FRUNCILLO, FELICE
 Distribuzione geografica
Continente #
EU - Europa 168
AS - Asia 113
NA - Nord America 52
SA - Sud America 7
OC - Oceania 4
AF - Africa 2
Totale 346
Nazione #
IT - Italia 88
SG - Singapore 75
US - Stati Uniti d'America 44
NL - Olanda 18
DE - Germania 16
FR - Francia 11
IN - India 11
HK - Hong Kong 9
CN - Cina 8
RU - Federazione Russa 8
BR - Brasile 7
CA - Canada 6
CH - Svizzera 6
GB - Regno Unito 6
AU - Australia 4
HU - Ungheria 4
IR - Iran 3
JP - Giappone 3
NO - Norvegia 3
UA - Ucraina 3
ES - Italia 2
FI - Finlandia 2
MX - Messico 2
MY - Malesia 2
AE - Emirati Arabi Uniti 1
KE - Kenya 1
MA - Marocco 1
PL - Polonia 1
PS - Palestinian Territory 1
Totale 346
Città #
Milan 13
Munich 12
Singapore 11
West Lafayette 11
Haarlem 8
Boardman 5
Hong Kong 5
Rome 5
Zurich 5
Bengaluru 4
Budapest 4
Nuremberg 4
Paris 4
Sydney 4
Beijing 3
Bologna 3
Montreal 3
Muret 3
Sunnyvale 3
Ashburn 2
Cheltenham 2
Dunstable 2
Florence 2
Getafe 2
Kozhikode 2
Kuala Lumpur 2
Kyiv 2
Mangalore 2
McLean 2
Mexico City 2
Montmirail 2
Moscow 2
Pastorano 2
Sapporo 2
Stavanger 2
Tehran 2
Turku 2
Xi'an 2
Belo Horizonte 1
Bismarck 1
Cheremkhovo 1
Council Bluffs 1
Denver 1
Gandhinagar 1
Gaza 1
Kolkata 1
London 1
Los Angeles 1
Nairobi 1
Naples 1
Noida 1
Oslo 1
Parma 1
Porto Alegre 1
Rabat 1
Reston 1
Rio de Janeiro 1
San Francisco 1
San Jose 1
Santana do Livramento 1
Sherbrooke 1
Sorocaba 1
Stroudsburg 1
São Paulo 1
Tabuleiro do Norte 1
The Dalles 1
Totale 176
Nome #
Multipole Expansion Approach for Rotor Noise Prediction 50
Guidance Algorithms for Precision Landing of a Launcher First-Stage 46
Low-Noise Propeller Optimization Via Blade Sweep and Uneven Spacing 31
Feasibility Analysis of the Ascent Trajectory of the Scramjet Hypersonic Experimental Vehicle 29
IDENTIFYING THE ACTIVE FLOW REGIONS IN ACOUSTIC-HYDRODYNAMIC FEEDBACK MECHANISMS 28
Structural Response Analysis of a Hypersonic Demonstrator Under Multi-Load Conditions During Stage Separation 26
Navigation Algorithms for Precision Re-entry of a Launcher First-Stage 26
null 24
Impact of Added Mass on the Control Laws Design 24
Propeller Optimization for Tonal Noise Reduction Using Spherical Harmonics Expansion and Blade Element Theory 21
null 18
Effects of Comprehensive Added Masses Modeling on Airship Equations of Motion and Dynamic Stability 14
Assessment of Added Masses Effects on Airship Dynamics and Stability 14
null 11
null 9
Totale 371
Categoria #
all - tutte 642
article - articoli 0
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 642


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2023/20247 0 0 0 0 0 0 0 0 0 0 4 3
2024/2025364 0 0 0 0 0 1 5 0 7 2 153 196
Totale 371