DE LUCA, LUIGI
 Distribuzione geografica
Continente #
NA - Nord America 19.363
EU - Europa 11.115
AS - Asia 7.767
SA - Sud America 1.439
AF - Africa 324
OC - Oceania 38
Continente sconosciuto - Info sul continente non disponibili 13
Totale 40.059
Nazione #
US - Stati Uniti d'America 18.844
RU - Federazione Russa 3.819
SG - Singapore 2.445
CN - Cina 2.360
IT - Italia 1.859
BR - Brasile 1.245
VN - Vietnam 1.126
UA - Ucraina 1.078
DE - Germania 810
SE - Svezia 732
FR - Francia 596
GB - Regno Unito 549
FI - Finlandia 528
KR - Corea 420
CA - Canada 408
IN - India 305
ES - Italia 237
IE - Irlanda 232
NL - Olanda 227
JP - Giappone 186
AT - Austria 162
MA - Marocco 122
TR - Turchia 109
JO - Giordania 106
HK - Hong Kong 98
BD - Bangladesh 85
IR - Iran 78
AR - Argentina 77
CI - Costa d'Avorio 74
PL - Polonia 70
MX - Messico 56
PK - Pakistan 56
BE - Belgio 54
IQ - Iraq 54
ZA - Sudafrica 41
GR - Grecia 40
ID - Indonesia 39
TW - Taiwan 35
IL - Israele 34
EC - Ecuador 32
SA - Arabia Saudita 31
CH - Svizzera 30
UZ - Uzbekistan 26
AE - Emirati Arabi Uniti 23
PH - Filippine 22
NZ - Nuova Zelanda 20
MY - Malesia 19
KE - Kenya 18
AU - Australia 17
CO - Colombia 17
KZ - Kazakistan 17
TH - Thailandia 17
PT - Portogallo 16
PY - Paraguay 16
RO - Romania 16
VE - Venezuela 16
DZ - Algeria 15
PE - Perù 15
EG - Egitto 14
AZ - Azerbaigian 13
EU - Europa 12
NP - Nepal 12
TT - Trinidad e Tobago 11
DO - Repubblica Dominicana 10
LB - Libano 10
CL - Cile 8
KG - Kirghizistan 8
MU - Mauritius 8
NG - Nigeria 8
BO - Bolivia 7
CR - Costa Rica 7
ET - Etiopia 7
JM - Giamaica 7
LT - Lituania 7
TN - Tunisia 7
LV - Lettonia 6
UY - Uruguay 6
CZ - Repubblica Ceca 5
EE - Estonia 5
OM - Oman 5
BY - Bielorussia 4
DK - Danimarca 4
HN - Honduras 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
GT - Guatemala 3
NO - Norvegia 3
AO - Angola 2
BG - Bulgaria 2
GA - Gabon 2
GD - Grenada 2
HR - Croazia 2
IS - Islanda 2
Totale 40.025
Città #
Ashburn 1.911
San Jose 1.483
Fairfield 1.349
Woodbridge 1.311
Singapore 1.240
Chandler 1.226
Ann Arbor 885
Wilmington 847
Houston 733
Santa Clara 666
Jacksonville 638
Milan 597
Seattle 550
Cambridge 499
Moscow 470
The Dalles 468
Hefei 456
Council Bluffs 445
Dearborn 427
Boardman 401
Beijing 376
Dallas 361
Seoul 327
Lawrence 302
Ottawa 290
Dong Ket 282
Medford 271
Lauterbourg 263
North Charleston 261
Los Angeles 236
Dublin 223
Helsinki 214
Málaga 207
Ho Chi Minh City 188
Hanoi 166
Tokyo 157
Vienna 147
New York 126
Buffalo 119
Amman 105
Des Moines 105
São Paulo 89
Orem 80
Abidjan 74
Hong Kong 71
Las Vegas 69
Redwood City 68
Washington 65
Amsterdam 64
San Diego 64
Giussano 60
Rome 59
Shanghai 59
Casablanca 57
Chennai 57
London 57
Kenitra 53
Brussels 52
Mumbai 52
Frankfurt am Main 50
Guangzhou 50
Bovisio Masciago 49
Norwalk 46
Munich 44
Warsaw 44
Nanjing 39
Rio de Janeiro 37
Chicago 34
Ankara 30
Denver 30
Tianjin 30
Belo Horizonte 29
Phoenix 29
Princeton 29
São José dos Campos 29
Mcallen 28
West Lafayette 28
Shenzhen 27
Atlanta 26
Changsha 26
Johannesburg 26
North York 26
Verona 26
Tashkent 25
Auburn Hills 24
Da Nang 24
Hangzhou 24
Riverside 24
Zhengzhou 24
Montreal 23
San Francisco 22
Taipei 22
Segrate 21
Tong 21
Xian 21
Haiphong 20
Kunming 20
Brooklyn 19
College Station 19
Columbus 19
Totale 23.662
Nome #
Advanced Hybrid Solid Fuels 445
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 318
Activated Aluminum Powders for Space Propulsion 298
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 295
Adiabatic Pyrolysis of Solid Propellants 287
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 284
Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation 251
Fracture Mechanics of Composite Solid Rocket Propellant Grains: Material Testing 248
Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants 245
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 236
Intrinsic Burning Stability of Solid Propellants with Variable Thermal Properties 235
Active Debris Multi-Removal Mission Concept Based on Hybrid Propulsion 231
Combustion of Metal Agglomerates in a Solid Rocket Core Flow 229
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 229
Active Space Debris Removal by a Hybrid Propulsion Module 227
Nano-Aluminum as Energetic Material for Rocket Propellants 216
Burning Rate Measurements on Damaged Propellant Samples Under Mechanical Loads 211
Analysis of Quasi-Steady and Transient Burning of Hybrid Fuels in a Laboratory-Scale Burner by an Optical Technique 210
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 207
Viscosity and regression rate of liquefying hybrid rocket fuels 205
Efficient Solid Rocket Propulsion for Access to Space 204
Dynamic Effects on Ignitability Limits of Solid PropellantsSubjected to Radiative Heating 202
Evaluation of paraffin-based fuels for hybrid rocket engines 202
Microstructure Effects in Aluminized Solid Rocket Propellants 201
Burn-Rate Measurement on Small-Scale Rocket Motors 200
Nonsteady Burning and Combustion Stability of Solid Propellants 197
Time-resolved burning of solid fuels for hybrid rocket propulsion 196
Physical and Ballistic Characterization of AlH3-Based Space Propellants 195
Feasibility Study of Paraffin-Based Fuels for Hybrid Rocket Engine Applications 193
Aluminized Gels or Clouds for Low Trust Applications 192
Experimental Investigations on Transient Burning of Nano-Aluminized Solid Rocket Propellants 191
Combustion of Metal Agglomerates in Solid Rocket Core Flow 191
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 188
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 188
A Wide Characterization of Aluminum Powders for Propellants 187
Experimental Investigation of the Condensed Combustion Products of Micro Aluminized Solid Rocket Propellants 186
Micro and Nano-Sized Metal Additives for Solid Fuels in Hybrid Rocket Lab-Scale Burner 186
Agglomeration of Aluminized Solid Rocket Propellants 185
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner 185
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 185
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons 185
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 184
Mechanical Characterization of Composite Solid Propellants 183
Experimental Investigation and Numerical Modeling of the Condensed Combustion Products of Micro and Nano-Aluminized Solid Propellants 183
Pocket Model for Aluminum Agglomeration Based on Propellant Microstructure 180
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 180
Agglomeration and Pocket Structures in Composite Solid Rocket Propellants 179
Active Space Debris Removal by Hybrid Engine Module 178
Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by Flame Models 177
Measuring Thermodynamic Properties of Burning Propellants 176
An Hybrid Microcombustor for Regression Rate Measurements 172
Gas Phase Velocity Measurements in Solid Rocket Propellants by Laser Doppler Anemometry 172
Nanoaluminum as a Solid Propellant Fuel 172
Advanced Aluminum Powders for Solid Propellants 172
Acoustic Emission of Underwater Burning Solid Rocket Propellants 171
A Global Characterization of Nano-Aluminized Propellants 171
Advanced Hybrid Propellant for a Moon Orbiter Thruster 171
