Benvenuti nell'Anagrafe della Ricerca d'Ateneo

BERNARDINI, Giovanni
 Distribuzione geografica
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Continente #
NA - Nord America 13.320
EU - Europa 11.772
AS - Asia 9.266
SA - Sud America 684
AF - Africa 287
OC - Oceania 31
Continente sconosciuto - Info sul continente non disponibili 17
Totale 35.377
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Nazione #
US - Stati Uniti d'America 13.132
CN - Cina 4.306
DK - Danimarca 2.853
SG - Singapore 2.507
GB - Regno Unito 2.461
RU - Federazione Russa 2.157
VN - Vietnam 1.366
IT - Italia 994
DE - Germania 978
SE - Svezia 501
BR - Brasile 458
UA - Ucraina 421
FR - Francia 359
FI - Finlandia 247
IN - India 238
IE - Irlanda 189
CI - Costa d'Avorio 151
AL - Albania 142
NL - Olanda 140
HK - Hong Kong 120
TR - Turchia 120
CA - Canada 100
JP - Giappone 87
BD - Bangladesh 85
KR - Corea 79
AR - Argentina 75
BE - Belgio 53
IQ - Iraq 52
ES - Italia 50
ID - Indonesia 45
PL - Polonia 44
ZA - Sudafrica 43
AT - Austria 40
PK - Pakistan 37
MX - Messico 36
CO - Colombia 35
EC - Ecuador 35
AU - Australia 29
PH - Filippine 27
VE - Venezuela 23
GR - Grecia 22
UZ - Uzbekistan 22
CL - Cile 21
MA - Marocco 21
CZ - Repubblica Ceca 20
CH - Svizzera 19
TH - Thailandia 17
MY - Malesia 15
EG - Egitto 14
AZ - Azerbaigian 13
RO - Romania 13
SA - Arabia Saudita 13
IR - Iran 12
TN - Tunisia 12
BO - Bolivia 11
IL - Israele 11
JM - Giamaica 11
JO - Giordania 11
PE - Perù 11
AE - Emirati Arabi Uniti 10
HU - Ungheria 10
PY - Paraguay 10
CR - Costa Rica 9
KE - Kenya 9
KZ - Kazakistan 9
LT - Lituania 9
TW - Taiwan 8
A2 - ???statistics.table.value.countryCode.A2??? 7
LB - Libano 7
LV - Lettonia 7
MD - Moldavia 7
NP - Nepal 7
DO - Repubblica Dominicana 6
ET - Etiopia 6
EU - Europa 6
PA - Panama 6
PS - Palestinian Territory 6
PT - Portogallo 6
SN - Senegal 6
KG - Kirghizistan 5
HR - Croazia 4
NG - Nigeria 4
NO - Norvegia 4
SY - Repubblica araba siriana 4
UY - Uruguay 4
AM - Armenia 3
BH - Bahrain 3
BS - Bahamas 3
BY - Bielorussia 3
DZ - Algeria 3
GE - Georgia 3
HN - Honduras 3
LK - Sri Lanka 3
LU - Lussemburgo 3
MN - Mongolia 3
RS - Serbia 3
SI - Slovenia 3
TT - Trinidad e Tobago 3
BG - Bulgaria 2
BN - Brunei Darussalam 2
Totale 35.323
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Città #
Southend 2.164
Woodbridge 1.537
Ashburn 1.171
Fairfield 1.163
San Jose 1.086
Singapore 1.040
Ann Arbor 819
Wilmington 748
Chandler 737
Beijing 621
Houston 589
Nanjing 577
Dong Ket 487
Seattle 430
Hefei 421
Dearborn 404
Boardman 396
Cambridge 364
Rome 338
Jacksonville 330
Dallas 328
Ho Chi Minh City 272
Princeton 260
Shenyang 226
Jinan 204
Hanoi 193
Dublin 188
Plano 180
Nanchang 166
Shanghai 152
Redwood City 144
Paris 143
Hebei 125
Changsha 121
Los Angeles 109
Pune 104
Hong Kong 102
Tianjin 94
Moscow 91
Helsinki 90
Jiaxing 88
New York 87
Izmir 80
Guangzhou 75
Frankfurt am Main 73
Zhengzhou 72
Hangzhou 71
Munich 70
San Diego 70
Milan 69
Tokyo 67
Seoul 65
Taizhou 62
Kunming 60
Orem 59
Santa Clara 58
São Paulo 56
The Dalles 53
London 52
Da Nang 51
Brussels 50
Ningbo 45
Orange 40
Taiyuan 37
Haikou 35
Altamura 34
Haiphong 34
Warsaw 34
Chennai 33
Washington 33
Chicago 29
Amsterdam 28
Johannesburg 27
Delft 26
Manchester 25
Yubileyny 25
Montreal 23
San Paolo di Civitate 23
Brooklyn 22
San Francisco 22
Toronto 22
Centrale 21
Turku 21
Vienna 21
Baghdad 20
Basingstoke 20
Fuzhou 20
Mumbai 20
Norwalk 19
Nürnberg 19
Stockholm 19
Tashkent 19
Alameda 18
Atlanta 18
Council Bluffs 18
Lanzhou 18
Torino 18
Buffalo 17
Lahore 17
Ottawa 17
Totale 21.059
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Nome #
Structural and Aeroelastic Modeling of Curved Rotor Blades Using a Galerkin Approach 425
A Spectral Formulation for Structural/Aeroelastic Modeling of Curved-Axis Rotor Blades 361
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft 337
Tiltrotor Cabin Noise Control Through Smart Actuators 323
Aeroacoustic Analysis of Helicopter Rotors in Ground Effect 298
Analysis of Vibrations of an Innovative Civil Tiltrotor 287
Parallel Blade-Vortex Interaction Modelling for Helicopter Rotor Noise Control Synthesis 284
Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation 283
A Boundary Element Method for the Aerodynamic Analysis of Aircraft in Arbitrary Motions 272
Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications 270
Synthesis of Active Twist Controller for Rotor Blade–Vortex Interaction Noise Alleviation 268
A Frequency Domain Approach for the Prediction of Tonal Noise Emitted by Rotors in Arbitrary Steady Motion 262
A Comprehensive Approach for the Optimal Control of Tiltrotor Cabin Noise Through Actively-Driven Piezoelectric Actuators 262
Rotorcraft Comprehensive Code Assessment for Blade-Vortex Interaction Conditions 252
Aeroelasticity of the PrandtlPlane: Body Freedom Flutter, Freeplay, and Limit Cycle Oscillation 251
NERONE: An Open-Source Based Tool for Aerodynamic Transonic Optimization of Nonplanar Wings 250
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Cylindrical Shells 249
A Boundary Integral Formulation for the Study of Vorticity-Generated Sound 242
Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices 242
A novel finite-element family for interior acoustics 242
A Novel Highly Accurate Finite-Element Family 241
Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuation 241
A Boundary Element Method for Aerodynamics and Aeroacoustics of Bodies in Arbitrary Motions 241
Recent Developments on a Boundary Element Method in Aerodynamics 240
A Spectral-BEM Formulation for Compact Sources Aeroacoustics 240
GARTEUR Activities on Acoustical Methods and Experiments for Studying on Acoustic Scattering 240
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 239
Active Twist Rotor Controller Identification for Blade-Vortex Interaction Noise Alleviation 239
Identification of rotor wake inflow finite-state models for flight dynamics simulations 238
A Boundary-Field Integral Formulation for Sound Scattering of Moving Bodies 237
Synthesis of Rotor BVI Noise Active Controller Through Efficient Aerodynamics/Aeroacoustics Solver 237
An Unsteady Aerodynamic Formulation for Efficient Rotor Tonal Noise Prediction 236
Assessment of Computational Models for the Effect of Aeroelasticity on BVI Noise Prediction 236
Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors 235
Structural Characterization of Rotor Blades Through Photogrammetry 235
A Boundary Integral Method in Rotor Aeroacoustics 234
Synthesis of a Rotor Noise Controller by Parallel Blade-Vortex Interaction Aeroelastic Modelling 233
Numerical characterization of helicopter noise hemispheres 233
A Boundary Element Method for the Aerodynamic Analysis of a Tiltrotor During Conversion 232
Simulation of Helicopter Noise in Maneuvering Flight 232
Optimal Design and Acoustic Assessment of Low-Vibration Rotor Blades 232
A Vorticity Formulation for Computational Fluid Dynamic and Aeroelastic Analyses of Viscous Flows 231
A Hermite High-Order Finite Element for Structural Optimal Design 229
Aeroelastic Modeling Effect in Rotor BVI Noise Prediction 228
Innovative Helicopter In-Flight Noise Monitoring Systems Enabled by Rotor-State Measurements 227
Acoustic Prediction of Helicopter Unsteady Manoeuvres 227
Helicopter Noise Footprint Prediction in Unsteady Maneuvers 227
Non-invasive dynamic measurement of helicopter blades 227
Cabin Noise Alleviation Through Fuselage Skin Embedded Smart Actuators 226
An Analytical-Numerical Aerodynamic Formulation for Efficient Aeroacoustics Analysis of Rotorcraft 226
Multidisciplinary Design Optimization for the Preliminary Design of Aeronautical Configurations 225
Aeroelastic Response of Helicopter Rotors Using a 3D Unsteady Aerodynamic Solver 224
Fully Coupled Structural-Unsteady Aerodynamics Modelling for Aeroelastic Response of Rotorcraft 224
Structural-Aeroelastic Finite Element Modeling for Advanced-Geometry Rotor Blades 223
A Space-Time Accurate Finite-State Inflow Model for Aeroelastic Applications 222
A Comparison of Boundary Integral Formulations for Sound Scattered by Moving Bodies 222
Spectral-Boundary-Integral Compact-Source Formulation for Aero-Hydroacoustics of Rotors 222
Acoustical Methods Towards Accurate Prediction of Rotorcraft Fuselage Scattering 221
