PORTO @ Archivio Istituzionale della Ricerca

MARSILIO, Roberto
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
EU - Europa 5326
NA - Nord America 5025
AS - Asia 691
SA - Sud America 17
OC - Oceania 11
AF - Africa 8
Continente sconosciuto - Info sul continente non disponibili 2
Totale 11080
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 4995
IT - Italia 1672
GB - Regno Unito 1074
DE - Germania 837
FR - Francia 692
UA - Ucraina 492
CN - Cina 282
TR - Turchia 202
SE - Svezia 155
RU - Federazione Russa 127
KR - Corea 75
NL - Olanda 72
FI - Finlandia 62
AT - Austria 46
IN - India 46
JP - Giappone 28
MY - Malesia 27
CA - Canada 21
BG - Bulgaria 20
TW - Taiwan 11
AP - ???statistics.table.value.countryCode.AP??? 10
AU - Australia 10
BE - Belgio 9
IE - Irlanda 9
IR - Iran 9
MX - Messico 9
VN - Vietnam 8
BR - Brasile 7
EU - Europa 7
AE - Emirati Arabi Uniti 6
CL - Cile 5
HR - Croazia 4
KZ - Kazakistan 4
ZA - Sudafrica 4
BY - Bielorussia 3
HK - Hong Kong 3
IL - Israele 3
RO - Romania 3
SG - Singapore 3
ES - Italia 2
ID - Indonesia 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
ET - Etiopia 1
GR - Grecia 1
IQ - Iraq 1
NG - Nigeria 1
NO - Norvegia 1
NZ - Nuova Zelanda 1
PE - Perù 1
PK - Pakistan 1
RS - Serbia 1
Totale 11080
Salva come PNG Salva come JPEG
Città #
Ashburn 1405
Southend 957
Seattle 563
Fairfield 451
Turin 298
Princeton 271
Jacksonville 250
Woodbridge 208
Houston 201
Ann Arbor 186
Wilmington 175
Izmir 170
Berlin 160
Chicago 141
San Ramon 139
Cambridge 135
Torino 121
Milan 89
Chandler 81
San Donato Milanese 69
Zhengzhou 66
Baltimore 63
Beijing 63
Helsinki 61
Zaporozhye 59
Pennsylvania Furnace 56
Overberg 55
Monopoli 51
Shanghai 50
Padua 49
Vienna 43
San Francisco 41
Rome 39
Bologna 34
Saint Petersburg 34
Malatya 27
Redwood City 24
Buffalo 19
Sofia 19
Hangzhou 15
Hyderabad 15
Rivoli 15
San Diego 15
Norwalk 14
Moscow 13
Redmond 13
Nanjing 12
Shenzhen 12
Asti 11
Falls Church 11
Fremont 11
Villanova 11
Guagnano 10
Moncalieri 10
Mountain View 10
Aosta 9
Genova 9
Melfi 9
Naples 9
Seoul 9
Varese 9
Austin 8
Ningbo 8
Toronto 8
Venaria Reale 8
Verona 8
Atlanta 7
Bardolino 7
Brescia 7
Brussels 7
Changsha 7
Dalian 7
Guangzhou 7
London 7
Melun 7
Montréal 7
Andrate 6
Birmingham 6
Florence 6
Nichelino 6
San Antonio 6
San Jose 6
Trieste 6
Washington 6
Boardman 5
Frankfurt 5
Lake Forest 5
Marco 5
Melito Di Napoli 5
Napoli 5
Novara 5
Novosibirsk 5
Samara 5
San Mateo 5
Savigliano 5
Alseno 4
Basking Ridge 4
Caserta 4
Chungnam 4
Cranfield 4
Totale 7408
Salva come PNG Salva come JPEG
Nome #
A Computational Method for Combustion in High Speed Flows 380
Numerical Simulation of Fluidic Thrust-Vectoring 310
A viscous inverse method for aerodynamic design 303
Interazione tra onde d'urto e strato limite: generazione di strutture vorticose in configurazioni tipo 'corner' 297
A computational approach to the simulation of controlled flows by synthetic jets actuators 245
A Numerical Method for the Study of Fluidic Thrust-Vectoring 224
A computational method for combustion in supersonic flows 221
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 218
A New Set of Boundary Conditions for Aerodynamic Design 216
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 210
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 207
A Shock-Fitting Spectral Method for the Study of Shock-Vortex Interactions 204
A Computational Method for Gas Turbine Engines 199
Numerical Simulation of Fluidic Thrust-Vectoring 197
Shock-induced separated structures in symmetric corner flows 196
A Numerical Method for Solving the Three-DimensionalParabolized Navier-Stokes Equations 195
Synthetic Jet Actuator Modeling for Flow Control Applications 189
Numerical Simulation of Transient Operations in Aeroengines 183
Shock-induced separated structures in symmetric corner flows 178
Euler Solver for 3D Inverse Problems 177
A numerical method for solving the three­dimensional Parabolized Navier-Stokes equations 177
Synthetic jet modeling for flow control applications 170
A CFD Method for Optimal Air-Intake Design 169
Asymmetric Vortical Solutions in Supersonic Corners:Steady 3D Space-marching Versus Time-Dependent Conical Results 166
Vortical Solutions in Supersonic Corner Flows 165
A Vortex-In-Cell Method for the Simulation of Viscous Flows 165
