PORTO @ Archivio Istituzionale della Ricerca

FERRERO, ANDREA
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
EU - Europa 6.597
AS - Asia 4.531
NA - Nord America 4.195
SA - Sud America 378
AF - Africa 77
OC - Oceania 8
Continente sconosciuto - Info sul continente non disponibili 5
Totale 15.791
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 4.091
IT - Italia 3.010
SG - Singapore 1.267
VN - Vietnam 1.189
NL - Olanda 1.039
CN - Cina 840
RU - Federazione Russa 582
FR - Francia 433
GB - Regno Unito 427
DE - Germania 421
KR - Corea 292
BR - Brasile 288
HK - Hong Kong 261
IN - India 146
IE - Irlanda 131
BE - Belgio 127
TR - Turchia 81
CA - Canada 70
ID - Indonesia 69
JP - Giappone 58
UA - Ucraina 56
FI - Finlandia 54
SE - Svezia 52
AT - Austria 49
BG - Bulgaria 40
TH - Thailandia 40
ES - Italia 39
PH - Filippine 35
CH - Svizzera 34
JO - Giordania 30
IR - Iran 28
AR - Argentina 27
BD - Bangladesh 27
TW - Taiwan 27
IQ - Iraq 26
MX - Messico 24
PK - Pakistan 22
MY - Malesia 19
PL - Polonia 19
AE - Emirati Arabi Uniti 16
DZ - Algeria 15
EC - Ecuador 15
PT - Portogallo 15
CL - Cile 13
UZ - Uzbekistan 13
ZA - Sudafrica 13
SA - Arabia Saudita 12
ET - Etiopia 10
KZ - Kazakistan 10
CO - Colombia 9
PY - Paraguay 9
EG - Egitto 8
GR - Grecia 8
KE - Kenya 8
RO - Romania 8
DK - Danimarca 7
HR - Croazia 7
PE - Perù 7
VE - Venezuela 7
AU - Australia 6
CZ - Repubblica Ceca 5
EU - Europa 5
LV - Lettonia 5
MA - Marocco 5
NP - Nepal 5
TN - Tunisia 5
AL - Albania 4
IS - Islanda 4
LB - Libano 3
LU - Lussemburgo 3
NG - Nigeria 3
NO - Norvegia 3
OM - Oman 3
BO - Bolivia 2
BY - Bielorussia 2
CI - Costa d'Avorio 2
HN - Honduras 2
IL - Israele 2
KG - Kirghizistan 2
LA - Repubblica Popolare Democratica del Laos 2
LT - Lituania 2
MD - Moldavia 2
RS - Serbia 2
SO - Somalia 2
AM - Armenia 1
BA - Bosnia-Erzegovina 1
BB - Barbados 1
BH - Bahrain 1
BW - Botswana 1
BZ - Belize 1
CM - Camerun 1
CR - Costa Rica 1
DJ - Gibuti 1
DO - Repubblica Dominicana 1
EE - Estonia 1
GE - Georgia 1
GT - Guatemala 1
GY - Guiana 1
HU - Ungheria 1
LK - Sri Lanka 1
Totale 15.777
Salva come PNG Salva come JPEG
Città #
Amsterdam 984
Turin 833
Singapore 775
Ashburn 639
San Jose 412
Hanoi 286
Ho Chi Minh City 284
Southend 270
Milan 260
Chandler 254
Beijing 214
Hong Kong 194
Seoul 193
Torino 187
Houston 173
Santa Clara 170
Princeton 151
Hefei 141
Dallas 137
Council Bluffs 132
Dublin 125
Fairfield 121
Los Angeles 111
Rome 108
Wilmington 98
Berlin 92
Boardman 91
Brussels 90
Ann Arbor 86
Seattle 79
Moscow 70
Cambridge 67
Lauterbourg 64
Da Nang 61
Woodbridge 49
Jakarta 47
Frankfurt am Main 46
New York 46
Buffalo 43
Catania 41
The Dalles 41
San Francisco 39
Haiphong 35
Vienna 35
San Donato Milanese 34
Savigliano 34
Sofia 34
Bologna 32
Bordeaux 31
Chicago 31
Helsinki 30
Nichelino 30
Istanbul 29
Munich 28
Tokyo 28
Zogno 28
Shanghai 27
Naples 26
Paris 26
São Paulo 26
Talence 26
Izmir 25
Bern 23
Durham 22
Jacksonville 21
Nuremberg 21
Toronto 21
Bangkok 20
London 20
Palermo 20
Lappeenranta 19
Genoa 18
Menlo Park 18
Orem 18
Falls Church 17
Hải Dương 17
Redwood City 16
Biên Hòa 15
Guangzhou 15
Montreal 14
Redondo Beach 14
Washington 14
Arlington 13
Bari 13
Changsha 13
Norwalk 13
Rivoli 13
West Lafayette 13
Cangzhou 12
Florence 12
North Bergen 12
Novara 12
Tashkent 12
Thái Nguyên 12
Warsaw 12
Liège 11
Montréal 11
Roccavione 11
San Ramon 11
Trezzano sul Naviglio 11
Totale 9.479
Salva come PNG Salva come JPEG
Nome #
Computational fluid dynamics for aerospace propulsion systems: an approach based on discontinuous finite elements 1.140
High-order DG Method for an Implicit LES of a Gas Turbine Cascade 1.090
