ABERGO, LUCA
 Distribuzione geografica
Continente #
EU - Europa 291
NA - Nord America 69
AS - Asia 46
AF - Africa 6
SA - Sud America 2
Totale 414
Nazione #
IT - Italia 208
US - Stati Uniti d'America 64
FI - Finlandia 23
ES - Italia 13
FR - Francia 13
IE - Irlanda 13
SG - Singapore 12
CN - Cina 10
PH - Filippine 9
IN - India 7
KR - Corea 7
BJ - Benin 5
CA - Canada 5
NL - Olanda 4
SI - Slovenia 4
BE - Belgio 3
GB - Regno Unito 3
AT - Austria 2
RU - Federazione Russa 2
VE - Venezuela 2
CI - Costa d'Avorio 1
CZ - Repubblica Ceca 1
DE - Germania 1
GR - Grecia 1
TR - Turchia 1
Totale 414
Città #
Milan 88
Helsinki 16
Dublin 13
Chandler 12
Seregno 10
Davao City 9
Singapore 9
Ashburn 8
Málaga 7
Boltiere 6
Giussano 6
Lappeenranta 6
Novara 6
Paris 6
Cotonou 5
Dallas 5
Meda 5
Songpa-gu 5
Bengaluru 4
Bled 4
Robbiate 4
Amsterdam 3
Beijing 3
Frosinone 3
Legnano 3
Montreal 3
Nova Milanese 3
Palaiseau 3
Shanghai 3
Bareggio 2
Bussero 2
Caserta 2
Châtillon 2
Coria del Río 2
Fairfield 2
Genoa 2
Ghaziabad 2
Lawrence 2
Liège 2
Medford 2
Moscow 2
Ottawa 2
Pastorano 2
Pozuelo de Alarcón 2
Toulouse 2
Trieste 2
Turin 2
Valencia 2
Vienna 2
Vigia 2
Xian 2
Abidjan 1
Ankara 1
Athens 1
Bardolino 1
Berlin 1
Boardman 1
Brescia 1
Bristol 1
Burlington 1
Cesana Brianza 1
Delft 1
Figino Serenza 1
Fort Worth 1
Hounslow 1
Kanpur 1
Knoxville 1
Lecco 1
Linyi 1
London 1
Miami 1
New York 1
Plzen 1
Redwood City 1
Rome 1
Saint-Gilles 1
San Jose 1
Saronno 1
Seattle 1
Washington 1
Wilmington 1
Zhengzhou 1
Totale 333
Nome #
Multi-Fidelity Numerical Approach to Aeroacoustics of Tandem Propellers in eVTOL Airplane Mode 92
Automatic Shape Optimization of a Non-Planar Wing Based on Discrete Adjoint and Radial Basis Function Mesh Deformation 89
Aerodynamic Optimization based on a Discrete Adjoint Framework and Radial Basis Function Mesh Deformation in SU2 50
Towards an open-source framework for Fluid–Structure Interaction using SU2, MBDyn and preCICE 45
Aerodynamic Shape Optimization Based on Discrete Adjoint and RBF 44
Acoustic and Aerodynamic Evaluation of DLR Small-Scale Rotor Configurations within Garteur AG26 34
Aeroacoustics computation for propellers based on harmonic balance solution 24
Unsteady Adjoint Optimization in SU2 Based on the Hybrid Harmonic Balance-URANS Approach 16
Adjoint-Based Aeroacoustic Optimization of Propeller Blades in Rotating Reference Frame 15
Aeroacustics computation based on harmonic balance solution 11
A Hybrid Bayesian-Adjoint Framework for Aerodynamic Shape Optimization 5
Acoustic and Aerodynamic Evaluation of POLIMI Tandem Propellers Configurations within GARTEUR AG26 1
Totale 426
Categoria #
all - tutte 1.747
article - articoli 575
book - libri 0
conference - conferenze 1.172
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 3.494


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/202273 0 0 0 0 3 7 0 31 15 11 2 4
2022/202370 2 3 2 2 3 8 11 6 6 17 2 8
2023/2024200 18 14 22 31 8 17 17 7 9 13 23 21
2024/202583 47 3 31 2 0 0 0 0 0 0 0 0
Totale 426