IRIS
SAVINO, RAFFAELE
 Distribuzione geografica
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Continente #
NA - Nord America 6.053
EU - Europa 6.007
AS - Asia 3.446
SA - Sud America 218
AF - Africa 43
OC - Oceania 28
Continente sconosciuto - Info sul continente non disponibili 8
Totale 15.803
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Nazione #
US - Stati Uniti d'America 5.673
IT - Italia 2.843
SG - Singapore 1.554
HK - Hong Kong 779
CN - Cina 747
DE - Germania 563
UA - Ucraina 539
RU - Federazione Russa 427
CA - Canada 372
GB - Regno Unito 342
FI - Finlandia 333
IE - Irlanda 295
SE - Svezia 222
BR - Brasile 168
NL - Olanda 145
IN - India 108
FR - Francia 70
JP - Giappone 65
ES - Italia 59
BE - Belgio 45
AT - Austria 38
AU - Australia 26
KR - Corea 26
TW - Taiwan 26
TR - Turchia 23
CL - Cile 22
CI - Costa d'Avorio 21
VN - Vietnam 20
PT - Portogallo 18
PH - Filippine 13
RO - Romania 13
AR - Argentina 12
PK - Pakistan 12
ID - Indonesia 11
IR - Iran 11
PL - Polonia 11
CZ - Repubblica Ceca 10
EG - Egitto 10
GR - Grecia 10
IL - Israele 7
BD - Bangladesh 6
EU - Europa 6
IQ - Iraq 6
LT - Lituania 6
TH - Thailandia 6
MX - Messico 5
QA - Qatar 5
AE - Emirati Arabi Uniti 4
BG - Bulgaria 4
BO - Bolivia 4
CH - Svizzera 4
CO - Colombia 4
DZ - Algeria 4
EC - Ecuador 4
NO - Norvegia 3
UZ - Uzbekistan 3
A1 - Anonimo 2
JO - Giordania 2
KZ - Kazakistan 2
MC - Monaco 2
NZ - Nuova Zelanda 2
PY - Paraguay 2
SA - Arabia Saudita 2
TZ - Tanzania 2
ZA - Sudafrica 2
AZ - Azerbaigian 1
BN - Brunei Darussalam 1
CR - Costa Rica 1
DK - Danimarca 1
DO - Repubblica Dominicana 1
EE - Estonia 1
GA - Gabon 1
GE - Georgia 1
HU - Ungheria 1
KE - Kenya 1
KG - Kirghizistan 1
LB - Libano 1
LU - Lussemburgo 1
MA - Marocco 1
MY - Malesia 1
NP - Nepal 1
PA - Panama 1
PE - Perù 1
PS - Palestinian Territory 1
SI - Slovenia 1
SN - Senegal 1
VE - Venezuela 1
Totale 15.803
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Città #
Chandler 904
Singapore 876
Hong Kong 746
Santa Clara 557
Jacksonville 527
Naples 464
Napoli 353
Millbury 316
Princeton 274
Munich 237
Montréal 222
Nanjing 206
Ashburn 170
Boston 167
Mcallen 142
Rome 131
Wilmington 121
Ottawa 117
Woodbridge 106
Amsterdam 97
Beijing 85
Houston 80
Des Moines 75
Milan 71
Kronberg 69
Nanchang 69
Ann Arbor 67
Centro 59
Hebei 58
Seattle 53
Caserta 51
Dublin 51
Cagliari 49
Salerno 49
Norwalk 46
Boardman 44
Shenyang 43
Jiaxing 41
Turin 41
Lawrence 38
Bologna 37
Torre Annunziata 37
Helsinki 36
Pune 36
Moscow 34
Changsha 32
Lappeenranta 32
Vienna 30
Casoria 28
Tianjin 28
The Dalles 23
Santiago 21
Taranto 21
Dong Ket 20
London 20
Falkenstein 19
Kunming 19
Redwood City 18
Falls Church 17
Tokyo 17
Dallas 16
Madrid 16
Shanghai 16
Brussels 15
Stuttgart 15
Casalnuovo di Napoli 13
Buenos Aires 12
Isernia 12
Orlando 12
Pompei 12
Potenza 12
Torino 12
Fairfield 11
Giugliano in Campania 11
Leuven 11
Melbourne 11
Melito di Napoli 11
Portici 11
Sapporo 11
Chennai 10
Cologne 10
Daytona Beach 10
Guangzhou 10
Meta 10
Nuremberg 10
Salò 10
Torre del Greco 10
Aversa 9
Carinola 9
Hyderabad 9
Italy 9
Maddaloni 9
Mumbai 9
Villaricca 9
Barcelona 8
Belo Horizonte 8
Brasília 8
Chilliwack 8
Hsinchu 8
Istanbul 8
Totale 8.828
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Nome #
Aerothermal Analysis of a Sample-Return Reentry Capsule 798
Mini-IRENE: Design Of Deployable Heat Shield Capsule For A Sounding Rocket Flight Experiment 285
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization 185
FORCE: A FORmation Flying SAR Based on CubEsat Assemblies 179
The Small Mars Satellite: a European small-size Mars lander 173
Aero-thermo-chemical characterization of ultra-high-temperature ceramics for aerospace applications 132
Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles 129
Experimental Characterization of an Impulsive Hydrogen Peroxide-based Rocket for Fine Orbit Control 117
Aerodynamic Analysis of the Aerospaceplane HYPLANE in Supersonic Rarefied Flow 110
Experimental and numerical assessment of regression rate and propulsive performance of 10N-class hybrid rockets for nanosatellite maneuvering 106
