FERLAUTO, MICHELE
 Distribuzione geografica
Continente #
EU - Europa 2.371
NA - Nord America 2.027
AS - Asia 1.793
AF - Africa 128
SA - Sud America 55
OC - Oceania 28
Totale 6.402
Nazione #
US - Stati Uniti d'America 1.935
IT - Italia 1.124
CN - Cina 923
IN - India 286
DE - Germania 232
FR - Francia 223
GB - Regno Unito 205
IR - Iran 131
JP - Giappone 118
KR - Corea 113
RU - Federazione Russa 84
CA - Canada 78
BE - Belgio 63
TR - Turchia 53
IE - Irlanda 50
UA - Ucraina 50
ES - Italia 43
NL - Olanda 40
VN - Vietnam 37
PK - Pakistan 34
CH - Svizzera 33
TN - Tunisia 32
EG - Egitto 28
SE - Svezia 28
DZ - Algeria 27
PL - Polonia 25
AU - Australia 23
BR - Brasile 22
ID - Indonesia 22
CZ - Repubblica Ceca 21
RO - Romania 19
GR - Grecia 18
ZA - Sudafrica 17
TW - Taiwan 14
AR - Argentina 13
AP - ???statistics.table.value.countryCode.AP??? 12
IL - Israele 11
SG - Singapore 11
AT - Austria 10
CL - Cile 10
IQ - Iraq 10
MX - Messico 10
ET - Etiopia 9
HK - Hong Kong 9
SK - Slovacchia (Repubblica Slovacca) 9
EE - Estonia 8
EU - Europa 8
MM - Myanmar 8
MY - Malesia 8
MA - Marocco 6
PT - Portogallo 6
TH - Thailandia 6
NO - Norvegia 5
NZ - Nuova Zelanda 5
AE - Emirati Arabi Uniti 4
KW - Kuwait 4
LK - Sri Lanka 4
RS - Serbia 4
VE - Venezuela 4
BG - Bulgaria 3
FI - Finlandia 3
HU - Ungheria 3
LT - Lituania 3
LU - Lussemburgo 3
NG - Nigeria 3
SA - Arabia Saudita 3
BO - Bolivia 2
CO - Colombia 2
CR - Costa Rica 2
GE - Georgia 2
IS - Islanda 2
KZ - Kazakistan 2
LA - Repubblica Popolare Democratica del Laos 2
LY - Libia 2
OM - Oman 2
PE - Perù 2
PH - Filippine 2
QA - Qatar 2
RE - Reunion 2
SI - Slovenia 2
TT - Trinidad e Tobago 2
AL - Albania 1
BD - Bangladesh 1
DK - Danimarca 1
KE - Kenya 1
LV - Lettonia 1
SC - Seychelles 1
Totale 6.402
Città #
Beijing 341
Hangzhou 275
Ashburn 240
Turin 217
Houston 177
Fairfield 154
Seattle 139
Shenzhen 106
Torino 94
Ann Arbor 86
Milan 84
Mountain View 74
Santa Cruz 68
San Ramon 62
Wilmington 62
Buffalo 60
Rome 59
Cambridge 57
Woodbridge 57
Dublin 51
Brussels 41
Nanjing 36
London 35
Genova 33
Bangalore 32
Varese 29
Asti 24
Fleming Island 24
Moscow 24
Seoul 24
Wuhan 24
Dong Ket 23
Toronto 23
Ankara 22
Bhubaneswar 22
Chennai 22
Chicago 22
Tehran 22
Tianjin 21
Zhenhua 20
Frankfurt 19
Islamabad 19
Tokyo 18
Cairo 17
Los Angeles 17
Bengaluru 16
Montréal 16
Paris 15
University Park 15
Vinnitsa 15
Boardman 14
Bologna 14
Brooklyn 14
Jakarta 14
Florence 13
Madrid 13
Naples 13
San Donato Milanese 13
Southend 13
Xian 13
Binasco 12
Chandler 12
Grytgöl 12
Kanpur 12
Kazan 12
Melbourne 12
Mumbai 12
Prague 12
San Diego 12
Scranton 12
Southampton 12
Caserta 11
Hanoi 11
Hyderabad 11
Shenyang 11
Braunschweig 10
Coimbatore 10
Daegu 10
Daejeon 10
Dalian 10
Jinan 10
Las Vegas 10
Saint-étienne-du-rouvray 10
Athens 9
Berlin 9
New Delhi 9
Palermo 9
Redmond 9
Singapore 9
Bellevue 8
Boulder 8
Cranfield 8
Harbin 8
Huntsville 8
Höst 8
Luzern 8
Novara 8
Novi Ligure 8
Pisa 8
Rivoli 8
Totale 3.685
Nome #
Numerical Simulation of Fluidic Thrust-Vectoring, file e384c42e-5378-d4b2-e053-9f05fe0a1d67 1.091
Set of Boundary Conditions for Aerodynamic Design, file e384c42d-f364-d4b2-e053-9f05fe0a1d67 825
Studio e Controllo di Strutture Vorticose di Parete, file e384c42e-2215-d4b2-e053-9f05fe0a1d67 711
An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations, file e384c42d-e586-d4b2-e053-9f05fe0a1d67 541
A Pseudo-Compressibility Method for Solving Inverse Problems based on the 3D Incompressible Euler Equations, file e384c42e-32e0-d4b2-e053-9f05fe0a1d67 502
INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION, file e384c42e-1cf1-d4b2-e053-9f05fe0a1d67 441
An Inverse Method of Designing the Cooling Passages of Turbine Blades Based on the Heat Adjoint Equation, file e384c42e-2cbe-d4b2-e053-9f05fe0a1d67 271
