Benvenuti nell'Anagrafe della Ricerca d'Ateneo

GENNARETTI, MASSIMO
 Distribuzione geografica
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Continente #
NA - Nord America 14.627
EU - Europa 13.762
AS - Asia 6.426
AF - Africa 157
OC - Oceania 18
Continente sconosciuto - Info sul continente non disponibili 11
SA - Sud America 11
Totale 35.012
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Nazione #
US - Stati Uniti d'America 14.590
CN - Cina 4.621
DK - Danimarca 4.061
GB - Regno Unito 3.955
DE - Germania 1.180
IT - Italia 1.029
VN - Vietnam 932
SE - Svezia 892
UA - Ucraina 797
FR - Francia 474
RU - Federazione Russa 355
SG - Singapore 347
FI - Finlandia 271
IE - Irlanda 261
AL - Albania 229
CI - Costa d'Avorio 146
TR - Turchia 144
HK - Hong Kong 117
NL - Olanda 82
IN - India 79
JP - Giappone 78
BE - Belgio 61
KR - Corea 43
CA - Canada 35
CZ - Repubblica Ceca 22
IR - Iran 20
RO - Romania 17
AU - Australia 16
AT - Austria 14
ES - Italia 12
CH - Svizzera 10
GR - Grecia 10
SA - Arabia Saudita 9
LT - Lituania 8
BR - Brasile 6
EU - Europa 6
HU - Ungheria 6
ID - Indonesia 5
UZ - Uzbekistan 5
A2 - ???statistics.table.value.countryCode.A2??? 4
NO - Norvegia 4
ZA - Sudafrica 4
EG - Egitto 3
IL - Israele 3
LV - Lettonia 3
MY - Malesia 3
PH - Filippine 3
AR - Argentina 2
AZ - Azerbaigian 2
BD - Bangladesh 2
KZ - Kazakistan 2
LA - Repubblica Popolare Democratica del Laos 2
LK - Sri Lanka 2
MA - Marocco 2
MD - Moldavia 2
NZ - Nuova Zelanda 2
PL - Polonia 2
TN - Tunisia 2
VE - Venezuela 2
A1 - Anonimo 1
EC - Ecuador 1
EE - Estonia 1
HR - Croazia 1
IM - Isola di Man 1
JM - Giamaica 1
JO - Giordania 1
KG - Kirghizistan 1
LU - Lussemburgo 1
MN - Mongolia 1
MX - Messico 1
NP - Nepal 1
PK - Pakistan 1
SK - Slovacchia (Repubblica Slovacca) 1
TH - Thailandia 1
TW - Taiwan 1
Totale 35.012
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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 380
Shenyang 362
Nanchang 312
Jinan 291
Plano 271
Dublin 261
Singapore 235
Hebei 229
Redwood City 217
Changsha 188
Jiaxing 171
Shanghai 168
Tianjin 168
Izmir 134
Zhengzhou 128
Hong Kong 117
Taizhou 98
San Diego 95
Hangzhou 93
Kunming 90
Guangzhou 87
Ningbo 85
Fuzhou 74
Tokyo 73
Orange 68
Hefei 64
Pune 64
Moscow 62
Brussels 59
Haikou 52
Taiyuan 52
Bremen 50
Dallas 50
Helsinki 49
Milan 48
New York 45
San Paolo di Civitate 44
Altamura 43
Seoul 40
London 37
Alameda 34
Washington 32
Lanzhou 31
Los Angeles 30
Lawrence 26
Fort Worth 22
Vélizy-villacoublay 21
Brno 20
Flushing 20
Nürnberg 20
Frankfurt am Main 17
Mountain View 17
Norwalk 15
Stevenage 15
Delft 14
Santa Clara 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
Atlanta 10
Auburn Hills 10
Chongqing 10
Ottawa 10
Tradate 10
Wuhan 10
Baotou 9
Chiswick 9
Istanbul 9
Paris 9
Riyadh 9
Tiel 9
Totale 23.949
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Nome #
Structural and Aeroelastic Modeling of Curved Rotor Blades Using a Galerkin Approach 346
ALGORITHM FOR IDENTIFICATION OF HELICOPTER OPEN-LOOP TRANSFER FUNCTIONS AND REDUCED-ORDER MODELING 297
A Spectral Formulation for Structural/Aeroelastic Modeling of Curved-Axis Rotor Blades 290
Boundary Integral Equation Methods for Aerodynamics 283
Assessment of a comprehensive aeroelastic tool for horizontal-axis wind turbine rotor analysis 252
Tiltrotor Cabin Noise Control Through Smart Actuators 248
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft 247
Parallel Blade-Vortex Interaction Modelling for Helicopter Rotor Noise Control Synthesis 230
Analysis of Vibrations of an Innovative Civil Tiltrotor 224
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 220
Aerodynamics and Aeroacoustics of Wings and Rotors via BEM -- Unsteady, Transonic and Viscous Effects 200
Synthesis of Active Twist Controller for Rotor Blade–Vortex Interaction Noise Alleviation 200
