FERLAUTO, MICHELE
 Distribuzione geografica
Continente #
NA - Nord America 6.821
EU - Europa 6.596
AS - Asia 1.799
SA - Sud America 208
AF - Africa 27
OC - Oceania 18
Continente sconosciuto - Info sul continente non disponibili 7
Totale 15.476
Nazione #
US - Stati Uniti d'America 6.750
IT - Italia 2.584
GB - Regno Unito 1.064
DE - Germania 832
FR - Francia 657
SG - Singapore 553
CN - Cina 503
UA - Ucraina 424
TR - Turchia 203
RU - Federazione Russa 202
IE - Irlanda 181
BR - Brasile 171
KR - Corea 170
SE - Svezia 164
IN - India 109
CH - Svizzera 91
AT - Austria 80
HK - Hong Kong 76
NL - Olanda 74
BE - Belgio 70
FI - Finlandia 66
CA - Canada 49
ID - Indonesia 42
JP - Giappone 33
MY - Malesia 27
BG - Bulgaria 26
VN - Vietnam 21
MX - Messico 18
AU - Australia 16
CL - Cile 15
EU - Europa 12
IR - Iran 12
TW - Taiwan 10
AP - ???statistics.table.value.countryCode.AP??? 9
RO - Romania 9
ZA - Sudafrica 9
CO - Colombia 8
ES - Italia 7
GR - Grecia 7
IL - Israele 7
AR - Argentina 6
PL - Polonia 6
VE - Venezuela 6
BD - Bangladesh 5
DK - Danimarca 5
DZ - Algeria 5
HR - Croazia 5
IQ - Iraq 5
PH - Filippine 5
UZ - Uzbekistan 5
AE - Emirati Arabi Uniti 4
BY - Bielorussia 4
KZ - Kazakistan 4
CZ - Repubblica Ceca 3
EG - Egitto 3
NP - Nepal 3
PT - Portogallo 3
SN - Senegal 3
HU - Ungheria 2
JO - Giordania 2
LT - Lituania 2
LU - Lussemburgo 2
LV - Lettonia 2
MU - Mauritius 2
NZ - Nuova Zelanda 2
PE - Perù 2
PK - Pakistan 2
BA - Bosnia-Erzegovina 1
CR - Costa Rica 1
ET - Etiopia 1
GI - Gibilterra 1
HN - Honduras 1
JM - Giamaica 1
KE - Kenya 1
KW - Kuwait 1
MA - Marocco 1
NG - Nigeria 1
NO - Norvegia 1
PA - Panama 1
QA - Qatar 1
RS - Serbia 1
SA - Arabia Saudita 1
SK - Slovacchia (Repubblica Slovacca) 1
TN - Tunisia 1
Totale 15.476
Città #
Ashburn 1.396
Southend 883
Turin 693
Fairfield 508
Seattle 478
Chandler 398
Houston 298
Princeton 277
Woodbridge 244
Ann Arbor 240
Wilmington 223
Singapore 214
Jacksonville 195
San Francisco 195
Torino 194
Cambridge 193
Milan 175
Dublin 173
Santa Clara 166
Berlin 163
San Ramon 155
Izmir 148
Boardman 144
Beijing 130
Rivoli 98
Asti 93
Des Moines 90
Bern 82
Chicago 78
Buffalo 75
San Donato Milanese 74
Council Bluffs 66
Brussels 59
Helsinki 58
Zhengzhou 58
Bologna 55
Shanghai 55
Vienna 50
Zaporozhye 47
Baltimore 45
Hyderabad 44
Jakarta 41
Hong Kong 39
Pennsylvania Furnace 39
Rome 39
Austin 37
Saint Petersburg 37
Overberg 34
Seoul 33
Istanbul 31
Monopoli 31
Redwood City 29
Padua 28
Gilroy 24
Fremont 23
Hangzhou 23
Borgosesia 21
London 21
San Diego 21
San Jose 21
Las Vegas 20
Washington 20
Sofia 19
Norwalk 18
Dalian 17
Montréal 17
Nanjing 17
Falls Church 16
Guangzhou 15
Toronto 15
Villanova 15
Dong Ket 14
Genoa 13
Moncalieri 13
Moscow 13
San Antonio 13
Dallas 12
Lake Forest 12
Malatya 12
Phoenix 12
Renton 12
Andover 11
Beinasco 11
Frankfurt am Main 11
Mountain View 11
Frankfurt 10
Frankfurt Am Main 10
Melbourne 10
Novara 10
Seongnam 10
Shenzhen 10
Yubileyny 10
Guagnano 9
Indiana 9
Varese 9
Atlanta 8
Clearwater 8
Cranfield 8
Florence 8
Muizenberg 8
Totale 10.078
Nome #
Set of Boundary Conditions for Aerodynamic Design 476
A Pseudo-Compressibility Method for Solving Inverse Problems based on the 3D Incompressible Euler Equations 474
An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations 467
An Inverse Method of Designing the Cooling Passages of Turbine Blades Based on the Heat Adjoint Equation 457
INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION 416
Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines 385
A viscous inverse method for aerodynamic design 355
Point vortex model for asymmetric inviscid wakes past bluff bodies 350
Studio e Controllo di Strutture Vorticose di Parete 336
Numerical Simulation of Fluidic Thrust-Vectoring 333
A computational approach to the simulation of controlled flows by synthetic jets actuators 281
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 267
A Numerical Method for the Study of Fluidic Thrust-Vectoring 258
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 244
A New Set of Boundary Conditions for Aerodynamic Design 243
Optimal Aerodynamic Design of Scramjet Facility Nozzles 236
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 231
Numerical Simulation of Fluidic Thrust-Vectoring 230
Optimal Inverse Method for Turbomachinery Design 221
Numerical Simulation of Transient Operations in Aeroengines 219
Synthetic Jet Actuator Modeling for Flow Control Applications 217
Reduced order modelling of full-span rotating stall for the flow control simulation of axial compressors 215
Coupling of optimization and inverse problem for aerodynamic shape design 211
Dynamics of Coherent Structures near a rotating Body 208
Synthetic jet modeling for flow control applications 200
Blade Camber Surface Optimization for Turbomachinery Design 200
A CFD Method for Optimal Air-Intake Design 200
Nozzles and Intakes Interacting with the External Flow: Design and Analysis 196
A Vortex-In-Cell Method for the Simulation of Viscous Flows 196
Design and Testing of a Low-Cost Extended-Range Pressure Measurement System for Aerospace Applications 183
Integrated Design and Analysys of Intakes and Nozzles in Air-Breathing Engines. 182
Fan and propeller design via inverse problem adjoint equations 179
