ZANOTTI, ALEX
 Distribuzione geografica
Continente #
EU - Europa 6.993
NA - Nord America 5.221
AS - Asia 2.103
SA - Sud America 220
AF - Africa 68
OC - Oceania 42
Continente sconosciuto - Info sul continente non disponibili 1
Totale 14.648
Nazione #
US - Stati Uniti d'America 5.078
IT - Italia 4.171
SG - Singapore 598
CN - Cina 514
DE - Germania 497
RU - Federazione Russa 343
AT - Austria 303
GB - Regno Unito 270
FI - Finlandia 211
ES - Italia 200
IE - Irlanda 181
BR - Brasile 169
FR - Francia 168
VN - Vietnam 158
SE - Svezia 144
IN - India 142
CA - Canada 133
NL - Olanda 127
HK - Hong Kong 115
PH - Filippine 100
KR - Corea 87
BE - Belgio 81
CH - Svizzera 72
ID - Indonesia 71
IR - Iran 63
JP - Giappone 63
UA - Ucraina 53
TR - Turchia 46
AU - Australia 41
SI - Slovenia 39
TW - Taiwan 33
JO - Giordania 29
DK - Danimarca 24
AR - Argentina 20
CI - Costa d'Avorio 20
PL - Polonia 18
PT - Portogallo 18
RO - Romania 16
BD - Bangladesh 14
CO - Colombia 14
GR - Grecia 11
AZ - Azerbaigian 10
BJ - Benin 10
BG - Bulgaria 9
PK - Pakistan 9
CY - Cipro 8
AE - Emirati Arabi Uniti 7
IL - Israele 7
MA - Marocco 7
NO - Norvegia 7
NG - Nigeria 6
PE - Perù 6
TH - Thailandia 6
CZ - Repubblica Ceca 5
IQ - Iraq 5
EC - Ecuador 4
ET - Etiopia 4
KE - Kenya 4
LT - Lituania 4
LV - Lettonia 4
MX - Messico 4
SC - Seychelles 4
ZA - Sudafrica 4
AL - Albania 3
CL - Cile 3
DZ - Algeria 3
EE - Estonia 3
HR - Croazia 3
KG - Kirghizistan 3
KZ - Kazakistan 3
MU - Mauritius 3
MY - Malesia 3
PA - Panama 3
SA - Arabia Saudita 3
VE - Venezuela 3
BY - Bielorussia 2
EG - Egitto 2
HU - Ungheria 2
LK - Sri Lanka 2
SK - Slovacchia (Repubblica Slovacca) 2
AM - Armenia 1
CG - Congo 1
CR - Costa Rica 1
DO - Repubblica Dominicana 1
EU - Europa 1
JM - Giamaica 1
MD - Moldavia 1
NP - Nepal 1
NZ - Nuova Zelanda 1
OM - Oman 1
PY - Paraguay 1
RS - Serbia 1
TJ - Tagikistan 1
Totale 14.648
Città #
Milan 1.807
Chandler 498
Fairfield 467
Woodbridge 345
Singapore 300
Ashburn 297
Vienna 286
Santa Clara 282
Ann Arbor 244
Seattle 226
Wilmington 211
Dublin 178
Houston 176
Cambridge 170
Málaga 154
Helsinki 144
Council Bluffs 142
Boardman 128
Dong Ket 116
Redwood City 106
Dearborn 99
Rome 94
Zibido San Giacomo 91
Amsterdam 87
Medford 85
Davao City 84
Lawrence 83
Crema 81
Shanghai 71
Beijing 63
Jakarta 60
Ottawa 59
Bovisio Masciago 54
Novara 54
Munich 52
Brussels 47
Pedrengo 47
Triggiano 47
Giussano 40
Los Angeles 40
Bern 39
Frankfurt am Main 38
London 38
Ciampino 37
Bareggio 36
Boltiere 36
Braunschweig 35
Redmond 35
Central 34
Bristol 32
Falkenstein 32
Luft 31
Aachen 30
Brescia 30
Glasgow 30
Jacksonville 30
Amman 29
Des Moines 28
Bled 27
Montreal 27
Hangzhou 26
Pavia 26
Washington 26
Fremont 24
Tokyo 24
Verona 24
Nanjing 23
Nuremberg 23
Taipei 23
San Diego 22
Bengaluru 21
Robbiate 21
São Paulo 21
Abidjan 20
Segrate 20
Xi'an 20
Nürnberg 19
Bresso 18
Hong Kong 18
Volterra 18
Ankara 17
Clifton 17
Muggiò 17
Saint-Gilles 17
Seregno 17
Tower Hamlets 17
Atlanta 16
Harbin 16
Monza 16
New York 16
Varese 16
Duncan 15
Las Vegas 15
Bogotá 14
Geumjeong-gu 14
Lecco 14
Manchester 14
Miami 14
Moscow 14
Norwalk 14
Totale 9.016
Nome #
Analysis of the Interactional Aerodynamics of the Vahana eVTOL Using a Medium Fidelity Open Source Tool 1.130
Mid-Fidelity Analysis of Unsteady Interactional Aerodynamics of Complex VTOL Configurations 381
Experimental Investigation of the Rotor-Wing Aerodynamic Interaction in a Tiltwing Aircraft in Hover 365
Simulation of Tiltrotor Maneuvers by a Coupled Multibody-Mid Fidelity Aerodynamic Solver 293
Wind-tunnel tests of the ERICA tiltrotor optimised air-intake 265
Coupled Multibody-Mid Fidelity Aerodynamic Solver for Tiltrotor Aeroelastic Simulation 251
Assessment of a Mid-Fidelity Numerical Approach for the Investigation of Tiltrotor Aerodynamics 239
Numerical assessment of an L-shaped Gurney flap for load control 226
A Coupled Multibody - Mid Fidelity Aerodynamic Tool for the Simulation of Tiltrotor Manoeuvres 222
Experimental investigation of a helicopter rotor with Gurney flaps 220
Design and Optimization of Innovative Tiltrotor Wing Control Surfaces Through Coupled Multibody - Mid-Fidelity Aerodynamics Simulations 208
