PORTO @ Archivio Istituzionale della Ricerca

MARSILIO, Roberto
 Distribuzione geografica
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Continente #
NA - Nord America 8.160
EU - Europa 7.963
AS - Asia 5.129
SA - Sud America 465
AF - Africa 77
OC - Oceania 26
Continente sconosciuto - Info sul continente non disponibili 3
Totale 21.823
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Nazione #
US - Stati Uniti d'America 8.070
IT - Italia 2.828
SG - Singapore 1.483
VN - Vietnam 1.324
GB - Regno Unito 1.144
DE - Germania 978
CN - Cina 929
FR - Francia 878
RU - Federazione Russa 626
UA - Ucraina 502
BR - Brasile 383
KR - Corea 345
TR - Turchia 239
HK - Hong Kong 210
IN - India 203
IE - Irlanda 180
SE - Svezia 159
FI - Finlandia 118
NL - Olanda 115
CH - Svizzera 113
AT - Austria 97
BE - Belgio 72
JP - Giappone 67
BD - Bangladesh 52
CA - Canada 44
TH - Thailandia 37
TW - Taiwan 34
IQ - Iraq 33
MY - Malesia 33
AR - Argentina 32
MX - Messico 31
ID - Indonesia 27
ES - Italia 25
BG - Bulgaria 24
AU - Australia 23
PH - Filippine 23
CI - Costa d'Avorio 18
ZA - Sudafrica 17
IR - Iran 16
PK - Pakistan 14
IL - Israele 12
MA - Marocco 12
RO - Romania 12
CL - Cile 11
PL - Polonia 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
EG - Egitto 5
HR - Croazia 5
OM - Oman 5
PT - Portogallo 5
SN - Senegal 5
DK - Danimarca 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
CR - Costa Rica 1
EE - Estonia 1
ET - Etiopia 1
FJ - Figi 1
GA - Gabon 1
GD - Grenada 1
GE - Georgia 1
GP - Guadalupe 1
GT - Guatemala 1
GY - Guiana 1
HN - Honduras 1
HT - Haiti 1
Totale 21.813
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Città #
Ashburn 1.788
Southend 957
Singapore 828
Turin 724
San Jose 602
Seattle 578
Fairfield 451
Chandler 329
Ho Chi Minh City 329
Hanoi 309
Princeton 271
Jacksonville 250
Milan 249
Woodbridge 208
Houston 202
Ann Arbor 186
Dallas 184
Beijing 180
Wilmington 175
Seoul 171
Dublin 170
Izmir 170
Berlin 162
Hong Kong 159
Santa Clara 158
Chicago 153
Council Bluffs 146
Boardman 141
San Ramon 139
Cambridge 135
Torino 121
Los Angeles 113
Bern 111
Helsinki 92
Lauterbourg 88
Rome 85
Zhengzhou 74
Hefei 73
Da Nang 70
San Donato Milanese 69
Baltimore 63
Vienna 63
Brussels 62
Buffalo 61
Shanghai 61
Zaporozhye 59
Pennsylvania Furnace 56
Overberg 55
Monopoli 51
New York 51
Padua 51
Bologna 50
Haiphong 50
San Francisco 50
Moscow 42
Borgosesia 34
Munich 34
Saint Petersburg 34
Des Moines 32
North Bergen 29
Frankfurt am Main 27
Malatya 27
Istanbul 26
London 26
Redwood City 24
São Paulo 24
Tokyo 24
Guangzhou 21
Hải Dương 20
Naples 20
Orem 20
Sofia 19
The Dalles 19
Abidjan 18
Hangzhou 18
Jakarta 18
Washington 18
Changsha 17
Hyderabad 17
Atlanta 16
Columbus 15
Nanjing 15
Nuremberg 15
Rivoli 15
San Diego 15
Bangkok 14
Can Tho 14
Norwalk 14
Shenzhen 14
Florence 13
Fremont 13
Genoa 13
Lappeenranta 13
Redmond 13
Redondo Beach 13
Thái Nguyên 13
Bremen 12
Bến Tre 12
Turku 12
Asti 11
Totale 13.076
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Nome #
Divertor Tokamak Test facility project: status of design and implementation 551
A Computational Method for Combustion in High Speed Flows 489
A viscous inverse method for aerodynamic design 413
Numerical Simulation of Fluidic Thrust-Vectoring 374
Interazione tra onde d'urto e strato limite: generazione di strutture vorticose in configurazioni tipo 'corner' 368
A Numerical Method for the Study of Fluidic Thrust-Vectoring 324
A computational approach to the simulation of controlled flows by synthetic jets actuators 323
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 311
A computational method for combustion in supersonic flows 296
A New Set of Boundary Conditions for Aerodynamic Design 295
Shock-induced separated structures in symmetric corner flows 294
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 289
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 286
A Shock-Fitting Spectral Method for the Study of Shock-Vortex Interactions 280
Numerical Simulation of Fluidic Thrust-Vectoring 279
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 276
Design of a large wind tunnel for risk assessment on-board Oil & Gas Platforms 275
Innovative concepts in the DTT neutral beam injector 273
Synthetic jet modeling for flow control applications 270
A Numerical Method for Solving the Three-DimensionalParabolized Navier-Stokes Equations 267
A Computational Method for Gas Turbine Engines 263
A numerical method for solving the three­dimensional Parabolized Navier-Stokes equations 263
Synthetic Jet Actuator Modeling for Flow Control Applications 263
Experimental Characterization of a Linear Aerospike Nozzle Flow 261
A CFD Method for Optimal Air-Intake Design 258
Shock-induced separated structures in symmetric corner flows 255
Numerical Simulation of Transient Operations in Aeroengines 253
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 247
Euler Solver for 3D Inverse Problems 244
A Vortex-In-Cell Method for the Simulation of Viscous Flows 244
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 240
