FERLAUTO, MICHELE
 Distribuzione geografica
Continente #
NA - Nord America 6.348
EU - Europa 5.964
AS - Asia 955
SA - Sud America 32
AF - Africa 23
OC - Oceania 17
Continente sconosciuto - Info sul continente non disponibili 7
Totale 13.346
Nazione #
US - Stati Uniti d'America 6.289
IT - Italia 2.204
GB - Regno Unito 1.057
DE - Germania 809
FR - Francia 613
UA - Ucraina 419
CN - Cina 402
IE - Irlanda 181
TR - Turchia 173
SE - Svezia 164
RU - Federazione Russa 117
KR - Corea 112
IN - India 99
CH - Svizzera 91
NL - Olanda 61
FI - Finlandia 54
AT - Austria 49
BE - Belgio 48
CA - Canada 47
HK - Hong Kong 36
JP - Giappone 33
MY - Malesia 27
BG - Bulgaria 22
VN - Vietnam 20
AU - Australia 15
CL - Cile 14
EU - Europa 12
IR - Iran 11
MX - Messico 11
SG - Singapore 11
BR - Brasile 10
AP - ???statistics.table.value.countryCode.AP??? 9
TW - Taiwan 9
ZA - Sudafrica 9
ES - Italia 7
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
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
CZ - Repubblica Ceca 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 13.346
Città #
Ashburn 1.373
Southend 883
Turin 547
Fairfield 508
Seattle 477
Chandler 398
Houston 298
Princeton 277
Woodbridge 244
Ann Arbor 240
Wilmington 223
Jacksonville 195
San Francisco 194
Torino 194
Cambridge 193
Dublin 173
Berlin 163
San Ramon 155
Izmir 148
Milan 136
Beijing 130
Rivoli 98
Asti 93
Des Moines 90
Bern 82
Chicago 78
Buffalo 75
San Donato Milanese 74
Zhengzhou 58
Council Bluffs 52
Boardman 51
Helsinki 51
Zaporozhye 47
Bologna 46
Vienna 46
Baltimore 45
Hyderabad 44
Brussels 41
Pennsylvania Furnace 39
Shanghai 39
Austin 37
Saint Petersburg 37
Overberg 34
Monopoli 31
Rome 31
Redwood City 29
Padua 28
Seoul 24
Fremont 23
Hangzhou 22
London 21
San Diego 21
San Jose 21
Las Vegas 20
Sofia 19
Norwalk 18
Montréal 17
Nanjing 17
Dalian 16
Falls Church 16
Washington 16
Toronto 15
Villanova 15
Dong Ket 14
Guangzhou 14
Genoa 13
Moncalieri 13
San Antonio 13
Dallas 12
Lake Forest 12
Malatya 12
Phoenix 12
Renton 12
Andover 11
Beinasco 11
Moscow 11
Mountain View 11
Frankfurt 10
Frankfurt Am Main 10
Melbourne 10
Novara 10
Seongnam 10
Guagnano 9
Indiana 9
Varese 9
Atlanta 8
Clearwater 8
Cranfield 8
Florence 8
Muizenberg 8
Ningbo 8
Osaka 8
Shenzhen 8
Bardolino 7
Changsha 7
Harbin 7
Henderson 7
Redmond 7
Southampton 7
Verona 7
Totale 9.187
Nome #
A Pseudo-Compressibility Method for Solving Inverse Problems based on the 3D Incompressible Euler Equations 441
Set of Boundary Conditions for Aerodynamic Design 428
An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations 427
An Inverse Method of Designing the Cooling Passages of Turbine Blades Based on the Heat Adjoint Equation 424
INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION 392
Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines 355
A viscous inverse method for aerodynamic design 329
Point vortex model for asymmetric inviscid wakes past bluff bodies 325
Numerical Simulation of Fluidic Thrust-Vectoring 323
Studio e Controllo di Strutture Vorticose di Parete 314
A computational approach to the simulation of controlled flows by synthetic jets actuators 257
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 235
A Numerical Method for the Study of Fluidic Thrust-Vectoring 233
A New Set of Boundary Conditions for Aerodynamic Design 230
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 223
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 221
Optimal Aerodynamic Design of Scramjet Facility Nozzles 221
Numerical Simulation of Fluidic Thrust-Vectoring 218
Numerical Simulation of Transient Operations in Aeroengines 205
Synthetic Jet Actuator Modeling for Flow Control Applications 205
Reduced order modelling of full-span rotating stall for the flow control simulation of axial compressors 202
Optimal Inverse Method for Turbomachinery Design 202
Coupling of optimization and inverse problem for aerodynamic shape design 200
Dynamics of Coherent Structures near a rotating Body 199
A CFD Method for Optimal Air-Intake Design 189
A Vortex-In-Cell Method for the Simulation of Viscous Flows 185
Synthetic jet modeling for flow control applications 183
Blade Camber Surface Optimization for Turbomachinery Design 183
Integrated Design and Analysys of Intakes and Nozzles in Air-Breathing Engines. 175
Nozzles and Intakes Interacting with the External Flow: Design and Analysis 175
A New Steklov-Poincaré Numerical Technique for Solving Prandtl-Batchelor Flows 166
