MAGRINI, ANDREA
 Distribuzione geografica
Continente #
NA - Nord America 766
EU - Europa 182
AS - Asia 81
Totale 1.029
Nazione #
US - Stati Uniti d'America 763
IT - Italia 121
CN - Cina 40
VN - Vietnam 36
FI - Finlandia 14
GB - Regno Unito 13
BE - Belgio 10
DE - Germania 9
SE - Svezia 6
NL - Olanda 3
PA - Panama 3
DK - Danimarca 2
IE - Irlanda 2
JP - Giappone 2
KR - Corea 2
RU - Federazione Russa 1
TR - Turchia 1
UA - Ucraina 1
Totale 1.029
Città #
Fairfield 164
Ashburn 74
Woodbridge 67
Seattle 55
Cambridge 52
Wilmington 48
Houston 47
Dong Ket 36
Ann Arbor 35
Chandler 31
Beijing 28
Padova 28
Medford 21
Princeton 21
Roxbury 18
San Diego 18
Des Moines 14
Helsinki 8
Cagliari 6
Lappeenranta 6
Gentbrugge 5
Los Angeles 5
Boardman 4
London 4
Munich 4
Pignone 4
Verona 4
Brendola 3
Gaggio 3
Modena 3
Nanjing 3
Panama City 3
Saint-Gilles 3
Treviso 3
Venice 3
Agordo 2
Albignasego 2
Bologna 2
Borås 2
Brussels 2
Buccinasco 2
Camposampiero 2
Castello di Godego 2
Cerveteri 2
Chengdu 2
Dublin 2
Falls Church 2
Kongens Lyngby 2
Naples 2
New Bedfont 2
Sernaglia della Battaglia 2
Vicenza 2
Battipaglia 1
Brescia 1
Bristol 1
Castegnero 1
Changsha 1
Chicago 1
Chiswick 1
Concordia Sagittaria 1
Cremona 1
Ferrara 1
Hebei 1
Hounslow 1
Jinan 1
Llansantffraid-ym-Mechain 1
Maglie 1
Milan 1
Montebelluna 1
Norwalk 1
Ogden 1
Palermo 1
Pordenone 1
Prescot 1
Quanzhou 1
Rome 1
San Giuliano Milanese 1
Sanayi 1
Shenyang 1
Taiyuan 1
Villadose 1
Volga 1
Washington 1
Totale 896
Nome #
Accurate 2-D Modelling of Transonic Compressor Cascade Aerodynamics 122
Conceptual-level evaluation of a variable stiffness skin for a morphing wing leading edge 117
Aerodynamic Optimization of a Morphing Leading Edge Airfoil with a Constant Arc Length Parameterization 87
Comparison of Constrained Parameterisation Strategies for Aerodynamic Optimisation of Morphing Leading Edge Airfoil 76
Supersonic compressor cascade shape optimization under multiple inlet Mach operating conditions 76
A review of installation effects of ultra-high bypass ratio engines 76
Aerodynamic Optimisation of a Morphing Leading Edge Airfoil 60
Study of Body Force Modelling for coupled fan/airframe simulations 51
Axial Rotor Design under Clean and Distortion Conditions using Mean-Line and CFD Methods 50
Two-objective optimization of a kaplan turbine draft tube using a response surface methodology 41
Inlet distortion simulations of a transonic fan with cfd and low-order methods 37
Sensitivity analysis of nacelle intake high-incidence aerodynamics including a body force fan model 32
Ultra-high bypass nacelle geometry design space exploration 30
Computational evaluation of turbo and electric powered simulators for wind tunnel tests of ultra-high bypass engines 25
Assessment of engine modelling on the installed aerodynamics of an ultra-high bypass turbofan 22
Comparison of nacelle models for the evaluation of an ultra-high bypass engine aerodynamics 21
Rans analysis of hl-crm at landing configuration with different flap deflections and engine representations 20
Investigation of HL-CRM aerodynamics with a UHBPR nacelle in powered-on condition 18
Installed performance of ultra-high bypass turbofans: estimation of power saving in optimised configurations 17
Design of short intakes for ultra-high bypass engines: preliminary exploration at fixed incidence 17
Maximisation of installed net resulting force through multi-level optimisation of an ultra-high bypass ratio engine nacelle 15
Study of geometric parameters for the design of short intakes with fan modelling 10
Analysis of Ultra-High Bypass Ratio Turbofan Nacelle Geometries With Conventional and Short Intakes at Take-Off and Cruise 10
Aeropropulsive assessment of engine installation at cruise for UHBPR turbofan with body force fan modelling 8
Aerodynamic Optimization of a Morphing Leading Edge Airfoil with a Constant Arc Length Parameterization 7
Development of a Reduced Order Model Based on Aerodynamic Influence Coefficients to Simulate Aeroelastic Phenomena in Axial Compressor Blades 7
CFD-Based Analysis of Installed Fuel Consumption and Aerodynamics of Transonic Transport Aircraft during Cruise Flight 6
Powered turbofan effects on aircraft aerodynamics at high-lift: A study on the NASA CRM-HL 6
Body Force Model Implementation of Transonic Rotor for Fan/Airframe Simulations 5
Analysis of installation aerodynamics and comparison of optimised configuration of an ultra-high bypass ratio turbofan nacelle 4
Totale 1.073
Categoria #
all - tutte 6.194
article - articoli 3.304
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 9.498


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/201952 0 0 0 0 0 0 0 0 0 0 14 38
2019/2020172 18 8 5 8 19 9 16 20 33 14 17 5
2020/2021266 10 6 19 15 8 44 16 21 39 15 16 57
2021/2022257 17 14 11 15 7 17 33 21 19 15 28 60
2022/2023157 35 0 5 4 17 16 8 18 16 5 23 10
2023/2024156 4 29 9 15 14 27 16 16 11 15 0 0
Totale 1.073