GENNARETTI, MASSIMO
 Distribuzione geografica
Continente #
EU - Europa 17.467
NA - Nord America 16.423
AS - Asia 11.509
SA - Sud America 1.161
AF - Africa 257
OC - Oceania 24
Continente sconosciuto - Info sul continente non disponibili 13
Totale 46.854
Nazione #
US - Stati Uniti d'America 16.259
CN - Cina 6.164
DK - Danimarca 4.062
GB - Regno Unito 4.023
RU - Federazione Russa 3.062
SG - Singapore 2.841
VN - Vietnam 1.494
DE - Germania 1.314
IT - Italia 1.210
BR - Brasile 936
SE - Svezia 913
FR - Francia 839
UA - Ucraina 810
FI - Finlandia 307
IE - Irlanda 265
AL - Albania 233
HK - Hong Kong 198
TR - Turchia 177
CI - Costa d'Avorio 148
NL - Olanda 135
IN - India 130
KR - Corea 110
JP - Giappone 105
AR - Argentina 90
CA - Canada 85
BE - Belgio 61
MX - Messico 51
BD - Bangladesh 50
ID - Indonesia 44
ZA - Sudafrica 42
EC - Ecuador 41
PL - Polonia 38
ES - Italia 34
AT - Austria 32
CZ - Repubblica Ceca 32
IQ - Iraq 28
PK - Pakistan 26
IR - Iran 23
PY - Paraguay 23
AU - Australia 21
CO - Colombia 17
RO - Romania 17
VE - Venezuela 17
MA - Marocco 16
SA - Arabia Saudita 16
GR - Grecia 15
EG - Egitto 13
LT - Lituania 13
UZ - Uzbekistan 13
CH - Svizzera 12
CL - Cile 12
KZ - Kazakistan 12
UY - Uruguay 11
AZ - Azerbaigian 10
IL - Israele 10
KE - Kenya 10
TN - Tunisia 10
PE - Perù 9
HU - Ungheria 8
JM - Giamaica 7
JO - Giordania 7
DZ - Algeria 6
ET - Etiopia 6
EU - Europa 6
LV - Lettonia 6
MY - Malesia 6
PA - Panama 6
PH - Filippine 6
BO - Bolivia 5
NO - Norvegia 5
NP - Nepal 5
A2 - ???statistics.table.value.countryCode.A2??? 4
AE - Emirati Arabi Uniti 4
CR - Costa Rica 4
DO - Repubblica Dominicana 4
LA - Repubblica Popolare Democratica del Laos 4
MN - Mongolia 4
BH - Bahrain 3
KG - Kirghizistan 3
LU - Lussemburgo 3
MD - Moldavia 3
NZ - Nuova Zelanda 3
SK - Slovacchia (Repubblica Slovacca) 3
BA - Bosnia-Erzegovina 2
EE - Estonia 2
GT - Guatemala 2
HR - Croazia 2
LK - Sri Lanka 2
OM - Oman 2
TH - Thailandia 2
A1 - Anonimo 1
AF - Afghanistan, Repubblica islamica di 1
AM - Armenia 1
AO - Angola 1
BB - Barbados 1
BG - Bulgaria 1
BN - Brunei Darussalam 1
BW - Botswana 1
BY - Bielorussia 1
CW - ???statistics.table.value.countryCode.CW??? 1
Totale 46.834
Città #
Southend 3.703
Woodbridge 2.194
Fairfield 1.567
Ashburn 1.331
Ann Arbor 1.176
Wilmington 1.145
Singapore 1.063
Chandler 974
Dong Ket 930
Nanjing 871
Houston 828
Beijing 807
Dearborn 696
Hefei 689
Jacksonville 612
Boardman 574
Seattle 559
Cambridge 502
Rome 474
Dallas 440
Princeton 427
Shenyang 365
Nanchang 312
Paris 301
Jinan 292
Plano 271
Dublin 265
Hebei 229
Redwood City 217
Ho Chi Minh City 203
Changsha 200
Hong Kong 198
Shanghai 177
Tianjin 174
Jiaxing 171
Moscow 159
Zhengzhou 136
Izmir 135
Los Angeles 120
Hanoi 109
New York 108
Guangzhou 104
Seoul 102
Tokyo 99
Taizhou 98
Hangzhou 97
San Diego 95
Kunming 92
Ningbo 85
Munich 84
São Paulo 81
Fuzhou 74
Milan 70
The Dalles 70
Orange 69
Pune 66
Brussels 59
Helsinki 53
Haikou 52
Taiyuan 52
London 51
Bremen 50
Frankfurt am Main 47
San Paolo di Civitate 44
Santa Clara 44
Altamura 43
Rio de Janeiro 36
Alameda 34
Washington 34
Yubileyny 34
Lanzhou 31
Atlanta 28
Brooklyn 28
Denver 28
San Francisco 28
Turku 28
Warsaw 27
Haiphong 26
Lawrence 26
Montreal 25
Hải Dương 24
Johannesburg 23
Orem 23
Stockholm 23
Chicago 22
Fort Worth 22
Biên Hòa 21
Columbus 21
Curitiba 21
Vélizy-villacoublay 21
Brno 20
Chennai 20
Flushing 20
Nürnberg 20
Boston 19
Da Nang 19
Manchester 19
Toronto 19
Vienna 19
Amsterdam 18
Totale 28.312
Nome #
Structural and Aeroelastic Modeling of Curved Rotor Blades Using a Galerkin Approach 398
ALGORITHM FOR IDENTIFICATION OF HELICOPTER OPEN-LOOP TRANSFER FUNCTIONS AND REDUCED-ORDER MODELING 357
A Spectral Formulation for Structural/Aeroelastic Modeling of Curved-Axis Rotor Blades 335
Assessment of a comprehensive aeroelastic tool for horizontal-axis wind turbine rotor analysis 325
Boundary Integral Equation Methods for Aerodynamics 313
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft 309
Tiltrotor Cabin Noise Control Through Smart Actuators 292
A Boundary-Field Integral Equation for Analysis of Cavity Acoustic Spectrum 275
