RE.PUBLIC@POLIMI pubblicazioni di ricerca del Politecnico di Milano

VIGEVANO, LUIGI
 Distribuzione geografica
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Continente #
NA - Nord America 5.707
EU - Europa 4.180
AS - Asia 1.953
SA - Sud America 691
AF - Africa 93
OC - Oceania 9
Continente sconosciuto - Info sul continente non disponibili 2
Totale 12.635
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Nazione #
US - Stati Uniti d'America 5.552
RU - Federazione Russa 1.368
IT - Italia 1.061
SG - Singapore 702
CN - Cina 625
BR - Brasile 601
UA - Ucraina 368
DE - Germania 287
VN - Vietnam 249
GB - Regno Unito 187
SE - Svezia 182
AT - Austria 179
FI - Finlandia 148
CA - Canada 126
FR - Francia 85
NL - Olanda 83
IN - India 77
IE - Irlanda 74
KR - Corea 63
ES - Italia 57
TR - Turchia 38
BE - Belgio 34
HK - Hong Kong 32
AR - Argentina 31
CH - Svizzera 25
BD - Bangladesh 24
ID - Indonesia 20
MX - Messico 20
ZA - Sudafrica 18
MA - Marocco 17
IQ - Iraq 16
PK - Pakistan 16
CO - Colombia 15
PY - Paraguay 13
CI - Costa d'Avorio 12
EG - Egitto 12
JO - Giordania 10
PL - Polonia 9
UY - Uruguay 8
DZ - Algeria 7
JP - Giappone 7
SA - Arabia Saudita 7
VE - Venezuela 7
AU - Australia 6
AZ - Azerbaigian 6
GR - Grecia 6
PH - Filippine 6
UZ - Uzbekistan 6
BJ - Benin 5
EC - Ecuador 5
IL - Israele 5
KZ - Kazakistan 5
MY - Malesia 5
NG - Nigeria 5
PE - Perù 5
SI - Slovenia 5
TH - Thailandia 5
KE - Kenya 4
MU - Mauritius 4
NO - Norvegia 4
NP - Nepal 4
AM - Armenia 3
CL - Cile 3
HR - Croazia 3
IR - Iran 3
NZ - Nuova Zelanda 3
OM - Oman 3
TN - Tunisia 3
AL - Albania 2
BO - Bolivia 2
BY - Bielorussia 2
DK - Danimarca 2
EU - Europa 2
JM - Giamaica 2
KG - Kirghizistan 2
KH - Cambogia 2
LB - Libano 2
PS - Palestinian Territory 2
PT - Portogallo 2
TW - Taiwan 2
AE - Emirati Arabi Uniti 1
AO - Angola 1
BA - Bosnia-Erzegovina 1
BH - Bahrain 1
BS - Bahamas 1
BW - Botswana 1
CD - Congo 1
CR - Costa Rica 1
CY - Cipro 1
CZ - Repubblica Ceca 1
DO - Repubblica Dominicana 1
EE - Estonia 1
ET - Etiopia 1
GE - Georgia 1
GY - Guiana 1
HN - Honduras 1
LC - Santa Lucia 1
LK - Sri Lanka 1
LT - Lituania 1
LY - Libia 1
Totale 12.628
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Città #
Fairfield 581
Ashburn 562
Woodbridge 469
Singapore 394
Milan 384
Chandler 358
Houston 308
Wilmington 303
Ann Arbor 287
Seattle 231
Moscow 209
Dallas 206
Cambridge 205
Jacksonville 205
Santa Clara 193
Vienna 176
Hefei 152
Dearborn 122
Beijing 121
Council Bluffs 113
Boardman 109
Lawrence 99
Dong Ket 74
Dublin 72
Medford 68
Los Angeles 65
Ottawa 65
Helsinki 49
São Paulo 49
Shanghai 45
Málaga 42
Buffalo 41
Ho Chi Minh City 39
Rome 38
Amsterdam 36
Princeton 32
Des Moines 31
Montreal 30
San Diego 28
Brussels 25
Hanoi 25
Kent 23
Pusan 23
Redwood City 23
Delft 21
Hong Kong 21
Rio de Janeiro 21
Bovisio Masciago 20
Izmir 20
Seoul 19
Frankfurt am Main 18
The Dalles 18
Munich 17
Falkenstein 16
Toronto 16
Atlanta 13
Columbus 13
Glasgow 13
New York 13
Zibido San Giacomo 13
Abidjan 12
Belo Horizonte 12
London 12
Norwalk 12
Verona 12
Leeds 11
Saronno 11
Seregno 11
Tianjin 11
Zurich 11
Amman 10
Casablanca 10
Sarezzo 10
Brasília 9
Brooklyn 9
Dhaka 9
Jakarta 9
Johannesburg 9
Monza 9
Nanjing 9
Paris 9
Porto Alegre 9
Campinas 8
Denver 8
Xi'an 8
Asunción 7
Auburn Hills 7
Bengaluru 7
Bogotá 7
Cairo 7
Central District 7
Changsha 7
Chicago 7
Goiânia 7
Guangzhou 7
Miami 7
Mountain View 7
North York 7
Robbiate 7
Seongnam 7
Totale 7.337
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Nome #
Computational Assessment of Wind Tunnel Flow in Closed and Open Section Model Rotor Tests 255
Multi-Fidelity Numerical Approach to Aeroacoustics of Tandem Propellers in eVTOL Airplane Mode 251
Assessment of the Vorticity Confinement Technique Applied to Rotorcraft Flows 228
Single Blade Computations of Helicopter Rotors in Forward Flight 208
Simulation of a Complete Helicopter: a CFD Approach to the Study of Interference Effects 201
A Node-Pair Finite Element/Volume Mesh Adaptation Technique for Compressible Flows Based on a Hierarchical Approach 197
CFD Prediction of Air Flow Past a Full Helicopter Configuration 194
Hybrid Grid Generation for Two-Dimensional High-Reynolds Flows 188
