Benvenuti nell'Anagrafe della Ricerca d'Ateneo

GENNARETTI, MASSIMO
 Distribuzione geografica
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Continente #
NA - Nord America 14.569
EU - Europa 13.551
AS - Asia 6.230
AF - Africa 155
OC - Oceania 14
Continente sconosciuto - Info sul continente non disponibili 11
SA - Sud America 10
Totale 34.540
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Nazione #
US - Stati Uniti d'America 14.542
CN - Cina 4.589
DK - Danimarca 4.061
GB - Regno Unito 3.940
DE - Germania 1.169
IT - Italia 996
VN - Vietnam 932
SE - Svezia 890
UA - Ucraina 797
FR - Francia 474
SG - Singapore 292
FI - Finlandia 266
IE - Irlanda 261
AL - Albania 229
RU - Federazione Russa 222
CI - Costa d'Avorio 144
TR - Turchia 144
IN - India 79
NL - Olanda 79
JP - Giappone 78
BE - Belgio 58
KR - Corea 43
CA - Canada 25
CZ - Repubblica Ceca 22
IR - Iran 20
RO - Romania 17
AT - Austria 13
AU - Australia 12
ES - Italia 12
CH - Svizzera 10
GR - Grecia 10
SA - Arabia Saudita 9
HK - Hong Kong 8
EU - Europa 6
HU - Ungheria 6
BR - Brasile 5
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
LT - Lituania 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 34.540
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Città #
Southend 3.703
Woodbridge 2.194
Fairfield 1.567
Ann Arbor 1.176
Wilmington 1.145
Chandler 974
Ashburn 960
Dong Ket 930
Nanjing 869
Houston 820
Dearborn 696
Jacksonville 612
Boardman 574
Seattle 554
Cambridge 502
Beijing 434
Princeton 427
Shenyang 362
Rome 361
Nanchang 312
Jinan 291
Plano 271
Dublin 261
Hebei 229
Redwood City 217
Changsha 188
Singapore 186
Jiaxing 171
Shanghai 168
Tianjin 167
Izmir 134
Zhengzhou 126
Taizhou 98
San Diego 95
Hangzhou 91
Kunming 90
Guangzhou 86
Ningbo 85
Fuzhou 73
Tokyo 73
Orange 68
Hefei 64
Pune 64
Brussels 56
Haikou 52
Taiyuan 52
Bremen 50
Dallas 50
New York 45
Helsinki 44
San Paolo di Civitate 44
Altamura 43
Milan 43
Seoul 40
Alameda 34
Lanzhou 31
Washington 31
London 30
Los Angeles 30
Lawrence 26
Fort Worth 22
Vélizy-villacoublay 21
Brno 20
Flushing 20
Nürnberg 20
Mountain View 17
Norwalk 15
Stevenage 15
Delft 14
Changchun 13
Luft 13
Bucharest 12
Redmond 12
Santa Clara 12
Xian 12
Amsterdam 11
Chengdu 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
Tradate 10
Wuhan 10
Baotou 9
Chiswick 9
Istanbul 9
Paris 9
Riyadh 9
Tiel 9
Vienna 9
Florence 8
Frankfurt am Main 8
Hong Kong 8
Munich 8
Totale 23.651
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Nome #
Structural and Aeroelastic Modeling of Curved Rotor Blades Using a Galerkin Approach 343
ALGORITHM FOR IDENTIFICATION OF HELICOPTER OPEN-LOOP TRANSFER FUNCTIONS AND REDUCED-ORDER MODELING 296
A Spectral Formulation for Structural/Aeroelastic Modeling of Curved-Axis Rotor Blades 289
Boundary Integral Equation Methods for Aerodynamics 283
Assessment of a comprehensive aeroelastic tool for horizontal-axis wind turbine rotor analysis 250
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft 245
Tiltrotor Cabin Noise Control Through Smart Actuators 245
Parallel Blade-Vortex Interaction Modelling for Helicopter Rotor Noise Control Synthesis 230
Analysis of Vibrations of an Innovative Civil Tiltrotor 222
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 219
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
Aerodynamics and Aeroacoustics of Wings and Rotors via BEM -- Unsteady, Transonic and Viscous Effects 199
Rotorcraft Aeroelastic Stability Using Robust Analysis 197
Aeroacoustoelasticity in State-Space Format Using CHIEF Regularization 196
Synthesis of Rotor BVI Noise Active Controller Through Efficient Aerodynamics/Aeroacoustics Solver 195
A boundary integral formulation for sound scattered by elastic moving bodies 194
Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation 193
Aeroacoustic Analysis of Helicopter Rotors in Ground Effect 191
A Boundary-Field Integral Equation for Analysis of Cavity Acoustic Spectrum 190
Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors 190
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Cylindrical Shells 190
A New Velocity Decomposition for Viscous Flows: Lighthill's Equivalent-Source Method Revisited 189
A Spectral-BEM Formulation for Compact Sources Aeroacoustics 189
A Frequency Domain Approach for the Prediction of Tonal Noise Emitted by Rotors in Arbitrary Steady Motion 189
Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings - A design perspective 188
An optimal control approach for alleviation of tiltrotor gust response 187
Aeroelastic Rotorcraft-Pilot Couplings: Problems and Methods 187
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
Aeroelastic Response of Helicopter Rotors Using a 3-D Unsteady Aerodynamic Solver 184
A Velocity-Potential-Based Boundary-Element Method for the Aeroacoustic Analysis of Rotors and Propellers in Arbitrary Motion 184
A BEM simulation of a wind tunnel with an open test section 184
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
A Retrospective Survey of Adverse Rotorcraft Pilot Couplings in European Perspective 179
A Finite-State Aeroelastic Model for Rotorcraft–Pilot Coupling Analysis 178
Numerical characterization of helicopter noise hemispheres 177
Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing­-Proprotor Aerodynamic Interaction 176