Shock-Fitting Method for Two-Dimensional Inviscid, Steady SupersonicFlows in Ducts 160
Numerical Simulations for Plug Nozzle Flowfields 159
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 154
Investigation of High Speed Flows over a Flat Plate 152
Frozen and Equilibrium Speeds of Sound in Non-equilibrium Flows 152
Inverse Problems for Advanced Nozzle Design. 145
Inverse Problem for Advance Nozzle Design 143
Numerical Approximation of Boundary Conditions for Initial-Boundary-Value Problems 140
Shock-Fitting Technique for High Speed Flows 140
Numerical Design of Dual-Bell Nozzle 140
Simulation of Jet Engine Transient by a CFD Method 140
An Eulerian-Lagrangian Method for Vortical Flow Simulations 138
Two-Dimensional Shock-Fitting for Inviscid, Steady, Supersonic, InternalFlows 134
Turbulent Model Validation for Spike Nozzle External Flows 133
Investigation of high speed flows over a flat plate 132
Computation of plug nozzle turbulent flowfields 128
Numerical Design of Dual-Bell Nozzles 127
Aerodynamic Design by Inverse Method 125
Interaction of Homogeneous Turbulence with a 3-D Shock Wave 123
High velocity flows over symmetric and asymmetric intake-type configurations 121
Implementation and Validation of the Spalart-AllmarasTurbulence Model for High Speed Flows 121
A Methodology to Solve External Flowfields in Aero-Spike Engines 120
Numerical Method for Designing 3D Turbomachinery Blade Rows 119
Studio Numerico dell'Interazione Tridimensionale Vortice-Urto 119
An Upwind 3D Space-Marching Procedure 117
Flussi Vorticosi Asimmetrici: Confronto tra due Metodi diCalcolo 115
Soluzioni Vorticose nei Flussi Supersonici Conici 115
Three-dimensional Numerical Simulation of Shock-VortexInteraction 112
High Velocity Flows over Symmetric and Asymmetric Intake-typeConfigurations 111
A Study of the Stability of Vortical Structures in Supersonic Inlets 109
Fluid-Dynamic Model of a Supersonic Jet Expansion: Comparison withExperimental Results 108
Inverse Problem for Spike Nozzle Design 108
Shock-Fitting in Three Space Dimensions 107
Non-equilibrium 3D Flows of Air Through Inlets 104
Una Metodologia Upwind per il calcolo di flussi Supersonici, Stazionari,Euleriani 103
Numerical Analysis of Supersonic Turbulent Flows over an Axisymmetric Afterbody 97
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 95
Numerical Analysis of the Supersonic Confluence Past a Jet-on Axisymmetric Afterbody 89
Shock Vector Control Technique for Aerospike Nozzles 78
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 76
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 75
Numerical simulation of the unsteady flowfield in complete propulsion systems 72
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 64
AI Assisted Detection of Shock Motions Inside a Transonic Duct 59
Numerical validation and analysis of supersonic retropropulsion test cases 57
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 57
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 55
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 51
Numerical Simulation of a Vectored Axisymmetric Nozzle 48
Design of a large wind tunnel for risk assessment on-board Oil & Gas Platforms 44
Computational Investigation of Injection Effects on Shock Vector Control Performance 41
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 39
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 21
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 16
Cold Gas Measurement System for Linear Aerospike Nozzles 13
Thermal-hydraulic and mechanical analysis of the Beam Line Components for the DTT Neutral Beam Injector 8
Technical summary of the injector for the CTT NBI system 7
Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector 1
Totale 11198
Salva come PNG Salva come JPEG
Categoria #
all - tutte 24210
article - articoli 4517
book - libri 0
conference - conferenze 17356
curatela - curatele 0
other - altro 1089
patent - brevetti 0
selected - selezionate 0
volume - volumi 1248
Totale 48420
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2017/20181555 0000 278211 363216 282948328
2018/20191451 6916206142 1599 389 152173324208
2019/20201349 1546048167 150122 102193 1681134131
2020/20211117 15613540146 78131 44104 401268235
2021/20221136 504910394 17121 4145 9189191245
2022/2023445 1222444336 00 00 0000
Totale 11198