Benvenuti nell'Anagrafe della Ricerca d'Ateneo

GENNARETTI, MASSIMO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 18.795
EU - Europa 18.098
AS - Asia 14.233
SA - Sud America 1.444
AF - Africa 362
OC - Oceania 35
Continente sconosciuto - Info sul continente non disponibili 14
Totale 52.981
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 18.531
CN - Cina 6.470
GB - Regno Unito 4.111
DK - Danimarca 4.063
SG - Singapore 3.724
RU - Federazione Russa 3.081
VN - Vietnam 2.323
DE - Germania 1.379
IT - Italia 1.370
BR - Brasile 1.069
SE - Svezia 918
FR - Francia 915
UA - Ucraina 828
FI - Finlandia 370
IN - India 284
IE - Irlanda 273
HK - Hong Kong 257
AL - Albania 236
TR - Turchia 213
NL - Olanda 159
CI - Costa d'Avorio 150
BD - Bangladesh 142
JP - Giappone 135
CA - Canada 134
AR - Argentina 129
KR - Corea 125
ID - Indonesia 76
ZA - Sudafrica 71
MX - Messico 69
BE - Belgio 67
IQ - Iraq 67
PK - Pakistan 60
EC - Ecuador 59
PL - Polonia 59
PH - Filippine 52
ES - Italia 51
CO - Colombia 48
VE - Venezuela 40
UZ - Uzbekistan 39
AT - Austria 37
CZ - Repubblica Ceca 37
PY - Paraguay 35
SA - Arabia Saudita 35
AU - Australia 32
TN - Tunisia 30
MA - Marocco 28
MY - Malesia 28
TH - Thailandia 28
RO - Romania 27
CL - Cile 23
IR - Iran 23
EG - Egitto 20
JO - Giordania 20
CH - Svizzera 18
GR - Grecia 18
KZ - Kazakistan 17
LT - Lituania 16
PE - Perù 15
AZ - Azerbaigian 14
KE - Kenya 14
NP - Nepal 14
BO - Bolivia 13
JM - Giamaica 13
ET - Etiopia 12
UY - Uruguay 12
CR - Costa Rica 11
DZ - Algeria 11
HU - Ungheria 11
IL - Israele 11
LV - Lettonia 11
TW - Taiwan 10
DO - Repubblica Dominicana 9
LB - Libano 9
PA - Panama 9
BH - Bahrain 6
EU - Europa 6
KG - Kirghizistan 6
PS - Palestinian Territory 6
SK - Slovacchia (Repubblica Slovacca) 6
AE - Emirati Arabi Uniti 5
HR - Croazia 5
MN - Mongolia 5
NG - Nigeria 5
NO - Norvegia 5
OM - Oman 5
A2 - ???statistics.table.value.countryCode.A2??? 4
BA - Bosnia-Erzegovina 4
GT - Guatemala 4
LA - Repubblica Popolare Democratica del Laos 4
SI - Slovenia 4
SN - Senegal 4
SY - Repubblica araba siriana 4
LU - Lussemburgo 3
MD - Moldavia 3
NI - Nicaragua 3
NZ - Nuova Zelanda 3
TJ - Tagikistan 3
BG - Bulgaria 2
BN - Brunei Darussalam 2
BS - Bahamas 2
Totale 52.927
Salva come PNG Salva come JPEG
Città #
Southend 3.703
Woodbridge 2.194
Fairfield 1.567
Singapore 1.495
Ashburn 1.482
San Jose 1.363
Ann Arbor 1.176
Wilmington 1.146
Chandler 974
Dong Ket 930
Nanjing 871
Houston 836
Beijing 813
Dearborn 696
Hefei 689
Jacksonville 615
Boardman 574
Seattle 563
Rome 507
Cambridge 503
Dallas 451
Ho Chi Minh City 442
Princeton 428
Shenyang 365
Paris 329
Nanchang 312
Hanoi 302
Jinan 292
Dublin 273
Plano 273
Hong Kong 233
Hebei 229
Redwood City 217
Changsha 200
Shanghai 181
Los Angeles 175
Tianjin 175
Jiaxing 171
Moscow 161
New York 152
Zhengzhou 136
Izmir 135
Orem 121
Tokyo 117
Helsinki 116
Guangzhou 107
São Paulo 107
Frankfurt am Main 106
Seoul 104
Hangzhou 99
Taizhou 98
San Diego 95
Kunming 92
Milan 92
Munich 85
Ningbo 85
Santa Clara 76
Fuzhou 74
London 73
Orange 70
Pune 70
The Dalles 70
Haiphong 67
Brussels 65
Da Nang 60
Chennai 52
Haikou 52
Taiyuan 52
Bremen 50
Warsaw 48
Montreal 44
San Paolo di Civitate 44
Altamura 43
Rio de Janeiro 41
Amsterdam 37
Manchester 36
Mumbai 36
Tashkent 36
Atlanta 35
Hải Dương 35
Washington 35
Alameda 34
Johannesburg 34
Yubileyny 34
San Francisco 33
Toronto 33
Brooklyn 32
Denver 31
Lanzhou 31
Buffalo 28
Turku 28
Chicago 27
Biên Hòa 26
Lawrence 26
Stockholm 26
Curitiba 25
Istanbul 25
Phoenix 25
Baghdad 22
Columbus 22
Totale 31.596
Salva come PNG Salva come JPEG
Nome #
Structural and Aeroelastic Modeling of Curved Rotor Blades Using a Galerkin Approach 425
ALGORITHM FOR IDENTIFICATION OF HELICOPTER OPEN-LOOP TRANSFER FUNCTIONS AND REDUCED-ORDER MODELING 390
A Spectral Formulation for Structural/Aeroelastic Modeling of Curved-Axis Rotor Blades 360
Assessment of a comprehensive aeroelastic tool for horizontal-axis wind turbine rotor analysis 354
Boundary Integral Equation Methods for Aerodynamics 340
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft 337
Tiltrotor Cabin Noise Control Through Smart Actuators 323
