FERLAUTO, MICHELE
 Distribuzione geografica
Continente #
EU - Europa 2172
NA - Nord America 1862
AS - Asia 1779
AF - Africa 128
SA - Sud America 53
OC - Oceania 26
Totale 6020
Nazione #
US - Stati Uniti d'America 1771
IT - Italia 1026
CN - Cina 922
IN - India 281
DE - Germania 227
GB - Regno Unito 205
FR - Francia 189
IR - Iran 131
JP - Giappone 118
KR - Corea 113
RU - Federazione Russa 84
CA - Canada 77
BE - Belgio 61
UA - Ucraina 50
TR - Turchia 49
ES - Italia 43
NL - Olanda 37
VN - Vietnam 37
TN - Tunisia 32
CH - Svizzera 30
PK - Pakistan 30
EG - Egitto 28
SE - Svezia 28
DZ - Algeria 27
PL - Polonia 25
AU - Australia 22
ID - Indonesia 22
BR - Brasile 21
CZ - Repubblica Ceca 21
RO - Romania 19
GR - Grecia 18
ZA - Sudafrica 17
TW - Taiwan 14
AP - ???statistics.table.value.countryCode.AP??? 12
AR - Argentina 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
AE - Emirati Arabi Uniti 4
KW - Kuwait 4
LK - Sri Lanka 4
NZ - Nuova Zelanda 4
RS - Serbia 4
VE - Venezuela 4
BG - Bulgaria 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
KE - Kenya 1
LV - Lettonia 1
SC - Seychelles 1
Totale 6020
Città #
Beijing 341
Hangzhou 275
Ashburn 223
Turin 193
Houston 177
Fairfield 154
Seattle 136
Shenzhen 106
Torino 92
Ann Arbor 86
Mountain View 74
Milan 72
Santa Cruz 68
San Ramon 62
Wilmington 62
Buffalo 58
Cambridge 57
Woodbridge 57
Rome 48
Brussels 39
Nanjing 36
London 35
Genova 33
Bangalore 32
Varese 29
Asti 24
Moscow 24
Seoul 24
Wuhan 24
Dong Ket 23
Toronto 23
Bhubaneswar 22
Chennai 22
Tehran 22
Tianjin 21
Zhenhua 20
Ankara 19
Frankfurt 19
Chicago 18
Tokyo 18
Cairo 17
Montréal 16
Bengaluru 15
Islamabad 15
Los Angeles 15
Paris 15
University Park 15
Vinnitsa 15
Boardman 14
Jakarta 14
Madrid 13
San Donato Milanese 13
Southend 13
Xian 13
Binasco 12
Grytgöl 12
Kanpur 12
Kazan 12
Melbourne 12
Mumbai 12
Prague 12
San Diego 12
Scranton 12
Southampton 12
Bologna 11
Florence 11
Hanoi 11
Hyderabad 11
Shenyang 11
Braunschweig 10
Daegu 10
Daejeon 10
Dalian 10
Jinan 10
Las Vegas 10
Naples 10
Saint-étienne-du-rouvray 10
Athens 9
Berlin 9
New Delhi 9
Singapore 9
Bellevue 8
Cranfield 8
Harbin 8
Huntsville 8
Höst 8
Luzern 8
Novara 8
Novi Ligure 8
Palermo 8
Pisa 8
Rivoli 8
Yokohama 8
Zaporozhye 8
Aachen 7
Fremont 7
Kharagpur 7
Muizenberg 7
Munich 7
Parma 7
Totale 3508
Nome #
Numerical Simulation of Fluidic Thrust-Vectoring, file e384c42e-5378-d4b2-e053-9f05fe0a1d67 1067
Set of Boundary Conditions for Aerodynamic Design, file e384c42d-f364-d4b2-e053-9f05fe0a1d67 808
Studio e Controllo di Strutture Vorticose di Parete, file e384c42e-2215-d4b2-e053-9f05fe0a1d67 635
An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations, file e384c42d-e586-d4b2-e053-9f05fe0a1d67 524
A Pseudo-Compressibility Method for Solving Inverse Problems based on the 3D Incompressible Euler Equations, file e384c42e-32e0-d4b2-e053-9f05fe0a1d67 488
INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION, file e384c42e-1cf1-d4b2-e053-9f05fe0a1d67 433
An Inverse Method of Designing the Cooling Passages of Turbine Blades Based on the Heat Adjoint Equation, file e384c42e-2cbe-d4b2-e053-9f05fe0a1d67 267
A viscous inverse method for aerodynamic design, file e384c42d-f2d8-d4b2-e053-9f05fe0a1d67 248
Point vortex model for asymmetric inviscid wakes past bluff bodies, file e384c42e-35c1-d4b2-e053-9f05fe0a1d67 219
Synthetic jet modeling for flow control applications, file e384c42d-feaa-d4b2-e053-9f05fe0a1d67 195
Nozzles and Intakes Interacting with the External Flow: Design and Analysis, file e384c42d-eed7-d4b2-e053-9f05fe0a1d67 145
Optimal Aerodynamic Design of Scramjet Facility Nozzles, file e384c430-3043-d4b2-e053-9f05fe0a1d67 135
Optimal Inverse Method for Turbomachinery Design, file e384c42d-f11f-d4b2-e053-9f05fe0a1d67 123
Active Flow Control in Supersonic Nozzles, file e384c430-38ba-d4b2-e053-9f05fe0a1d67 123
Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines, file e384c42d-e587-d4b2-e053-9f05fe0a1d67 121