Aeroacoustic Analysis of Helicopter Rotors in Ground Effect 268
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 263
A BEM simulation of a wind tunnel with an open test section 263
Analysis of Vibrations of an Innovative Civil Tiltrotor 263
Parallel Blade-Vortex Interaction Modelling for Helicopter Rotor Noise Control Synthesis 260
A boundary integral formulation for sound scattered by elastic moving bodies 258
Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation 251
Rotorcraft Aeroelastic Stability Using Robust Analysis 248
A Frequency Domain Approach for the Prediction of Tonal Noise Emitted by Rotors in Arbitrary Steady Motion 244
A Boundary Element Method for Aerodynamics of Wings and Rotors 242
Synthesis of Active Twist Controller for Rotor Blade–Vortex Interaction Noise Alleviation 241
Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings - A design perspective 240
A Boundary Integral Method in Rotor Aeroacoustics 239
A Boundary Integral Method for Unified Transonic Aerodynamic and Aeroacoustic Analysis of Hovering Rotors 239
Aeroacoustoelasticity in State-Space Format Using CHIEF Regularization 236
Aerodynamics and Aeroacoustics of Wings and Rotors via BEM -- Unsteady, Transonic and Viscous Effects 234
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Cylindrical Shells 233
Analysis of Helicopter Vibratory Hub Loads Alleviation By Cyclic Trailing-Edge Blade Flap Actuation 231
Assessment of a FEM-based Formulation for Horizontal Axis Wind Turbine Rotors Aeroelasticity 230
A Finite-State Aeroelastic Model for Rotorcraft–Pilot Coupling Analysis 230
An optimal control approach for alleviation of tiltrotor gust response 228
Assessment of Helicopter Pilot-in-the-Loop Models 228
Adverse Rotorcraft Pilot Couplings - Past, Present and Future Challenges 225
Aeroelastic Response of Helicopter Rotors Using a 3-D Unsteady Aerodynamic Solver 223
A Boundary Element Method for the Aerodynamics and Aeroacoustics of Bodies in Arbitrary Motions 222
Rotorcraft Comprehensive Code Assessment for Blade-Vortex Interaction Conditions 222
GARTEUR Activities on Acoustical Methods and Experiments for Studying on Acoustic Scattering 222
A Boundary Integral Method for Aeroacoustics of Rotors 222
Synthesis of Rotor BVI Noise Active Controller Through Efficient Aerodynamics/Aeroacoustics Solver 222
A Spatial Repetitive Controller Applied to an Aeroelastic Model for Wind Turbines 221
A Spectral-BEM Formulation for Compact Sources Aeroacoustics 220
Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications 220
Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices 220
A New Velocity Decomposition for Viscous Flows: Lighthill's Equivalent-Source Method Revisited 219
Assessment of a state-space aeroelastic rotor model for rotorcraft flight dynamics 219
A Velocity-Potential-Based Boundary-Element Method for the Aeroacoustic Analysis of Rotors and Propellers in Arbitrary Motion 217
Boundary Integral Transonics for Wings and Rotors 216
A Boundary Element Method for the Potential, Compressible Aerodynamics of Bodies in Arbitrary Motion 216
Effects of Biodynamic Feedthrough in Rotorcraft/Pilot Coupling: Collective Bounce Case 215
Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors 215
Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuation 214
Numerical characterization of helicopter noise hemispheres 213
Synthesis of a Rotor Noise Controller by Parallel Blade-Vortex Interaction Aeroelastic Modelling 212
A Retrospective Survey of Adverse Rotorcraft Pilot Couplings in European Perspective 212
Aeroelastic Rotorcraft-Pilot Couplings: Problems and Methods 212
Identification of rotor wake inflow finite-state models for flight dynamics simulations 212
Active Twist Rotor Controller Identification for Blade-Vortex Interaction Noise Alleviation 212
Simulation of Helicopter Noise in Maneuvering Flight 211
Innovative Helicopter In-Flight Noise Monitoring Systems Enabled by Rotor-State Measurements 211
Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing­-Proprotor Aerodynamic Interaction 210
An Unsteady Aerodynamic Formulation for Efficient Rotor Tonal Noise Prediction 210
