Benvenuti nell'Anagrafe della Ricerca d'Ateneo

BERNARDINI, Giovanni
 Distribuzione geografica
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Continente #
NA - Nord America 10.317
EU - Europa 8.686
AS - Asia 4.088
AF - Africa 155
OC - Oceania 23
Continente sconosciuto - Info sul continente non disponibili 14
SA - Sud America 9
Totale 23.292
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Nazione #
US - Stati Uniti d'America 10.282
CN - Cina 3.044
DK - Danimarca 2.851
GB - Regno Unito 2.345
DE - Germania 816
IT - Italia 798
VN - Vietnam 488
SE - Svezia 483
UA - Ucraina 408
SG - Singapore 212
IE - Irlanda 181
FI - Finlandia 163
CI - Costa d'Avorio 148
AL - Albania 137
FR - Francia 136
RU - Federazione Russa 126
IN - India 111
TR - Turchia 85
NL - Olanda 73
JP - Giappone 49
BE - Belgio 45
CA - Canada 29
ES - Italia 29
KR - Corea 29
AU - Australia 21
CH - Svizzera 16
HK - Hong Kong 16
GR - Grecia 15
CZ - Repubblica Ceca 13
AT - Austria 12
HU - Ungheria 9
IR - Iran 9
A2 - ???statistics.table.value.countryCode.A2??? 7
RO - Romania 7
BD - Bangladesh 6
EU - Europa 6
ID - Indonesia 6
MD - Moldavia 6
IL - Israele 5
IQ - Iraq 5
PL - Polonia 4
AR - Argentina 3
AZ - Azerbaigian 3
MA - Marocco 3
PT - Portogallo 3
UZ - Uzbekistan 3
BR - Brasile 2
EG - Egitto 2
KG - Kirghizistan 2
KZ - Kazakistan 2
LK - Sri Lanka 2
LV - Lettonia 2
MX - Messico 2
NO - Norvegia 2
NZ - Nuova Zelanda 2
PA - Panama 2
PK - Pakistan 2
TN - Tunisia 2
A1 - Anonimo 1
BG - Bulgaria 1
BO - Bolivia 1
CL - Cile 1
DO - Repubblica Dominicana 1
EC - Ecuador 1
EE - Estonia 1
HR - Croazia 1
IM - Isola di Man 1
JM - Giamaica 1
JO - Giordania 1
LA - Repubblica Popolare Democratica del Laos 1
LU - Lussemburgo 1
ME - Montenegro 1
MN - Mongolia 1
MO - Macao, regione amministrativa speciale della Cina 1
MY - Malesia 1
PH - Filippine 1
SA - Arabia Saudita 1
SY - Repubblica araba siriana 1
TH - Thailandia 1
VE - Venezuela 1
Totale 23.292
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Città #
Southend 2.164
Woodbridge 1.536
Fairfield 1.163
Ann Arbor 819
Ashburn 792
Wilmington 747
Chandler 737
Houston 583
Nanjing 575
Dong Ket 487
Seattle 429
Dearborn 404
Boardman 394
Beijing 365
Cambridge 362
Jacksonville 328
Rome 274
Princeton 259
Shenyang 224
Jinan 199
Dublin 181
Plano 179
Nanchang 166
Redwood City 144
Shanghai 143
Singapore 139
Hebei 125
Changsha 112
Pune 102
Jiaxing 88
Tianjin 85
Izmir 80
San Diego 70
Hangzhou 64
Taizhou 62
Zhengzhou 62
Kunming 60
Guangzhou 56
Dallas 50
Hefei 47
Ningbo 44
Brussels 43
Tokyo 41
Milan 40
Orange 38
Taiyuan 35
Haikou 34
Altamura 33
Washington 33
Helsinki 30
London 27
New York 26
Seoul 26
San Paolo di Civitate 23
Delft 22
Centrale 21
Fuzhou 20
Norwalk 19
Nürnberg 19
Alameda 18
Lanzhou 18
Torino 18
Los Angeles 16
Hong Kong 15
Lawrence 15
Redmond 15
Bremen 14
Brno 13
Sevilla 13
Munich 12
Vélizy-villacoublay 12
Amsterdam 11
Renton 11
Fort Worth 10
Mountain View 10
Stuttgart 10
Atlanta 9
Chengdu 9
Madrid 9
Santa Clara 9
Stevenage 9
Sunnyvale 9
Toronto 9
Vienna 9
Auburn Hills 8
Cranfield 8
Flushing 8
Lappeenranta 8
Ottawa 8
Torre del Greco 8
Tradate 8
Frankfurt am Main 7
Rotterdam 7
Saint Paul 7
Wuhan 7
Athens 6
Centro 6
Chisinau 6
Chiswick 6
Florence 6
Totale 15.847
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Nome #
Structural and Aeroelastic Modeling of Curved Rotor Blades Using a Galerkin Approach 344
A Spectral Formulation for Structural/Aeroelastic Modeling of Curved-Axis Rotor Blades 289
Tiltrotor Cabin Noise Control Through Smart Actuators 247
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft 245
Parallel Blade-Vortex Interaction Modelling for Helicopter Rotor Noise Control Synthesis 230
Analysis of Vibrations of an Innovative Civil Tiltrotor 222
