MUNGIGUERRA, STEFANO
 Distribuzione geografica
Continente #
EU - Europa 838
NA - Nord America 681
AS - Asia 124
OC - Oceania 4
SA - Sud America 4
Continente sconosciuto - Info sul continente non disponibili 1
Totale 1652
Nazione #
US - Stati Uniti d'America 630
IT - Italia 549
CN - Cina 86
GB - Regno Unito 71
DE - Germania 69
CA - Canada 51
UA - Ucraina 40
AT - Austria 25
BE - Belgio 16
IN - India 16
IE - Irlanda 14
NL - Olanda 11
FR - Francia 9
PT - Portogallo 8
RO - Romania 6
AU - Australia 4
HK - Hong Kong 4
IL - Israele 4
JP - Giappone 4
PL - Polonia 4
SE - Svezia 4
CL - Cile 3
CZ - Repubblica Ceca 3
ES - Italia 3
TR - Turchia 3
TW - Taiwan 3
GR - Grecia 2
IR - Iran 2
AE - Emirati Arabi Uniti 1
CO - Colombia 1
EU - Europa 1
FI - Finlandia 1
LB - Libano 1
MC - Monaco 1
RU - Federazione Russa 1
SI - Slovenia 1
Totale 1652
Città #
Chandler 155
Napoli 70
Naples 54
Munich 53
Mcallen 49
Montréal 42
Beijing 34
Millbury 31
Des Moines 28
Lawrence 28
Vienna 25
Boston 24
Centro 24
Rome 21
Milan 16
Nanjing 16
Torre Annunziata 16
Wilmington 15
Woodbridge 13
Caserta 10
Salò 10
Fairfield 9
Princeton 9
Ottawa 8
Qualiano 8
Redwood City 8
Ashburn 7
Daytona Beach 7
Villaricca 7
Amsterdam 6
Carinola 6
Changsha 6
Leuven 6
Norwalk 6
Orlando 6
Portici 6
Salerno 6
Brussels 5
Cagliari 5
Chennai 5
Frattamaggiore 5
Hebei 5
Huntsville 5
Lecce 5
Leverano 5
Montecorvino Rovella 5
Mumbai 5
Pompei 5
Potenza 5
Corsico 4
Enschede 4
Houston 4
Mugnano Di Napoli 4
Nanchang 4
Padova 4
Redmond 4
Sant'Antimo 4
Wanchai 4
Avella 3
Aversa 3
Bologna 3
Darmstadt 3
Dearborn 3
Guangzhou 3
Kingston 3
London 3
Pago Veiano 3
Ponzano Veneto 3
Pozzuoli 3
Prague 3
Santiago 3
Taipei 3
Turin 3
Agropoli 2
Altamura 2
Barcelona 2
Barlassina 2
Baudour 2
Casavatore 2
Castellammare Di Stabia 2
Cervia 2
Desio 2
Dublin 2
Foshan 2
Hefei 2
Hertford 2
Italy 2
Izmir 2
Jacksonville 2
Jiaxing 2
Karaj 2
Lod 2
Lymington 2
Melito Di Napoli 2
Odessa 2
Palermo 2
Palo Alto 2
Phoenix 2
San Jose 2
Saviano 2
Totale 1040
Nome #
Computational Evaluation of Aero-Thermo-Dynamic Loads and Effect of Catalyticity in an Arc-Jet Wind Tunnel 218
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 165
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 139
Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications 96
Computational Fluid-dynamic Simulations of Hybrid Rocket Internal Flow Including Discharge Nozzle 73
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 62
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 44
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed 44
Experimental Investigation of Capillary-Driven Two-Phase Flow in Water/Butanol under Reduced Gravity Conditions 40
Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles 39
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 38
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 38
Aerodynamic study of airframe-engine integration of a supersonic business jet 37
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 37
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 35
Aero-thermo-dynamic Characterization of Large-scale Near-zero Ablation Thermal Protection Systems in Ultra-High-Temperature Ceramic Matrix Composites 34
Rarefied aerodynamics of a deployable re-entry capsule 33
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 33
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 33
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 33
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 31
Improved aero-thermal resistance capabilities of ZrB2-based ceramics in hypersonic environment for increasing SiC content 31
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 27
The application of computational thermo-fluid-dynamics to the simulation of hybrid rocket internal ballistics with classical or liquefying fuels: A review 26
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake 25
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 24
Design and testing of a paraffin-based hybrid rocket demonstrator 24
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 23
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 22
An Improvement of the Gas-surface Interaction and Entrainment Models for Paraffin-based Fuels in Hybrid Rocket Engines 22
Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment 21
Effect of PAN-based and pitch-based carbon fibres on microstructure and properties of continuous Cf/ZrB2-SiC UHTCMCs 21
Characterization of novel ceramic composites for rocket nozzles in high-temperature harsh environments 21
Self-ReWetting capillary flow under evaporation and condensation processes in parabolic flight conditions 20
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 20
Testing ultra-high -temperature ceramics for thermal protection and rocket applications 19
Testing 1kN Paraffin-Based Hybrid Rocket Engine 19
Development and flight test of a suborbital re-entry demonstrator 17
Assessment of a deployable aerodynamic control system for microsatellites recovery 17
Study on Aerodynamic Stability of a Deployable Aerobraking Re-entry Capsule 13
New Entrainment Model for Modelling the Regression Rate in Hybrid Rocket Engines 13
Testing and Characterization of Near-Zero-Ablation Fibre-reinforced Ultra High Temperature Ceramics for Aerospace 11
Qualification and reusability of long and short fibre-reinforced ultra-refractory composites for aerospace thermal protection systems 11
A new firing test campaign on the 1000 N thrust-class Hyprob hybrid rocket engine 9
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 8
Aerodynamics and flight mechanics activities for a suborbital flight test of a deployable heat shield capsule 6
Compositionally complex catalytic oxide beds free of noble metals for H2O2 fuelled monopropellant thrusters 1
Totale 1773
Categoria #
all - tutte 3411
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 3411


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2017/20186 0000 00 00 0006
2018/2019108 9643 819 325 19120
2019/2020442 52337 698 5346 34645818
2020/2021275 1793227 1129 1215 5047206
2021/2022343 1661220 224 922 39227695
2022/2023554 39452226 6972 2668 7519867
Totale 1773