DE LUCA, LUIGI
 Distribuzione geografica
Continente #
NA - Nord America 20.063
EU - Europa 12.049
AS - Asia 7.879
SA - Sud America 1.456
AF - Africa 324
Continente sconosciuto - Info sul continente non disponibili 187
OC - Oceania 38
Totale 41.996
Nazione #
US - Stati Uniti d'America 19.447
RU - Federazione Russa 3.819
IT - Italia 2.780
SG - Singapore 2.454
CN - Cina 2.367
BR - Brasile 1.258
VN - Vietnam 1.206
UA - Ucraina 1.078
DE - Germania 814
SE - Svezia 733
FR - Francia 596
GB - Regno Unito 551
FI - Finlandia 528
CA - Canada 452
KR - Corea 420
IN - India 312
ES - Italia 239
IE - Irlanda 232
NL - Olanda 227
JP - Giappone 189
AT - Austria 162
MA - Marocco 122
TR - Turchia 111
JO - Giordania 106
HK - Hong Kong 98
BD - Bangladesh 86
AR - Argentina 79
IR - Iran 78
CI - Costa d'Avorio 74
PL - Polonia 71
MX - Messico 56
PK - Pakistan 56
BE - Belgio 55
IQ - Iraq 54
ZA - Sudafrica 41
GR - Grecia 40
ID - Indonesia 40
TW - Taiwan 35
IL - Israele 34
EC - Ecuador 33
SA - Arabia Saudita 31
CH - Svizzera 30
UZ - Uzbekistan 26
AE - Emirati Arabi Uniti 25
PH - Filippine 22
JM - Giamaica 21
NZ - Nuova Zelanda 20
CR - Costa Rica 19
MY - Malesia 19
KE - Kenya 18
AU - Australia 17
CO - Colombia 17
KZ - Kazakistan 17
PT - Portogallo 17
PY - Paraguay 17
TH - Thailandia 17
RO - Romania 16
TT - Trinidad e Tobago 16
VE - Venezuela 16
DZ - Algeria 15
PE - Perù 15
EG - Egitto 14
AZ - Azerbaigian 13
EU - Europa 12
NP - Nepal 12
DO - Repubblica Dominicana 10
LB - Libano 10
NI - Nicaragua 9
CL - Cile 8
KG - Kirghizistan 8
MU - Mauritius 8
NG - Nigeria 8
BO - Bolivia 7
ET - Etiopia 7
GT - Guatemala 7
HN - Honduras 7
LT - Lituania 7
TN - Tunisia 7
LV - Lettonia 6
SV - El Salvador 6
UY - Uruguay 6
CZ - Repubblica Ceca 5
EE - Estonia 5
OM - Oman 5
BB - Barbados 4
BY - Bielorussia 4
DK - Danimarca 4
HU - Ungheria 4
LK - Sri Lanka 4
RS - Serbia 4
SI - Slovenia 4
SN - Senegal 4
SY - Repubblica araba siriana 4
AL - Albania 3
BH - Bahrain 3
GE - Georgia 3
NO - Norvegia 3
AO - Angola 2
BG - Bulgaria 2
GA - Gabon 2
Totale 41.785
Città #
Ashburn 1.958
San Jose 1.489
Fairfield 1.349
Woodbridge 1.312
Singapore 1.244
Chandler 1.226
Milan 906
Ann Arbor 885
Wilmington 848
Houston 739
Santa Clara 681
Jacksonville 639
Council Bluffs 597
Seattle 550
Cambridge 501
Moscow 470
The Dalles 468
Hefei 456
Dearborn 430
Boardman 401
Beijing 380
Dallas 372
Seoul 327
Lawrence 302
Ottawa 290
Dong Ket 282
Medford 271
Lauterbourg 263
North Charleston 261
Los Angeles 240
Dublin 223
Helsinki 214
Málaga 207
Ho Chi Minh City 206
Hanoi 194
Rome 177
Tokyo 160
Vienna 147
New York 130
Buffalo 122
Des Moines 107
Amman 105
São Paulo 91
Orem 80
Abidjan 74
Hong Kong 71
Las Vegas 71
Redwood City 68
San Diego 67
Washington 67
Amsterdam 64
Giussano 60
London 59
Shanghai 59
Casablanca 57
Chennai 57
Kenitra 53
Brussels 52
Mumbai 52
Frankfurt am Main 50
Guangzhou 50
Bovisio Masciago 49
Norwalk 46
Warsaw 45
Munich 44
Chicago 42
Nanjing 39
Rio de Janeiro 38
Denver 36
Atlanta 35
Naples 34
Verona 34
Phoenix 33
Bologna 32
Ankara 30
Da Nang 30
Princeton 30
Tianjin 30
Turin 30
Belo Horizonte 29
São José dos Campos 29
West Lafayette 29
Mcallen 28
North York 27
Shenzhen 27
Changsha 26
Johannesburg 26
Riverside 26
Brooklyn 25
Montreal 25
Tashkent 25
Auburn Hills 24
Haiphong 24
Hangzhou 24
San Francisco 24
Zhengzhou 24
Taipei 22
Columbus 21
Palermo 21
Segrate 21
Totale 24.515
Nome #
Advanced Hybrid Solid Fuels 454
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 329
Activated Aluminum Powders for Space Propulsion 306
Adiabatic Pyrolysis of Solid Propellants 302
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 300
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 297
Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation 279