Analysis of Helicopter Vibratory Hub Loads Alleviation By Cyclic Trailing-Edge Blade Flap Actuation 199
Aeroacoustoelasticity in State-Space Format Using CHIEF Regularization 198
Rotorcraft Aeroelastic Stability Using Robust Analysis 198
A boundary integral formulation for sound scattered by elastic moving bodies 198
Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation 196
Synthesis of Rotor BVI Noise Active Controller Through Efficient Aerodynamics/Aeroacoustics Solver 195
Aeroacoustic Analysis of Helicopter Rotors in Ground Effect 194
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Cylindrical Shells 192
A Boundary-Field Integral Equation for Analysis of Cavity Acoustic Spectrum 191
A Frequency Domain Approach for the Prediction of Tonal Noise Emitted by Rotors in Arbitrary Steady Motion 191
A New Velocity Decomposition for Viscous Flows: Lighthill's Equivalent-Source Method Revisited 190
A Spectral-BEM Formulation for Compact Sources Aeroacoustics 190
Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors 190
An optimal control approach for alleviation of tiltrotor gust response 189
Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings - A design perspective 189
Aeroelastic Rotorcraft-Pilot Couplings: Problems and Methods 188
A BEM simulation of a wind tunnel with an open test section 187
Aeroelastic Response of Helicopter Rotors Using a 3-D Unsteady Aerodynamic Solver 186
A Velocity-Potential-Based Boundary-Element Method for the Aeroacoustic Analysis of Rotors and Propellers in Arbitrary Motion 186
Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices 186
Innovative Helicopter In-Flight Noise Monitoring Systems Enabled by Rotor-State Measurements 185
A Finite-State Aeroelastic Model for Rotorcraft–Pilot Coupling Analysis 183
A Retrospective Survey of Adverse Rotorcraft Pilot Couplings in European Perspective 182
Helicopter Noise Footprint Prediction in Unsteady Maneuvers 182
Assessment of a FEM-based Formulation for Horizontal Axis Wind Turbine Rotors Aeroelasticity 181
Assessment of Helicopter Pilot-in-the-Loop Models 181
Active Twist Rotor Controller Identification for Blade-Vortex Interaction Noise Alleviation 181
Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing­-Proprotor Aerodynamic Interaction 179
Numerical characterization of helicopter noise hemispheres 179
Assessment of a state-space aeroelastic rotor model for rotorcraft flight dynamics 178
Effects of Biodynamic Feedthrough in Rotorcraft/Pilot Coupling: Collective Bounce Case 177
A Boundary Element Method for the Aerodynamics and Aeroacoustics of Bodies in Arbitrary Motions 176
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 176
Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuation 176
Synthesis of a Rotor Noise Controller by Parallel Blade-Vortex Interaction Aeroelastic Modelling 175
An Unsteady Aerodynamic Formulation for Efficient Rotor Tonal Noise Prediction 175
Simulation of Helicopter Noise in Maneuvering Flight 175
Rotorcraft Comprehensive Code Assessment for Blade-Vortex Interaction Conditions 175
Adverse Rotorcraft Pilot Couplings - Past, Present and Future Challenges 175
Optimal Design and Acoustic Assessment of Low-Vibration Rotor Blades 175
A Third-Order Boundary Element Method for Exterior Acoustics with Applications to Scattering by Rigid and Elastic Shells 173
Forces and Moments in Incompressible Quasi-Potential Flows 173
An Analytical-Numerical Aerodynamic Formulation for Efficient Aeroacoustics Analysis of Rotorcraft 173
Identification of rotor wake inflow finite-state models for flight dynamics simulations 173
Boundary Integral Transonics for Wings and Rotors 171
ASSESSMENT OF A STATE-SPACE AEROELASTIC ROTOR MODEL FOR ROTORCRAFT DYNAMICS ANALYSIS 171
GARTEUR Activities on Acoustical Methods and Experiments for Studying on Acoustic Scattering 171
