FERLAUTO, MICHELE
 Distribuzione geografica
Continente #
NA - Nord America 6.573
EU - Europa 6.160
AS - Asia 1.233
SA - Sud America 32
AF - Africa 23
OC - Oceania 18
Continente sconosciuto - Info sul continente non disponibili 7
Totale 14.046
Nazione #
US - Stati Uniti d'America 6.514
IT - Italia 2.342
GB - Regno Unito 1.062
DE - Germania 818
FR - Francia 615
CN - Cina 445
UA - Ucraina 422
SG - Singapore 191
IE - Irlanda 181
TR - Turchia 173
SE - Svezia 164
KR - Corea 139
RU - Federazione Russa 119
IN - India 105
CH - Svizzera 91
NL - Olanda 67
BE - Belgio 64
FI - Finlandia 59
HK - Hong Kong 57
AT - Austria 50
CA - Canada 47
JP - Giappone 33
BG - Bulgaria 27
MY - Malesia 27
VN - Vietnam 20
AU - Australia 16
CL - Cile 14
EU - Europa 12
IR - Iran 12
MX - Messico 11
BR - Brasile 10
AP - ???statistics.table.value.countryCode.AP??? 9
ES - Italia 9
TW - Taiwan 9
ZA - Sudafrica 9
GR - Grecia 7
RO - Romania 7
CO - Colombia 6
PL - Polonia 6
DK - Danimarca 5
HR - Croazia 5
PH - Filippine 5
AE - Emirati Arabi Uniti 4
BY - Bielorussia 4
DZ - Algeria 4
BD - Bangladesh 3
CZ - Repubblica Ceca 3
EG - Egitto 3
IL - Israele 3
KZ - Kazakistan 3
PT - Portogallo 3
SN - Senegal 3
AR - Argentina 2
HU - Ungheria 2
ID - Indonesia 2
JO - Giordania 2
LT - Lituania 2
LU - Lussemburgo 2
LV - Lettonia 2
MU - Mauritius 2
NZ - Nuova Zelanda 2
UZ - Uzbekistan 2
CR - Costa Rica 1
ET - Etiopia 1
GI - Gibilterra 1
IQ - Iraq 1
NG - Nigeria 1
NO - Norvegia 1
PK - Pakistan 1
RS - Serbia 1
SA - Arabia Saudita 1
Totale 14.046
Città #
Ashburn 1.385
Southend 883
Turin 612
Fairfield 508
Seattle 477
Chandler 398
Houston 298
Princeton 277
Woodbridge 244
Ann Arbor 240
Wilmington 223
Jacksonville 195
San Francisco 195
Torino 194
Cambridge 193
Dublin 173
Berlin 163
Milan 157
San Ramon 155
Izmir 148
Boardman 144
Singapore 142
Beijing 130
Rivoli 98
Asti 93
Des Moines 90
Bern 82
Chicago 78
Buffalo 75
San Donato Milanese 74
Zhengzhou 58
Helsinki 54
Shanghai 54
Brussels 53
Council Bluffs 52
Bologna 49
Zaporozhye 47
Vienna 46
Baltimore 45
Hyderabad 44
Pennsylvania Furnace 39
Austin 37
Saint Petersburg 37
Overberg 34
Seoul 33
Rome 32
Monopoli 31
Redwood City 29
Padua 28
Santa Clara 27
Gilroy 24
Fremont 23
Hangzhou 22
London 21
San Diego 21
San Jose 21
Washington 21
Hong Kong 20
Las Vegas 20
Sofia 19
Norwalk 18
Montréal 17
Nanjing 17
Dalian 16
Falls Church 16
Guangzhou 15
Toronto 15
Villanova 15
Dong Ket 14
Genoa 13
Moncalieri 13
San Antonio 13
Dallas 12
Lake Forest 12
Malatya 12
Phoenix 12
Renton 12
Andover 11
Beinasco 11
Borgosesia 11
Moscow 11
Mountain View 11
Frankfurt 10
Frankfurt Am Main 10
Melbourne 10
Novara 10
Seongnam 10
Guagnano 9
Indiana 9
New York 9
Shenzhen 9
Varese 9
Atlanta 8
Clearwater 8
Cranfield 8
Florence 8
Muizenberg 8
Ningbo 8
Osaka 8
Piscataway 8
Totale 9.621
Nome #
A Pseudo-Compressibility Method for Solving Inverse Problems based on the 3D Incompressible Euler Equations 464
Set of Boundary Conditions for Aerodynamic Design 444
An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations 442
An Inverse Method of Designing the Cooling Passages of Turbine Blades Based on the Heat Adjoint Equation 441
INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION 401
Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines 371
Point vortex model for asymmetric inviscid wakes past bluff bodies 339
A viscous inverse method for aerodynamic design 339
Studio e Controllo di Strutture Vorticose di Parete 325
Numerical Simulation of Fluidic Thrust-Vectoring 324
A computational approach to the simulation of controlled flows by synthetic jets actuators 271
A Numerical Method for the Study of Fluidic Thrust-Vectoring 243
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 242
A New Set of Boundary Conditions for Aerodynamic Design 239
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 228
Optimal Aerodynamic Design of Scramjet Facility Nozzles 225
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 224
Numerical Simulation of Fluidic Thrust-Vectoring 224
Optimal Inverse Method for Turbomachinery Design 211
Synthetic Jet Actuator Modeling for Flow Control Applications 210
Numerical Simulation of Transient Operations in Aeroengines 208
Reduced order modelling of full-span rotating stall for the flow control simulation of axial compressors 206
Coupling of optimization and inverse problem for aerodynamic shape design 204
Dynamics of Coherent Structures near a rotating Body 202
A CFD Method for Optimal Air-Intake Design 192
Blade Camber Surface Optimization for Turbomachinery Design 191
A Vortex-In-Cell Method for the Simulation of Viscous Flows 190
Nozzles and Intakes Interacting with the External Flow: Design and Analysis 184
Synthetic jet modeling for flow control applications 184
Integrated Design and Analysys of Intakes and Nozzles in Air-Breathing Engines. 177
