GENNARETTI, MASSIMO
 Distribuzione geografica
Continente #
NA - Nord America 13.851
EU - Europa 13.431
AS - Asia 5.647
AF - Africa 153
OC - Oceania 14
Continente sconosciuto - Info sul continente non disponibili 11
SA - Sud America 8
Totale 33.115
Nazione #
US - Stati Uniti d'America 13.833
CN - Cina 4.432
DK - Danimarca 4.060
GB - Regno Unito 3.959
DE - Germania 1.136
VN - Vietnam 932
SE - Svezia 890
IT - Italia 868
UA - Ucraina 796
FR - Francia 453
FI - Finlandia 260
IE - Irlanda 260
AL - Albania 229
RU - Federazione Russa 222
BE - Belgio 153
CI - Costa d'Avorio 144
TR - Turchia 138
IN - India 79
NL - Olanda 70
IR - Iran 20
CA - Canada 18
RO - Romania 17
AU - Australia 12
ES - Italia 10
GR - Grecia 10
AT - Austria 9
CH - Svizzera 9
SA - Arabia Saudita 9
HK - Hong Kong 8
CZ - Repubblica Ceca 7
EU - Europa 6
JP - Giappone 6
BR - Brasile 5
HU - Ungheria 5
KR - Corea 5
SG - Singapore 5
A2 - ???statistics.table.value.countryCode.A2??? 4
ZA - Sudafrica 4
MY - Malesia 3
NO - Norvegia 3
MA - Marocco 2
MD - Moldavia 2
NZ - Nuova Zelanda 2
TN - Tunisia 2
VE - Venezuela 2
A1 - Anonimo 1
AR - Argentina 1
BD - Bangladesh 1
EG - Egitto 1
HR - Croazia 1
IL - Israele 1
IM - Isola di Man 1
KG - Kirghizistan 1
KZ - Kazakistan 1
LU - Lussemburgo 1
MN - Mongolia 1
NP - Nepal 1
PH - Filippine 1
PK - Pakistan 1
TW - Taiwan 1
UZ - Uzbekistan 1
Totale 33.115
Città #
Southend 3.703
Woodbridge 2.194
Fairfield 1.567
Ann Arbor 1.176
Wilmington 1.145
Chandler 974
Dong Ket 930
Ashburn 871
Nanjing 867
Houston 820
Dearborn 696
Jacksonville 612
Seattle 554
Cambridge 502
Princeton 427
Beijing 425
Shenyang 362
Rome 333
Nanchang 312
Jinan 291
Plano 271
Dublin 260
Hebei 229
Redwood City 217
Changsha 188
Jiaxing 169
Tianjin 167
Brussels 151
Shanghai 147
Izmir 134
Zhengzhou 126
Taizhou 98
San Diego 95
Hangzhou 91
Kunming 90
Ningbo 85
Guangzhou 83
Fuzhou 73
Orange 68
Hefei 64
Pune 64
Haikou 52
Taiyuan 52
Bremen 50
Boardman 49
New York 45
San Paolo di Civitate 44
Altamura 41
Helsinki 40
London 40
Milan 36
Alameda 34
Lanzhou 31
Washington 30
Lawrence 26
Fort Worth 22
Vélizy-villacoublay 21
Flushing 20
Nürnberg 20
Mountain View 17
Dallas 16
Norwalk 15
Stevenage 15
Delft 14
Changchun 13
Luft 13
Bucharest 12
Redmond 12
Xian 12
Chengdu 11
Düsseldorf 11
Falls Church 11
Nettuno 11
Renton 11
Verona 11
Atlanta 10
Auburn Hills 10
Chiswick 10
Chongqing 10
Wuhan 10
Baotou 9
Paris 9
Riyadh 9
Tiel 9
Florence 8
Hong Kong 8
Sevilla 8
Torino 8
Centro 7
Cranfield 7
Genova 7
Hounslow 7
Los Angeles 7
Rotterdam 7
Stuttgart 7
Vienna 7
Kilburn 6
Napoli 6
Saint Paul 6
Sharif 6
Totale 22.687
Nome #
Structural and Aeroelastic Modeling of Curved Rotor Blades Using a Galerkin Approach 337
A Spectral Formulation for Structural/Aeroelastic Modeling of Curved-Axis Rotor Blades 286
ALGORITHM FOR IDENTIFICATION OF HELICOPTER OPEN-LOOP TRANSFER FUNCTIONS AND REDUCED-ORDER MODELING 277
Boundary Integral Equation Methods for Aerodynamics 273
Assessment of a comprehensive aeroelastic tool for horizontal-axis wind turbine rotor analysis 247
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft 242
Tiltrotor Cabin Noise Control Through Smart Actuators 242
Parallel Blade-Vortex Interaction Modelling for Helicopter Rotor Noise Control Synthesis 229
Analysis of Vibrations of an Innovative Civil Tiltrotor 222
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 213
Aerodynamics and Aeroacoustics of Wings and Rotors via BEM -- Unsteady, Transonic and Viscous Effects 199
Synthesis of Active Twist Controller for Rotor Blade–Vortex Interaction Noise Alleviation 197
Analysis of Helicopter Vibratory Hub Loads Alleviation By Cyclic Trailing-Edge Blade Flap Actuation 195
Rotorcraft Aeroelastic Stability Using Robust Analysis 193
Aeroacoustoelasticity in State-Space Format Using CHIEF Regularization 192