A Boundary-Field Integral Equation for Analysis of Cavity Acoustic Spectrum 304
Aeroacoustic Analysis of Helicopter Rotors in Ground Effect 297
A BEM simulation of a wind tunnel with an open test section 288
A boundary integral formulation for sound scattered by elastic moving bodies 287
Analysis of Vibrations of an Innovative Civil Tiltrotor 287
Parallel Blade-Vortex Interaction Modelling for Helicopter Rotor Noise Control Synthesis 284
Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation 283
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 281
Rotorcraft Aeroelastic Stability Using Robust Analysis 270
A Retrospective Survey of Adverse Rotorcraft Pilot Couplings in European Perspective 269
Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications 269
Synthesis of Active Twist Controller for Rotor Blade–Vortex Interaction Noise Alleviation 268
A Boundary Integral Method in Rotor Aeroacoustics 267
A Boundary Element Method for Aerodynamics of Wings and Rotors 265
A Boundary Integral Method for Unified Transonic Aerodynamic and Aeroacoustic Analysis of Hovering Rotors 265
A Frequency Domain Approach for the Prediction of Tonal Noise Emitted by Rotors in Arbitrary Steady Motion 262
Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings - A design perspective 261
Aeroacoustoelasticity in State-Space Format Using CHIEF Regularization 259
Aerodynamics and Aeroacoustics of Wings and Rotors via BEM -- Unsteady, Transonic and Viscous Effects 257
A Boundary Integral Method for Aeroacoustics of Rotors 256
A Finite-State Aeroelastic Model for Rotorcraft–Pilot Coupling Analysis 256
A Boundary Element Method for the Aerodynamics and Aeroacoustics of Bodies in Arbitrary Motions 253
Rotorcraft Comprehensive Code Assessment for Blade-Vortex Interaction Conditions 252
An optimal control approach for alleviation of tiltrotor gust response 250
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Cylindrical Shells 249
A Spatial Repetitive Controller Applied to an Aeroelastic Model for Wind Turbines 247
Aeroelastic Response of Helicopter Rotors Using a 3-D Unsteady Aerodynamic Solver 246
Assessment of a FEM-based Formulation for Horizontal Axis Wind Turbine Rotors Aeroelasticity 246
Assessment of Helicopter Pilot-in-the-Loop Models 246
Analysis of Helicopter Vibratory Hub Loads Alleviation By Cyclic Trailing-Edge Blade Flap Actuation 245
Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuation 241
Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices 241
A Boundary Element Method for the Potential, Compressible Aerodynamics of Bodies in Arbitrary Motion 240
A Combined Interior--Exterior Model for Propeller Acoustics 240
Individual blade repetitive control for horizontal-axis wind turbines 240
Adverse Rotorcraft Pilot Couplings - Past, Present and Future Challenges 240
A Spectral-BEM Formulation for Compact Sources Aeroacoustics 239
GARTEUR Activities on Acoustical Methods and Experiments for Studying on Acoustic Scattering 239
Active Twist Rotor Controller Identification for Blade-Vortex Interaction Noise Alleviation 239
Identification of rotor wake inflow finite-state models for flight dynamics simulations 238
A Velocity-Potential-Based Boundary-Element Method for the Aeroacoustic Analysis of Rotors and Propellers in Arbitrary Motion 237
A Boundary-Field Integral Formulation for Sound Scattering of Moving Bodies 237
Synthesis of Rotor BVI Noise Active Controller Through Efficient Aerodynamics/Aeroacoustics Solver 237
Boundary Integral Transonics for Wings and Rotors 236
An Unsteady Aerodynamic Formulation for Efficient Rotor Tonal Noise Prediction 236
Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors 235
Assessment of a state-space aeroelastic rotor model for rotorcraft flight dynamics 235
Synthesis of a Rotor Noise Controller by Parallel Blade-Vortex Interaction Aeroelastic Modelling 233
Numerical characterization of helicopter noise hemispheres 233
Simulation of Helicopter Noise in Maneuvering Flight 232
Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing­-Proprotor Aerodynamic Interaction 231