High-Speed Trains: Prediction of Micro-Pressure Wave Radiation from Tunnel Portals 188
GARTEUR activities on acoustical methods and experiments for studying on acoustic scattering 188
Numerical modelling of the aerodynamic interference between helicopter and ground obstacles 181
On the Boundary Layer/Riblets Interaction Mechanisms and the Prediction of Turbulent Drag Reduction 178
The Blind-Test Activity of the GOAHEAD Project 173
Incompressible Navier-Stokes Solutions by a Triangular Spectral/p Element Projection Method 172
Roe Linearization for the van der Waals Gas 171
Assessment of CFD Methods Against Experimental Flow Measurements for Helicopter Flows 170
Aeroacoustic modeling of helicopter transonic rotor noise 169
CFD Prediction of Air Flow Past a Full Helicopter Configuration 165
An Edge-Based Mesh Adaption Technique for Two-Dimensional Compressible Flows on Unstructured Grids 163
Mathematical Modeling of NOx Emission Reduction by the Use of Reburn Technologies in Utility Boilers 163
Influence of Wind-Tunnel Walls in Helicopter Aerodynamics Predictions 160
Assessment of Thermodynamic Models for Dense Gas Dynamics 160
Low Dissipation Entropy Fix for Positivity Preserving Roe's Scheme 159
An Evaluation of Roe's Scheme Generalizations for Equilibrium Real Gas Flows 158
The Effect of Far-Field Boundary Conditions on Tip Vortex Path Prediction in Hovering 157
Numerical investigations of the vortex feature-based vorticity confinement models for the assessment in three-dimensional vortex-dominated flows 154
Finite Element/Volume Solution to Axisymmetric Conservation Laws 150
Assessment of the Vortex Feature-Based Vorticity Confinement Method Applied to Rotor Aerodynamics and Aeroacoustics 149
Assessment of CFD Methods Against Experimental Flow Measurements for Helicopter Flows 148
Accurate Omega-Psi Spectral Solution of the Singular Driven Cavity Problem 145
Evaluation of Acoustic Shielding Effects from a Generic GARTEUR Helicopter Configuration 145
Sonic Boom Propagation Revisited: a Nonlinear Geometrical Acoustic Model 143
EROS - a Common European Euler Code for the Analysis of the Helicopter Rotor Flowfield 140
Kinetic Node-Pair Formulation for Two-Dimensional Flows from Continuum to Transitional Regime 139
Numerical Analysis of the Effect of Different Nose Shapes on Train Aerodynamic Performance 137
Sonic Boom Propagation with a Nonlinear Geometrical Acoustic Model 135
Design of a Generic Rotor Noise Source for Helicopter Fuselage Scattering Tests 134
Fast Free Wake: a Possible Approach to Real-Time Rotor Wake Simulation 131
Simulation of a Complete Helicopter: a CFD Approach to the Study of Interference Effects 131
Numerical Solution of Under-Resolved Detonations 129
An Emission Surface Approach for Noise Propagation from High Speed Sources 128
Shaft Angle Corrections for Rotor Tests in a Closed Section Wind Tunnel 126
An Efficient Helicopter Main Rotor Trim Method Based on Computational Fluid Dynamics 124
Evaluation of Tilt-Rotor Performance with a CFD Method 124
Acoustical Methods and Experiments for Studying Rotorcraft Fuselage Scattering 124
A Fast Chemistry Model for Coal-Gas Reburning 123
Riduzione della resistenza di attrito in correnti turbolente e altezza di protrusione di correnti scanalate 120
A Reduced Order Methodology for the Parametric Analysis of Rotor Aerodynamics 119
CFD Analysis of Tilt-Rotor Performance in Steady Flow 119
An Edge-based Anisotropic Mesh Adaptation Technique for Unstructured Hybrid Grids in Two Dimensions 118
A Node-Pair BGK Kinetic Scheme for Flows at Moderate Knudsen Numbers 117
Experimental Validation of Tilt-Rotor Aerodynamic Predictions 115
A Nonlinear Geometrical Acoustic Model for Sonic Boom Propagation 113
Wind Tunnel Corrections for Isolated Rotor Tests 113
An Investigation of Roe's Linearization and Average for Ideal and Real Gases 112
Factorized Implicit Upwind Methods Applied to Inviscid Flows at High Mach Number 111
NOx Emissions in Combustion Systems of Coal Fired Furnaces with a Reducing Environment: Predictions and Measurements 111
Prediction of Complete Helicopter Aerodynamics at Low- and High-Speed Conditions 110
