FERLAUTO, MICHELE
 Distribuzione geografica
Continente #
NA - Nord America 9.906
EU - Europa 8.064
AS - Asia 5.649
SA - Sud America 566
Continente sconosciuto - Info sul continente non disponibili 364
AF - Africa 79
OC - Oceania 25
Totale 24.653
Nazione #
US - Stati Uniti d'America 9.622
IT - Italia 3.223
SG - Singapore 1.666
VN - Vietnam 1.250
GB - Regno Unito 1.122
CN - Cina 1.068
DE - Germania 928
FR - Francia 809
RU - Federazione Russa 519
UA - Ucraina 438
BR - Brasile 429
KR - Corea 381
HK - Hong Kong 287
IN - India 272
TR - Turchia 222
SE - Svezia 189
IE - Irlanda 186
CA - Canada 177
AT - Austria 106
NL - Olanda 100
FI - Finlandia 98
CH - Svizzera 95
BD - Bangladesh 84
BE - Belgio 76
JP - Giappone 74
ID - Indonesia 58
MX - Messico 38
AR - Argentina 34
IQ - Iraq 34
PH - Filippine 34
MY - Malesia 33
ES - Italia 32
TH - Thailandia 32
CO - Colombia 29
TW - Taiwan 29
BG - Bulgaria 27
IL - Israele 22
PL - Polonia 22
ZA - Sudafrica 22
AU - Australia 21
CL - Cile 21
EC - Ecuador 18
VE - Venezuela 18
CR - Costa Rica 17
SA - Arabia Saudita 15
PK - Pakistan 14
IR - Iran 13
RO - Romania 13
EU - Europa 12
UZ - Uzbekistan 12
AP - ???statistics.table.value.countryCode.AP??? 9
JM - Giamaica 9
KZ - Kazakistan 9
DZ - Algeria 8
EG - Egitto 8
GR - Grecia 8
HN - Honduras 8
MA - Marocco 8
HR - Croazia 7
NI - Nicaragua 7
NP - Nepal 7
SC - Seychelles 7
SN - Senegal 7
TT - Trinidad e Tobago 7
AE - Emirati Arabi Uniti 6
CZ - Repubblica Ceca 6
DK - Danimarca 6
JO - Giordania 6
OM - Oman 6
PY - Paraguay 6
GT - Guatemala 5
LT - Lituania 5
PE - Perù 5
PT - Portogallo 5
BO - Bolivia 4
BY - Bielorussia 4
ET - Etiopia 4
HU - Ungheria 4
LV - Lettonia 4
TN - Tunisia 4
KW - Kuwait 3
NG - Nigeria 3
NZ - Nuova Zelanda 3
SV - El Salvador 3
AL - Albania 2
AM - Armenia 2
AZ - Azerbaigian 2
BA - Bosnia-Erzegovina 2
BB - Barbados 2
CW - ???statistics.table.value.countryCode.CW??? 2
DO - Repubblica Dominicana 2
GP - Guadalupe 2
KE - Kenya 2
KG - Kirghizistan 2
LU - Lussemburgo 2
MU - Mauritius 2
NO - Norvegia 2
PR - Porto Rico 2
QA - Qatar 2
RS - Serbia 2
Totale 24.274
Città #
Ashburn 2.124
Southend 883
Singapore 861
Turin 805
San Jose 653
Fairfield 508
Seattle 485
Chandler 398
Ho Chi Minh City 330
Milan 307
Houston 304
Hanoi 285
Princeton 278
Beijing 249
Santa Clara 244
Woodbridge 244
Ann Arbor 240
Wilmington 224
Hong Kong 211
San Francisco 207
Council Bluffs 206
Jacksonville 198
Torino 194
Cambridge 193
Seoul 185
Dublin 178
Berlin 166
Boardman 156
San Ramon 155
Izmir 148
Buffalo 120
Los Angeles 119
Chicago 114
Lauterbourg 98
Rivoli 98
Asti 93
Dallas 91
Des Moines 91
Bern 82
San Donato Milanese 74
Helsinki 69
North Bergen 67
Rome 67
Shanghai 67
Zhengzhou 66
Da Nang 63
Brussels 61
New York 60
Bologna 59
Vienna 56
Haiphong 53
Baltimore 50
Hyderabad 49
Zaporozhye 47
Hefei 44
Jakarta 42
Istanbul 39
Pennsylvania Furnace 39
Phoenix 39
Austin 37
Saint Petersburg 37
Overberg 34
Toronto 34
Frankfurt am Main 32
Monopoli 31
Moscow 30
Washington 30
Guangzhou 29
London 29
Padua 29
Redwood City 29
Hangzhou 25
Gilroy 24
Las Vegas 24
Tokyo 24
Fremont 23
Atlanta 22
San Diego 22
Borgosesia 21
Lappeenranta 21
Munich 21
Nanjing 21
Bari 20
Martina Franca 20
Montreal 20
São Paulo 20
Nuremberg 19
Orem 19
Sofia 19
Verona 19
Columbus 18
Norwalk 18
Dalian 17
Hải Dương 17
Montréal 17
Falls Church 16
San Antonio 16
The Dalles 16
Denver 15
Naples 15
Totale 14.586
Nome #
An Inverse Method of Designing the Cooling Passages of Turbine Blades Based on the Heat Adjoint Equation 619
An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations 616
A Pseudo-Compressibility Method for Solving Inverse Problems based on the 3D Incompressible Euler Equations 612