Aeroelastic Analysis of Blades Cascades Through Aerodynamic Reduced-Order Modeling 170
A Time-Dependent-Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors 169
A Boundary Integral Method in Rotor Aeroacoustics 168
A Unified Boundary Integral Methodology for Aerodynamics and Aeroacoustics of Rotors 168
Evaluation of noise excess for pushing propeller aircraft by CFD aeroacoustic calculation 168
A Boundary Element Method for Aerodynamics of Wings and Rotors 168
Lighthill Transpiration Velocity Revisited: an Exact Formulation 168
Whirl Flutter Analysis of Prop-Rotors Using Unsteady Aerodynamics Reduced-Order Models 167
A General Theory of Potential Aerodynamics with Applications to Helicopter Rotor-Fuselage Interaction 167
Multiblade Reduced-Order Aerodynamics for State-Space Aeroelastic Modeling of Rotors 167
Aeroacoustic Analysis of Propeller-Fuselage Interaction 166
Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications 166
A Unified Approach for Aerodynamics and Aeroacoustics of Rotors in Compressible Potential Flows 165
Structural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor Blades 165
A Boundary Integral Method for Unified Transonic Aerodynamic and Aeroacoustic Analysis of Hovering Rotors 164
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 162
A Boundary Element Method for the Potential, Compressible Aerodynamics of Bodies in Arbitrary Motion 161
A High Order Boundary Element Formulation for Potential Incompressible Aerodynamics 161
Finite-State Aerodynamic Modelling for Gust Load Alleviation of Wing-Tail Configurations 160
A Third-Order Boundary Element Method Scattering of Elastic Shells 160
Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors 159
A Boundary Integral Method for Aeroacoustics of Rotors 159
Investigation on a High-Frequency Controller for Rotor BVI Noise Alleviation 159
Assessment of Computational Models for the Effect of Aeroelasticity on BVI Noise Prediction 157
Spectral-Boundary-Integral Compact-Source Formulation for Aero-Hydroacoustics of Rotors 157
Aeroacoustoelastic Modeling for Cabin Noise Alleviation in Propeller--Driven Aircraft 156
Rotorcraft-pilot coupling analysis through state-space aerodynamic modelling 156
A Boundary Element Method for the Aerodynamic Analysis of Aircraft in Arbitrary Motion 155
Frequency-Domain Method for Discrete Frequency Noise Prediction of Rotors in Arbitrary Steady Motion 155
Time-Dependent Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors 155
Fully Coupled Structural-Unsteady Aerodynamics Modelling for Aeroelastic Response of Rotorcraft 153
Aircraft Cabin Tonal Noise Alleviation Through Fuselage Skin Embedded Piezoelectric Actuators 153
A Novel Potential-Flow Boundary Integral Formulation for Helicopter Rotors in BVI Conditions 152
Acoustical Methods Towards Accurate Prediction of Rotorcraft Fuselage Scattering 152
Lighthill Equation-based Boundary Integral Formulations for Sound Scattering of Moving Bodies 152
Coupled Free-Wake-Aerodynamics/Blade-Dynamics Analyses of Rotors in Forward Flight 151
A Combined Interior--Exterior Model for Propeller Acoustics 151
Integrated Aeroacoustoelastic Modeling for the Analysis of the Propeller--Driven Cabin Noise 151
Vibratory Analysis of an Innovative Civil Tiltrotor 150
A Space-Time Accurate Finite-State Inflow Model for Aeroelastic Applications 150
State-Space Rotor Aeroelastic Modeling for Real-Time Helicopter Flight Simulation 150
Totale 18.184
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Categoria #
all - tutte 99.973
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 99.973
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20203.521 0 0 0 0 0 0 1.098 753 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
2024/20251.499 90 153 662 182 180 213 19 0 0 0 0 0
Totale 36.062