Agglomeration in Solid Rocket Propellants: Novel Experimental and Modeling Methods 171
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 171
Pure Paraffin Waxes Analysis for Hybrid Rocket Solid Fuels: Rheological, Thermal and Mechanical Characterization 170
Aluminized Solid Propellant Combustion Under Vibratory Conditions 169
Thermal behavior and decomposition kinetics of composite solid propellants in the presence of amide burning rate suppressants 169
Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum 168
Nano-Composites for Rocket Solid Propellants 168
Innovative Metal Fuels for Solid Rocket Propulsion 167
Intrinsic Stability of Energetic Solids Burning under Thermal Radiation 166
Intrinsic Structural-Ballistic Interactions in Composite Energetic Materials. Part I: Experiments 166
Activation of Micrometric Aluminum - Metal Oxide Mixtures by Mechanical Milling 166
Time-resolved regression rate of innovative hybrid solid fuel formulations 166
Ballistics and Condensed Residues of Aluminized Solid Rocket Propellants 165
Aggregation Vs. Agglomeration in Metallized Solid Rocket Propellants 164
Ballistic effectiveness of Zr-containing composite solid propellants as a function of binder nature and mass fraction 163
Advances in Hybrid Propulsion 163
Grain Processing Effects on Steady Burning Rate in Small Scale Test Motors 162
A Critical Review of Solid Rocket Propellant Transient Flame Models 162
PDL of Micro and Nanoaluminized Laboratory Propellants for Space Applications 161
Experimental Laboratory Characterization of Charring Thermal Insulators 160
Nanoparticles for Solid Rocket Propulsion 160
Theoretical Analysis of Hydrides in Solid and Hybrid Rocket Propulsion 160
Acoustic Response of a Model Rocket Chamber 159
Burning of Aluminized Solid Rocket Propellants: from Micrometric to Nanometric Fuel Size 159
Active Debris Removal Space Mission Concepts Based on Hybrid Propulsion 159
Ballistic Properties of Nano-Aluminized High-Energy Materials (HEM) 158
Solid-Fuel Regression Rate Modeling for Hybrid Rockets 158
Steady and Unsteady Burning Behavior of Solid Rocket Propellants 157
Characterization of a Family of Paraffin-Based Solid Fuels 157
Combustion Mechanism of Ammonium-Nitrate-Based Propellants 156
Active Debris Removal of a Cosmos-3M Second Stage by Hybrid Rocket Module 155
Intrinsic Stability of Pressure-Driven Solid Propellant Burning with Variable Thermal Properties 154
Burning Rate Fundamentals 154
Active De-Orbiting Systems of Launcher Upper Stages and Spacecraft Based on Hybrid Gas Rocket Engines 153
Comparing AP- and AN-based Propellants with Low Aluminum Content 152
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 152
Extinction Theories and Experiments 150
Burning of Nano-Aluminized Composite Rocket Propellants 150
Characterization of nAl powders for rocket propulsion 150
Comparing Ballistics of AP- vs. ADN-based Composite Solid Rocket Propellants 150
Radiation-Driven Burning of Energetic Solid Materials with Phase Transition 149
Ignition and Extinction of Solid Rocket Propellants 149
Burning Rate Measurement on Small-Scale Rocket Motors 149
Totale 18.834
Categoria #
all - tutte 108.767
article - articoli 26.368
book - libri 0
conference - conferenze 72.011
curatela - curatele 4.433
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 5.955
Totale 217.534


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021538 0 0 0 0 0 0 0 0 0 0 0 538
2021/20222.357 111 302 188 116 414 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
2025/202615.315 2.927 2.749 913 1.259 793 885 2.194 862 737 1.531 305 160
Totale 40.233