Benvenuti nell'Anagrafe della Ricerca d'Ateneo

BERNARDINI, Giovanni
 Distribuzione geografica
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Continente #
NA - Nord America 9.789
EU - Europa 8.495
AS - Asia 3.682
AF - Africa 149
OC - Oceania 22
Continente sconosciuto - Info sul continente non disponibili 14
SA - Sud America 6
Totale 22.157
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Nazione #
US - Stati Uniti d'America 9.761
CN - Cina 2.933
DK - Danimarca 2.851
GB - Regno Unito 2.345
DE - Germania 795
IT - Italia 682
VN - Vietnam 488
SE - Svezia 483
UA - Ucraina 408
IE - Irlanda 179
FI - Finlandia 154
CI - Costa d'Avorio 144
AL - Albania 136
FR - Francia 132
RU - Federazione Russa 126
IN - India 111
TR - Turchia 85
NL - Olanda 62
BE - Belgio 45
ES - Italia 23
CA - Canada 22
AU - Australia 20
CH - Svizzera 15
GR - Grecia 15
AT - Austria 9
HK - Hong Kong 9
IR - Iran 9
JP - Giappone 9
HU - Ungheria 8
A2 - ???statistics.table.value.countryCode.A2??? 7
KR - Corea 7
RO - Romania 7
EU - Europa 6
MD - Moldavia 6
BD - Bangladesh 5
IL - Israele 5
IQ - Iraq 5
SG - Singapore 5
PL - Polonia 3
PT - Portogallo 3
AR - Argentina 2
BR - Brasile 2
KG - Kirghizistan 2
MA - Marocco 2
MX - Messico 2
NZ - Nuova Zelanda 2
PA - Panama 2
PK - Pakistan 2
TN - Tunisia 2
A1 - Anonimo 1
BG - Bulgaria 1
CL - Cile 1
DO - Repubblica Dominicana 1
EE - Estonia 1
EG - Egitto 1
HR - Croazia 1
IM - Isola di Man 1
JM - Giamaica 1
JO - Giordania 1
KZ - Kazakistan 1
LU - Lussemburgo 1
LV - Lettonia 1
ME - Montenegro 1
MN - Mongolia 1
MO - Macao, regione amministrativa speciale della Cina 1
NO - Norvegia 1
PH - Filippine 1
SA - Arabia Saudita 1
SY - Repubblica araba siriana 1
VE - Venezuela 1
Totale 22.157
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Città #
Southend 2.164
Woodbridge 1.536
Fairfield 1.163
Ann Arbor 819
Wilmington 747
Chandler 737
Ashburn 714
Houston 583
Nanjing 575
Dong Ket 487
Seattle 429
Dearborn 404
Beijing 365
Cambridge 362
Jacksonville 328
Princeton 259
Rome 239
Shenyang 224
Jinan 199
Dublin 179
Plano 179
Nanchang 166
Redwood City 144
Hebei 125
Shanghai 119
Changsha 112
Pune 102
Jiaxing 88
Tianjin 85
Izmir 80
San Diego 70
Hangzhou 64
Taizhou 62
Zhengzhou 62
Kunming 60
Guangzhou 54
Hefei 47
Ningbo 44
Brussels 43
Boardman 40
Orange 38
Taiyuan 35
Haikou 34
Altamura 33
Washington 33
Milan 29
London 27
New York 26
Helsinki 24
San Paolo di Civitate 23
Delft 22
Centrale 21
Fuzhou 20
Norwalk 19
Nürnberg 19
Alameda 18
Lanzhou 18
Torino 18
Lawrence 15
Redmond 15
Bremen 14
Sevilla 13
Dallas 12
Vélizy-villacoublay 12
Los Angeles 11
Renton 11
Fort Worth 10
Mountain View 10
Stuttgart 10
Atlanta 9
Chengdu 9
Madrid 9
Stevenage 9
Sunnyvale 9
Auburn Hills 8
Cranfield 8
Flushing 8
Hong Kong 8
Vienna 8
Rotterdam 7
Saint Paul 7
Toronto 7
Wuhan 7
Athens 6
Centro 6
Chisinau 6
Chiswick 6
Florence 6
Kilburn 6
Luft 6
Ottawa 6
Tiel 6
Walnut 6
Baotou 5
Changchun 5
Falls Church 5
Genova 5
Lappeenranta 5
Orvieto 5
Torquay 5
Totale 15.057
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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 287
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft 239
Tiltrotor Cabin Noise Control Through Smart Actuators 238
Parallel Blade-Vortex Interaction Modelling for Helicopter Rotor Noise Control Synthesis 226
Analysis of Vibrations of an Innovative Civil Tiltrotor 217
Aeroelasticity of the PrandtlPlane: Body Freedom Flutter, Freeplay, and Limit Cycle Oscillation 201
Synthesis of Active Twist Controller for Rotor Blade–Vortex Interaction Noise Alleviation 193
A Boundary Element Method for the Aerodynamic Analysis of Aircraft in Arbitrary Motions 192
A Vorticity Formulation for Computational Fluid Dynamic and Aeroelastic Analyses of Viscous Flows 191
Synthesis of Rotor BVI Noise Active Controller Through Efficient Aerodynamics/Aeroacoustics Solver 191
Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors 189
A Comprehensive Approach for the Optimal Control of Tiltrotor Cabin Noise Through Actively-Driven Piezoelectric Actuators 188
A Spectral-BEM Formulation for Compact Sources Aeroacoustics 187
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 187
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Cylindrical Shells 187
Recent Developments on a Boundary Element Method in Aerodynamics 186
A Frequency Domain Approach for the Prediction of Tonal Noise Emitted by Rotors in Arbitrary Steady Motion 185
Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation 185
NERONE: An Open-Source Based Tool for Aerodynamic Transonic Optimization of Nonplanar Wings 185
Multidisciplinary Design Optimization for the Preliminary Design of Aeronautical Configurations 182
Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices 182
Aeroacoustic Analysis of Helicopter Rotors in Ground Effect 182
Innovative Helicopter In-Flight Noise Monitoring Systems Enabled by Rotor-State Measurements 181
Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors 177
Helicopter Noise Footprint Prediction in Unsteady Maneuvers 177
Assessment of Computational Models for the Effect of Aeroelasticity on BVI Noise Prediction 177
Integrated Aerodynamic/Aeroacoustic Analysis of a Tiltrotor During Conversion 176
A Velocity-Potential-Based Boundary-Element Method for the Aeroacoustic Analysis of Rotors and Propellers in Arbitrary Motion 176
Multidisciplinary Design and Optimization for Fluid-Structure Interactions 175
Cabin Noise Alleviation Through Fuselage Skin Embedded Smart Actuators 175
Simulation of Helicopter Noise in Maneuvering Flight 175
Active Twist Rotor Controller Identification for Blade-Vortex Interaction Noise Alleviation 175
Singularities in BIEs for the Laplace Equation; Joukowski Trailing–Edge Conjecture Revisited 174
Structural Characterization of Rotor Blades Through Photogrammetry 173
Aeroelastic Response of Helicopter Rotors Using a 3D Unsteady Aerodynamic Solver 172
Synthesis of a Rotor Noise Controller by Parallel Blade-Vortex Interaction Aeroelastic Modelling 172
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 172
Non-invasive dynamic measurement of helicopter blades 172
A novel finite-element family for interior acoustics 172
An Unsteady Aerodynamic Formulation for Efficient Rotor Tonal Noise Prediction 171
An Analytical-Numerical Aerodynamic Formulation for Efficient Aeroacoustics Analysis of Rotorcraft 170
Numerical characterization of helicopter noise hemispheres 170
A simple, but efficient aeroacoustic model of jets 169
Rotorcraft Comprehensive Code Assessment for Blade-Vortex Interaction Conditions 168
Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuation 168
Optimal Design and Acoustic Assessment of Low-Vibration Rotor Blades 168
Identification of rotor wake inflow finite-state models for flight dynamics simulations 166
A Novel Potential-Flow Boundary Integral Formulation for Helicopter Rotors in BVI Conditions 166
A Boundary Element Method for Aerodynamics and Aeroacoustics of Bodies in Arbitrary Motions 166
GARTEUR Activities on Acoustical Methods and Experiments for Studying on Acoustic Scattering 165
Structural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor Blades 163
Analysis of Helicopter Vibratory Hub Loads Alleviation by Cyclic Trailing–Edge Blade Flap Actuation 161
A Novel Highly Accurate Finite-Element Family 161
Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing–Proprotor Aerodynamic Interaction 159
Photogrammetric Detection Technique for Rotor Blades Structural Characterization 159
Investigation on a High-Frequency Controller for Rotor BVI Noise Alleviation 156
Multidisciplinary Design Optimization for Aircraft Configurations 155
