PORTO @ Archivio Istituzionale della Ricerca

MARSILIO, Roberto
 Distribuzione geografica
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Continente #
NA - Nord America 8.480
EU - Europa 8.136
AS - Asia 5.240
SA - Sud America 488
Continente sconosciuto - Info sul continente non disponibili 236
AF - Africa 77
OC - Oceania 26
Totale 22.683
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Nazione #
US - Stati Uniti d'America 8.357
IT - Italia 2.973
SG - Singapore 1.527
VN - Vietnam 1.326
GB - Regno Unito 1.145
DE - Germania 983
CN - Cina 932
FR - Francia 882
RU - Federazione Russa 626
UA - Ucraina 502
BR - Brasile 390
KR - Corea 345
TR - Turchia 240
HK - Hong Kong 212
IN - India 206
IE - Irlanda 181
SE - Svezia 162
FI - Finlandia 118
NL - Olanda 116
CH - Svizzera 113
BD - Bangladesh 105
AT - Austria 97
BE - Belgio 73
JP - Giappone 70
CA - Canada 53
TH - Thailandia 37
AR - Argentina 35
ES - Italia 35
TW - Taiwan 34
IQ - Iraq 33
MY - Malesia 33
MX - Messico 32
ID - Indonesia 27
BG - Bulgaria 24
AU - Australia 23
PH - Filippine 23
CI - Costa d'Avorio 18
ZA - Sudafrica 17
CO - Colombia 16
IR - Iran 16
PK - Pakistan 14
EC - Ecuador 13
IL - Israele 12
MA - Marocco 12
PL - Polonia 12
RO - Romania 12
VE - Venezuela 12
CL - Cile 11
UZ - Uzbekistan 11
AP - ???statistics.table.value.countryCode.AP??? 10
JO - Giordania 10
KZ - Kazakistan 10
JM - Giamaica 8
AE - Emirati Arabi Uniti 7
DZ - Algeria 7
EU - Europa 7
NP - Nepal 7
SA - Arabia Saudita 7
CR - Costa Rica 6
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
PE - Perù 4
PY - Paraguay 4
TT - Trinidad e Tobago 4
AL - Albania 3
AZ - Azerbaigian 3
BY - Bielorussia 3
KE - Kenya 3
NI - Nicaragua 3
TG - Togo 3
BO - Bolivia 2
DO - Repubblica Dominicana 2
GD - Grenada 2
GR - Grecia 2
HN - Honduras 2
HU - Ungheria 2
KG - Kirghizistan 2
LU - Lussemburgo 2
MT - Malta 2
NZ - Nuova Zelanda 2
PR - Porto Rico 2
QA - Qatar 2
RS - Serbia 2
SV - El Salvador 2
TN - Tunisia 2
AO - Angola 1
AW - Aruba 1
BB - Barbados 1
BH - Bahrain 1
DM - Dominica 1
EE - Estonia 1
ET - Etiopia 1
FJ - Figi 1
Totale 22.435
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Città #
Ashburn 1.830
Southend 957
Singapore 830
Turin 736
San Jose 615
Seattle 579
Fairfield 451
Ho Chi Minh City 331
Chandler 329
Hanoi 309
Milan 290
Princeton 271
Jacksonville 250
Woodbridge 208
Houston 206
Council Bluffs 193
Ann Arbor 186
Dallas 186
Santa Clara 183
Beijing 180
Wilmington 175
Seoul 171
Dublin 170
Izmir 170
Berlin 162
Hong Kong 161
Chicago 155
Boardman 141
San Ramon 139
Cambridge 135
Torino 121
Los Angeles 117
Bern 111
Rome 106
Helsinki 92
Lauterbourg 88
Zhengzhou 74
Hefei 73
Da Nang 70
San Donato Milanese 69
Buffalo 65
Baltimore 64
Brussels 63
Vienna 63
Shanghai 61
Zaporozhye 59
New York 56
Pennsylvania Furnace 56
Overberg 55
Bologna 52
Padua 52
Monopoli 51
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
São Paulo 25
Redwood City 24
Tokyo 24
Naples 22
Figino 21
Guangzhou 21
Washington 21
Hải Dương 20
Orem 20
Sofia 19
The Dalles 19
Abidjan 18
Hangzhou 18
Jakarta 18
Changsha 17
Hyderabad 17
Atlanta 16
Florence 16
Bari 15
Columbus 15
Nanjing 15
Nuremberg 15
Rivoli 15
San Diego 15
Bangkok 14
Can Tho 14
Martina Franca 14
Norwalk 14
Shenzhen 14
Denver 13
Fremont 13
Genoa 13
Lappeenranta 13
Redmond 13
Redondo Beach 13
Thái Nguyên 13
Totale 13.335
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Nome #
Divertor Tokamak Test facility project: status of design and implementation 611
A Computational Method for Combustion in High Speed Flows 495
A viscous inverse method for aerodynamic design 418
Numerical Simulation of Fluidic Thrust-Vectoring 380
Interazione tra onde d'urto e strato limite: generazione di strutture vorticose in configurazioni tipo 'corner' 373
A computational approach to the simulation of controlled flows by synthetic jets actuators 327
A Numerical Method for the Study of Fluidic Thrust-Vectoring 327
Shock-induced separated structures in symmetric corner flows 317
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 313
A computational method for combustion in supersonic flows 299
A New Set of Boundary Conditions for Aerodynamic Design 297
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 288
Numerical Simulation of Fluidic Thrust-Vectoring 287
Innovative concepts in the DTT neutral beam injector 285
Design of a large wind tunnel for risk assessment on-board Oil & Gas Platforms 285
A Shock-Fitting Spectral Method for the Study of Shock-Vortex Interactions 284
Synthetic jet modeling for flow control applications 283
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 279
Experimental Characterization of a Linear Aerospike Nozzle Flow 273
A Numerical Method for Solving the Three-DimensionalParabolized Navier-Stokes Equations 272
A numerical method for solving the three­dimensional Parabolized Navier-Stokes equations 268
Synthetic Jet Actuator Modeling for Flow Control Applications 266
A Computational Method for Gas Turbine Engines 265
Shock-induced separated structures in symmetric corner flows 258
A CFD Method for Optimal Air-Intake Design 258
Numerical Simulation of Transient Operations in Aeroengines 256
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 252
