Benvenuti nell'Anagrafe della Ricerca d'Ateneo

GENNARETTI, MASSIMO
 Distribuzione geografica
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Continente #
EU - Europa 16.497
NA - Nord America 14.701
AS - Asia 6.543
AF - Africa 165
SA - Sud America 54
OC - Oceania 18
Continente sconosciuto - Info sul continente non disponibili 11
Totale 37.989
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Nazione #
US - Stati Uniti d'America 14.664
CN - Cina 4.622
DK - Danimarca 4.061
GB - Regno Unito 3.955
RU - Federazione Russa 3.018
DE - Germania 1.198
IT - Italia 1.062
VN - Vietnam 933
SE - Svezia 892
UA - Ucraina 798
FR - Francia 475
SG - Singapore 448
FI - Finlandia 271
IE - Irlanda 263
AL - Albania 229
CI - Costa d'Avorio 146
TR - Turchia 146
HK - Hong Kong 118
NL - Olanda 82
IN - India 79
JP - Giappone 78
BE - Belgio 61
BR - Brasile 43
KR - Corea 43
CA - Canada 35
CZ - Repubblica Ceca 24
IR - Iran 21
AT - Austria 20
RO - Romania 17
AU - Australia 16
ES - Italia 13
CH - Svizzera 11
GR - Grecia 10
SA - Arabia Saudita 9
LT - Lituania 8
AZ - Azerbaigian 7
HU - Ungheria 7
EU - Europa 6
MA - Marocco 6
ZA - Sudafrica 6
AR - Argentina 5
ID - Indonesia 5
LV - Lettonia 5
NO - Norvegia 5
UZ - Uzbekistan 5
A2 - ???statistics.table.value.countryCode.A2??? 4
EG - Egitto 4
IL - Israele 3
MY - Malesia 3
PH - Filippine 3
PK - Pakistan 3
PL - Polonia 3
VE - Venezuela 3
BD - Bangladesh 2
EC - Ecuador 2
EE - Estonia 2
KG - Kirghizistan 2
KZ - Kazakistan 2
LA - Repubblica Popolare Democratica del Laos 2
LK - Sri Lanka 2
LU - Lussemburgo 2
MD - Moldavia 2
MN - Mongolia 2
NZ - Nuova Zelanda 2
TN - Tunisia 2
A1 - Anonimo 1
AM - Armenia 1
CO - Colombia 1
HR - Croazia 1
IM - Isola di Man 1
JM - Giamaica 1
JO - Giordania 1
KE - Kenya 1
MX - Messico 1
NP - Nepal 1
SK - Slovacchia (Repubblica Slovacca) 1
TH - Thailandia 1
TW - Taiwan 1
Totale 37.989
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Città #
Southend 3.703
Woodbridge 2.194
Fairfield 1.567
Ann Arbor 1.176
Wilmington 1.145
Ashburn 980
Chandler 974
Dong Ket 930
Nanjing 869
Houston 820
Dearborn 696
Jacksonville 612
Boardman 574
Seattle 554
Cambridge 502
Beijing 435
Princeton 427
Rome 396
Shenyang 362
Nanchang 312
Jinan 291
Plano 271
Dublin 263
Singapore 236
Hebei 229
Redwood City 217
Changsha 188
Jiaxing 171
Shanghai 168
Tianjin 168
Moscow 158
Izmir 134
Zhengzhou 128
Hong Kong 118
Taizhou 98
San Diego 95
Hangzhou 93
Kunming 90
Guangzhou 87
Ningbo 85
Fuzhou 74
Tokyo 73
Orange 68
Hefei 64
Pune 64
Brussels 59
Milan 56
Haikou 52
Taiyuan 52
Bremen 50
Dallas 50
Helsinki 49
New York 46
San Paolo di Civitate 44
Altamura 43
Los Angeles 40
Seoul 40
London 37
Alameda 34
Yubileyny 34
Washington 32
Lanzhou 31
Lawrence 26
Fort Worth 22
Vélizy-villacoublay 21
Brno 20
Flushing 20
Nürnberg 20
Frankfurt am Main 18
Mountain View 17
Santa Clara 16
Norwalk 15
Stevenage 15
Delft 14
Changchun 13
Luft 13
Toronto 13
Bucharest 12
Chengdu 12
Redmond 12
Xian 12
Amsterdam 11
Düsseldorf 11
Eitensheim 11
Falls Church 11
Nettuno 11
Renton 11
Torre del Greco 11
Verona 11
Vienna 11
Atlanta 10
Auburn Hills 10
Chongqing 10
Falkenstein 10
Ottawa 10
Tradate 10
Wuhan 10
Baotou 9
Chiswick 9
Istanbul 9
Totale 24.115
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Nome #
Structural and Aeroelastic Modeling of Curved Rotor Blades Using a Galerkin Approach 366
ALGORITHM FOR IDENTIFICATION OF HELICOPTER OPEN-LOOP TRANSFER FUNCTIONS AND REDUCED-ORDER MODELING 314
A Spectral Formulation for Structural/Aeroelastic Modeling of Curved-Axis Rotor Blades 306
Boundary Integral Equation Methods for Aerodynamics 288
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft 273
Assessment of a comprehensive aeroelastic tool for horizontal-axis wind turbine rotor analysis 272
Tiltrotor Cabin Noise Control Through Smart Actuators 264
Parallel Blade-Vortex Interaction Modelling for Helicopter Rotor Noise Control Synthesis 243
Analysis of Vibrations of an Innovative Civil Tiltrotor 236
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 228