A New Velocity Decomposition for Viscous Flows: Lighthill's Equivalent-Source Method Revisited 231
Effects of Biodynamic Feedthrough in Rotorcraft/Pilot Coupling: Collective Bounce Case 231
Optimal Design and Acoustic Assessment of Low-Vibration Rotor Blades 231
ASSESSMENT OF A STATE-SPACE AEROELASTIC ROTOR MODEL FOR ROTORCRAFT DYNAMICS ANALYSIS 229
Aeroelastic Rotorcraft-Pilot Couplings: Problems and Methods 229
A Comparison Among Some Aeroelastic Models for the Stability Analysis of a Flap-Lag-Torsion Helicopter Rotor in Hover 228
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 228
Forces and Moments in Incompressible Quasi-Potential Flows 227
Evaluation of noise excess for pushing propeller aircraft by CFD aeroacoustic calculation 227
A Boundary Integral Equation Method for the Aerodynamic Analysis of Rotors in Forward Flight in Potential, Compressible Flows 227
Innovative Helicopter In-Flight Noise Monitoring Systems Enabled by Rotor-State Measurements 227
Acoustic Prediction of Helicopter Unsteady Manoeuvres 227
Helicopter Noise Footprint Prediction in Unsteady Maneuvers 227
Theoretical and Numerical Issues for Hydroacoustic Applications of the Ffowcs Williams-Hawkings Equation 227
An Analytical-Numerical Aerodynamic Formulation for Efficient Aeroacoustics Analysis of Rotorcraft 226
A Boundary Element Method for the Aerodynamic Analysis of Aircraft in Arbitrary Motion 223
Fully Coupled Structural-Unsteady Aerodynamics Modelling for Aeroelastic Response of Rotorcraft 223
A Space-Time Accurate Finite-State Inflow Model for Aeroelastic Applications 222
A Comparison of Boundary Integral Formulations for Sound Scattered by Moving Bodies 222
Acoustical Methods Towards Accurate Prediction of Rotorcraft Fuselage Scattering 221
Spectral-Boundary-Integral Compact-Source Formulation for Aero-Hydroacoustics of Rotors 221
Whirl Flutter Analysis of Prop-Rotors Using Unsteady Aerodynamics Reduced-Order Models 220
Rotorcraft-pilot coupling analysis through state-space aerodynamic modelling 220
Structural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor Blades 219
A Third-Order Boundary Element Method for Exterior Acoustics with Applications to Scattering by Rigid and Elastic Shells 218
A Boundary Element Method for the Aerodynamic Analysis Rotors in Arbitrary Motion 218
Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors 215
Acoustical Methods and Experiments for Studying Rotorcraft Fuselage Scattering 215
Finite-State Aerodynamic Modelling for Gust Load Alleviation of Wing-Tail Configurations 214
Aircraft and Rotorcraft Pilot Coupling: A Survey of Recent Research Activities Within the European Project ARISTOTEL 212
A High Order Boundary Element Formulation for Potential Incompressible Aerodynamics 211
A Time-Dependent-Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors 211
Lighthill Equation-based Boundary Integral Formulations for Sound Scattering of Moving Bodies 211
Multiblade Reduced-Order Aerodynamics for State-Space Aeroelastic Modeling of Rotors 211
Evaluation of Rotorcraft Aeroelastic Stability Using Robust Analysis 210
Lighthill Transpiration Velocity Revisited: an Exact Formulation 209
A Comprehensive Approach for the Optimal Control of Tiltrotor Cabin Noise Through Activel-Driven Piezoelectric Actuators 209
A Unified Boundary Integral Methodology for Aerodynamics and Aeroacoustics of Rotors 208
A Unified Approach for Aerodynamics and Aeroacoustics of Rotors in Compressible Potential Flows 208
Aeroelastic Analysis of Blades Cascades Through Aerodynamic Reduced-Order Modeling 208
Assessment of Computational Models for the Effect of Aeroelasticity on BVI Noise Prediction 208
A Boundary-Field Integral Equation for Identification of Acoustic Spectrum of Cavities 207
Totale 24.693
Salva come PNG Salva come JPEG
Categoria #
all - tutte 155.763
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 155.763
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.053 0 0 0 0 0 0 0 0 0 0 0 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
2025/202613.013 825 1.601 678 1.951 1.241 713 1.593 250 1.401 1.922 593 245
Totale 54.040