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

ZANOTTI, ALEX
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
EU - Europa 12.360
NA - Nord America 7.610
AS - Asia 4.339
SA - Sud America 867
AF - Africa 212
OC - Oceania 57
Continente sconosciuto - Info sul continente non disponibili 1
Totale 25.446
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 7.379
RU - Federazione Russa 4.624
IT - Italia 4.583
CN - Cina 1.472
SG - Singapore 1.268
BR - Brasile 716
DE - Germania 653
GB - Regno Unito 367
AT - Austria 339
VN - Vietnam 310
NL - Olanda 272
FR - Francia 252
FI - Finlandia 235
ES - Italia 215
IE - Irlanda 211
IN - India 199
KR - Corea 183
HK - Hong Kong 182
CA - Canada 167
SE - Svezia 156
JP - Giappone 104
PH - Filippine 102
MA - Marocco 92
ID - Indonesia 90
BE - Belgio 86
CH - Svizzera 77
TR - Turchia 77
UA - Ucraina 69
IR - Iran 65
AR - Argentina 61
AU - Australia 50
TW - Taiwan 44
PL - Polonia 43
BD - Bangladesh 42
SI - Slovenia 39
MX - Messico 38
JO - Giordania 37
CI - Costa d'Avorio 33
EC - Ecuador 29
TH - Thailandia 25
CO - Colombia 24
DK - Danimarca 24
ZA - Sudafrica 22
IQ - Iraq 21
PT - Portogallo 21
PK - Pakistan 17
RO - Romania 17
GR - Grecia 15
AE - Emirati Arabi Uniti 13
AZ - Azerbaigian 13
SA - Arabia Saudita 13
BG - Bulgaria 10
BJ - Benin 10
IL - Israele 10
LT - Lituania 10
CL - Cile 9
VE - Venezuela 9
CY - Cipro 8
ET - Etiopia 8
JM - Giamaica 8
KE - Kenya 8
DZ - Algeria 7
NG - Nigeria 7
NO - Norvegia 7
PE - Perù 7
UZ - Uzbekistan 7
CZ - Repubblica Ceca 6
KZ - Kazakistan 6
NZ - Nuova Zelanda 6
PY - Paraguay 6
LV - Lettonia 5
MY - Malesia 5
NP - Nepal 5
RS - Serbia 5
SC - Seychelles 5
AL - Albania 4
KG - Kirghizistan 4
PA - Panama 4
TN - Tunisia 4
UY - Uruguay 4
EE - Estonia 3
HR - Croazia 3
KH - Cambogia 3
MU - Mauritius 3
OM - Oman 3
AM - Armenia 2
BF - Burkina Faso 2
BO - Bolivia 2
BS - Bahamas 2
BY - Bielorussia 2
CR - Costa Rica 2
EG - Egitto 2
HN - Honduras 2
HU - Ungheria 2
KW - Kuwait 2
LK - Sri Lanka 2
NI - Nicaragua 2
SK - Slovacchia (Repubblica Slovacca) 2
SN - Senegal 2
TZ - Tanzania 2
Totale 25.425
Salva come PNG Salva come JPEG
Città #
Milan 2.026
Ashburn 1.023
Dallas 814
Singapore 755
Moscow 617
Chandler 498
Fairfield 467
Hefei 385
Woodbridge 345
Vienna 317
Santa Clara 298
Ann Arbor 244
Seattle 236
Beijing 217
Wilmington 212
Dublin 208
Houston 184
Cambridge 170
Málaga 154
Helsinki 147
Council Bluffs 143
Boardman 133
Los Angeles 133
Rome 123
Amsterdam 121
Dong Ket 116
Redwood City 106
Dearborn 99
Zibido San Giacomo 91
Seoul 86
Medford 85
Casablanca 84
Davao City 84
Lawrence 83
Crema 81
Buffalo 79
Kent 79
Shanghai 79
Frankfurt am Main 78
Munich 67
São Paulo 67
London 66
Jakarta 65
Hong Kong 62
Ottawa 59
Novara 55
Bovisio Masciago 54
Brussels 52
Tokyo 51
Ho Chi Minh City 49
New York 47
Pedrengo 47
Triggiano 47
Montreal 45
Delft 44
Pavia 43
Aachen 41
Bern 40
Giussano 40
Brescia 38
Bristol 38
Hanoi 38
Amman 37
Ciampino 37
Bareggio 36
Boltiere 36
Braunschweig 35
Redmond 35
Central 34
Abidjan 32
Falkenstein 32
Glasgow 32
Luft 31
Atlanta 30
Bengaluru 30
Jacksonville 30
Des Moines 28
Hangzhou 28
Manchester 28
Washington 28
Bled 27
Tianjin 27
Turin 27
Verona 27
Nuremberg 26
Guangzhou 25
Nanjing 25
The Dalles 25
Warsaw 25
Ankara 24
Chicago 24
Fremont 24
Istanbul 24
Lappeenranta 24