Fracture Mechanics of Composite Solid Rocket Propellant Grains: Material Testing 261
Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants 250
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 240
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 238
Intrinsic Burning Stability of Solid Propellants with Variable Thermal Properties 237
Combustion of Metal Agglomerates in a Solid Rocket Core Flow 234
Active Debris Multi-Removal Mission Concept Based on Hybrid Propulsion 233
Active Space Debris Removal by a Hybrid Propulsion Module 232
Evaluation of paraffin-based fuels for hybrid rocket engines 232
Nano-Aluminum as Energetic Material for Rocket Propellants 228
Analysis of Quasi-Steady and Transient Burning of Hybrid Fuels in a Laboratory-Scale Burner by an Optical Technique 223
Burning Rate Measurements on Damaged Propellant Samples Under Mechanical Loads 217
Microstructure Effects in Aluminized Solid Rocket Propellants 215
Efficient Solid Rocket Propulsion for Access to Space 212
Burn-Rate Measurement on Small-Scale Rocket Motors 210
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 210
Viscosity and regression rate of liquefying hybrid rocket fuels 209
Dynamic Effects on Ignitability Limits of Solid PropellantsSubjected to Radiative Heating 207
Aluminized Gels or Clouds for Low Trust Applications 203
Physical and Ballistic Characterization of AlH3-Based Space Propellants 202
Nonsteady Burning and Combustion Stability of Solid Propellants 201
Feasibility Study of Paraffin-Based Fuels for Hybrid Rocket Engine Applications 201
Time-resolved burning of solid fuels for hybrid rocket propulsion 200
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 198
Experimental Investigations on Transient Burning of Nano-Aluminized Solid Rocket Propellants 197
Combustion of Metal Agglomerates in Solid Rocket Core Flow 197
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 196
A Wide Characterization of Aluminum Powders for Propellants 195
Agglomeration of Aluminized Solid Rocket Propellants 195
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 195
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner 193
Mechanical Characterization of Composite Solid Propellants 190
Micro and Nano-Sized Metal Additives for Solid Fuels in Hybrid Rocket Lab-Scale Burner 190
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons 190
Experimental Investigation of the Condensed Combustion Products of Micro Aluminized Solid Rocket Propellants 188
Measuring Thermodynamic Properties of Burning Propellants 187
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 187
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 187
A Global Characterization of Nano-Aluminized Propellants 186
Agglomeration and Pocket Structures in Composite Solid Rocket Propellants 186
Experimental Investigation and Numerical Modeling of the Condensed Combustion Products of Micro and Nano-Aluminized Solid Propellants 185
Pure Paraffin Waxes Analysis for Hybrid Rocket Solid Fuels: Rheological, Thermal and Mechanical Characterization 184
Pocket Model for Aluminum Agglomeration Based on Propellant Microstructure 183
Active Space Debris Removal by Hybrid Engine Module 182
Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by Flame Models 181
Nano-Composites for Rocket Solid Propellants 181
Activation of Micrometric Aluminum - Metal Oxide Mixtures by Mechanical Milling 179
An Hybrid Microcombustor for Regression Rate Measurements 178
Gas Phase Velocity Measurements in Solid Rocket Propellants by Laser Doppler Anemometry 178
Acoustic Emission of Underwater Burning Solid Rocket Propellants 178
Advanced Aluminum Powders for Solid Propellants 178