A viscous inverse method for aerodynamic design, file e384c42d-f2d8-d4b2-e053-9f05fe0a1d67 258
Point vortex model for asymmetric inviscid wakes past bluff bodies, file e384c42e-35c1-d4b2-e053-9f05fe0a1d67 222
Synthetic jet modeling for flow control applications, file e384c42d-feaa-d4b2-e053-9f05fe0a1d67 201
Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines, file e384c42d-e587-d4b2-e053-9f05fe0a1d67 158
Nozzles and Intakes Interacting with the External Flow: Design and Analysis, file e384c42d-eed7-d4b2-e053-9f05fe0a1d67 150
Optimal Aerodynamic Design of Scramjet Facility Nozzles, file e384c430-3043-d4b2-e053-9f05fe0a1d67 148
Active Flow Control in Supersonic Nozzles, file e384c430-38ba-d4b2-e053-9f05fe0a1d67 136
A New Steklov-Poincaré Numerical Technique for Solving Prandtl-Batchelor Flows, file e384c430-303b-d4b2-e053-9f05fe0a1d67 126
Optimal Inverse Method for Turbomachinery Design, file e384c42d-f11f-d4b2-e053-9f05fe0a1d67 125
Blade Camber Surface Optimization for Turbomachinery Design, file e384c42d-f122-d4b2-e053-9f05fe0a1d67 99
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring, file e384c42f-4c3e-d4b2-e053-9f05fe0a1d67 79
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL, file e384c430-819d-d4b2-e053-9f05fe0a1d67 69
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike, file e384c433-52c4-d4b2-e053-9f05fe0a1d67 34
A viscous inverse method for aerodynamic design, file e384c42d-f2d6-d4b2-e053-9f05fe0a1d67 30
An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations, file e384c42d-e588-d4b2-e053-9f05fe0a1d67 24
Numerical Simulation of a Vectored Axisymmetric Nozzle, file e384c432-c8a6-d4b2-e053-9f05fe0a1d67 22
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method, file e384c434-27f3-d4b2-e053-9f05fe0a1d67 21
AI Based Shock-Wave Detection by Using a Pressure Sensor Array, file e384c434-64f2-d4b2-e053-9f05fe0a1d67 21
Parametric Generation and Computational Analysis of a REST Inlet, file e384c430-f5fa-d4b2-e053-9f05fe0a1d67 18
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike, file e384c433-db32-d4b2-e053-9f05fe0a1d67 16
Multi-fidelity sparse polynomial chaos expansion based on Gaussian process regression and least angle regression, file e384c433-0ab4-d4b2-e053-9f05fe0a1d67 14
Characteristic-based formulation of boundary conditions for preconditioned or non-preconditioned flow equations, file e384c430-c7ef-d4b2-e053-9f05fe0a1d67 13
Cold Gas Measurement System for Linear Aerospike Nozzles, file 65632998-4b9e-47bd-b128-b89749884867 12
Reduced order modeling of thermal transients in high-performance engineering systems, file e384c430-c7f0-d4b2-e053-9f05fe0a1d67 10
CFD-based Fluidic Thrust Vectoring model for fighter aircraft, file e384c430-f697-d4b2-e053-9f05fe0a1d67 10
Optimal aerodynamic design of hypersonic inlets by using streamline-tracing techniques, file e384c432-4138-d4b2-e053-9f05fe0a1d67 9
A Numerical Method for the Study of Fluidic Thrust-Vectoring, file e384c42f-15f8-d4b2-e053-9f05fe0a1d67 6
A fault/failure detection algorithm based on a grid of virtual sensors for engine health monitoring, file e384c431-085a-d4b2-e053-9f05fe0a1d67 6
Shock Vector Control Technique for Aerospike Nozzles, file e384c431-28e8-d4b2-e053-9f05fe0a1d67 6
Aerodynamic Design of Inward-Turning Inlets with Shape Transition, file e384c432-c8a7-d4b2-e053-9f05fe0a1d67 6
Computational Investigation of Injection Effects on Shock Vector Control Performance, file e384c430-356e-d4b2-e053-9f05fe0a1d67 5
Sensitivity Analysis for Model with Dependent Inputs Using Sparse Polynomial Chaos Expansions, file e384c433-b7e8-d4b2-e053-9f05fe0a1d67 5
Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle, file e384c433-fd31-d4b2-e053-9f05fe0a1d67 5
Impeller Design and Performance Analysis of Aviation Fuel Pump Based on the Inverse Method, file bb5a203f-ef41-4449-a2f3-e47aea92f40b 4