Frequency-Domain Method for Discrete Frequency Noise Prediction of Rotors in Arbitrary Steady Motion 153
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Fuselages of Turboprop Aircraft 153
Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications 152
Aircraft Cabin Tonal Noise Alleviation Through Fuselage Skin Embedded Piezoelectric Actuators 150
Spectral-Boundary-Integral Compact-Source Formulation for Aero-Hydroacoustics of Rotors 150
A Boundary Element Method for the Aerodynamic Analysis of a Tiltrotor During Conversion 149
A Boundary Integral Formulation for the Study of Vorticity-Generated Sound 148
On the Vorticity Generated Sound for Moving Surfaces 147
Fully Coupled Structural-Unsteady Aerodynamics Modelling for Aeroelastic Response of Rotorcraft 146
Parallel Blade-Vortex Interaction Analyses and Rotor Noise Control Synthesis 146
Flapping Wing Aeroelasticity Using Corotational FEM and 3D Panel Method 145
A Boundary Integral Method in Rotor Aeroacoustics 144
Aerodynamics for MDO of an Innovative Configuration 144
A Hermite High-Order Finite Element for Structural Optimal Design 144
Acoustical Methods Towards Accurate Prediction of Rotorcraft Fuselage Scattering 144
Lighthill Equation-based Boundary Integral Formulations for Sound Scattering of Moving Bodies 144
A Viscous-Flow Decomposition with Aerodynamic and Aeroelastic Applications 142
Vibratory Analysis of an Innovative Civil Tiltrotor 142
A Space-Time Accurate Finite-State Inflow Model for Aeroelastic Applications 142
Pressure-Feedback Based Blade-Vortex Interaction Noise Controller for Helicopter Rotors 142
Analysis of Blade Deformation Effect on Rotor BVI Noise Prediction 142
A Hermite-Interpolation Finite Element for Structural Dynamics 141
Boundary Element Method for Aerodynamic Analysis of Bluff Bodies 140
Acoustic Prediction of Helicopter Unsteady Manoeuvres 138
Sound Synthesis Approach for Noise Annoyance Assessment of Rotorcraft Operations 138
Singularities in Discretized BIE’s for Laplace’s Equation; Trailing–Edge Conditions in Aerodynamics 137
Aerodynamic Issues in MDO for Preliminary Design 137
A Quasi Static Condensation and a Hermite Finite-Element for Structural Dynamics 137
Multi-Disciplinary Optimization for the Conceptual Design of Innovative Aircraft Configurations 136
Optimization of Rotorcraft Noise Abatement Trajectories 135
ROSAA: The European Solution to Connect Aeroelasticity, Aerodynamics and Acoustics Codes in a Unique User-Friendly Rotorcraft Simulation System 134
A Boundary Element Method for the Aerodynamic Analysis of Rotors in Arbitrary Motions 134
Acoustical Methods and Experiments for Studying Rotorcraft Fuselage Scattering 133
Combined Action of Variable-Stiffness Devices and Trailing-Edge Flap for Helicopter Hub Loads Reduction 132
Sound Scattered by a Helicopter Fuselage in Descent Flight Condition 132
MDO for Preliminary Design of a Highly Innovative Configuration 131
Blade Vortex Interaction 2D Modelling for Rotor Noise Control Synthesis 131
A Boundary-Field Integral Formulation for Sound Scattering of Moving Bodies 130
Genetic Algorithm with Surrogate Wake Inflow Models for Helicopter Rotor Optimal Design 130
A Comparison of Boundary Integral Formulations for Sound Scattered by Moving Bodies 129
MDO of an Innovative Configuration - Aerodynamic Issues 128
Rotor Dynamic Wake Inflow Finite-State Modeling 128
Totale 16.549
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Categoria #
all - tutte 56.772
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 56.772
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/20191.454 0 0 0 0 0 0 0 0 0 0 754 700
2019/20205.220 1.180 383 312 336 333 442 707 511 665 121 165 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
2023/20241.587 88 92 104 60 281 328 248 312 17 36 21 0
Totale 23.057