Fan and propeller design via inverse problem adjoint equations 170
Design and Testing of a Low-Cost Extended-Range Pressure Measurement System for Aerospace Applications 170
A New Steklov-Poincaré Numerical Technique for Solving Prandtl-Batchelor Flows 168
A class of non-reflecting boundary conditions for turbomachinery design. 164
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 162
Inverse Problems for Advanced Nozzle Design. 161
Propfan Optimization Based on Inverse Problem Adjoint Equations 160
The Clean Sky 2 MIDAS Project - an Innovative Modular, Digital and Integrated Air Data System for Fly-by-Wire Applications 160
An Eulerian-Lagrangian Method for Vortical Flow Simulations 157
Active Flow Control in Supersonic Nozzles 156
Aeroelastic Analysis and Optimal Design of Axial Multistage Fans and Compressors 153
Dinamica di strutture vorticose nel campo di moto di un rotore cuspidato 153
Numerical Design of Dual-Bell Nozzles 151
Aerodynamic Design by Inverse Method 151
Computation of plug nozzle turbulent flowfields 149
Numerical Design of Dual-Bell Nozzle 149
Simulazione numerica di Strutture vorticose di parete 147
Simulation of Jet Engine Transient by a CFD Method 146
Influence of the Facility Nozzle Design in the Unsteady Response of Direct-Connect Scramjet Combustors 144
Optimization based on Inverse Problem for Aerodynamic Shape Design: Preliminary Results 141
Aerodynamic Design via Inverse Problem Solution in Three-Dimensional Incompressible Flows 137
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 135
Hollow Vortices in Shear 132
Investigation of the Snow Cornice Effect 131
Experimental Characterization of a Linear Aerospike Nozzle Flow 117
Design of Inlet Distortion Generators for Direct-Connect Scramjet Combustors 110
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 108
AI Assisted Detection of Shock Motions Inside a Transonic Duct 107
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 99
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 98
Shock Vector Control Technique for Aerospike Nozzles 96
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 90
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 89
Reduced order modeling of thermal transients in high-performance engineering systems 88
Numerical simulation of the unsteady flowfield in complete propulsion systems 86
Optimal aerodynamic design of hypersonic inlets by using streamline-tracing techniques 85
Characteristic-based formulation of boundary conditions for preconditioned or non-preconditioned flow equations 77
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 76
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 75
Aerodynamic Design of Inward-Turning Inlets with Shape Transition 74
Cold Gas Measurement System for Linear Aerospike Nozzles 71
A fault/failure detection algorithm based on a grid of virtual sensors for engine health monitoring 70
Numerical Simulation of a Vectored Axisymmetric Nozzle 65
Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle 64
An improved stall prediction model for axial compressor stage based on diffuser analogy 63
Parametric Generation and Computational Analysis of a REST Inlet 61
Design and Optimization of an Inward-Turning Inlet with Rectangular-To-Ellipse Shape Transition 61
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model 58
null 58
Sensitivity Analysis for Model with Dependent Inputs Using Sparse Polynomial Chaos Expansions 56
Multi-fidelity sparse polynomial chaos expansion based on Gaussian process regression and least angle regression 55
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 52
Influence of Hot Flow Conditions on Nozzle Performances 50
Numerical and Experimental Assessment of a Linear Aerospike 49
Computational Investigation of Injection Effects on Shock Vector Control Performance 47
Stator re-stagger optimization in multistage axial compressor 44
Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike 32
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 30
Impeller Design and Performance Analysis of Aviation Fuel Pump Based on the Inverse Method 23
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 22
Passive Control of Vortices in the Wake of a Bluff Body 20
A Framework for Testing Differential Throttling in Linear Aerospike Nozzle 15
AI-Based Detection of Surge and Rotating Stall in Axial Compressors via Dynamic Model Parameter Estimation 7
Totale 14.340
Categoria #
all - tutte 38.730
article - articoli 13.050
book - libri 0
conference - conferenze 23.256
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.781
Totale 76.817


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.289 0 0 0 175 204 164 125 214 194 126 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
2023/2024796 49 60 42 67 54 82 57 67 57 60 101 100
2024/2025505 54 309 109 33 0 0 0 0 0 0 0 0
Totale 14.340