Helicopter drag reduction by vortex generators 204
A novel approach for reconstructing pressure from PIV velocity measurements 204
Aerodynamic Interaction Between Rotor and Tilting Wing in Hovering Flight Condition 200
Experimental investigation of the unsteady aerodynamics of FOWT through PIV and hot-wire wake measurements 198
Wind-tunnel tests of a heavy-class helicopter optimised for drag reduction 192
Assessment of 2D/3D Numerical Modeling for Deep Dynamic Stall Experiments 186
Wind-Tunnel Tests of a Tilt-Rotor Aircraft 183
Numerical and Experimental Study of Wake Redirection Techniques in a Boundary Layer Wind Tunnel 179
Experimental assessment of an active L-shaped tab for dynamic stall control 172
Experimental-Numerical Investigation of a Pitching Airfoil in Deep Dynamic Stall 168
Coupling Mid-Fidelity Aerodynamics and Multibody Dynamics for the Aeroelastic Analysis of Rotary-Wing Vehicles 167
Experimental Investigation on a 1/4 Scaled Model of an High-Performance Tiltwing Aircraft in Hover 165
Flow Field Around the Flapping Flag 165
Analysis of the loads acting on the rotor of a helicopter model close to an obstacle in moderate windy conditions 165
Experimental Investigation on the Aerodynamic Interaction Between a Helicopter and Ground Obstacles 164
Experimental Investigation of the Dynamic Stall Phenomenon on a NACA 23012 Oscillating Airfoil 159
Experimental-Numerical Investigation of Rotor-Rotor Aerodynamic Interactions for eVTOL Aircraft Configurations 153
Stereo particle image velocimetry set up for measurements in the wake of scaled wind turbines 152
Perpendicular blade–vortex-interaction over an oscillating airfoil in light dynamic stall 150
Experimental study of a helicopter model in shipboard operations 150
Robustness and limits of vortex generator effectiveness in helicopter drag reduction 149
Mid-Fidelity Numerical Approach to Tiltrotor Aerodynamics 142
Experimental evaluation of the aerodynamic performance of a large-scale high-lift morphing wing 142
PIV characterization of a separated flow controlled by a DBD actuator 141
Aerodynamic interaction between tandem overlapping propellers in eVTOL airplane mode flight condition 140
An Experimental Set up for the Study of Helicopter and Building Aerodynamic Interaction 139
Stall control by plasma actuators: Characterization along the airfoil span 136
Experimental Investigation of a Trailing Edge L-shaped Tab on a Pitching Airfoil in Deep Dynamic Stall Conditions 135
Experimental Tests and CFD Simulations on a Tiltwing Aircraft in Hover 134
Numerical Investigation of Three-Dimensional Effects on Deep Dynamic Stall Experiments 132
Experimental Investigation of Unsteady Inflow for a Helicopter Model in Shipboard Operations 130
Stereo Particle Image Velocimetry Measurements of Perpendicular Blade-Vortex Interaction over an Oscillating Airfoil 128
Unsteady load assessment of a scaled-helicopter model in a ship airwake 126
Multi-Fidelity Numerical Approach to Aeroacoustics of Tandem Propellers in eVTOL Airplane Mode 124
Dynamic Stall Inducted by Blade Vortex Interaction in Helicopter Descending Flight 124
A Test Rig to Assess the Effectiveness of Drag Reduction Devices on a Heavy-Class Helicopter 118
Oscillating Aerofoil and Perpendicular Vortex Interaction 116
Bayesian calibration of a low order aerodynamic model for the design of unconventional tail empennages 115
Reconstructing Pressure from PIV Velocity Measurements: a Novel Approach 115
Helicopter-Obstacle Aerodynamic Interaction in Windy Conditions 114
Mid-fidelity approach to aerodynamic simulations of unconventional VTOL aircraft configurations 112
Wake Measurements behind an Oscillating Airfoil in Dynamic Stall Conditions 111
MONNALISA: Modelling Nonlinear Aerodynamics of Lifting Surfaces 109
Parallel Blade-Vortex Interaction on Pitching Airfoil 106
Aerodynamic interaction between tandem propellers in eVTOL transition flight configurations 105
Aerodynamic Evaluation 104
An Experimental Set Up for the Study of the Retreating Blade Dynamic Stall 104
Helicopter Noise in Urban Flight 104
Optimized ERICA Engine Intake Wind Tunnel Test 102
Wind tunnel testing of a wind turbine in complex terrain 101