Turbomachinery design by a swarm-based optimization method coupled with a CFD solver 528
A robust and adaptive recovery-based discontinuous Galerkin method for the numerical solution of convection-diffusion equations 390
Dual-bell nozzle with fluidic control of transition for space launchers 324
Rheological and Mechanical Characterization of 3D Printable Solid Propellant Slurry 312
Adaptive CFD schemes for aerospace propulsion 305
Feedback filtering in discontinuous Galerkin methods for Euler equations 285
Multiphysics Modeling for Combustion Instability in Paraffin-Fueled Hybrid Rocket Engines 266
A zonal Galerkin-free POD model for incompressible flows 265
Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance 257
RANS simulation of secondary flows in a low pressure turbine cascade: Influence of inlet boundary layer profile 257
Multi physics modelling for a hybrid rocket engine with liquefying fuel: a sensitivity analysis on combustion instability 254
Advancements in Photocurable Solid Propellantsfor Additive Manufacturing 249
Design Optimization of a Mg/CO2 Hybrid Rocket Engine for Mars Ascent Vehicles 246
Evaluation of UV-Curable Solid Rocket Propellants’ Properties for Advanced 3D Printing Technologies 237
Multi-objective Optimization of Electric Pumps for Hybrid Rocket Engines 228
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 228
Emission-Driven Hybrid Rocket Engine Optimization for Small Launchers 227
Numerical investigation of different configurations for hydrogen fuelled jet engine combustors 221
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 220
Preliminary study of a resonant igniter for Rocket Engines 217
Data-driven modeling of broadband trailing-edge noise 214
Machine learning methods for the simulation of turbulent flows in turbomachinery 202
FIELD INVERSION AND MACHINE LEARNING STRATEGIES FOR IMPROVING RANS MODELLING IN TURBOMACHINERY 201
Mixed Averaging Procedures 199
Swirl Injection Modeling for Paraffin-Based Hybrid Rocket Engines Combustion Instabilities 199
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 196
A Numerical Study of the Spanwise Turbulence Past a Cylinder Flow 185
Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction 179
The role of uncertainty in data-driven turbulence modelling 175
Field inversion for data-augmented RANS modelling in turbomachinery flows 173
RANS Simulations of Advanced Nozzle Performance and Retro-Flow Interactions for Vertical Landing of Reusable Launch Vehicles 172
SENSITIVITY ANALYSIS OF ANALYTICAL MODELS FOR THE PREDICTION OF TRAILING-EDGE NOISE 170
Simulation of secondary flows in turbomachinery by the discontinuous Galerkin method 168
Contribution to Case C1.2b: Flow over the NACA0012 airfoil ­ transonic case 168
Numerical Validation of a Swirl Injection Model for a Paraffin-Based Hybrid Rocket Engine 167
RANS closure approximation by artificial neural networks 166
Contribution to Case C1.3: Flat plate boundary layer 165
Low-Order Models for Low-Frequency Combustion Instability in Hybrid Rocket Engines 165
Pintle Injector Spray Study via Physics-Based Spray Model and Generative Adversarial Networks 160
Numerical investigation for performance prediction of gas dynamic resonant igniters 160
Registration-based model reduction of parameterized two-dimensional conservation laws 160
Fluidic control of transition in a dual-bell nozzle 157
Multiphysics Modelling of a Hybrid Rocket Engine 157
Comparison of Methods for Thermodynamic Modelling of Cryogenic Storage Systems for Aerospace Applications 156
Shock Vector Control Technique for Aerospike Nozzles 156
Integrated Numerical Modeling of a Hydrogen Turbofan Engine and Fuel System With Alternative Thermodynamic Cycles 156