A Pseudo-Compressibility Method for Solving Inverse Problems based on the 3D Incompressible Euler Equations, file e384c42e-32e1-d4b2-e053-9f05fe0a1d67 4
A computational approach to the simulation of controlled flows by synthetic jets actuators, file e384c42e-34ff-d4b2-e053-9f05fe0a1d67 4
Design and Optimization of an Inward-Turning Inlet with Rectangular-To-Ellipse Shape Transition, file e384c431-09bd-d4b2-e053-9f05fe0a1d67 4
Fluidic Thrust Vectoring for Annular Aerospike Nozzle, file e384c432-6170-d4b2-e053-9f05fe0a1d67 4
Stator re-stagger optimization in multistage axial compressor, file e384c433-c571-d4b2-e053-9f05fe0a1d67 4
On the Use of Vortex Identification for the Optimization of Trapped Vortex Devices, file 0b80a795-3b83-4cc7-b8ff-967eb75faecd 3
Experimental Characterization of a Linear Aerospike Nozzle Flow, file 4e1e94fd-7d4e-4f9f-bdc3-fabbd4764d11 3
Reduced order modelling of full-span rotating stall for the flow control simulation of axial compressors, file e384c42e-36f9-d4b2-e053-9f05fe0a1d67 3
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model, file e384c430-a8cb-d4b2-e053-9f05fe0a1d67 3
The Clean Sky 2 MIDAS Project - an Innovative Modular, Digital and Integrated Air Data System for Fly-by-Wire Applications, file e384c430-e493-d4b2-e053-9f05fe0a1d67 3
Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle, file e384c431-01a3-d4b2-e053-9f05fe0a1d67 3
Stator re-stagger optimization in multistage axial compressor, file e384c433-d110-d4b2-e053-9f05fe0a1d67 3
Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle, file 0e88c42f-fa94-49e1-8c9e-8a5cb9a5997d 2
Numerical Simulation of Fluidic Thrust-Vectoring, file 37965fb6-959b-4534-8898-f8f25be5660d 2
A Vortex-In-Cell Method for the Simulation of Viscous Flows, file e384c42f-e501-d4b2-e053-9f05fe0a1d67 2
Numerical simulation of the unsteady flowfield in complete propulsion systems, file e384c430-2191-d4b2-e053-9f05fe0a1d67 2
An improved stall prediction model for axial compressor stage based on diffuser analogy, file e384c434-d9d9-d4b2-e053-9f05fe0a1d67 2
Numerical and Experimental Assessment of a Linear Aerospike, file 8be83c42-7f56-4bca-8522-570eab07450b 1
Simulation of Jet Engine Transient by a CFD Method, file e384c42d-f396-d4b2-e053-9f05fe0a1d67 1
INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION, file e384c42e-1cf0-d4b2-e053-9f05fe0a1d67 1
Point vortex model for asymmetric inviscid wakes past bluff bodies, file e384c42e-302c-d4b2-e053-9f05fe0a1d67 1
Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring, file e384c42f-01f7-d4b2-e053-9f05fe0a1d67 1
Design and Testing of a Low-Cost Extended-Range Pressure Measurement System for Aerospace Applications, file e384c42f-8b60-d4b2-e053-9f05fe0a1d67 1
On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles, file e384c42f-e182-d4b2-e053-9f05fe0a1d67 1
Influence of the Facility Nozzle Design in the Unsteady Response of Direct-Connect Scramjet Combustors, file e384c42f-e335-d4b2-e053-9f05fe0a1d67 1
Inverse Problems for Advanced Nozzle Design., file e384c431-165a-d4b2-e053-9f05fe0a1d67 1
Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle, file e384c433-fd30-d4b2-e053-9f05fe0a1d67 1
Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring, file e384c434-cead-d4b2-e053-9f05fe0a1d67 1
Totale 6.512
Categoria #
all - tutte 12.716
article - articoli 7.205
book - libri 0
conference - conferenze 4.517
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 24.438


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019155 0 0 0 0 0 0 0 0 17 36 54 48
2019/2020550 65 33 30 72 53 37 57 57 73 23 30 20
2020/2021422 16 38 32 35 31 68 15 31 35 38 44 39
2021/2022567 42 29 26 112 78 37 53 26 17 28 92 27
2022/2023437 23 39 79 44 23 70 42 27 43 24 21 2
2023/202498 1 1 0 7 4 22 7 41 15 0 0 0
Totale 6.512