Euler Solver for 3D Inverse Problems 246
A Vortex-In-Cell Method for the Simulation of Viscous Flows 246
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 244
Innovative Concepts in the Design of DTT Neutral Beam Injector. 241
Numerical Simulations for Plug Nozzle Flowfields 238
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 236
Frozen and Equilibrium Speeds of Sound in Non-equilibrium Flows 234
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 234
Asymmetric Vortical Solutions in Supersonic Corners:Steady 3D Space-marching Versus Time-Dependent Conical Results 232
Vortical Solutions in Supersonic Corner Flows 228
Numerical and Experimental Assessment of a Linear Aerospike 225
Shock-Fitting Technique for High Speed Flows 221
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector 219
An Eulerian-Lagrangian Method for Vortical Flow Simulations 216
Shock-Fitting Method for Two-Dimensional Inviscid, Steady SupersonicFlows in Ducts 216
Inverse Problem for Advance Nozzle Design 214
Numerical Approximation of Boundary Conditions for Initial-Boundary-Value Problems 212
Numerical Design of Dual-Bell Nozzles 211
Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike 210
Computation of plug nozzle turbulent flowfields 209
Investigation of High Speed Flows over a Flat Plate 209
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 206
AI Assisted Detection of Shock Motions Inside a Transonic Duct 206
Numerical Study of the Flowfield in a Differentially-Throttled Linear Aerospike 204
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 204
Two-Dimensional Shock-Fitting for Inviscid, Steady, Supersonic, InternalFlows 201
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 201
Aerodynamic Design by Inverse Method 196
Inverse Problems for Advanced Nozzle Design. 196
Flussi Vorticosi Asimmetrici: Confronto tra due Metodi diCalcolo 194
Cold Gas Measurement System for Linear Aerospike Nozzles 194
Numerical Design of Dual-Bell Nozzle 193
Simulation of Jet Engine Transient by a CFD Method 193
Numerical Method for Designing 3D Turbomachinery Blade Rows 192
A Methodology to Solve External Flowfields in Aero-Spike Engines 192
Studio Numerico dell'Interazione Tridimensionale Vortice-Urto 191
High velocity flows over symmetric and asymmetric intake-type configurations 190
An Upwind 3D Space-Marching Procedure 190
Investigation of high speed flows over a flat plate 189
Interaction of Homogeneous Turbulence with a 3-D Shock Wave 188
Technical summary of the injector for the CTT NBI system 183
Soluzioni Vorticose nei Flussi Supersonici Conici 182
A Study of the Stability of Vortical Structures in Supersonic Inlets 179
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 179
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 176
Implementation and Validation of the Spalart-AllmarasTurbulence Model for High Speed Flows 174
Non-equilibrium 3D Flows of Air Through Inlets 174
A Framework for Testing Differential Throttling in Linear Aerospike Nozzle 173
Three-dimensional Numerical Simulation of Shock-VortexInteraction 171
Differential Throttling in Linear Aerospike: A Combined Experimental and Numerical Study 166
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector. 166
Turbulent Model Validation for Spike Nozzle External Flows 166
Fluid-Dynamic Model of a Supersonic Jet Expansion: Comparison withExperimental Results 165
Shock Vector Control Technique for Aerospike Nozzles 163
Shock-Fitting in Three Space Dimensions 162
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 162
Inverse Problem for Spike Nozzle Design 160
High Velocity Flows over Symmetric and Asymmetric Intake-typeConfigurations 159
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 158
Una Metodologia Upwind per il calcolo di flussi Supersonici, Stazionari,Euleriani 158
Influence of Hot Flow Conditions on Nozzle Performances 155
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 155
Numerical simulation of the unsteady flowfield in complete propulsion systems 152
Assessment of a Thrust Measurement System for Supersonic Nozzles 149
Passive Control of Vortices in the Wake of a Bluff Body 148
A Two-Dimensional Analysis of the Flowfield and Performances of Linear Aerospikes During Differential Throttling 145
Numerical validation and analysis of supersonic retropropulsion test cases 145
Numerical Analysis of Supersonic Turbulent Flows over an Axisymmetric Afterbody 144
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 140
Numerical Analysis of the Supersonic Confluence Past a Jet-on Axisymmetric Afterbody 139
Numerical Simulation of a Vectored Axisymmetric Nozzle 121
Vectorized Thrust Measurement for Aerospace Propulsion Nozzles 111
Totale 22.346
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Categoria #
all - tutte 66.968
article - articoli 14.417
book - libri 0
conference - conferenze 47.257
curatela - curatele 0
other - altro 2.846
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.448
Totale 133.936
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.086 0 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
2025/20266.532 405 338 468 475 305 386 964 458 1.465 651 171 446
2026/2027472 282 190 0 0 0 0 0 0 0 0 0 0
Totale 22.683