Aeroelasticity of the PrandtlPlane: Body Freedom Flutter, Freeplay, and Limit Cycle Oscillation 204
Synthesis of Active Twist Controller for Rotor Blade–Vortex Interaction Noise Alleviation 200
A Boundary Element Method for the Aerodynamic Analysis of Aircraft in Arbitrary Motions 196
A Vorticity Formulation for Computational Fluid Dynamic and Aeroelastic Analyses of Viscous Flows 195
Synthesis of Rotor BVI Noise Active Controller Through Efficient Aerodynamics/Aeroacoustics Solver 195
Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation 194
A Comprehensive Approach for the Optimal Control of Tiltrotor Cabin Noise Through Actively-Driven Piezoelectric Actuators 194
NERONE: An Open-Source Based Tool for Aerodynamic Transonic Optimization of Nonplanar Wings 193
Recent Developments on a Boundary Element Method in Aerodynamics 192
Aeroacoustic Analysis of Helicopter Rotors in Ground Effect 192
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Cylindrical Shells 191
Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors 190
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
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 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
Multidisciplinary Design Optimization for the Preliminary Design of Aeronautical Configurations 185
Helicopter Noise Footprint Prediction in Unsteady Maneuvers 182
Active Twist Rotor Controller Identification for Blade-Vortex Interaction Noise Alleviation 181
Assessment of Computational Models for the Effect of Aeroelasticity on BVI Noise Prediction 181
Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors 180
Structural Characterization of Rotor Blades Through Photogrammetry 180
Numerical characterization of helicopter noise hemispheres 179
A Velocity-Potential-Based Boundary-Element Method for the Aeroacoustic Analysis of Rotors and Propellers in Arbitrary Motion 179
Multidisciplinary Design and Optimization for Fluid-Structure Interactions 178
Cabin Noise Alleviation Through Fuselage Skin Embedded Smart Actuators 178
Integrated Aerodynamic/Aeroacoustic Analysis of a Tiltrotor During Conversion 178
Singularities in BIEs for the Laplace Equation; Joukowski Trailing–Edge Conjecture Revisited 178
A novel finite-element family for interior acoustics 178
Aeroelastic Response of Helicopter Rotors Using a 3D Unsteady Aerodynamic Solver 176
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 176
Simulation of Helicopter Noise in Maneuvering Flight 175
Non-invasive dynamic measurement of helicopter blades 175
Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuation 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
A Novel Potential-Flow Boundary Integral Formulation for Helicopter Rotors in BVI Conditions 172
Identification of rotor wake inflow finite-state models for flight dynamics simulations 171
A Boundary Element Method for Aerodynamics and Aeroacoustics of Bodies in Arbitrary Motions 171
GARTEUR Activities on Acoustical Methods and Experiments for Studying on Acoustic Scattering 170
A simple, but efficient aeroacoustic model of jets 169
A Novel Highly Accurate Finite-Element Family 168
Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications 165
Structural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor Blades 164
Analysis of Helicopter Vibratory Hub Loads Alleviation by Cyclic Trailing–Edge Blade Flap Actuation 162
Photogrammetric Detection Technique for Rotor Blades Structural Characterization 161
Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing–Proprotor Aerodynamic Interaction 160
Multidisciplinary Design Optimization for Aircraft Configurations 160
Investigation on a High-Frequency Controller for Rotor BVI Noise Alleviation 159