Numerical Simulations for Plug Nozzle Flowfields 234
Frozen and Equilibrium Speeds of Sound in Non-equilibrium Flows 232
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 231
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 228
Innovative Concepts in the Design of DTT Neutral Beam Injector. 227
Asymmetric Vortical Solutions in Supersonic Corners:Steady 3D Space-marching Versus Time-Dependent Conical Results 226
Vortical Solutions in Supersonic Corner Flows 225
Shock-Fitting Technique for High Speed Flows 218
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector 216
Numerical and Experimental Assessment of a Linear Aerospike 214
An Eulerian-Lagrangian Method for Vortical Flow Simulations 214
Shock-Fitting Method for Two-Dimensional Inviscid, Steady SupersonicFlows in Ducts 212
Inverse Problem for Advance Nozzle Design 210
Numerical Approximation of Boundary Conditions for Initial-Boundary-Value Problems 209
Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike 208
Numerical Design of Dual-Bell Nozzles 208
Computation of plug nozzle turbulent flowfields 206
Investigation of High Speed Flows over a Flat Plate 206
AI Assisted Detection of Shock Motions Inside a Transonic Duct 204
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 201
Two-Dimensional Shock-Fitting for Inviscid, Steady, Supersonic, InternalFlows 199
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 199
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 197
Aerodynamic Design by Inverse Method 193
Cold Gas Measurement System for Linear Aerospike Nozzles 193
Inverse Problems for Advanced Nozzle Design. 192
Numerical Method for Designing 3D Turbomachinery Blade Rows 191
Numerical Design of Dual-Bell Nozzle 191
A Methodology to Solve External Flowfields in Aero-Spike Engines 189
Interaction of Homogeneous Turbulence with a 3-D Shock Wave 188
An Upwind 3D Space-Marching Procedure 188
Simulation of Jet Engine Transient by a CFD Method 188
High velocity flows over symmetric and asymmetric intake-type configurations 186
Studio Numerico dell'Interazione Tridimensionale Vortice-Urto 186
Investigation of high speed flows over a flat plate 186
Flussi Vorticosi Asimmetrici: Confronto tra due Metodi diCalcolo 180
Soluzioni Vorticose nei Flussi Supersonici Conici 180
Numerical Study of the Flowfield in a Differentially-Throttled Linear Aerospike 179
A Study of the Stability of Vortical Structures in Supersonic Inlets 177
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 177
Technical summary of the injector for the CTT NBI system 175
Implementation and Validation of the Spalart-AllmarasTurbulence Model for High Speed Flows 174
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 171
Non-equilibrium 3D Flows of Air Through Inlets 170
Three-dimensional Numerical Simulation of Shock-VortexInteraction 168
A Framework for Testing Differential Throttling in Linear Aerospike Nozzle 166
Fluid-Dynamic Model of a Supersonic Jet Expansion: Comparison withExperimental Results 162
Turbulent Model Validation for Spike Nozzle External Flows 161
High Velocity Flows over Symmetric and Asymmetric Intake-typeConfigurations 158
Inverse Problem for Spike Nozzle Design 158
Shock-Fitting in Three Space Dimensions 158
Shock Vector Control Technique for Aerospike Nozzles 158
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 158
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 156
Una Metodologia Upwind per il calcolo di flussi Supersonici, Stazionari,Euleriani 154
Influence of Hot Flow Conditions on Nozzle Performances 153
Differential Throttling in Linear Aerospike: A Combined Experimental and Numerical Study 151
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 151
Numerical simulation of the unsteady flowfield in complete propulsion systems 148
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector. 146
Numerical Analysis of Supersonic Turbulent Flows over an Axisymmetric Afterbody 144
Passive Control of Vortices in the Wake of a Bluff Body 143
Numerical validation and analysis of supersonic retropropulsion test cases 143
A Two-Dimensional Analysis of the Flowfield and Performances of Linear Aerospikes During Differential Throttling 138
Assessment of a Thrust Measurement System for Supersonic Nozzles 138
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 136
Numerical Analysis of the Supersonic Confluence Past a Jet-on Axisymmetric Afterbody 134
Numerical Simulation of a Vectored Axisymmetric Nozzle 120
Vectorized Thrust Measurement for Aerospace Propulsion Nozzles 102
Totale 21.806
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Categoria #
all - tutte 64.097
article - articoli 13.813
book - libri 0
conference - conferenze 45.137
curatela - curatele 0
other - altro 2.760
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.387
Totale 128.194
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202135 0 0 0 0 0 0 0 0 0 0 0 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
2025/20266.368 405 338 468 475 305 386 964 458 1.465 651 171 282
Totale 22.047