FERLAUTO, MICHELE
 Distribuzione geografica
Continente #
NA - Nord America 8.688
EU - Europa 7.701
AS - Asia 5.580
SA - Sud America 545
Continente sconosciuto - Info sul continente non disponibili 362
AF - Africa 71
OC - Oceania 25
Totale 22.972
Nazione #
US - Stati Uniti d'America 8.540
IT - Italia 2.950
SG - Singapore 1.660
VN - Vietnam 1.249
GB - Regno Unito 1.106
CN - Cina 1.058
DE - Germania 917
FR - Francia 805
RU - Federazione Russa 497
UA - Ucraina 434
BR - Brasile 417
KR - Corea 381
HK - Hong Kong 283
IN - India 260
TR - Turchia 219
IE - Irlanda 186
SE - Svezia 170
AT - Austria 106
FI - Finlandia 98
NL - Olanda 97
CH - Svizzera 95
BD - Bangladesh 80
CA - Canada 78
BE - Belgio 74
JP - Giappone 72
ID - Indonesia 57
MX - Messico 36
IQ - Iraq 34
PH - Filippine 34
MY - Malesia 33
AR - Argentina 32
ES - Italia 30
TH - Thailandia 30
TW - Taiwan 29
BG - Bulgaria 27
CO - Colombia 27
ZA - Sudafrica 22
AU - Australia 21
CL - Cile 20
PL - Polonia 20
EC - Ecuador 17
VE - Venezuela 17
IR - Iran 13
PK - Pakistan 13
RO - Romania 13
EU - Europa 12
UZ - Uzbekistan 12
AP - ???statistics.table.value.countryCode.AP??? 9
CR - Costa Rica 9
KZ - Kazakistan 9
SA - Arabia Saudita 9
DZ - Algeria 8
GR - Grecia 8
IL - Israele 8
MA - Marocco 8
EG - Egitto 7
HR - Croazia 7
NP - Nepal 7
SN - Senegal 7
AE - Emirati Arabi Uniti 6
CZ - Repubblica Ceca 6
JM - Giamaica 6
JO - Giordania 6
PY - Paraguay 6
DK - Danimarca 5
OM - Oman 5
PE - Perù 5
PT - Portogallo 5
BY - Bielorussia 4
ET - Etiopia 4
LV - Lettonia 4
TN - Tunisia 4
BO - Bolivia 3
HN - Honduras 3
HU - Ungheria 3
LT - Lituania 3
NG - Nigeria 3
NZ - Nuova Zelanda 3
AL - Albania 2
AZ - Azerbaigian 2
BA - Bosnia-Erzegovina 2
BB - Barbados 2
DO - Repubblica Dominicana 2
GP - Guadalupe 2
GT - Guatemala 2
KE - Kenya 2
KG - Kirghizistan 2
KW - Kuwait 2
LU - Lussemburgo 2
MU - Mauritius 2
NI - Nicaragua 2
QA - Qatar 2
RS - Serbia 2
SK - Slovacchia (Repubblica Slovacca) 2
SV - El Salvador 2
TT - Trinidad e Tobago 2
AM - Armenia 1
BH - Bahrain 1
CG - Congo 1
CI - Costa d'Avorio 1
Totale 22.601
Città #
Ashburn 1.690
Southend 883
Singapore 860
Turin 794
San Jose 595
Fairfield 508
Seattle 483
Chandler 398
Ho Chi Minh City 329
Houston 301
Hanoi 285
Princeton 277
Beijing 248
Woodbridge 244
Milan 243
Ann Arbor 240
Santa Clara 232
Wilmington 223
Hong Kong 207
San Francisco 205
Jacksonville 197
Torino 194
Cambridge 193
Seoul 185
Dublin 178
Berlin 166
San Ramon 155
Boardman 151
Izmir 148
Council Bluffs 129
Buffalo 115
Los Angeles 107
Lauterbourg 98
Rivoli 98
Asti 93
Des Moines 91
Chicago 83
Bern 82
Dallas 77
San Donato Milanese 74
Helsinki 69
Shanghai 67
Zhengzhou 66
Da Nang 63
Brussels 61
Bologna 56
Vienna 56
North Bergen 54
Rome 54
Haiphong 53
Baltimore 49
Hyderabad 49
Zaporozhye 47
Hefei 44
New York 44
Jakarta 42
Pennsylvania Furnace 39
Austin 37
Istanbul 37
Saint Petersburg 37
Overberg 34
Frankfurt am Main 31
Monopoli 31
Moscow 30
Guangzhou 29
Redwood City 29
Padua 28
Hangzhou 25
London 25
Gilroy 24
Washington 24
Fremont 23
Las Vegas 23
San Diego 22
Tokyo 22
Borgosesia 21
Lappeenranta 21
Nanjing 21
Phoenix 21
Toronto 21
Munich 20
São Paulo 20
Sofia 19
Norwalk 18
Nuremberg 18
Orem 18
Columbus 17
Dalian 17
Hải Dương 17
Montréal 17
Falls Church 16
Martina Franca 16
Atlanta 15
Springfield 15
Villanova 15
Dong Ket 14
Genoa 14
San Antonio 14
Suzhou 14
Thái Nguyên 14
Totale 13.716
Nome #
An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations 593
An Inverse Method of Designing the Cooling Passages of Turbine Blades Based on the Heat Adjoint Equation 588
A Pseudo-Compressibility Method for Solving Inverse Problems based on the 3D Incompressible Euler Equations 581
Set of Boundary Conditions for Aerodynamic Design 578
INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION 476
Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines 472
Point vortex model for asymmetric inviscid wakes past bluff bodies 450
Studio e Controllo di Strutture Vorticose di Parete 444
A viscous inverse method for aerodynamic design 418
Numerical Simulation of Fluidic Thrust-Vectoring 378
Optimal Inverse Method for Turbomachinery Design 330
A Numerical Method for the Study of Fluidic Thrust-Vectoring 326
A computational approach to the simulation of controlled flows by synthetic jets actuators 325
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 312
A New Set of Boundary Conditions for Aerodynamic Design 296
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 289
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 287
Optimal Aerodynamic Design of Scramjet Facility Nozzles 287
Numerical Simulation of Fluidic Thrust-Vectoring 284
Synthetic jet modeling for flow control applications 282
Nozzles and Intakes Interacting with the External Flow: Design and Analysis 274
Experimental Characterization of a Linear Aerospike Nozzle Flow 273
Dynamics of Coherent Structures near a rotating Body 273
Reduced order modelling of full-span rotating stall for the flow control simulation of axial compressors 266
Synthetic Jet Actuator Modeling for Flow Control Applications 265
Blade Camber Surface Optimization for Turbomachinery Design 264
The Clean Sky 2 MIDAS Project - an Innovative Modular, Digital and Integrated Air Data System for Fly-by-Wire Applications 264
A CFD Method for Optimal Air-Intake Design 258
Numerical Simulation of Transient Operations in Aeroengines 256
Coupling of optimization and inverse problem for aerodynamic shape design 251
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 250
A Vortex-In-Cell Method for the Simulation of Viscous Flows 246
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 243
Design and Testing of a Low-Cost Extended-Range Pressure Measurement System for Aerospace Applications 242
Fan and propeller design via inverse problem adjoint equations 240
Integrated Design and Analysys of Intakes and Nozzles in Air-Breathing Engines. 236
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 235
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 232
A class of non-reflecting boundary conditions for turbomachinery design. 227
Numerical and Experimental Assessment of a Linear Aerospike 224
Hollow Vortices in Shear 224
Propfan Optimization Based on Inverse Problem Adjoint Equations 220
An Eulerian-Lagrangian Method for Vortical Flow Simulations 216
A New Steklov-Poincaré Numerical Technique for Solving Prandtl-Batchelor Flows 212
Numerical Design of Dual-Bell Nozzles 211
Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike 210
Computation of plug nozzle turbulent flowfields 209
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 206
AI Assisted Detection of Shock Motions Inside a Transonic Duct 205
Simulazione numerica di Strutture vorticose di parete 204
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 204
Active Flow Control in Supersonic Nozzles 201
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 200
Aeroelastic Analysis and Optimal Design of Axial Multistage Fans and Compressors 199
Numerical Study of the Flowfield in a Differentially-Throttled Linear Aerospike 198
Investigation of the Snow Cornice Effect 198
Influence of the Facility Nozzle Design in the Unsteady Response of Direct-Connect Scramjet Combustors 198
Aerodynamic Design by Inverse Method 196
Inverse Problems for Advanced Nozzle Design. 196
Cold Gas Measurement System for Linear Aerospike Nozzles 194
Simulation of Jet Engine Transient by a CFD Method 193