Numerical Evaluation of Aircraft Aerodynamic Static and Dynamic Stability Derivatives by a Mid-Fidelity Approach 100
A Non-Linear Unsteady Vortex Lattice Method for Aeroelastic Rotor Loads Evaluation 99
Simulation and Testing of Helicopter-Ship Aerodynamic Interaction 99
Wind Tunnel Assessment of the Computational Framework for Helicopter Fuselage Drag Reduction Using Vortex Generators 99
Numerical Investigation of Perpendicular Blade-Vortex-interaction on a Pitching Airfoil in Light Dynamic Stall 98
Experimental-Numerical Investigation of the Dynamic Stall Phenomenon over the NACA 23012 Airfoil 97
Experimental Assessment of Tiltrotor Air-Intake Duct Shape Optimization 97
Design of a Generic Rotor Noise Source for Helicopter Fuselage Scattering Tests 95
Wind Tunnel Investigation of a Helicopter Model in Shipboard Operations 94
Numerical Investigation of the Rotor-Rotor Aerodynamic Interaction for eVTOL Aircraft Configurations 93
Wind tunnel test of full-scale wing-propeller system of a eVTOL aircraft 90
Risposta direzionale di una sonda a filo caldo triplo e sua taratura 89
Numerical Investigation of Wing-Propeller Aerodynamic Interaction Through a Vortex Particle-Based Aerodynamic Solver 87
Evaluation of Acoustic Shielding Effects from a Generic GARTEUR Helicopter Configuration 87
Experimental-Numerical Investigation of the Retreating Blade Dynamic Stall 86
Measurement of the Rotor Blade Section Aerodynamic Coefficients by Particle Image Velocimetry 85
Infrared Thermography Measurements over a Tail-Plane Model of a Large Passenger Aircraft 85
Experimental Evaluation of an Active Controlled L-Shaped Tab for Dynamic Stall Alleviation 83
Towards a Wind Tunnel Testing Environment for Rotorcraft Operations Close to Obstacles 82
Experimental Investigation of Perpendicular Vortex Interaction by Stereo Particle Image Velocimetry 81
Numerical Investigation of the Rotor-Rotor Aerodynamic Interaction of EVTOL Configurations by a Mid-Fidelity Approach 81
Experimental investigation of wing-propeller aerodynamic interaction in eVTOL configurations 74
Wind Tunnel Open Section Characterization for Rotorcraft Tests 73
Experimental Method for Drag Measurement of an Oscillating Airfoil in Dynamic Stall Condition 71
Multi-Fidelity Assessment of the Aerodynamic Performances of Unconventional Aircraft Tail Configurations 70
Experimental Study of the Aerodynamic Interaction between Side-by-Side Propellers in eVTOL Airplane Mode through Stereoscopic Particle Image Velocimetry 69
Rotor / Rotor Aerodynamic Interactions – a GARTEUR Action Group 68
A non-linear unsteady vortex-lattice method for rotorcraft applications 67
Experimental Evaluation of an L-Shaped Tab to be Used as an Active Gurney Flap for Dynamic Stall Control 66
Mid-Fidelity Numerical Approach for the Calculation of the Aerodynamic Static and Dynamic Stability Derivatives 64
Wind Tunnel Tests of ERICA Tilt-Rotor Modular Model 63
Editorial of the Special Issue: Rotary Wing Aerodynamics 63
Mid-fidelity numerical approach for the investigation of wing-propeller aerodynamic interaction 61
Acoustic and aerodynamic evaluation of DLR small-scale rotor configurations within GARTEUR AG26 61
Experimental Numerical Study of Small Amplitude Oscillations of a Pitching Airfoil 60
Wind-tunnel measurements of the airflow pattern above the collector of different shielded and unshielded precipitation gauges 60
Experimental Investigation of Perpendicular Vortex Interaction over an Oscillating Airfoil in Dynamic Stall Conditions 59
Validation of Numerical Models for the Investigation of Dynamic Stall Phenomenon 59
Acoustic and Aerodynamic Evaluation of DLR Small-Scale Rotor Configurations within Garteur AG26 57
Totale 14.006
Categoria #
all - tutte 41.102
article - articoli 18.852
book - libri 0
conference - conferenze 21.589
curatela - curatele 208
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 453
Totale 82.204


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020273 0 0 0 0 0 0 0 0 0 80 131 62
2020/20211.346 53 37 66 111 116 117 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
2024/20253.682 323 82 185 277 934 380 315 411 631 144 0 0
Totale 14.966