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 178
Thermal behavior and decomposition kinetics of composite solid propellants in the presence of amide burning rate suppressants 178
Advanced Hybrid Propellant for a Moon Orbiter Thruster 176
Nanoaluminum as a Solid Propellant Fuel 176
Innovative Metal Fuels for Solid Rocket Propulsion 174
Agglomeration in Solid Rocket Propellants: Novel Experimental and Modeling Methods 173
Aggregation Vs. Agglomeration in Metallized Solid Rocket Propellants 172
Active De-Orbiting Systems of Launcher Upper Stages and Spacecraft Based on Hybrid Gas Rocket Engines 171
Combustion Mechanism of Ammonium-Nitrate-Based Propellants 171
Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum 171
Aluminized Solid Propellant Combustion Under Vibratory Conditions 170
Time-resolved regression rate of innovative hybrid solid fuel formulations 170
Intrinsic Stability of Energetic Solids Burning under Thermal Radiation 169
Intrinsic Structural-Ballistic Interactions in Composite Energetic Materials. Part I: Experiments 169
Burning of Aluminized Solid Rocket Propellants: from Micrometric to Nanometric Fuel Size 168
Ballistics and Condensed Residues of Aluminized Solid Rocket Propellants 168
Characterization of a Family of Paraffin-Based Solid Fuels 168
Theoretical Analysis of Hydrides in Solid and Hybrid Rocket Propulsion 167
A Critical Review of Solid Rocket Propellant Transient Flame Models 166
Ballistic effectiveness of Zr-containing composite solid propellants as a function of binder nature and mass fraction 165
Ballistic Properties of Nano-Aluminized High-Energy Materials (HEM) 164
Grain Processing Effects on Steady Burning Rate in Small Scale Test Motors 164
Advances in Hybrid Propulsion 164
Nanoparticles for Solid Rocket Propulsion 164
PDL of Micro and Nanoaluminized Laboratory Propellants for Space Applications 163
Comparing Ballistics of AP- vs. ADN-based Composite Solid Rocket Propellants 163
Acoustic Response of a Model Rocket Chamber 161
Steady and Unsteady Burning Behavior of Solid Rocket Propellants 161
Experimental Laboratory Characterization of Charring Thermal Insulators 161
Comparing AP- and AN-based Propellants with Low Aluminum Content 161
Active Debris Removal Space Mission Concepts Based on Hybrid Propulsion 161
Solid-Fuel Regression Rate Modeling for Hybrid Rockets 161
Burning Rate Fundamentals 160
Active Debris Removal of a Cosmos-3M Second Stage by Hybrid Rocket Module 159
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 158
Intrinsic Stability of Pressure-Driven Solid Propellant Burning with Variable Thermal Properties 156
Extinction Theories and Experiments 156
Burning Rate Measurement on Small-Scale Rocket Motors 155
Burning of Nano-Aluminized Composite Rocket Propellants 155
Approaching Solid Propellant Heterogeneity for Agglomerate Size Prediction 155
Comparison Between Nano-Sized Aluminum Powders with Different Coatings: Physical Analyses and Performance Test 155
Radiation-Driven Burning of Energetic Solid Materials with Phase Transition 154
Totale 19.537
Categoria #
all - tutte 114.414
article - articoli 27.531
book - libri 0
conference - conferenze 75.984
curatela - curatele 4.677
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 6.222
Totale 228.828


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20222.246 0 302 188 116 414 78 87 121 85 165 156 534
2022/20233.023 432 287 92 256 326 369 15 195 470 268 186 127
2023/20241.373 124 253 66 128 82 195 108 77 17 125 69 129
2024/20254.716 143 85 136 107 898 266 145 581 739 266 675 675
2025/202616.413 2.927 2.749 913 1.259 793 885 2.194 862 737 1.531 305 1.258
2026/2027665 343 322 0 0 0 0 0 0 0 0 0 0
Totale 41.996