Synthesis of Rotor BVI Noise Active Controller Through Efficient Aerodynamics/Aeroacoustics Solver 191
Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors 189
A Spectral-BEM Formulation for Compact Sources Aeroacoustics 187
A boundary integral formulation for sound scattered by elastic moving bodies 187
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Cylindrical Shells 187
Aeroacoustic Analysis of Helicopter Rotors in Ground Effect 186
A New Velocity Decomposition for Viscous Flows: Lighthill's Equivalent-Source Method Revisited 185
Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices 185
A Frequency Domain Approach for the Prediction of Tonal Noise Emitted by Rotors in Arbitrary Steady Motion 184
Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation 184
A Boundary-Field Integral Equation for Analysis of Cavity Acoustic Spectrum 183
Aeroelastic Rotorcraft-Pilot Couplings: Problems and Methods 183
Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings - A design perspective 182
A Velocity-Potential-Based Boundary-Element Method for the Aeroacoustic Analysis of Rotors and Propellers in Arbitrary Motion 181
An optimal control approach for alleviation of tiltrotor gust response 181
Innovative Helicopter In-Flight Noise Monitoring Systems Enabled by Rotor-State Measurements 181
Aeroelastic Response of Helicopter Rotors Using a 3-D Unsteady Aerodynamic Solver 179
Assessment of a FEM-based Formulation for Horizontal Axis Wind Turbine Rotors Aeroelasticity 179
Helicopter Noise Footprint Prediction in Unsteady Maneuvers 178
Assessment of Helicopter Pilot-in-the-Loop Models 176
A Retrospective Survey of Adverse Rotorcraft Pilot Couplings in European Perspective 175
Active Twist Rotor Controller Identification for Blade-Vortex Interaction Noise Alleviation 175
Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing­-Proprotor Aerodynamic Interaction 173
Simulation of Helicopter Noise in Maneuvering Flight 173
Synthesis of a Rotor Noise Controller by Parallel Blade-Vortex Interaction Aeroelastic Modelling 172
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 172
Effects of Biodynamic Feedthrough in Rotorcraft/Pilot Coupling: Collective Bounce Case 172
An Unsteady Aerodynamic Formulation for Efficient Rotor Tonal Noise Prediction 171
An Analytical-Numerical Aerodynamic Formulation for Efficient Aeroacoustics Analysis of Rotorcraft 171
Numerical characterization of helicopter noise hemispheres 171
Assessment of a state-space aeroelastic rotor model for rotorcraft flight dynamics 170
A Finite-State Aeroelastic Model for Rotorcraft–Pilot Coupling Analysis 169
Boundary Integral Transonics for Wings and Rotors 168
Forces and Moments in Incompressible Quasi-Potential Flows 168
A BEM simulation of a wind tunnel with an open test section 168
Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuation 168
Optimal Design and Acoustic Assessment of Low-Vibration Rotor Blades 168
Rotorcraft Comprehensive Code Assessment for Blade-Vortex Interaction Conditions 167
A Third-Order Boundary Element Method for Exterior Acoustics with Applications to Scattering by Rigid and Elastic Shells 166
A Boundary Element Method for the Aerodynamics and Aeroacoustics of Bodies in Arbitrary Motions 166
Aeroelastic Analysis of Blades Cascades Through Aerodynamic Reduced-Order Modeling 166
Adverse Rotorcraft Pilot Couplings - Past, Present and Future Challenges 166
GARTEUR Activities on Acoustical Methods and Experiments for Studying on Acoustic Scattering 166
A Unified Boundary Integral Methodology for Aerodynamics and Aeroacoustics of Rotors 165
Identification of rotor wake inflow finite-state models for flight dynamics simulations 165
ASSESSMENT OF A STATE-SPACE AEROELASTIC ROTOR MODEL FOR ROTORCRAFT DYNAMICS ANALYSIS 164
