BETTELLA, ALBERTO
 Distribuzione geografica
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Continente #
NA - Nord America 2.106
EU - Europa 306
AS - Asia 219
OC - Oceania 2
SA - Sud America 1
Totale 2.634
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Nazione #
US - Stati Uniti d'America 2.101
CN - Cina 146
DE - Germania 74
FI - Finlandia 67
IT - Italia 62
GB - Regno Unito 30
SG - Singapore 26
SE - Svezia 22
UA - Ucraina 22
IN - India 20
VN - Vietnam 14
IE - Irlanda 10
ES - Italia 7
CA - Canada 5
FR - Francia 5
AE - Emirati Arabi Uniti 4
AT - Austria 3
AU - Australia 2
BE - Belgio 2
HK - Hong Kong 2
IQ - Iraq 2
TR - Turchia 2
CH - Svizzera 1
CL - Cile 1
KR - Corea 1
MY - Malesia 1
NL - Olanda 1
TW - Taiwan 1
Totale 2.634
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Città #
Fairfield 316
Chandler 267
Woodbridge 198
Ashburn 169
Ann Arbor 162
Houston 138
Seattle 136
Wilmington 131
Cambridge 102
Jacksonville 55
Beijing 51
Princeton 41
Medford 37
Roxbury 34
Nanjing 31
Helsinki 29
Boardman 28
Des Moines 25
New York 20
San Diego 19
Singapore 17
Dong Ket 14
Padova 13
Redwood City 12
Shenyang 12
Dublin 10
Hebei 9
Nanchang 9
Bonndorf 6
Cagliari 6
Norwalk 5
Rome 5
Abu Dhabi 4
Chennai 4
Kharkiv 4
Kunming 4
London 4
Madrid 4
Nürnberg 4
Xi'an 4
Bengaluru 3
Calgary 3
Changsha 3
Cranfield 3
Guangzhou 3
Hangzhou 3
Jiaxing 3
Jinan 3
Munich 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
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
Dallas 1
Falls Church 1
Flavin 1
Gaiarine 1
Gunzenhausen 1
Hounslow 1
Islington 1
Lendinara 1
Longare 1
Melbourne 1
Milan 1
Montreal 1
Mountain View 1
Naples 1
Pasadena 1
Perth 1
Purcellville 1
Sankt Augustin 1
Seoul 1
Stuttgart 1
Tianjin 1
Torino 1
Totale 2.239
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Nome #
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 171
Hypervelocity experiments of impact cratering and catastrophic disruption of targets representative of minor bodies of the Solar System 115
Analysis of transient vibrations on complex targets representing elementary configurations of GOCE satellite 108
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 97
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 95
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets 93
Selecting materials to protect inflatable structures from the space environment 89
Computational Fluid Dynamics Simulation of Regression Rate in Hybrid Rockets 89
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 89
Numerical Modeling of Paraffin-Based Fuels Behavior 88
SPONGE: a Sounding Rocket Experiment for PMDs 85
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 85
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 85
Testing and CFD Simulation of Diaphragm Hybrid Rocket Motors 76
Mini launcher vehicle University program Based on Hybrid propulsion 74
Optimization of a H2O2 Gas Generator for a Hybrid Rocket Engine 74
Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior 73
The "Vortex Reloaded" project: experimental investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 72
EUCLID satellite: Sloshing model development through computational fluid dynamics 71
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 70
Feasibility Study for a Throttleable Hybrid Rocket Motor for Soft Landing 61
EUCLID satellite: Development of a lumped parameter model for sloshing description 60
Experimental Characterization of a Hydrogen Peroxide Simulator 58
Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take Off 57
Generation and propagation of vibrations on satellite structures and planetary bodies after hypervelocity impacts 54
Numerical and Experimental Activities in Support of the Development of Hybrid Rocket Engine for Soft-Landing Applications 53
Feasibility Study of Hybrid Propulsion System for Sounding Rocket Application 49
Analysis of GOCE's disturbances induced by hypervelocity impact 47
Advanced CFD Investigation for Predicting Regression Rate in Hybrid Rockets49th AIAA/ASME/SAE/ASEE Joint PropulsionConference 46
Analysis of Fluid-dynamic Systems to Increase Combustion Efficiency in Hybrid Rockets 42
Numerical Investigation of Pressure-Fed Solutions for Paraffin-Based Hybrid Rocket Motors 40
CFD Simulation in Support of SPARTAN Research Program 39
Testing of a Hydrogen Peroxide Simulator for a Hybrid Rocket Engine 39
Analysis of the vibration environment induced on spacecraft components by hypervelocity impact 38
Feasibility Study of Hybrid Propulsion System for Sounding Rocket Application 37
Numerical Simulations of an H2O2 Vortex Hybrid Rocket Motor 37
Numerical and Experimental Activities in Support of the Development of Hybrid-Rocket Engine for softlanding applications 37
CFD Simulation of Regression Rate in Hybrid Rockets 36
Development of 20 kN hybrid rocket booster 28
Totale 2.657
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Categoria #
all - tutte 9.155
article - articoli 2.564
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 11.719
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/201949 0 0 0 0 0 0 0 0 0 0 0 49
2019/2020540 85 15 8 33 64 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
2023/2024244 12 27 9 29 6 26 31 46 10 6 24 18
Totale 2.657