REYNOLDS STRESS CORRECTION BY MACHINE LEARNING METHODS WITH PHYSICAL CONSTRAINTS 153
Contribution to Case C1.6: Vortex transport 152
Contribution to Case C1.2: Transonic Ringleb flow 152
A Comparison of Local and Global Strategies for Exploiting Field Inversion on Separated Flows at Low Reynolds Number 151
A hybrid numerical flux for supersonic flows with application to rocket nozzles 150
Reynolds stress correction by data assimilation methods with physical constraints 149
Global and local POD models for the prediction of compressible flows with DG methods 148
Dual-bell nozzle for space launchers with fluidic control of transition 145
Contribution to Case C1.1: Inviscid Flow through a Channel with a Smooth Bump 144
A Numerical Method for Burnback Analysis of UV-cured Solid Rocket Propellant Grains 141
The Filtering Approach as a Tool for Modeling and Analyzing Turbulence 141
Uncertainty propagation in field inversion for turbulence modelling in turbomachinery 140
A study on the statistical convergence of turbulence simulations around a cylinder 139
Unstructured discretisation of a non-local transition model for turbomachinery flows 134
An hybrid numerical flux for supersonic flows with application to rocket nozzles 133
Data-Driven Aeroacoustic Modelling: Trailing-Edge Noise 127
Plasma Actuator–Assisted Rocket Nozzle for Improved Launcher Performance 126
Reduced order modelling for turbomachinery shape design 126
Enhancing turbulence modeling with data-driven approaches: a focus on the field inversion and machine learning paradigm 124
Control of a Supersonic Inlet in Off-Design Conditions with Plasma Actuators and Bleed 123
Parametric study of transition fluidic control in a dual-bell nozzle 120
A numerical study on automatic mesh refinement for the simulation of Edney shock-shock interactions 116
A penalisation approach to simulate root compressors 116
Preliminary Validation and Sensitivity Analysis on a Eulerian/Lagrangian RANS Approach for Liquid Injection in Supersonic Crossflow 115
Reduction of Chemical Kinetic Mechanisms for Oxygen/Methane Liquid Rocket Engines 100
Inverse Design of Additive Manufactured Rocket Propellant Grains with Non-Uniform Properties 96
NOx Emission Prediction of a Lean Premixed Hydrogen Combustor via Reactor Network Analysis 87
Optimization of Solid Rocket Motor Grains Exploiting Non-Uniform Ballistic Properties of 3D-Printed Propellants 86
A Chemical Reactor Network methodology for estimating NOx emissions under non-premixed lean hydrogen combustion with water injection 74
A machine-learning based approach for multi-scale optimisation of heat exchangers with lattice-like topology 64
Multi-Fidelity Modeling of a Lean Premixed Swirl-Stabilized Hydrogen Burner with Axial Air Injection 61
Generalizable Graph Neural Operators for Field Inversion Based RANS Corrections 61
Reduced-Order Modeling and Active Subspace to Support Shape Optimization of Centrifugal Pumps 10
Totale 16.176
Salva come PNG Salva come JPEG
Categoria #
all - tutte 39.023
article - articoli 15.302
book - libri 0
conference - conferenze 19.870
curatela - curatele 0
other - altro 2.045
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 76.240
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202164 0 0 0 0 0 0 0 0 0 0 23 41
2021/20221.221 29 28 42 88 52 107 148 107 96 119 184 221
2022/20231.283 84 163 43 112 117 142 90 118 175 64 90 85
2023/20241.069 44 86 69 64 67 120 97 172 80 50 118 102
2024/20252.616 67 202 127 273 191 152 219 222 354 182 260 367
2025/20267.301 407 304 412 505 362 375 1.035 654 2.470 714 63 0
Totale 16.176