Aerodynamic Control System for a Deployable Re-entry Capsule 106
Computational Fluid-dynamic Simulations of Hybrid Rocket Internal Flow Including Discharge Nozzle 102
Aerodynamic Control System for a Deployable Re-Entry Capsule 100
DSMC Aero-Thermo-Dynamic Analysis of a Deployable Capsule for Mars Entry 99
Development and flight test of a suborbital re-entry demonstrator 95
HYBRID ROCKETS WITH NOZZLE IN ULTRA-HIGH-TEMPERATURE CERAMIC COMPOSITES 94
Aerodynamic study of airframe-engine integration of a supersonic business jet 93
Mini Irene Project: Ground Demonstrator Plasma Wind Tunnel Testing 92
Aerodinamica parte I fondamenti e principi 90
IRENE - Italian re-entry nacelle for microgravity experiments 86
Aero-Thermo-Dynamic Analysis of a Low Ballistic Coefficient Deployable Capsule in Earth Re-Entry 86
Hypersonic boost-glide systems: Flight mechanics and plasma parameters evaluation through aero-thermo-chemical computational fluid dynamics 78
Adjustable aerobraking heat shield for Satellites deployment and recovery 78
CONVENZIONE NATURALE E ALLA MARANGONI IN SISTEMI LIQUIDI PARZIALMENTE MISCIBILI 76
Non-linear aero-elastic response of a multi-layer TPS 76
CHARACTERIZATION OF CARBON-FIBER REINFORCED ULTRA-HIGH-TEMPERATURE CERAMIC MATRIX COMPOSITES IN ARC-JET ENVIRONMENT 73
Analisi delle prestazioni di ugelli a spina con gas reagenti 72
Ablation tests on HfC- and TaC-based ceramics for aeropropulsive applications 71
Arc-jet wind tunnel characterization of ultra-high-temperature ceramic matrix composites 71
Heat transfer characteristics of flat plate pulsating heat pipe using self-rewetting fluids 70
Design and testing of a monopropellant thruster based on N2O decomposition in Pd/Al2O3 pellets catalytic bed 70
70 MW plasma wind tunnel up-grades for ESA Aurora TPS testing 69
Thermal performance of self-rewetting fluid heat pipe containing dilute solutions of polymer-capped silver nanoparticles synthesized by microwave-polyol process 69
Experimental characterization of a hydrogen peroxide-based thruster for small satellites 67
A benchmark study on the thermal conductivity of nanofluids 67
Spazio: oltre 50 anni di storia in Campania 67
Small Mars satellite: A low-cost system for Mars exploration 66
Design and Testing of a Paraffin-Based 1000 N HRE Breadboard 66
Assessment of a deployable aerodynamic control system for microsatellites recovery 64
Mini-IRENE: The First European Flight Experiment Of A Deployable Heat Shield 64
Visualization of liquid distribution and dry-out in a single-channel heat pipe with different wettability 64
Mixed-Compression Supersonic Intake and Engine–Airframe Integration 63
Upgrading of an Arc-heated Flow Facility for Reentry Simulation 63
Heat pipes for space applications 63
The Small Mars System 63
Aerothermal analysis of an advanced hot structure for hypersonic flight tests 62
3D Analysis of crystal/melt interface shape and Marangoni flow instability in solidifying liquid bridges 62
Thermo-chemical surface instabilities of SiC-ZrB 2 ceramics in high enthalpy dissociated supersonic airflows 62
Mini IRENE - Deployable Heat Shield For Suborbital Flight Test 62
Aero-thermo-dynamic Characterization of Large-scale Near-zero Ablation Thermal Protection Systems in Ultra-High-Temperature Ceramic Matrix Composites 62
Recent Advances in Microgravity Fluid Dynamics 61
Heat transfer fluids 61
Experimental and numerical simulation, by an arc-jet facility, of hypersonic flow in Titan's atmosphere 61
Aerothermodynamic and system analysis of a small hypersonic airplane (Hyplane) 61
The interaction between drops and solidification front in presence of Marangoni effect 60
Combined surface tension and buoyancy driven convection around a bubble on a heated surface 60
A study of a high lift wing-body configuration for low earth orbit re-entry. 60
Aerothermodynamic and stability analyses of a deployable re-entry capsule 60
Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer 60
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket 60
Planetary entry simulation 58