Fan and propeller design via inverse problem adjoint equations 164
Design and Testing of a Low-Cost Extended-Range Pressure Measurement System for Aerospace Applications 162
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 161
Inverse Problems for Advanced Nozzle Design. 159
A class of non-reflecting boundary conditions for turbomachinery design. 157
Propfan Optimization Based on Inverse Problem Adjoint Equations 156
An Eulerian-Lagrangian Method for Vortical Flow Simulations 153
Active Flow Control in Supersonic Nozzles 152
Aeroelastic Analysis and Optimal Design of Axial Multistage Fans and Compressors 151
Dinamica di strutture vorticose nel campo di moto di un rotore cuspidato 149
Numerical Design of Dual-Bell Nozzles 148
The Clean Sky 2 MIDAS Project - an Innovative Modular, Digital and Integrated Air Data System for Fly-by-Wire Applications 148
Computation of plug nozzle turbulent flowfields 146
Numerical Design of Dual-Bell Nozzle 146
Aerodynamic Design by Inverse Method 145
Simulation of Jet Engine Transient by a CFD Method 143
Simulazione numerica di Strutture vorticose di parete 141
Influence of the Facility Nozzle Design in the Unsteady Response of Direct-Connect Scramjet Combustors 139
Aerodynamic Design via Inverse Problem Solution in Three-Dimensional Incompressible Flows 135
Optimization based on Inverse Problem for Aerodynamic Shape Design: Preliminary Results 134
Investigation of the Snow Cornice Effect 128
Hollow Vortices in Shear 127
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 124
Design of Inlet Distortion Generators for Direct-Connect Scramjet Combustors 104
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 100
AI Assisted Detection of Shock Motions Inside a Transonic Duct 99
Experimental Characterization of a Linear Aerospike Nozzle Flow 95
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 91
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 91
Shock Vector Control Technique for Aerospike Nozzles 89
Reduced order modeling of thermal transients in high-performance engineering systems 86
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 82
Numerical simulation of the unsteady flowfield in complete propulsion systems 80
Optimal aerodynamic design of hypersonic inlets by using streamline-tracing techniques 79
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 77
Characteristic-based formulation of boundary conditions for preconditioned or non-preconditioned flow equations 73
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 72
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 68
Cold Gas Measurement System for Linear Aerospike Nozzles 64
Aerodynamic Design of Inward-Turning Inlets with Shape Transition 63
A fault/failure detection algorithm based on a grid of virtual sensors for engine health monitoring 60
An improved stall prediction model for axial compressor stage based on diffuser analogy 60
Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle 59
Numerical Simulation of a Vectored Axisymmetric Nozzle 58
Design and Optimization of an Inward-Turning Inlet with Rectangular-To-Ellipse Shape Transition 57
Parametric Generation and Computational Analysis of a REST Inlet 56
Multi-fidelity sparse polynomial chaos expansion based on Gaussian process regression and least angle regression 52
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model 50
Sensitivity Analysis for Model with Dependent Inputs Using Sparse Polynomial Chaos Expansions 47
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 47
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 45
Computational Investigation of Injection Effects on Shock Vector Control Performance 43
Influence of Hot Flow Conditions on Nozzle Performances 42
Stator re-stagger optimization in multistage axial compressor 40
Numerical and Experimental Assessment of a Linear Aerospike 36
Impeller Design and Performance Analysis of Aviation Fuel Pump Based on the Inverse Method 17
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 14
Totale 13.629
Categoria #
all - tutte 34.099
article - articoli 11.423
book - libri 0
conference - conferenze 20.446
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.649
Totale 67.617


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019776 0 0 0 0 0 0 0 0 0 179 341 256
2019/20201.717 212 112 104 175 204 164 125 214 194 126 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
2023/2024590 49 60 42 67 54 82 57 67 57 55 0 0
Totale 13.629