GALFETTI, LUCIANO
 Distribuzione geografica
Continente #
NA - Nord America 14.895
EU - Europa 11.922
AS - Asia 6.968
SA - Sud America 1.201
AF - Africa 383
OC - Oceania 53
Continente sconosciuto - Info sul continente non disponibili 6
Totale 35.428
Nazione #
US - Stati Uniti d'America 14.494
RU - Federazione Russa 4.289
IT - Italia 3.450
CN - Cina 2.016
SG - Singapore 1.978
BR - Brasile 1.028
VN - Vietnam 1.000
UA - Ucraina 614
DE - Germania 610
FR - Francia 540
SE - Svezia 537
KR - Corea 425
FI - Finlandia 385
GB - Regno Unito 362
CA - Canada 312
IN - India 295
ES - Italia 249
JP - Giappone 211
IE - Irlanda 208
NL - Olanda 178
AT - Austria 152
MA - Marocco 145
HK - Hong Kong 128
TR - Turchia 122
JO - Giordania 115
CI - Costa d'Avorio 107
CH - Svizzera 92
ID - Indonesia 83
BD - Bangladesh 80
PH - Filippine 79
PL - Polonia 72
BE - Belgio 70
IR - Iran 66
TW - Taiwan 66
AR - Argentina 54
MX - Messico 51
IQ - Iraq 47
PK - Pakistan 44
ZA - Sudafrica 40
EC - Ecuador 33
AE - Emirati Arabi Uniti 28
AU - Australia 28
SA - Arabia Saudita 28
NZ - Nuova Zelanda 25
CO - Colombia 23
GR - Grecia 22
KZ - Kazakistan 21
TH - Thailandia 21
IL - Israele 19
KE - Kenya 19
DZ - Algeria 17
EG - Egitto 17
VE - Venezuela 17
UZ - Uzbekistan 15
CL - Cile 14
MY - Malesia 14
PT - Portogallo 14
PY - Paraguay 11
RO - Romania 11
AZ - Azerbaigian 10
DO - Repubblica Dominicana 10
HU - Ungheria 10
NP - Nepal 10
TN - Tunisia 9
BO - Bolivia 8
CZ - Repubblica Ceca 8
LT - Lituania 8
TT - Trinidad e Tobago 8
BG - Bulgaria 7
NG - Nigeria 7
PE - Perù 7
OM - Oman 6
CR - Costa Rica 5
DK - Danimarca 5
EU - Europa 5
LV - Lettonia 5
SY - Repubblica araba siriana 5
UY - Uruguay 5
AL - Albania 4
ET - Etiopia 4
KG - Kirghizistan 4
MU - Mauritius 4
QA - Qatar 4
RS - Serbia 4
AO - Angola 3
BH - Bahrain 3
EE - Estonia 3
GE - Georgia 3
HN - Honduras 3
LB - Libano 3
LK - Sri Lanka 3
PS - Palestinian Territory 3
SN - Senegal 3
BB - Barbados 2
BW - Botswana 2
BZ - Belize 2
GA - Gabon 2
IS - Islanda 2
KW - Kuwait 2
LA - Repubblica Popolare Democratica del Laos 2
Totale 35.394
Città #
Ashburn 1.783
San Jose 1.184
Milan 1.141
Singapore 1.074
Fairfield 992
Woodbridge 953
Chandler 831
Wilmington 641
Houston 589
Santa Clara 587
Ann Arbor 577
Moscow 564
Seattle 438
Cambridge 363
Council Bluffs 353
Jacksonville 351
Hefei 346
Beijing 335
Seoul 333
The Dalles 329
Dallas 291
Dearborn 253
Boardman 250
Lawrence 226
Dong Ket 225
Medford 221
Ottawa 215
Málaga 207
Lauterbourg 201
Dublin 200
Helsinki 186
Ho Chi Minh City 183
Los Angeles 177
Tokyo 177
North Charleston 161
Hanoi 140
Vienna 136
Redwood City 126
Buffalo 116
Amman 114
New York 114
Abidjan 107
Rome 104
Hong Kong 95
Kenitra 92
São Paulo 74
Des Moines 71
Shanghai 71
Bern 68
Frankfurt am Main 68
Marnate 65
Orem 64
Bovisio Masciago 63
Segrate 62
Redmond 59
Jakarta 58
Ciampino 56
Taipei 53
Brussels 52
Guangzhou 51
Amsterdam 49
Mumbai 49
Davao City 47
Warsaw 46
San Diego 45
Istanbul 40
Las Vegas 40
Zhengzhou 40
Norwalk 38
Casablanca 37
Chicago 36
London 35
Monza 35
Phoenix 35
Chennai 34
Nanjing 34
Stockholm 32
Washington 32
Basingstoke 31
Giussano 31
Hangzhou 31
Rio de Janeiro 29
Da Nang 28
Rho 28
Changsha 27
Denver 27
Mountain View 26
Montreal 25
Belo Horizonte 24
West Lafayette 23
Xian 23
Gavirate 22
Johannesburg 22
Brooklyn 21
Falkenstein 20
Toronto 20
Ankara 19
Haiphong 18
Kunming 18
Trezzano Sul Naviglio 18
Totale 20.251
Nome #
Advanced Hybrid Solid Fuels 438
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 333
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 297
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 296
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 292
Combustion Processes in Hybrid Rockets 289
A method for mechanical activation of powders by means of balls 287
Iron oxide as solid propellant catalyst: A detailed characterization 282
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 281
Aerospace Propulsion Research Activities at SPlab. Overview and Results 280
Burning Behavior Investigation of a Vortex Flow Pancake Hybrid Rocket Engine 273
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 268
Preliminary kinetic characterization of lithium-aluminum based hydrides for airbreathing propulsion 265
Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-Based Formulations 263
Paraffin-based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization 258
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 257
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization 254
Aluminum Particle Size Influence on Ignition and Combustion of AP/HTPB/Al Solid Rocket Propellants 253
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications 253
Development of an intrusive technique for particles collection in rockets plume 251
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization 249
Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation 248
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 235
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 235
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 234
A Wide Characterization of Paraffin-based Fuels Mixed with Styrene-based Thermoplastic Polymers for Hybrid Propulsion 232
Detailed Properties of Iron Oxide Solid Propellant Catalyst 231
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 228
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 227
A Parametric Study of the Effect of Liquid Fuel Entrainment on the Combustion Characteristics of a Paraffin-Based Hybrid Rocket Motor 222
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 221
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 220