A Time-Dependent-Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors 164
Evaluation of noise excess for pushing propeller aircraft by CFD aeroacoustic calculation 163
A General Theory of Potential Aerodynamics with Applications to Helicopter Rotor-Fuselage Interaction 163
Structural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor Blades 163
Multiblade Reduced-Order Aerodynamics for State-Space Aeroelastic Modeling of Rotors 163
Lighthill Transpiration Velocity Revisited: an Exact Formulation 163
A Unified Approach for Aerodynamics and Aeroacoustics of Rotors in Compressible Potential Flows 162
Aeroacoustic Analysis of Propeller-Fuselage Interaction 162
Whirl Flutter Analysis of Prop-Rotors Using Unsteady Aerodynamics Reduced-Order Models 161
A High Order Boundary Element Formulation for Potential Incompressible Aerodynamics 157
Reduced-order modeling for linearized aeroelasticity of fixed wings in transonic flight 157
Aeroacoustoelastic Modeling for Cabin Noise Alleviation in Propeller--Driven Aircraft 156
Investigation on a High-Frequency Controller for Rotor BVI Noise Alleviation 156
Finite-State Aerodynamic Modelling for Gust Load Alleviation of Wing-Tail Configurations 155
A Boundary Integral Method in Rotor Aeroacoustics 154
Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors 154
A Third-Order Boundary Element Method Scattering of Elastic Shells 154
A Boundary Element Method for Aerodynamics of Wings and Rotors 154
Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications 154
A Boundary Element Method for the Potential, Compressible Aerodynamics of Bodies in Arbitrary Motion 153
Frequency-Domain Method for Discrete Frequency Noise Prediction of Rotors in Arbitrary Steady Motion 153
Assessment of Computational Models for the Effect of Aeroelasticity on BVI Noise Prediction 152
A Boundary Integral Method for Unified Transonic Aerodynamic and Aeroacoustic Analysis of Hovering Rotors 150
Aircraft Cabin Tonal Noise Alleviation Through Fuselage Skin Embedded Piezoelectric Actuators 150
Spectral-Boundary-Integral Compact-Source Formulation for Aero-Hydroacoustics of Rotors 150
Time-Dependent Coefficient Reduced-Order Model for Unsteady Aerodynamics of Proprotors 150
Integrated Aeroacoustoelastic Modeling for the Analysis of the Propeller--Driven Cabin Noise 148
A Boundary Element Method for the Aerodynamic Analysis of Aircraft in Arbitrary Motion 147
Fully Coupled Structural-Unsteady Aerodynamics Modelling for Aeroelastic Response of Rotorcraft 147
A Novel Potential-Flow Boundary Integral Formulation for Helicopter Rotors in BVI Conditions 147
Rotorcraft-pilot coupling analysis through state-space aerodynamic modelling 147
Parallel Blade-Vortex Interaction Analyses and Rotor Noise Control Synthesis 147
Coupled Free-Wake-Aerodynamics/Blade-Dynamics Analyses of Rotors in Forward Flight 146
Lighthill Equation-based Boundary Integral Formulations for Sound Scattering of Moving Bodies 146
A Space-Time Accurate Finite-State Inflow Model for Aeroelastic Applications 145
Theoretical and Numerical Issues for Hydroacoustic Applications of the Ffowcs Williams-Hawkings Equation 145
Acoustical Methods Towards Accurate Prediction of Rotorcraft Fuselage Scattering 144
Pressure-Feedback Based Blade-Vortex Interaction Noise Controller for Helicopter Rotors 143
State-Space Rotor Aeroelastic Modeling for Real-Time Helicopter Flight Simulation 143
Totale 17.575
Categoria #
all - tutte 76.863
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 76.863


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/20192.501 0 0 0 0 0 0 0 0 23 220 1.159 1.099
2019/20208.029 1.821 639 352 490 525 681 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
2022/20233.594 435 514 230 309 267 758 93 367 329 62 114 116
2023/20241.683 145 121 124 87 263 358 249 318 18 0 0 0
Totale 34.144