A Boundary-Field Integral Equation for Analysis of Cavity Acoustic Spectrum 216
Synthesis of Active Twist Controller for Rotor Blade–Vortex Interaction Noise Alleviation 215
A boundary integral formulation for sound scattered by elastic moving bodies 214
Rotorcraft Aeroelastic Stability Using Robust Analysis 213
Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation 212
Aeroacoustic Analysis of Helicopter Rotors in Ground Effect 210
A BEM simulation of a wind tunnel with an open test section 207
Analysis of Helicopter Vibratory Hub Loads Alleviation By Cyclic Trailing-Edge Blade Flap Actuation 206
Aerodynamics and Aeroacoustics of Wings and Rotors via BEM -- Unsteady, Transonic and Viscous Effects 206
Aeroacoustoelasticity in State-Space Format Using CHIEF Regularization 205
A Frequency Domain Approach for the Prediction of Tonal Noise Emitted by Rotors in Arbitrary Steady Motion 205
Synthesis of Rotor BVI Noise Active Controller Through Efficient Aerodynamics/Aeroacoustics Solver 203
Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings - A design perspective 202
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Cylindrical Shells 200
An optimal control approach for alleviation of tiltrotor gust response 199
A Finite-State Aeroelastic Model for Rotorcraft–Pilot Coupling Analysis 198
A Spectral-BEM Formulation for Compact Sources Aeroacoustics 197
Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors 197
Assessment of a FEM-based Formulation for Horizontal Axis Wind Turbine Rotors Aeroelasticity 196
Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices 196
A Velocity-Potential-Based Boundary-Element Method for the Aeroacoustic Analysis of Rotors and Propellers in Arbitrary Motion 194
GARTEUR Activities on Acoustical Methods and Experiments for Studying on Acoustic Scattering 194
Assessment of Helicopter Pilot-in-the-Loop Models 194
Aeroelastic Response of Helicopter Rotors Using a 3-D Unsteady Aerodynamic Solver 193
A New Velocity Decomposition for Viscous Flows: Lighthill's Equivalent-Source Method Revisited 193
Helicopter Noise Footprint Prediction in Unsteady Maneuvers 193
A Boundary Element Method for Aerodynamics of Wings and Rotors 192
Innovative Helicopter In-Flight Noise Monitoring Systems Enabled by Rotor-State Measurements 192
Aeroelastic Rotorcraft-Pilot Couplings: Problems and Methods 192
Active Twist Rotor Controller Identification for Blade-Vortex Interaction Noise Alleviation 192
A Boundary Element Method for the Aerodynamics and Aeroacoustics of Bodies in Arbitrary Motions 191
Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuation 191
Adverse Rotorcraft Pilot Couplings - Past, Present and Future Challenges 190
Identification of rotor wake inflow finite-state models for flight dynamics simulations 189
A Boundary Integral Method for Unified Transonic Aerodynamic and Aeroacoustic Analysis of Hovering Rotors 189
Assessment of a state-space aeroelastic rotor model for rotorcraft flight dynamics 189
A Boundary Integral Method in Rotor Aeroacoustics 188
A Retrospective Survey of Adverse Rotorcraft Pilot Couplings in European Perspective 188
Numerical characterization of helicopter noise hemispheres 188
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 186
Optimal Design and Acoustic Assessment of Low-Vibration Rotor Blades 186
Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing­-Proprotor Aerodynamic Interaction 185
Effects of Biodynamic Feedthrough in Rotorcraft/Pilot Coupling: Collective Bounce Case 185
An Analytical-Numerical Aerodynamic Formulation for Efficient Aeroacoustics Analysis of Rotorcraft 185
Synthesis of a Rotor Noise Controller by Parallel Blade-Vortex Interaction Aeroelastic Modelling 184
An Unsteady Aerodynamic Formulation for Efficient Rotor Tonal Noise Prediction 184
Simulation of Helicopter Noise in Maneuvering Flight 184
Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications 184