Preliminary results of the sounding rocket experiment on oscillatory Marangoni flows in liquid bridge 58
Self-rewetting heat transfer fluids and nano-brines for space heat pipes 58
Transient Computational Thermofluid-Dynamic Simulation of Hybrid Rocket Internal Ballistics 58
Design and testing of a paraffin-based hybrid rocket demonstrator 58
Buoyancy and Marangoni effects in an evaporating drop 58
Preliminary design and study of 5N HTP monopropellant thruster for small satellites 57
Influenza dell'effetto Marangoni sull'efficienza di heat pipes per applicazioni spaziali 57
Studio aerotermodinamico di sistemi di protezione termica innovativi per velivoli ipersonici 56
A study on self-rewetting fluids for heat transfer in microgravity 56
Surface tension-driven flows and applications 56
Analisi sperimentale su materiale composito paravampe Teseo/Milas-Fremm 56
Rarefied aerodynamics of a deployable re-entry capsule 56
Effect of hypersonic flow chemical composition on the oxidation behavior of a super-strong UHTC 56
MODELLING OF PARAFFIN-BASED FUEL COMBUSTION IN HYBRID ROCKETS 56
Compatibility of the microgravity environment of the International Space Station with Fluid and Material Science experimentation 55
Computational Fluid-Dynamic Simulations of the Internal Ballistics of Hybrid Rocket Burning Paraffin-based Fuel 55
Transient Marangoni convection in hanging evaporating drops 54
Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment 54
Innovative heat pipes with self-rewetting fluids under normal and reduced gravity conditions 53
Conceptual design of de-orbit and re-entry modules for standard CubeSats 53
Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment 53
The Ghibli plasma wind tunnel: description of the new CIRA PWT facility 52
Aerothermodynamic Study of an Advanced Thermal Protection System 52
Heat transfer in ultra-high temperature advanced ceramics under high enthalpy arc-jet conditions 52
Recent development on heat pipes for ground and space applications 52
Recent advancements in experimental and numerical characterization of paraffin-based fuels for hybrid rocket application 52
Ultra-High-Temperature Testing of Sintered ZrB2-based Ceramic Composites in Atmospheric Re-entry Environment 52
Improved aero-thermal resistance capabilities of ZrB2-based ceramics in hypersonic environment for increasing SiC content 52
Self-consistent surface-temperature boundary condition for iquefying-fuel-based hybrid rockets internal-ballistics simulation 52
Compatibility of the microgravity environment of the international space station with fluid and material science experimentation 51
Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles 50
The Fluid-dynamic disturbances induced on the ISS based on the first acceleration measurements on board the Space Station 50
Numerical and experimental analysis of surface catalycity effects for Martian atmosphere entry 50
Preliminary Validation of Fluid-Structure Interaction Modeling for Hypersonic Deployable Re-Entry Systems 50
Experimental investigation of N2O decomposition with pd∕al2 o3 cylindrical pellets catalyst 50
Aerodynamic analysis of a flap-based deployable re-entry system in different flight conditions 49
The Importance of an accurate knowledge of the Microgravity environment for potential ISS users 49
The Fluid-dynamic disturbances induced on the ISS based on the first acceleration measurements on board the Space Station 49
Dissolution and solutal convection in partially miscible liquid systems 49
Totale 7.965
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Categoria #
all - tutte 60.462
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 60.462
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020470 0 0 0 0 0 0 0 0 0 124 159 187
2020/20211.494 43 115 185 143 129 193 131 43 222 84 160 46
2021/20221.737 53 22 19 47 27 66 40 82 298 94 242 747
2022/20232.207 353 179 96 235 240 262 37 207 254 115 174 55
2023/20242.027 104 224 112 133 126 172 107 254 66 169 373 187
2024/20254.667 488 663 94 117 379 443 786 568 899 230 0 0
Totale 16.313