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 175
Effects of Biodynamic Feedthrough in Rotorcraft/Pilot Coupling: Collective Bounce Case 175
Simulation of Helicopter Noise in Maneuvering Flight 175
Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuation 175
Assessment of a state-space aeroelastic rotor model for rotorcraft flight dynamics 175
Synthesis of a Rotor Noise Controller by Parallel Blade-Vortex Interaction Aeroelastic Modelling 174
An Unsteady Aerodynamic Formulation for Efficient Rotor Tonal Noise Prediction 174
Rotorcraft Comprehensive Code Assessment for Blade-Vortex Interaction Conditions 174
Optimal Design and Acoustic Assessment of Low-Vibration Rotor Blades 174
An Analytical-Numerical Aerodynamic Formulation for Efficient Aeroacoustics Analysis of Rotorcraft 173
Forces and Moments in Incompressible Quasi-Potential Flows 172
A Boundary Element Method for the Aerodynamics and Aeroacoustics of Bodies in Arbitrary Motions 172
Adverse Rotorcraft Pilot Couplings - Past, Present and Future Challenges 171
Identification of rotor wake inflow finite-state models for flight dynamics simulations 171
Boundary Integral Transonics for Wings and Rotors 170
A Third-Order Boundary Element Method for Exterior Acoustics with Applications to Scattering by Rigid and Elastic Shells 170
ASSESSMENT OF A STATE-SPACE AEROELASTIC ROTOR MODEL FOR ROTORCRAFT DYNAMICS ANALYSIS 170
GARTEUR Activities on Acoustical Methods and Experiments for Studying on Acoustic Scattering 170
Aeroelastic Analysis of Blades Cascades Through Aerodynamic Reduced-Order Modeling 169
A Unified Boundary Integral Methodology for Aerodynamics and Aeroacoustics of Rotors 168
Evaluation of noise excess for pushing propeller aircraft by CFD aeroacoustic calculation 167
A Time-Dependent-Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors 167
Multiblade Reduced-Order Aerodynamics for State-Space Aeroelastic Modeling of Rotors 167
Lighthill Transpiration Velocity Revisited: an Exact Formulation 167
A General Theory of Potential Aerodynamics with Applications to Helicopter Rotor-Fuselage Interaction 166
A Boundary Integral Method in Rotor Aeroacoustics 165
Whirl Flutter Analysis of Prop-Rotors Using Unsteady Aerodynamics Reduced-Order Models 165
A Boundary Element Method for Aerodynamics of Wings and Rotors 165
Aeroacoustic Analysis of Propeller-Fuselage Interaction 165
A Unified Approach for Aerodynamics and Aeroacoustics of Rotors in Compressible Potential Flows 164
Structural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor Blades 164
Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications 163
A High Order Boundary Element Formulation for Potential Incompressible Aerodynamics 161
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 161
A Boundary Integral Method for Unified Transonic Aerodynamic and Aeroacoustic Analysis of Hovering Rotors 161
Finite-State Aerodynamic Modelling for Gust Load Alleviation of Wing-Tail Configurations 160
A Boundary Element Method for the Potential, Compressible Aerodynamics of Bodies in Arbitrary Motion 159
Investigation on a High-Frequency Controller for Rotor BVI Noise Alleviation 159
Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors 158
A Third-Order Boundary Element Method Scattering of Elastic Shells 158
Spectral-Boundary-Integral Compact-Source Formulation for Aero-Hydroacoustics of Rotors 157
Aeroacoustoelastic Modeling for Cabin Noise Alleviation in Propeller--Driven Aircraft 156
A Boundary Integral Method for Aeroacoustics of Rotors 156
Assessment of Computational Models for the Effect of Aeroelasticity on BVI Noise Prediction 155
Rotorcraft-pilot coupling analysis through state-space aerodynamic modelling 155
Frequency-Domain Method for Discrete Frequency Noise Prediction of Rotors in Arbitrary Steady Motion 154
Time-Dependent Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors 154
A Boundary Element Method for the Aerodynamic Analysis of Aircraft in Arbitrary Motion 153
Aircraft Cabin Tonal Noise Alleviation Through Fuselage Skin Embedded Piezoelectric Actuators 153
Fully Coupled Structural-Unsteady Aerodynamics Modelling for Aeroelastic Response of Rotorcraft 152
A Novel Potential-Flow Boundary Integral Formulation for Helicopter Rotors in BVI Conditions 151
Integrated Aeroacoustoelastic Modeling for the Analysis of the Propeller--Driven Cabin Noise 151
Acoustical Methods Towards Accurate Prediction of Rotorcraft Fuselage Scattering 151
Lighthill Equation-based Boundary Integral Formulations for Sound Scattering of Moving Bodies 151
Coupled Free-Wake-Aerodynamics/Blade-Dynamics Analyses of Rotors in Forward Flight 149
Vibratory Analysis of an Innovative Civil Tiltrotor 149
A Combined Interior--Exterior Model for Propeller Acoustics 149
A Space-Time Accurate Finite-State Inflow Model for Aeroelastic Applications 149
Parallel Blade-Vortex Interaction Analyses and Rotor Noise Control Synthesis 149
Totale 18.046
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Categoria #
all - tutte 93.079
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 93.079
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20205.217 0 0 0 490 525 681 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
2024/20251.023 90 153 662 118 0 0 0 0 0 0 0 0
Totale 35.586