Xi'an 24
San Diego 23
Taipei 23
Paris 22
Monza 21
Redondo Beach 21
Totale 13.422
Salva come PNG Salva come JPEG
Nome #
Analysis of the Interactional Aerodynamics of the Vahana eVTOL Using a Medium Fidelity Open Source Tool 1.301
Experimental Investigation of the Rotor-Wing Aerodynamic Interaction in a Tiltwing Aircraft in Hover 445
Mid-Fidelity Analysis of Unsteady Interactional Aerodynamics of Complex VTOL Configurations 440
Simulation of Tiltrotor Maneuvers by a Coupled Multibody-Mid Fidelity Aerodynamic Solver 383
Assessment of a Mid-Fidelity Numerical Approach for the Investigation of Tiltrotor Aerodynamics 378
Coupled Multibody-Mid Fidelity Aerodynamic Solver for Tiltrotor Aeroelastic Simulation 361
Wind-tunnel tests of the ERICA tiltrotor optimised air-intake 346
A Coupled Multibody - Mid Fidelity Aerodynamic Tool for the Simulation of Tiltrotor Manoeuvres 343
A novel approach for reconstructing pressure from PIV velocity measurements 318
Design and Optimization of Innovative Tiltrotor Wing Control Surfaces Through Coupled Multibody - Mid-Fidelity Aerodynamics Simulations 307
Aerodynamic Interaction Between Rotor and Tilting Wing in Hovering Flight Condition 297
Experimental investigation of a helicopter rotor with Gurney flaps 296
Numerical assessment of an L-shaped Gurney flap for load control 290
An Experimental Set up for the Study of Helicopter and Building Aerodynamic Interaction 283
Helicopter drag reduction by vortex generators 272
Assessment of 2D/3D Numerical Modeling for Deep Dynamic Stall Experiments 269
Acoustic and aerodynamic evaluation of DLR small-scale rotor configurations within GARTEUR AG26 262
Coupling Mid-Fidelity Aerodynamics and Multibody Dynamics for the Aeroelastic Analysis of Rotary-Wing Vehicles 262
Experimental Investigation on a 1/4 Scaled Model of an High-Performance Tiltwing Aircraft in Hover 259
Aerodynamic interaction between tandem overlapping propellers in eVTOL airplane mode flight condition 259
Aerodynamic Evaluation 255
Multi-Fidelity Numerical Approach to Aeroacoustics of Tandem Propellers in eVTOL Airplane Mode 251
Aerodynamic interaction between tandem propellers in eVTOL transition flight configurations 250
Experimental Investigation on the Aerodynamic Interaction Between a Helicopter and Ground Obstacles 247
Experimental evaluation of the aerodynamic performance of a large-scale high-lift morphing wing 247
Experimental Tests and CFD Simulations on a Tiltwing Aircraft in Hover 246
Experimental investigation of the unsteady aerodynamics of FOWT through PIV and hot-wire wake measurements 246
Wind-tunnel tests of a heavy-class helicopter optimised for drag reduction 245
Analysis of the loads acting on the rotor of a helicopter model close to an obstacle in moderate windy conditions 242
A Non-Linear Unsteady Vortex Lattice Method for Aeroelastic Rotor Loads Evaluation 233
A Test Rig to Assess the Effectiveness of Drag Reduction Devices on a Heavy-Class Helicopter 229
Numerical Evaluation of Aircraft Aerodynamic Static and Dynamic Stability Derivatives by a Mid-Fidelity Approach 227
Bayesian calibration of a low order aerodynamic model for the design of unconventional tail empennages 227
Wind-Tunnel Tests of a Tilt-Rotor Aircraft 226