Wind Tunnel Open Section Characterization for Rotorcraft Tests 110
Numerical Modelling of the Aerodynamic Interference Between Helicopter and Ground Obstacles 109
A Consistent Finite-Volume Formulation for the Solution of the Non-Linear Potential Flow over a Rotor Blade 108
A Kinetic Node-Pair Scheme for Continuum-Transitional Flows 108
A Node-Pair Finite Element / Finite Volume Mesh Adaptation Technique for Compressible Flows 107
Evaluation of Rotor Blade Models for Rotor Outwash 107
The Influence of the Temperature Fluctuations Variance on NO Predictions for a Gas Flame 106
A Fast Chemistry Model for Coal-Gas Reburning 106
Computational Assessment of Flow Breakdown in Closed Section Model Rotor Tests 106
Alcuni aspetti della simulazione di flussi ipersonici 2D su superfici inclinate 104
The Influence of the Temperature Fluctuations Variance on NO Predictions for a Gas Flame 103
Efficient Rotor Aerodynamics Predictions with an Euler Method 103
Trimmed Actuator Disk Modeling for Helicopter Rotor 103
Numerical Simulations of Under-Expanded Nozzle Flows of Dense Gases 102
Numerical Simulation of Hypersonic Transitional Flows by Means of a Kinetic Node-Pair Approach 102
NOx Emissions in Combustion Systems of Coal Fired Furnaces with a Reducing Environment: Predictions and Measurements 98
Experimental and Numerical Analysis of Hydrogen Enriched Natural Gas Swirl Burner 98
CFD Analysis of Wind Tunnel Flow in Open Section Model Rotor Tests 96
A Nonlinear Model for Sonic Boom Propagation in a Windy Stratified Atmosphere 95
Flow-Structure Interaction of the Oscillating Circular Cylinder in the Lock-in Region: Computational Versus Experimental Approach Comparison 94
Simulation of Compressible Lamin for ar Flows with Hybrid Grids 91
Development of a Common European Unsteady Full Potential CFD Code for Helicopter Rotors in Hover and Forward Flight 91
Investigation of Hypersonic Flow in the VKI H3 Wind Tunnel: from Facility Characterization to Boundary-Layer Interaction over Low-Temperature Ablators 91
The Influence of the Temperature Fluctuations Variance on NO Predictions for a Gas Flame 89
Full Potential and Euler Solutions for Transonic Unsteady Flow 88
Comparison Between Two Complementary Approaches for Predicting Nox Emissions in the Furnaces of Utility Boilers 85
Influence of Thermodynamic Models on Nonclassical Shock-Tube Flow Simulations 83
Modelling and Experimental Issues in Turbulent Combustion 77
Outline and Application of GEROS: a European Grid Generator for Rotorcraft Simulation Methods 77
Tilt-Rotor Aerodynamics Activities During the Nicetrip Project 77
EROS: a European Euler Code for Helicopter Rotor Flow Simulations 76
Scale-Up Procedure from Pilot Plant Tests to Full Size Power Plant Results: Experimentation Vs. Mathematical Modelling 75
Node-Pair Representation for Compressible Laminar Flows 75
Numerical Approximation of the Transonic Flow over a Pitching Airfoil 71
CFD Analysis of a Gas-on-Coal Reburn Combustion System 70
The Influence of Spatial Discretisation on the Calculation of Steady Turbulent Flow 68
First Results of the EROS European Unsteady Euler Code on Overlapping Grids 68
Simulazione di correnti ricircolanti con un metodo di raffinamento locale della griglia 67
NOx Emissions from a Large Scale Coal-Fired Furnace 62
Scale-Up Procedure from Pilot Plant Tests to Full Size Power Plant Results: Experimentation Vs. Mathematical Modelling 61
Code to Code Comparison of Aircraft-Mode Tilt-Rotor Aerodynamics 61
Simulazione di correnti separate attorno a profili alari in regime comprimibile 60
Totale 12.562
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Categoria #
all - tutte 35.086
article - articoli 12.480
book - libri 0
conference - conferenze 20.670
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 819
Totale 69.055
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021642 0 0 0 0 0 64 91 113 69 102 45 158
2021/2022816 39 118 41 29 80 33 26 58 71 44 115 162
2022/2023986 130 30 46 111 107 142 5 83 129 80 98 25
2023/2024529 40 90 32 68 28 72 27 38 10 37 31 56
2024/20251.932 29 22 76 54 265 211 154 205 279 94 255 288
2025/20263.430 1.038 966 474 563 323 66 0 0 0 0 0 0
Totale 12.699