BETTELLA, ALBERTO
 Distribuzione geografica
Continente #
NA - Nord America 2.289
EU - Europa 361
AS - Asia 342
OC - Oceania 2
SA - Sud America 1
Totale 2.995
Nazione #
US - Stati Uniti d'America 2.284
CN - Cina 185
SG - Singapore 98
DE - Germania 82
IT - Italia 72
FI - Finlandia 68
FR - Francia 31
GB - Regno Unito 31
UA - Ucraina 26
SE - Svezia 22
IN - India 20
VN - Vietnam 14
IE - Irlanda 10
AE - Emirati Arabi Uniti 7
ES - Italia 7
TR - Turchia 7
HK - Hong Kong 6
CA - Canada 5
RU - Federazione Russa 5
AT - Austria 3
AU - Australia 2
BE - Belgio 2
IQ - Iraq 2
CH - Svizzera 1
CL - Cile 1
KR - Corea 1
MY - Malesia 1
NL - Olanda 1
TW - Taiwan 1
Totale 2.995
Città #
Fairfield 316
Chandler 267
Woodbridge 198
Ashburn 180
Ann Arbor 162
Houston 138
Seattle 136
Wilmington 131
Cambridge 102
Singapore 82
Santa Clara 72
Boardman 67
Jacksonville 55
Beijing 53
Princeton 41
Medford 37
Roxbury 34
Nanjing 31
Helsinki 30
Des Moines 25
New York 20
San Diego 19
Padova 16
Dong Ket 14
Dublin 12
Redwood City 12
Shenyang 12
Hebei 9
Nanchang 9
Abu Dhabi 7
Rome 7
Bonndorf 6
Cagliari 6
Frankfurt am Main 6
London 5
Norwalk 5
Chennai 4
Dallas 4
Hong Kong 4
Kharkiv 4
Kunming 4
Kyiv 4
Madrid 4
Munich 4
Nürnberg 4
Xi'an 4
Çankaya 4
Bengaluru 3
Calgary 3
Changsha 3
Cranfield 3
Guangzhou 3
Hangzhou 3
Jiaxing 3
Jinan 3
Ogden 3
Tappahannock 3
A Coruña 2
Anzio 2
Borås 2
Bremen 2
Bruchsal 2
Centro 2
Conegliano 2
Hefei 2
Indiana 2
Leicester 2
Los Angeles 2
Rewāri 2
Samsun 2
Shanghai 2
Stillwater 2
Taranto 2
Trento 2
Verona 2
Vienna 2
Alghero 1
Aprilia 1
Baghdad 1
Baracaldo 1
Brigg 1
Capriolo 1
Carol Stream 1
Chengdu 1
Costa Mesa 1
Falls Church 1
Flavin 1
Gaiarine 1
Gunzenhausen 1
Göttingen 1
Hounslow 1
Islington 1
Lendinara 1
Longare 1
Melbourne 1
Milan 1
Montreal 1
Mountain View 1
Naples 1
Pasadena 1
Totale 2.458
Nome #
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 177
Hypervelocity experiments of impact cratering and catastrophic disruption of targets representative of minor bodies of the Solar System 121
Analysis of transient vibrations on complex targets representing elementary configurations of GOCE satellite 116
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 103
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets 103
SPONGE: a Sounding Rocket Experiment for PMDs 102
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 102
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 101
Numerical Modeling of Paraffin-Based Fuels Behavior 100
Computational Fluid Dynamics Simulation of Regression Rate in Hybrid Rockets 97
Selecting materials to protect inflatable structures from the space environment 93
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 93
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 93
EUCLID satellite: Sloshing model development through computational fluid dynamics 87
Mini launcher vehicle University program Based on Hybrid propulsion 86
The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 82
Testing and CFD Simulation of Diaphragm Hybrid Rocket Motors 81
Optimization of a H2O2 Gas Generator for a Hybrid Rocket Engine 81
Generation and propagation of vibrations on satellite structures and planetary bodies after hypervelocity impacts 80
Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior 79
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 78
Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take Off 70
Feasibility Study for a Throttleable Hybrid Rocket Motor for Soft Landing 69
EUCLID satellite: Development of a lumped parameter model for sloshing description 69
Experimental Characterization of a Hydrogen Peroxide Simulator 65
Numerical and Experimental Activities in Support of the Development of Hybrid Rocket Engine for Soft-Landing Applications 60
Feasibility Study of Hybrid Propulsion System for Sounding Rocket Application 57
Advanced CFD Investigation for Predicting Regression Rate in Hybrid Rockets49th AIAA/ASME/SAE/ASEE Joint PropulsionConference 57
Analysis of GOCE's disturbances induced by hypervelocity impact 56
Analysis of Fluid-dynamic Systems to Increase Combustion Efficiency in Hybrid Rockets 53
Numerical and Experimental Activities in Support of the Development of Hybrid-Rocket Engine for softlanding applications 51
CFD Simulation in Support of SPARTAN Research Program 47
Feasibility Study of Hybrid Propulsion System for Sounding Rocket Application 46
CFD Simulation of Regression Rate in Hybrid Rockets 46
Testing of a Hydrogen Peroxide Simulator for a Hybrid Rocket Engine 46
Analysis of the vibration environment induced on spacecraft components by hypervelocity impact 45
Numerical Investigation of Pressure-Fed Solutions for Paraffin-Based Hybrid Rocket Motors 44
Numerical Simulations of an H2O2 Vortex Hybrid Rocket Motor 43
Development of 20 kN hybrid rocket booster 39
Totale 3.018
Categoria #
all - tutte 11.199
article - articoli 3.013
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 14.212


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020335 0 0 0 0 0 36 45 68 51 52 67 16
2020/2021540 11 16 12 79 178 31 9 42 62 14 50 36
2021/2022359 3 51 30 11 29 12 11 36 33 5 32 106
2022/2023482 78 65 16 50 86 81 0 28 42 3 26 7
2023/2024250 12 27 9 29 6 26 31 46 10 6 24 24
2024/2025355 1 80 51 54 127 42 0 0 0 0 0 0
Totale 3.018