Experimental study of a helicopter model in shipboard operations 224
Robustness and limits of vortex generator effectiveness in helicopter drag reduction 223
Perpendicular blade–vortex-interaction over an oscillating airfoil in light dynamic stall 220
MONNALISA: Modelling Nonlinear Aerodynamics of Lifting Surfaces 218
Experimental-Numerical Investigation of Rotor-Rotor Aerodynamic Interactions for eVTOL Aircraft Configurations 218
Experimental Investigation of a Trailing Edge L-shaped Tab on a Pitching Airfoil in Deep Dynamic Stall Conditions 217
Helicopter-Obstacle Aerodynamic Interaction in Windy Conditions 209
Experimental-Numerical Investigation of a Pitching Airfoil in Deep Dynamic Stall 207
Experimental assessment of an active L-shaped tab for dynamic stall control 207
Experimental Investigation of Unsteady Inflow for a Helicopter Model in Shipboard Operations 203
Reconstructing Pressure from PIV Velocity Measurements: a Novel Approach 202
Numerical and Experimental Study of Wake Redirection Techniques in a Boundary Layer Wind Tunnel 202
A non-linear unsteady vortex-lattice method for rotorcraft applications 199
Mid-Fidelity Numerical Approach to Tiltrotor Aerodynamics 199
Parallel Blade-Vortex Interaction on Pitching Airfoil 198
Stereo particle image velocimetry set up for measurements in the wake of scaled wind turbines 195
PIV characterization of a separated flow controlled by a DBD actuator 195
An Experimental Set Up for the Study of the Retreating Blade Dynamic Stall 193
Experimental and Numerical Analysis of Aerodynamic Interaction Between Wing and Propeller 189
Flow Field Around the Flapping Flag 189
Wind tunnel test of full-scale wing-propeller system of a eVTOL aircraft 188
Experimental Investigation of the Dynamic Stall Phenomenon on a NACA 23012 Oscillating Airfoil 186
Experimental Assessment of Tiltrotor Air-Intake Duct Shape Optimization 185
Numerical Investigation of Three-Dimensional Effects on Deep Dynamic Stall Experiments 185
Acoustic and Aerodynamic Evaluation of POLIMI Tandem Propellers Configurations within GARTEUR AG26 184
Numerical Investigation of Perpendicular Blade-Vortex-interaction on a Pitching Airfoil in Light Dynamic Stall 184
Stall control by plasma actuators: Characterization along the airfoil span 182
Infrared Thermography Measurements over a Tail-Plane Model of a Large Passenger Aircraft 182
Acoustic and Aerodynamic Evaluation of DLR Small-Scale Rotor Configurations within Garteur AG26 181
Unsteady load assessment of a scaled-helicopter model in a ship airwake 181
Dynamic Stall Inducted by Blade Vortex Interaction in Helicopter Descending Flight 179
Simulation and Testing of Helicopter-Ship Aerodynamic Interaction 177
Wind Tunnel Assessment of the Computational Framework for Helicopter Fuselage Drag Reduction Using Vortex Generators 175
Experimental Investigation of the Aerodynamic Interaction Between Overlapping Propellers in Tandem for eVTOL Airplane-Mode Flight Conditions 173
Wind Tunnel Experiments on Parallel Blade–Vortex Interaction with Static and Oscillating Airfoil 173
Numerical Investigation of Wing-Propeller Aerodynamic Interaction Through a Vortex Particle-Based Aerodynamic Solver 171
Aerodynamic and aeroacoustics investigation of tandem propellers in hover for eVTOL configurations 170