Helicopter Noise Footprint Prediction in Unsteady Maneuvers 210
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 209
A Combined Interior--Exterior Model for Propeller Acoustics 209
Optimal Design and Acoustic Assessment of Low-Vibration Rotor Blades 209
ASSESSMENT OF A STATE-SPACE AEROELASTIC ROTOR MODEL FOR ROTORCRAFT DYNAMICS ANALYSIS 208
Individual blade repetitive control for horizontal-axis wind turbines 208
Theoretical and Numerical Issues for Hydroacoustic Applications of the Ffowcs Williams-Hawkings Equation 205
A Third-Order Boundary Element Method for Exterior Acoustics with Applications to Scattering by Rigid and Elastic Shells 203
An Analytical-Numerical Aerodynamic Formulation for Efficient Aeroacoustics Analysis of Rotorcraft 203
A Boundary-Field Integral Formulation for Sound Scattering of Moving Bodies 202
A Boundary Element Method for the Aerodynamic Analysis of Aircraft in Arbitrary Motion 200
Forces and Moments in Incompressible Quasi-Potential Flows 200
A Space-Time Accurate Finite-State Inflow Model for Aeroelastic Applications 200
Whirl Flutter Analysis of Prop-Rotors Using Unsteady Aerodynamics Reduced-Order Models 199
Evaluation of noise excess for pushing propeller aircraft by CFD aeroacoustic calculation 199
Fully Coupled Structural-Unsteady Aerodynamics Modelling for Aeroelastic Response of Rotorcraft 199
Spectral-Boundary-Integral Compact-Source Formulation for Aero-Hydroacoustics of Rotors 198
Aircraft and Rotorcraft Pilot Coupling: A Survey of Recent Research Activities Within the European Project ARISTOTEL 197
Structural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor Blades 197
Acoustic Prediction of Helicopter Unsteady Manoeuvres 197
Acoustical Methods and Experiments for Studying Rotorcraft Fuselage Scattering 197
Rotorcraft-pilot coupling analysis through state-space aerodynamic modelling 197
A Time-Dependent-Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors 196
A Boundary Integral Equation Method for the Aerodynamic Analysis of Rotors in Forward Flight in Potential, Compressible Flows 196
A Comparison Among Some Aeroelastic Models for the Stability Analysis of a Flap-Lag-Torsion Helicopter Rotor in Hover 196
Aeroelastic Analysis of Blades Cascades Through Aerodynamic Reduced-Order Modeling 196
Assessment of Computational Models for the Effect of Aeroelasticity on BVI Noise Prediction 195
A Comparison of Boundary Integral Formulations for Sound Scattered by Moving Bodies 194
A Unified Boundary Integral Methodology for Aerodynamics and Aeroacoustics of Rotors 193
Acoustical Methods Towards Accurate Prediction of Rotorcraft Fuselage Scattering 193
Lighthill Equation-based Boundary Integral Formulations for Sound Scattering of Moving Bodies 193
Lighthill Transpiration Velocity Revisited: an Exact Formulation 193
Finite-State Aerodynamic Modelling for Gust Load Alleviation of Wing-Tail Configurations 192
A High Order Boundary Element Formulation for Potential Incompressible Aerodynamics 192
Evaluation of Rotorcraft Aeroelastic Stability Using Robust Analysis 192
A General Theory of Potential Aerodynamics with Applications to Helicopter Rotor-Fuselage Interaction 192
Multiblade Reduced-Order Aerodynamics for State-Space Aeroelastic Modeling of Rotors 192
Toward an Integration of Aerodynamics and Aeroacoustics of Rotors 192
Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors 191
Adverse Rotorcraft-Pilot Coupling: Recent Research Activities in Europe 191
A Unified Approach for Aerodynamics and Aeroacoustics of Rotors in Compressible Potential Flows 190
Totale 22.373
Categoria #
all - tutte 138.994
article - articoli 0
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 138.994


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20213.684 0 0 0 0 0 231 683 977 298 310 132 1.053
2021/20222.331 77 288 51 52 543 86 203 128 241 103 137 422
2022/20233.530 435 514 230 309 267 758 79 354 324 49 100 111
2023/20242.166 132 110 119 70 240 358 249 318 20 98 143 309
2024/20256.464 90 153 662 182 180 213 2.049 1.331 575 105 443 481
2025/20266.885 825 1.601 678 1.951 1.241 589 0 0 0 0 0 0
Totale 47.912