Set of Boundary Conditions for Aerodynamic Design 605
INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION 499
Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines 491
Studio e Controllo di Strutture Vorticose di Parete 482
Point vortex model for asymmetric inviscid wakes past bluff bodies 470
A viscous inverse method for aerodynamic design 443
Numerical Simulation of Fluidic Thrust-Vectoring 390
Optimal Inverse Method for Turbomachinery Design 356
A computational approach to the simulation of controlled flows by synthetic jets actuators 340
A Numerical Method for the Study of Fluidic Thrust-Vectoring 338
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring 331
A New Set of Boundary Conditions for Aerodynamic Design 323
Numerical Simulation of Fluidic Thrust-Vectoring 307
Experimental Characterization of a Linear Aerospike Nozzle Flow 303
Nozzles and Intakes Interacting with the External Flow: Design and Analysis 300
Optimal Aerodynamic Design of Scramjet Facility Nozzles 299
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring 298
A 2-D Viscous Inverse Problem Method for Aerodynamics Design 295
Synthetic jet modeling for flow control applications 291
Dynamics of Coherent Structures near a rotating Body 281
Blade Camber Surface Optimization for Turbomachinery Design 280
The Clean Sky 2 MIDAS Project - an Innovative Modular, Digital and Integrated Air Data System for Fly-by-Wire Applications 279
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle 276
Synthetic Jet Actuator Modeling for Flow Control Applications 275
Reduced order modelling of full-span rotating stall for the flow control simulation of axial compressors 275
Coupling of optimization and inverse problem for aerodynamic shape design 269
Numerical Simulation of Transient Operations in Aeroengines 264
A CFD Method for Optimal Air-Intake Design 264
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method 261
Design and Testing of a Low-Cost Extended-Range Pressure Measurement System for Aerospace Applications 254
A Vortex-In-Cell Method for the Simulation of Viscous Flows 253
CFD-based Fluidic Thrust Vectoring model for fighter aircraft 252
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike 252
Integrated Design and Analysys of Intakes and Nozzles in Air-Breathing Engines. 251
Fan and propeller design via inverse problem adjoint equations 248
Numerical and Experimental Assessment of a Linear Aerospike 238
Hollow Vortices in Shear 235
Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike 234
Numerical Study of the Flowfield in a Differentially-Throttled Linear Aerospike 234
A class of non-reflecting boundary conditions for turbomachinery design. 234
A New Steklov-Poincaré Numerical Technique for Solving Prandtl-Batchelor Flows 232
Computation of plug nozzle turbulent flowfields 231
Propfan Optimization Based on Inverse Problem Adjoint Equations 230
Numerical Design of Dual-Bell Nozzles 225
An Eulerian-Lagrangian Method for Vortical Flow Simulations 224
AI Assisted Detection of Shock Motions Inside a Transonic Duct 222
Active Flow Control in Supersonic Nozzles 216
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles 215
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike 215
AI Based Shock-Wave Detection by Using a Pressure Sensor Array 215
Investigation of the Snow Cornice Effect 209
Aeroelastic Analysis and Optimal Design of Axial Multistage Fans and Compressors 209
Aerodynamic Design by Inverse Method 209
Simulazione numerica di Strutture vorticose di parete 208
Influence of the Facility Nozzle Design in the Unsteady Response of Direct-Connect Scramjet Combustors 206
Numerical Design of Dual-Bell Nozzle 205