Aeroacoustic Numerical Characterization of Propellers Interaction 220
A simple, but efficient aeroacoustic model of jets 219
Multidisciplinary Design and Optimization for Fluid-Structure Interactions 218
A Hermite-Interpolation Finite Element for Structural Dynamics 217
Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors 217
A Velocity-Potential-Based Boundary-Element Method for the Aeroacoustic Analysis of Rotors and Propellers in Arbitrary Motion 217
Acoustical Methods and Experiments for Studying Rotorcraft Fuselage Scattering 215
A Novel Potential-Flow Boundary Integral Formulation for Helicopter Rotors in BVI Conditions 213
Integrated Aerodynamic/Aeroacoustic Analysis of a Tiltrotor During Conversion 212
Lighthill Equation-based Boundary Integral Formulations for Sound Scattering of Moving Bodies 211
A Boundary Element Method for the Aerodynamic Analysis of Rotors in Arbitrary Motions 211
Multidisciplinary Design Optimization for Aircraft Configurations 208
Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing–Proprotor Aerodynamic Interaction 207
Singularities in BIEs for the Laplace Equation; Joukowski Trailing–Edge Conjecture Revisited 205
Photogrammetric Detection Technique for Rotor Blades Structural Characterization 202
Flapping Wing Aeroelasticity Using Corotational FEM and 3D Panel Method 200
Vibratory Analysis of an Innovative Civil Tiltrotor 199
Identification of Coaxial-Rotors Dynamic Wake Inflow for Flight Dynamics and Aeroelastic Applications 199
Investigation on a High-Frequency Controller for Rotor BVI Noise Alleviation 199
Boundary Element Method for Aerodynamic Analysis of Bluff Bodies 198
Analysis of Helicopter Vibratory Hub Loads Alleviation by Cyclic Trailing–Edge Blade Flap Actuation 197
Space-time accurate finite-state dynamic inflow modeling for aeromechanics of rotorcraft 197
Surrogate Models for Propeller Noise Emission and Aerodynamic Performance 197
State-Space Coaxial Rotors Inflow Modelling Derived from High-Fidelity Aerodynamic Simulations 195
Frequency-Domain Method for Discrete Frequency Noise Prediction of Rotors in Arbitrary Steady Motion 194
Parallel Blade-Vortex Interaction Analyses and Rotor Noise Control Synthesis 194
Genetic Algorithm with Surrogate Wake Inflow Models for Helicopter Rotor Optimal Design 194
Optimal Design of Tonal Noise Control Inside Smart-Stiffened Fuselages of Turboprop Aircraft 194
A Finite Element Model for Structural and Aeroelastic Analysis of Rotary Wings with Advanced Blade Geometry 193
ROSAA: The European Solution to Connect Aeroelasticity, Aerodynamics and Acoustics Codes in a Unique User-Friendly Rotorcraft Simulation System 192
Aircraft Cabin Tonal Noise Alleviation Through Fuselage Skin Embedded Piezoelectric Actuators 190
Aerodynamics for MDO of an Innovative Configuration 189
MANOEUVRES - An Effort Towards Quieter, Reliable Rotorcraft Terminal Procedures 189
Blade Vortex Interaction 2D Modelling for Rotor Noise Control Synthesis 189
Singularities in Discretized BIE’s for Laplace’s Equation; Trailing–Edge Conditions in Aerodynamics 188
Aerodynamic Issues in MDO for Preliminary Design 187
Multi-Disciplinary Optimization for the Conceptual Design of Innovative Aircraft Configurations 186
Sound Synthesis Approach for Noise Annoyance Assessment of Rotorcraft Operations 186
Conceptual all-electric retrofit of helicopters: review, technological outlook and a sample design 186
Analysis of Blade Deformation Effect on Rotor BVI Noise Prediction 183
Combined Action of Variable-Stiffness Devices and Trailing-Edge Flap for Helicopter Hub Loads Reduction 182
A Quasi Static Condensation and a Hermite Finite-Element for Structural Dynamics 182
Totale 22.833
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Categoria #
all - tutte 111.502
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 111.502
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
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
2024/20254.574 63 129 473 117 73 148 1.519 978 379 86 275 334
2025/20268.335 689 1.051 351 837 820 479 1.201 217 948 995 593 154
2026/202740 40 0 0 0 0 0 0 0 0 0 0 0
Totale 36.301