Multi-Fidelity Assessment of the Aerodynamic Performances of Unconventional Aircraft Tail Configurations 169
Wake Measurements behind an Oscillating Airfoil in Dynamic Stall Conditions 167
Experimental Aeroacoustics Investigation of Interacting Tandem Propellers in Hover 166
Optimized ERICA Engine Intake Wind Tunnel Test 166
Mid-fidelity approach to aerodynamic simulations of unconventional VTOL aircraft configurations 165
Stereo Particle Image Velocimetry Measurements of Perpendicular Blade-Vortex Interaction over an Oscillating Airfoil 164
Experimental investigation of wing-propeller aerodynamic interaction in eVTOL configurations 163
Wind tunnel testing of a wind turbine in complex terrain 162
Measurement of the Rotor Blade Section Aerodynamic Coefficients by Particle Image Velocimetry 160
Towards a Wind Tunnel Testing Environment for Rotorcraft Operations Close to Obstacles 160
Wind Tunnel Investigation of a Helicopter Model in Shipboard Operations 159
Rotor / Rotor Aerodynamic Interactions – a GARTEUR Action Group 158
Helicopter Noise in Urban Flight 156
Mid-fidelity numerical approach for the investigation of wing-propeller aerodynamic interaction 154
Experimental Evaluation of an Active Controlled L-Shaped Tab for Dynamic Stall Alleviation 153
Numerical Characterization of the Aeroacoustics of Tandem Propellers in Hover 151
Wind-tunnel experimental investigation on rotor-rotor aerodynamic interaction in compound helicopter configuration 146
Evaluation of Acoustic Shielding Effects from a Generic GARTEUR Helicopter Configuration 145
Experimental Evaluation of an L-Shaped Tab to be Used as an Active Gurney Flap for Dynamic Stall Control 144
Stochastic Simulation of Ship Airwake in Helicopter Shipboard Operation 143
Aerodynamic interaction between wing and propeller in eVTOL airplane mode flight condition 142
Experimental Investigation of Vortex Ring State Conditions for Archer Maker eVTOL Tilter Propeller 141
Experimental-Numerical Investigation of the Dynamic Stall Phenomenon over the NACA 23012 Airfoil 137
Oscillating Aerofoil and Perpendicular Vortex Interaction 137
Numerical Investigation of the Rotor-Rotor Aerodynamic Interaction of EVTOL Configurations by a Mid-Fidelity Approach 137
Experimental Wind-Tunnel Testing of Rotor/Wake Aerodynamic Interactions on a Compound Helicopter 136
Experimenting Rotorcraft Flight in Complex Environmental Conditions Using the Wind Tunnel: Helicopter Ship Landing Case 135
Risposta direzionale di una sonda a filo caldo triplo e sua taratura 134
Design of a Generic Rotor Noise Source for Helicopter Fuselage Scattering Tests 134
Totale 22.289
Salva come PNG Salva come JPEG
Categoria #
all - tutte 60.541
article - articoli 27.509
book - libri 0
conference - conferenze 32.045
curatela - curatele 303
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 684
Totale 121.082
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021963 0 0 0 0 0 117 66 80 103 134 227 236
2021/20221.749 92 124 296 163 174 76 121 112 140 74 182 195
2022/20232.255 190 92 143 228 221 251 91 168 305 256 126 184
2023/20241.748 99 135 115 169 116 148 213 126 128 178 140 181
2024/20255.972 323 82 185 277 934 380 315 411 631 279 491 1.664
2025/20268.524 2.916 2.410 988 1.156 903 151 0 0 0 0 0 0
Totale 25.780