Cold Gas Measurement System for Linear Aerospike Nozzles 204
Inverse Problems for Advanced Nozzle Design. 202
Simulation of Jet Engine Transient by a CFD Method 200
Dinamica di strutture vorticose nel campo di moto di un rotore cuspidato 199
Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle 199
Optimization based on Inverse Problem for Aerodynamic Shape Design: Preliminary Results 196
A Framework for Testing Differential Throttling in Linear Aerospike Nozzle 191
Aerodynamic Design via Inverse Problem Solution in Three-Dimensional Incompressible Flows 191
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL 191
Fluidic Thrust Vectoring for Annular Aerospike Nozzle 189
Differential Throttling in Linear Aerospike: A Combined Experimental and Numerical Study 186
An improved stall prediction model for axial compressor stage based on diffuser analogy 186
Design of Inlet Distortion Generators for Direct-Connect Scramjet Combustors 185
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices 176
Shock Vector Control Technique for Aerospike Nozzles 175
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring 175
Assessment of a Thrust Measurement System for Supersonic Nozzles 174
AI-Based Detection of Surge and Rotating Stall in Axial Compressors via Dynamic Model Parameter Estimation 173
Influence of Hot Flow Conditions on Nozzle Performances 173
Passive Control of Vortices in the Wake of a Bluff Body 166
A Two-Dimensional Analysis of the Flowfield and Performances of Linear Aerospikes During Differential Throttling 164
Numerical simulation of the unsteady flowfield in complete propulsion systems 162
Optimal aerodynamic design of hypersonic inlets by using streamline-tracing techniques 161
A Dual-Attention Model for Non-Contact Multi-Fault PCB Diagnosis Based on Scaler Magnetic Field and Fault Relation Feature 155
A Non-Contact PCB Multi-Fault Diagnosis Algorithm Based on Scalar Magnetic Field Fusion Feature and Transformer Architecture 154
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model 150
Impeller Design and Performance Analysis of Aviation Fuel Pump Based on the Inverse Method 148
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle 147
Reduced order modeling of thermal transients in high-performance engineering systems 142
Vectorized Thrust Measurement for Aerospace Propulsion Nozzles 141
Multi-fidelity sparse polynomial chaos expansion based on Gaussian process regression and least angle regression 132
A Non-Contact AI-Based Approach to Multi-Failure Detection in Avionic Systems 131
A fault/failure detection algorithm based on a grid of virtual sensors for engine health monitoring 131
Sensitivity Analysis for Model with Dependent Inputs Using Sparse Polynomial Chaos Expansions 131
Characteristic-based formulation of boundary conditions for preconditioned or non-preconditioned flow equations 130
Numerical Simulation of a Vectored Axisymmetric Nozzle 129
Aerodynamic Design of Inward-Turning Inlets with Shape Transition 126
Stator re-stagger optimization in multistage axial compressor 111
Design and Optimization of an Inward-Turning Inlet with Rectangular-To-Ellipse Shape Transition 108
Parametric Generation and Computational Analysis of a REST Inlet 103
Computational Investigation of Injection Effects on Shock Vector Control Performance 99
Totale 24.474
Categoria #
all - tutte 68.295
article - articoli 23.697
book - libri 0
conference - conferenze 41.116
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.505
Totale 135.613


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022905 0 0 0 0 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
2026/20272.000 264 213 527 864 132 0 0 0 0 0 0 0
Totale 24.653