set of Boundary Conditions for Aerodynamic Design 293
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 288
Shock-induced separated structures in symmetric corner flows 286
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 282
Numerical Simulation of Fluidic Thrust-Vectoring 277
A Shock-Fitting Spectral Method for the Study of Shock-Vortex Interactions 277
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 272
Synthetic jet modeling for flow control applications 267
A Numerical Method for Solving the Three-DimensionalParabolized Navier-Stokes Equations 266
Design of a large wind tunnel for risk assessment on-board Oil & Gas Platforms 266
A Computational Method for Gas Turbine Engines 262
A numerical method for solving the three­dimensional Parabolized Navier-Stokes equations 262
Synthetic Jet Actuator Modeling for Flow Control Applications 262
Experimental Characterization of a Linear Aerospike Nozzle Flow 259
Innovative concepts in the DTT neutral beam injector 258
A CFD Method for Optimal Air-Intake Design 256
Shock-induced separated structures in symmetric corner flows 253
Numerical Simulation of Transient Operations in Aeroengines 251
A Vortex-In-Cell Method for the Simulation of Viscous Flows 243
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 242
Euler Solver for 3D Inverse Problems 240
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 236
Numerical Simulations for Plug Nozzle Flowfields 232
Frozen and Equilibrium Speeds of Sound in Non-equilibrium Flows 229
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 228
Asymmetric Vortical Solutions in Supersonic Corners:Steady 3D Space-marching Versus Time-Dependent Conical Results 225
Vortical Solutions in Supersonic Corner Flows 223
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 220
Shock-Fitting Technique for High Speed Flows 217
Innovative Concepts in the Design of DTT Neutral Beam Injector. 215
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector 213
An Eulerian-Lagrangian Method for Vortical Flow Simulations 213
Numerical and Experimental Assessment of a Linear Aerospike 212
Shock-Fitting Method for Two-Dimensional Inviscid, Steady SupersonicFlows in Ducts 211
Inverse Problem for Advance Nozzle Design 209
Numerical Design of Dual-Bell Nozzles 207
Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike 205
Numerical Approximation of Boundary Conditions for Initial-Boundary-Value Problems 205
Computation of plug nozzle turbulent flowfields 205
Investigation of High Speed Flows over a Flat Plate 205
AI Assisted Detection of Shock Motions Inside a Transonic Duct 203
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 200
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 196
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 196
Two-Dimensional Shock-Fitting for Inviscid, Steady, Supersonic, InternalFlows 195
Cold Gas Measurement System for Linear Aerospike Nozzles 192
Aerodynamic Design by Inverse Method 191
Numerical Method for Designing 3D Turbomachinery Blade Rows 190
Inverse Problems for Advanced Nozzle Design. 190
Numerical Design of Dual-Bell Nozzle 189
An Upwind 3D Space-Marching Procedure 187
A Methodology to Solve External Flowfields in Aero-Spike Engines 187
Simulation of Jet Engine Transient by a CFD Method 187
High velocity flows over symmetric and asymmetric intake-type configurations 185
Interaction of Homogeneous Turbulence with a 3-D Shock Wave 185
Investigation of high speed flows over a flat plate 185
Studio Numerico dell'Interazione Tridimensionale Vortice-Urto 181
Soluzioni Vorticose nei Flussi Supersonici Conici 179
Flussi Vorticosi Asimmetrici: Confronto tra due Metodi diCalcolo 178
A Study of the Stability of Vortical Structures in Supersonic Inlets 175
Technical summary of the injector for the CTT NBI system 172
Numerical Study of the Flowfield in a Differentially-Throttled Linear Aerospike 172
Implementation and Validation of the Spalart-AllmarasTurbulence Model for High Speed Flows 169
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 169
Three-dimensional Numerical Simulation of Shock-VortexInteraction 167
Non-equilibrium 3D Flows of Air Through Inlets 167
A Framework for Testing Differential Throttling in Linear Aerospike Nozzle 165
Fluid-Dynamic Model of a Supersonic Jet Expansion: Comparison withExperimental Results 161
Turbulent Model Validation for Spike Nozzle External Flows 159
High Velocity Flows over Symmetric and Asymmetric Intake-typeConfigurations 157
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 157
Shock-Fitting in Three Space Dimensions 156
Shock Vector Control Technique for Aerospike Nozzles 156
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 155
Inverse Problem for Spike Nozzle Design 155
Una Metodologia Upwind per il calcolo di flussi Supersonici, Stazionari,Euleriani 153
Influence of Hot Flow Conditions on Nozzle Performances 151
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 147
Numerical simulation of the unsteady flowfield in complete propulsion systems 146
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector. 141
Numerical Analysis of Supersonic Turbulent Flows over an Axisymmetric Afterbody 141
Numerical validation and analysis of supersonic retropropulsion test cases 141
Differential Throttling in Linear Aerospike: A Combined Experimental and Numerical Study 140
Passive Control of Vortices in the Wake of a Bluff Body 138
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 135
Numerical Analysis of the Supersonic Confluence Past a Jet-on Axisymmetric Afterbody 131
A Two-Dimensional Analysis of the Flowfield and Performances of Linear Aerospikes During Differential Throttling 126
Assessment of a Thrust Measurement System for Supersonic Nozzles 120
Numerical Simulation of a Vectored Axisymmetric Nozzle 119
Vectorized Thrust Measurement for Aerospace Propulsion Nozzles 100
Computational Investigation of Injection Effects on Shock Vector Control Performance 86
Totale 21.385
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Categoria #
all - tutte 61.725
article - articoli 13.388
book - libri 0
conference - conferenze 43.285
curatela - curatele 0
other - altro 2.707
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.345
Totale 123.450
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021117 0 0 0 0 0 0 0 0 0 0 82 35
2021/20221.118 50 48 100 93 17 118 41 43 90 89 191 238
2022/20231.387 120 240 43 125 134 190 119 62 134 19 69 132
2023/2024870 51 74 45 63 66 126 57 105 53 61 79 90
2024/20252.599 49 278 97 286 197 138 242 151 371 258 252 280
2025/20265.935 400 334 466 472 300 384 958 454 1.447 644 76 0
Totale 21.501