ASSESSMENT OF A STATE-SPACE AEROELASTIC ROTOR MODEL FOR ROTORCRAFT DYNAMICS ANALYSIS 183
Rotorcraft Comprehensive Code Assessment for Blade-Vortex Interaction Conditions 182
Boundary Integral Transonics for Wings and Rotors 181
A Boundary Element Method for the Potential, Compressible Aerodynamics of Bodies in Arbitrary Motion 180
Aeroelastic Analysis of Blades Cascades Through Aerodynamic Reduced-Order Modeling 179
A Third-Order Boundary Element Method for Exterior Acoustics with Applications to Scattering by Rigid and Elastic Shells 178
Forces and Moments in Incompressible Quasi-Potential Flows 178
A Boundary Integral Method for Aeroacoustics of Rotors 178
A Unified Boundary Integral Methodology for Aerodynamics and Aeroacoustics of Rotors 176
A Time-Dependent-Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors 175
A Unified Approach for Aerodynamics and Aeroacoustics of Rotors in Compressible Potential Flows 174
A General Theory of Potential Aerodynamics with Applications to Helicopter Rotor-Fuselage Interaction 174
Whirl Flutter Analysis of Prop-Rotors Using Unsteady Aerodynamics Reduced-Order Models 173
Evaluation of noise excess for pushing propeller aircraft by CFD aeroacoustic calculation 173
Aeroacoustic Analysis of Propeller-Fuselage Interaction 173
Structural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor Blades 173
Multiblade Reduced-Order Aerodynamics for State-Space Aeroelastic Modeling of Rotors 173
Lighthill Transpiration Velocity Revisited: an Exact Formulation 173
A Combined Interior--Exterior Model for Propeller Acoustics 171
Spectral-Boundary-Integral Compact-Source Formulation for Aero-Hydroacoustics of Rotors 171
A Boundary Element Method for the Aerodynamic Analysis of Aircraft in Arbitrary Motion 170
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 170
Finite-State Aerodynamic Modelling for Gust Load Alleviation of Wing-Tail Configurations 169
Fully Coupled Structural-Unsteady Aerodynamics Modelling for Aeroelastic Response of Rotorcraft 169
A Spatial Repetitive Controller Applied to an Aeroelastic Model for Wind Turbines 169
A High Order Boundary Element Formulation for Potential Incompressible Aerodynamics 168
Rotorcraft-pilot coupling analysis through state-space aerodynamic modelling 168
A Third-Order Boundary Element Method Scattering of Elastic Shells 167
Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors 166
A Boundary Integral Equation Method for the Aerodynamic Analysis of Rotors in Forward Flight in Potential, Compressible Flows 166
A Space-Time Accurate Finite-State Inflow Model for Aeroelastic Applications 166
Acoustical Methods Towards Accurate Prediction of Rotorcraft Fuselage Scattering 165
Aeroacoustoelastic Modeling for Cabin Noise Alleviation in Propeller--Driven Aircraft 164
Frequency-Domain Method for Discrete Frequency Noise Prediction of Rotors in Arbitrary Steady Motion 164
Lighthill Equation-based Boundary Integral Formulations for Sound Scattering of Moving Bodies 164
Investigation on a High-Frequency Controller for Rotor BVI Noise Alleviation 164
A Comprehensive Approach for the Optimal Control of Tiltrotor Cabin Noise Through Activel-Driven Piezoelectric Actuators 164
Vibratory Analysis of an Innovative Civil Tiltrotor 163
Assessment of Computational Models for the Effect of Aeroelasticity on BVI Noise Prediction 162
Acoustic Prediction of Helicopter Unsteady Manoeuvres 162
Parallel Blade-Vortex Interaction Analyses and Rotor Noise Control Synthesis 162
A Boundary-Field Integral Formulation for Sound Scattering of Moving Bodies 161
Totale 19.343
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Categoria #
all - tutte 106.393
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 106.393
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20202.423 0 0 0 0 0 0 0 753 1.096 200 273 101
2020/20214.866 212 226 251 164 329 231 683 977 298 310 132 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
2024/20254.477 90 153 662 182 180 213 2.049 948 0 0 0 0
Totale 39.040