A New Steklov-Poincaré Numerical Technique for Solving Prandtl-Batchelor Flows, file e384c430-303b-d4b2-e053-9f05fe0a1d67 115
Blade Camber Surface Optimization for Turbomachinery Design, file e384c42d-f122-d4b2-e053-9f05fe0a1d67 79
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL, file e384c430-819d-d4b2-e053-9f05fe0a1d67 64
Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring, file e384c42f-4c3e-d4b2-e053-9f05fe0a1d67 62
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
Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike, file e384c433-52c4-d4b2-e053-9f05fe0a1d67 21
Numerical Simulation of a Vectored Axisymmetric Nozzle, file e384c432-c8a6-d4b2-e053-9f05fe0a1d67 20
Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method, file e384c434-27f3-d4b2-e053-9f05fe0a1d67 18
Multi-fidelity sparse polynomial chaos expansion based on Gaussian process regression and least angle regression, file e384c433-0ab4-d4b2-e053-9f05fe0a1d67 13
Characteristic-based formulation of boundary conditions for preconditioned or non-preconditioned flow equations, file e384c430-c7ef-d4b2-e053-9f05fe0a1d67 12
Parametric Generation and Computational Analysis of a REST Inlet, file e384c430-f5fa-d4b2-e053-9f05fe0a1d67 12
CFD-based Fluidic Thrust Vectoring model for fighter aircraft, file e384c430-f697-d4b2-e053-9f05fe0a1d67 10
A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike, file e384c433-db32-d4b2-e053-9f05fe0a1d67 10
AI Based Shock-Wave Detection by Using a Pressure Sensor Array, file e384c434-64f2-d4b2-e053-9f05fe0a1d67 9
Optimal aerodynamic design of hypersonic inlets by using streamline-tracing techniques, file e384c432-4138-d4b2-e053-9f05fe0a1d67 8
Reduced order modeling of thermal transients in high-performance engineering systems, file e384c430-c7f0-d4b2-e053-9f05fe0a1d67 7
A Numerical Method for the Study of Fluidic Thrust-Vectoring, file e384c42f-15f8-d4b2-e053-9f05fe0a1d67 6
Shock Vector Control Technique for Aerospike Nozzles, file e384c431-28e8-d4b2-e053-9f05fe0a1d67 6
Cold Gas Measurement System for Linear Aerospike Nozzles, file 65632998-4b9e-47bd-b128-b89749884867 5
Computational Investigation of Injection Effects on Shock Vector Control Performance, file e384c430-356e-d4b2-e053-9f05fe0a1d67 5
A fault/failure detection algorithm based on a grid of virtual sensors for engine health monitoring, file e384c431-085a-d4b2-e053-9f05fe0a1d67 5
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
Aerodynamic Design of Inward-Turning Inlets with Shape Transition, file e384c432-c8a7-d4b2-e053-9f05fe0a1d67 4
Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle, file e384c433-fd31-d4b2-e053-9f05fe0a1d67 4
Reduced order modelling of full-span rotating stall for the flow control simulation of axial compressors, file e384c42e-36f9-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
Sensitivity Analysis for Model with Dependent Inputs Using Sparse Polynomial Chaos Expansions, file e384c433-b7e8-d4b2-e053-9f05fe0a1d67 3
Stator re-stagger optimization in multistage axial compressor, file e384c433-c571-d4b2-e053-9f05fe0a1d67 3
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
Stator re-stagger optimization in multistage axial compressor, file e384c433-d110-d4b2-e053-9f05fe0a1d67 2
An improved stall prediction model for axial compressor stage based on diffuser analogy, file e384c434-d9d9-d4b2-e053-9f05fe0a1d67 2
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
Numerical Simulation of Fluidic Thrust-Vectoring, file e384c42f-45c8-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 6130
Categoria #
all - tutte 11551
article - articoli 6754
book - libri 0
conference - conferenze 3950
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 22255


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2017/2018762 0000 0129 216174 20414187
2018/2019249 2851413 1012 77 17345448
2019/2020549 64333072 5337 5757 73233020
2020/2021422 16383235 3168 1531 35384439
2021/2022567 422926112 7837 5326 17289227
2022/2023155 23397914 00 00 0000
Totale 6130