Spectral-Boundary-Integral Compact-Source Formulation for Aero-Hydroacoustics of Rotors 157
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Fuselages of Turboprop Aircraft 157
A Hermite High-Order Finite Element for Structural Optimal Design 156
A Boundary Element Method for the Aerodynamic Analysis of a Tiltrotor During Conversion 155
Frequency-Domain Method for Discrete Frequency Noise Prediction of Rotors in Arbitrary Steady Motion 155
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 Boundary Integral Formulation for the Study of Vorticity-Generated Sound 152
Acoustical Methods Towards Accurate Prediction of Rotorcraft Fuselage Scattering 152
A Boundary Integral Method in Rotor Aeroacoustics 151
On the Vorticity Generated Sound for Moving Surfaces 151
Lighthill Equation-based Boundary Integral Formulations for Sound Scattering of Moving Bodies 151
A Space-Time Accurate Finite-State Inflow Model for Aeroelastic Applications 150
Flapping Wing Aeroelasticity Using Corotational FEM and 3D Panel Method 150
Parallel Blade-Vortex Interaction Analyses and Rotor Noise Control Synthesis 150
Vibratory Analysis of an Innovative Civil Tiltrotor 149
Pressure-Feedback Based Blade-Vortex Interaction Noise Controller for Helicopter Rotors 148
Aerodynamics for MDO of an Innovative Configuration 147
Analysis of Blade Deformation Effect on Rotor BVI Noise Prediction 147
A Viscous-Flow Decomposition with Aerodynamic and Aeroelastic Applications 146
A Hermite-Interpolation Finite Element for Structural Dynamics 146
Acoustic Prediction of Helicopter Unsteady Manoeuvres 146
Boundary Element Method for Aerodynamic Analysis of Bluff Bodies 145
Sound Synthesis Approach for Noise Annoyance Assessment of Rotorcraft Operations 143
Singularities in Discretized BIE’s for Laplace’s Equation; Trailing–Edge Conditions in Aerodynamics 142
Acoustical Methods and Experiments for Studying Rotorcraft Fuselage Scattering 142
A Boundary Element Method for the Aerodynamic Analysis of Rotors in Arbitrary Motions 142
A Quasi Static Condensation and a Hermite Finite-Element for Structural Dynamics 142
Blade Vortex Interaction 2D Modelling for Rotor Noise Control Synthesis 142
Aerodynamic Issues in MDO for Preliminary Design 141
ROSAA: The European Solution to Connect Aeroelasticity, Aerodynamics and Acoustics Codes in a Unique User-Friendly Rotorcraft Simulation System 141
Multi-Disciplinary Optimization for the Conceptual Design of Innovative Aircraft Configurations 140
A Boundary-Field Integral Formulation for Sound Scattering of Moving Bodies 139
MDO for Preliminary Design of a Highly Innovative Configuration 138
A Comparison of Boundary Integral Formulations for Sound Scattered by Moving Bodies 138
Optimization of Rotorcraft Noise Abatement Trajectories 136
Genetic Algorithm with Surrogate Wake Inflow Models for Helicopter Rotor Optimal Design 136
Sound Scattered by a Helicopter Fuselage in Descent Flight Condition 136
Combined Action of Variable-Stiffness Devices and Trailing-Edge Flap for Helicopter Hub Loads Reduction 135
Conceptual all-electric retrofit of helicopters: review, technological outlook and a sample design 134
MDO of an Innovative Configuration - Aerodynamic Issues 132
Totale 17.049
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Categoria #
all - tutte 69.322
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 69.322
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20203.009 0 0 0 0 333 442 707 511 665 121 165 65
2020/20213.054 128 151 128 76 252 136 409 663 198 221 124 568
2021/20221.864 71 179 54 64 345 67 239 115 150 93 102 385
2022/20232.251 268 329 146 220 196 491 24 213 231 13 71 49
2023/20241.882 88 92 104 60 281 328 248 312 17 36 126 190
2024/2025852 63 129 473 117 70 0 0 0 0 0 0 0
Totale 24.204