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 219
Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine 218
Trade-Off Analysis of a New Liquid Rocket Engine 216
Nano-Aluminum as Energetic Material for Rocket Propellants 214
Numerical Simulation of HTPB Combustion in a 2D Hybrid Slab Combustor 206
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 204
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 202
Efficient Solid Rocket Propulsion for Access to Space 201
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 200
2D Numerical Simulation of Combustion Processes in a Slab Hybrid Rocket Motor 199
An Italian Network to Improve Hybrid Rocket Performance: Strategy and Results 199
Microstructure Effects in Aluminized Solid Rocket Propellants 198
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 198
Time-resolved burning of solid fuels for hybrid rocket propulsion 195
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization 195
Towards High-Performing Paraffin-Based Fuels Exploiting the Armored Grain Concept 194
Experimental Investigation of Solid Fuels for Hybrid Rocket Propulsion 193
Aging Effects on Nano-Sized Aluminum Reactivity 193
Physical and Ballistic Characterization of AlH3-Based Space Propellants 191
Experimental Investigations on Transient Burning of Nano-Aluminized Solid Rocket Propellants 187
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 187
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Conceptual and Detailed Design 187
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 187
An experimental investigation of convective heat transfer at evaporation of kerosene and water in the closed volume 186
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 186
Regression Rate and Combustion Efficiency in a Vortex-Flow Hybrid Rocket Engine 185
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 184
Experimental Investigation of the Condensed Combustion Products of Micro Aluminized Solid Rocket Propellants 183
Paraffin-Based Fuels For Hybrid Propulsion: Characterization Of Waxes And Its Blends 183
Aging of ADN Rocket Propellant Formulations with Desmophen-Based Elastomer Binder 183
Overview of a supersonic probe for solid propellant rocket CCP collection 183
A Wide Characterization of Aluminum Powders for Propellants 182
Actualization of an efficient throttleable laser propulsion mode 182
Flame Surface Modification of Polyethylene Sheets 181
Characterization of ADN/GAP-Based and ADN/Desmophen-Based Propellant Formulations and Comparison with AP Analogues 179
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 179
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Application of Quasi-1D Engineering Model and 2D Axisymmetric CFD 179
Experimental Investigation and Numerical Modeling of the Condensed Combustion Products of Micro and Nano-Aluminized Solid Propellants 178
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine 177
Mechanical Characterization of Composite Solid Propellants 177
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 177
Paraffin-Based Solid Fuels for Hybrid Propulsion Filled with Lithium Aluminum Hydride: Thermal, Mechanical and Ballistic Characterization 173
Hydrogen Generation from Aluminum Composites Hydrolysis for Space Propulsion 171
An Hybrid Microcombustor for Regression Rate Measurements 171
Aging of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements 171
Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain 171
A Global Characterization of Nano-Aluminized Propellants 169
Ageing of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements, Sol-Gel and GPC Analysis 169
Pure Paraffin Waxes Analysis for Hybrid Rocket Solid Fuels: Rheological, Thermal and Mechanical Characterization 169
Flame Surface Modification of Polyethylene Sheets 168
Advanced Hybrid Propellant for a Moon Orbiter Thruster 168
Nanoaluminum as a Solid Propellant Fuel 168
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 168
Nano-Composites for Rocket Solid Propellants 166
Simulation Code for Hybrid Rocket Combustion 165
Effect of mechanical activation on the reactivity of composites for flameless heaters 165
Experimental Visualizations of Entrainment Phenomena in Wax-Based Fuels for Hybrid Space Propulsion 163
Advances in Hybrid Propulsion 162
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 162
Ballistics and Condensed Residues of Aluminized Solid Rocket Propellants 161
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 160
Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 159
PDL of Micro and Nanoaluminized Laboratory Propellants for Space Applications 158
Nanoparticles for Solid Rocket Propulsion 158
Ballistic Properties of Nano-Aluminized High-Energy Materials (HEM) 157
Experimental Laboratory Characterization of Charring Thermal Insulators 157
Ageing Behaviour of Composite Rocket Propellant Formulations Investigated by DMA, SGA, and GPC 157
Vortex combustion in a hybrid rocket motor 157
Totale 20.742
Categoria #
all - tutte 90.839
article - articoli 17.904
book - libri 0
conference - conferenze 66.654
curatela - curatele 618
other - altro 0
patent - brevetti 1.248
selected - selezionate 0
volume - volumi 4.415
Totale 181.678


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021861 0 0 0 0 0 0 0 0 0 236 140 485
2021/20222.075 113 249 131 107 322 118 126 139 74 137 196 363
2022/20232.627 348 257 120 164 244 258 45 170 394 285 155 187
2023/20241.415 92 214 63 125 103 218 154 78 24 129 59 156
2024/20254.758 112 102 156 118 984 275 169 463 598 256 635 890
2025/202613.403 2.850 2.417 780 957 707 776 2.108 821 670 1.317 0 0
Totale 35.644