Dinamica di strutture vorticose nel campo di moto di un rotore cuspidato 192
Numerical Design of Dual-Bell Nozzle 192
Optimization based on Inverse Problem for Aerodynamic Shape Design: Preliminary Results 189
Aerodynamic Design via Inverse Problem Solution in Three-Dimensional Incompressible Flows 186
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 178
Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle 176
Design of Inlet Distortion Generators for Direct-Connect Scramjet Combustors 175
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 173
A Framework for Testing Differential Throttling in Linear Aerospike Nozzle 169
An improved stall prediction model for axial compressor stage based on diffuser analogy 166
Shock Vector Control Technique for Aerospike Nozzles 162
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 161
Differential Throttling in Linear Aerospike: A Combined Experimental and Numerical Study 159
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 157
Influence of Hot Flow Conditions on Nozzle Performances 154
Numerical simulation of the unsteady flowfield in complete propulsion systems 151
Optimal aerodynamic design of hypersonic inlets by using streamline-tracing techniques 149
Assessment of a Thrust Measurement System for Supersonic Nozzles 148
Passive Control of Vortices in the Wake of a Bluff Body 146
A Two-Dimensional Analysis of the Flowfield and Performances of Linear Aerospikes During Differential Throttling 145
AI-Based Detection of Surge and Rotating Stall in Axial Compressors via Dynamic Model Parameter Estimation 144
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 138
Reduced order modeling of thermal transients in high-performance engineering systems 137
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model 136
Impeller Design and Performance Analysis of Aviation Fuel Pump Based on the Inverse Method 129
A Dual-Attention Model for Non-Contact Multi-Fault PCB Diagnosis Based on Scaler Magnetic Field and Fault Relation Feature 127
A Non-Contact PCB Multi-Fault Diagnosis Algorithm Based on Scalar Magnetic Field Fusion Feature and Transformer Architecture 123
Characteristic-based formulation of boundary conditions for preconditioned or non-preconditioned flow equations 122
Numerical Simulation of a Vectored Axisymmetric Nozzle 121
A fault/failure detection algorithm based on a grid of virtual sensors for engine health monitoring 120
Multi-fidelity sparse polynomial chaos expansion based on Gaussian process regression and least angle regression 120
Aerodynamic Design of Inward-Turning Inlets with Shape Transition 118
Sensitivity Analysis for Model with Dependent Inputs Using Sparse Polynomial Chaos Expansions 117
Vectorized Thrust Measurement for Aerospace Propulsion Nozzles 109
A Non-Contact AI-Based Approach to Multi-Failure Detection in Avionic Systems 103
Stator re-stagger optimization in multistage axial compressor 101
Design and Optimization of an Inward-Turning Inlet with Rectangular-To-Ellipse Shape Transition 99
Parametric Generation and Computational Analysis of a REST Inlet 98
Computational Investigation of Injection Effects on Shock Vector Control Performance 87
Totale 22.886
Categoria #
all - tutte 63.511
article - articoli 21.857
book - libri 0
conference - conferenze 38.353
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.391
Totale 126.112


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.119 0 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
2024/20252.490 48 304 102 332 233 104 212 136 369 206 246 198
2025/20266.331 384 342 335 493 340 437 1.071 445 1.361 620 181 322
2026/2027319 264 55 0 0 0 0 0 0 0 0 0 0
Totale 22.972