A New Steklov-Poincaré Numerical Technique for Solving Prandtl-Batchelor Flows 178
The Clean Sky 2 MIDAS Project - an Innovative Modular, Digital and Integrated Air Data System for Fly-by-Wire Applications 178
A class of non-reflecting boundary conditions for turbomachinery design. 171
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 169
Inverse Problems for Advanced Nozzle Design. 168
An Eulerian-Lagrangian Method for Vortical Flow Simulations 165
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 165
Propfan Optimization Based on Inverse Problem Adjoint Equations 164
Numerical Design of Dual-Bell Nozzles 162
Active Flow Control in Supersonic Nozzles 162
Simulazione numerica di Strutture vorticose di parete 158
Computation of plug nozzle turbulent flowfields 158
Aeroelastic Analysis and Optimal Design of Axial Multistage Fans and Compressors 158
Dinamica di strutture vorticose nel campo di moto di un rotore cuspidato 158
Aerodynamic Design by Inverse Method 156
Simulation of Jet Engine Transient by a CFD Method 155
Numerical Design of Dual-Bell Nozzle 153
Experimental Characterization of a Linear Aerospike Nozzle Flow 151
Influence of the Facility Nozzle Design in the Unsteady Response of Direct-Connect Scramjet Combustors 150
Optimization based on Inverse Problem for Aerodynamic Shape Design: Preliminary Results 145
Investigation of the Snow Cornice Effect 142
Aerodynamic Design via Inverse Problem Solution in Three-Dimensional Incompressible Flows 141
Hollow Vortices in Shear 141
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 133
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 129
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 126
AI Assisted Detection of Shock Motions Inside a Transonic Duct 121
Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike 118
Design of Inlet Distortion Generators for Direct-Connect Scramjet Combustors 117
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 113
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 111
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 109
Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle 108
Shock Vector Control Technique for Aerospike Nozzles 101
Optimal aerodynamic design of hypersonic inlets by using streamline-tracing techniques 99
Reduced order modeling of thermal transients in high-performance engineering systems 96
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 96
Numerical simulation of the unsteady flowfield in complete propulsion systems 95
An improved stall prediction model for axial compressor stage based on diffuser analogy 94
Cold Gas Measurement System for Linear Aerospike Nozzles 88
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 87
Characteristic-based formulation of boundary conditions for preconditioned or non-preconditioned flow equations 86
Numerical and Experimental Assessment of a Linear Aerospike 80
Aerodynamic Design of Inward-Turning Inlets with Shape Transition 80
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 80
A fault/failure detection algorithm based on a grid of virtual sensors for engine health monitoring 77
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model 76
Influence of Hot Flow Conditions on Nozzle Performances 75
Numerical Simulation of a Vectored Axisymmetric Nozzle 70
Design and Optimization of an Inward-Turning Inlet with Rectangular-To-Ellipse Shape Transition 68
Parametric Generation and Computational Analysis of a REST Inlet 67
Multi-fidelity sparse polynomial chaos expansion based on Gaussian process regression and least angle regression 65
Sensitivity Analysis for Model with Dependent Inputs Using Sparse Polynomial Chaos Expansions 65
A Framework for Testing Differential Throttling in Linear Aerospike Nozzle 59
Stator re-stagger optimization in multistage axial compressor 58
Computational Investigation of Injection Effects on Shock Vector Control Performance 54
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 53
Numerical Study of the Flowfield in a Differentially-Throttled Linear Aerospike 47
AI-Based Detection of Surge and Rotating Stall in Axial Compressors via Dynamic Model Parameter Estimation 43
Passive Control of Vortices in the Wake of a Bluff Body 40
Impeller Design and Performance Analysis of Aviation Fuel Pump Based on the Inverse Method 39
A Non-Contact PCB Multi-Fault Diagnosis Algorithm Based on Scalar Magnetic Field Fusion Feature and Transformer Architecture 27
A Non-Contact AI-Based Approach to Multi-Failure Detection in Avionic Systems 26
A Two-Dimensional Analysis of the Flowfield and Performances of Linear Aerospikes During Differential Throttling 14
Totale 15.804
Categoria #
all - tutte 44.592
article - articoli 15.319
book - libri 0
conference - conferenze 26.653
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.920
Totale 88.484


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020213 0 0 0 0 0 0 0 0 0 126 49 38
2020/20211.384 211 162 72 147 88 194 48 99 76 136 98 53
2021/20221.225 106 62 51 101 24 138 57 48 82 98 177 281
2022/20231.558 138 254 47 123 165 209 182 79 127 21 97 116
2023/2024793 49 60 42 67 54 82 57 67 57 60 101 97
2024/20251.972 48 304 102 332 233 104 212 136 369 132 0 0
Totale 15.804