FAENZA, MARTINA
 Distribuzione geografica
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Continente #
NA - Nord America 1.177
EU - Europa 164
AS - Asia 107
Totale 1.448
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Nazione #
US - Stati Uniti d'America 1.169
CN - Cina 68
DE - Germania 55
FI - Finlandia 31
IT - Italia 27
GB - Regno Unito 20
VN - Vietnam 14
IN - India 10
SE - Svezia 10
IE - Irlanda 8
CA - Canada 7
FR - Francia 7
KR - Corea 5
UA - Ucraina 4
QA - Qatar 3
TR - Turchia 3
AE - Emirati Arabi Uniti 2
CZ - Repubblica Ceca 1
MX - Messico 1
NL - Olanda 1
SG - Singapore 1
TW - Taiwan 1
Totale 1.448
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Città #
Fairfield 188
Chandler 158
Ashburn 127
Woodbridge 105
Houston 86
Seattle 84
Wilmington 72
Cambridge 67
Ann Arbor 61
Beijing 24
Medford 21
Princeton 21
Des Moines 20
Roxbury 17
Nanjing 16
Boardman 14
Dong Ket 14
New York 14
Helsinki 11
San Diego 11
Dublin 8
Cagliari 6
Ottawa 5
Chennai 4
Hebei 4
Norwalk 4
Rome 4
Shenyang 4
Xi'an 4
Bonndorf 3
Doha 3
London 3
Munich 3
Nanchang 3
Nürnberg 3
Seoul 3
Abu Dhabi 2
Ascot 2
Borås 2
Bremen 2
Changsha 2
Gwanak-gu 2
Hamburg 2
Jacksonville 2
Padova 2
Redwood City 2
Samsun 2
Shanghai 2
Aprilia 1
Atlanta 1
Flavin 1
Hefei 1
Hounslow 1
Jiaxing 1
Jinan 1
Kunming 1
Lendinara 1
Pasadena 1
Pune 1
San Donato Milanese 1
Sankt Augustin 1
Stuttgart 1
Tappahannock 1
Tianjin 1
Toulouse 1
Victoria 1
Weston-super-Mare 1
Wuhan 1
Zapopan 1
Totale 1.240
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Nome #
The "Vortex Reloaded" project: numerical investigation on fully tangential vortex injection in N2O - paraffin hybrid motors 171
Numerical and Experimental Investigation on Vortex Injection in Hybrid Rocket Motors 96
CFD Simulation of a Hybrid Rocket Motor with Liquid Injection 95
A numerical model to analyze the transient behavior and instabilities on hybrid rocket motors 88
Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors 85
Numerical Investigation of Hybrid Motors for the EU FP7 SPARTAN Program 84
Low Power RF Plasma Thruster Experimental Characterization 83
Optimization of a H2O2 Gas Generator for a Hybrid Rocket Engine 73
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 71
Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines 69
Feasibility Study for a Throttleable Hybrid Rocket Motor for Soft Landing 59
Experimental Characterization of a Hydrogen Peroxide Simulator 57
Numerical and Experimental Characterization of Throttleable Hybrid Propulsion Systems. Caratterizzazione Numerica e Sperimentale di Sistemi Propulsivi Ibridi a Spinta Variabile 57
Numerical and Experimental Activities in Support of the Development of Hybrid Rocket Engine for Soft-Landing Applications 52
Feasibility Study for Throttleable Hybrid Rocket Motor for Soft Landing 47
Advanced CFD Investigation for Predicting Regression Rate in Hybrid Rockets49th AIAA/ASME/SAE/ASEE Joint PropulsionConference 45
Analysis of Fluid-dynamic Systems to Increase Combustion Efficiency in Hybrid Rockets 42
Testing of a Hydrogen Peroxide Simulator for a Hybrid Rocket Engine 38
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
Totale 1.459
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Categoria #
all - tutte 4.799
article - articoli 628
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 5.427
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019113 0 0 0 0 0 0 0 0 0 24 50 39
2019/2020292 48 13 5 15 32 18 24 38 29 23 43 4
2020/2021334 7 7 10 45 149 5 5 18 33 8 24 23
2021/2022192 1 16 14 6 19 5 2 20 23 2 17 67
2022/2023277 47 43 8 27 45 47 1 19 18 3 12 7
2023/2024126 7 10 5 16 2 19 14 53 0 0 0 0
Totale 1.459