RE.PUBLIC@POLIMI pubblicazioni di ricerca del Politecnico di Milano

DE LUCA, LUIGI
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 13.955
EU - Europa 6.241
AS - Asia 2.709
SA - Sud America 209
AF - Africa 119
OC - Oceania 25
Continente sconosciuto - Info sul continente non disponibili 12
Totale 23.270
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 13.597
IT - Italia 1.734
UA - Ucraina 1.078
SG - Singapore 990
DE - Germania 730
SE - Svezia 724
CN - Cina 468
VN - Vietnam 463
FI - Finlandia 419
GB - Regno Unito 416
CA - Canada 341
IE - Irlanda 220
ES - Italia 217
IN - India 194
FR - Francia 192
BR - Brasile 181
AT - Austria 152
KR - Corea 123
JO - Giordania 95
NL - Olanda 95
RU - Federazione Russa 88
TR - Turchia 79
CI - Costa d'Avorio 74
IR - Iran 65
BE - Belgio 49
GR - Grecia 39
JP - Giappone 36
HK - Hong Kong 31
PK - Pakistan 27
IL - Israele 25
CH - Svizzera 16
PL - Polonia 16
RO - Romania 15
ID - Indonesia 14
NZ - Nuova Zelanda 14
AE - Emirati Arabi Uniti 13
PH - Filippine 13
EU - Europa 12
TW - Taiwan 12
AU - Australia 11
MX - Messico 11
EG - Egitto 9
MA - Marocco 9
AZ - Azerbaigian 8
MU - Mauritius 8
KG - Kirghizistan 7
NG - Nigeria 7
PT - Portogallo 7
UZ - Uzbekistan 7
AR - Argentina 6
DZ - Algeria 6
LV - Lettonia 6
MY - Malesia 6
PE - Perù 6
EC - Ecuador 5
EE - Estonia 5
TH - Thailandia 5
BD - Bangladesh 4
CO - Colombia 4
DK - Danimarca 4
IQ - Iraq 4
LK - Sri Lanka 4
RS - Serbia 4
CL - Cile 3
CZ - Repubblica Ceca 3
DO - Repubblica Dominicana 3
LB - Libano 3
SY - Repubblica araba siriana 3
HU - Ungheria 2
LA - Repubblica Popolare Democratica del Laos 2
NO - Norvegia 2
SA - Arabia Saudita 2
ZA - Sudafrica 2
AL - Albania 1
AN - Antille olandesi 1
BG - Bulgaria 1
BO - Bolivia 1
BY - Bielorussia 1
CR - Costa Rica 1
CY - Cipro 1
ET - Etiopia 1
HR - Croazia 1
IS - Islanda 1
KE - Kenya 1
KZ - Kazakistan 1
LT - Lituania 1
LU - Lussemburgo 1
MK - Macedonia 1
NP - Nepal 1
PA - Panama 1
PY - Paraguay 1
QA - Qatar 1
SN - Senegal 1
TM - Turkmenistan 1
TN - Tunisia 1
UY - Uruguay 1
VE - Venezuela 1
YE - Yemen 1
Totale 23.270
Salva come PNG Salva come JPEG
Città #
Fairfield 1.357
Woodbridge 1.310
Chandler 1.227
Ann Arbor 885
Ashburn 867
Wilmington 853
Houston 728
Jacksonville 638
Santa Clara 620
Singapore 582
Seattle 546
Milan 542
Cambridge 502
Dearborn 427
Council Bluffs 329
Boardman 321
Lawrence 303
Ottawa 289
Dong Ket 282
Medford 271
Dublin 214
Málaga 206
Beijing 171
Vienna 144
Helsinki 116
Des Moines 102
Amman 95
Abidjan 74
Redwood City 68
San Diego 63
Giussano 60
Washington 59
Los Angeles 54
Bovisio Masciago 49
Amsterdam 47
Brussels 47
Norwalk 46
New York 45
Rome 45
Seoul 44
Munich 34
Nanjing 33
Chennai 32
Princeton 30
Mcallen 28
West Lafayette 28
Shanghai 27
Verona 26
North York 25
Auburn Hills 24
Riverside 24
Ankara 22
Mumbai 22
Segrate 21
Tong 21
Xian 21
College Station 19
London 19
Seongnam 19
Zhengzhou 18
Zibido San Giacomo 18
Delft 17
Hong Kong 16
Montréal 16
Mountain View 16
Kunming 15
Clifton 14
Gavirate 14
Hefei 14
Tokyo 14
Ciampino 13
Monza 13
Seregno 13
Istanbul 12
Omsk 12
Jakarta 11
São Paulo 11
Tehran 11
Imam 10
Padova 10
The Dalles 10
Tomsk 10
Torre Del Greco 10
Auckland 9
Changsha 9
Frankfurt am Main 9
Gangnam-gu 9
Izmir 9
Moscow 9
Nave 9
Tel Aviv 9
Delhi 8
Falkenstein 8
Karlsruhe 8
Kharagpur 8
Baku 7
Castellanza 7
Chengdu 7
Dronten 7
Guangzhou 7
Totale 15.560
Salva come PNG Salva come JPEG
Nome #
Advanced Hybrid Solid Fuels 342
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 230
Activated Aluminum Powders for Space Propulsion 198
Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation 192
Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants 188
Fracture Mechanics of Composite Solid Rocket Propellant Grains: Material Testing 182
Adiabatic Pyrolysis of Solid Propellants 176
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 176
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 174
Intrinsic Burning Stability of Solid Propellants with Variable Thermal Properties 174
Dynamic Effects on Ignitability Limits of Solid PropellantsSubjected to Radiative Heating 155
Combustion of Metal Agglomerates in a Solid Rocket Core Flow 154
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 143
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 142
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner 141
Analysis of Quasi-Steady and Transient Burning of Hybrid Fuels in a Laboratory-Scale Burner by an Optical Technique 141
Efficient Solid Rocket Propulsion for Access to Space 139
Microstructure Effects in Aluminized Solid Rocket Propellants 138
Nonsteady Burning and Combustion Stability of Solid Propellants 137
Viscosity and regression rate of liquefying hybrid rocket fuels 137
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons 136
Gas Phase Velocity Measurements in Solid Rocket Propellants by Laser Doppler Anemometry 135
Active Debris Multi-Removal Mission Concept Based on Hybrid Propulsion 134
Evaluation of paraffin-based fuels for hybrid rocket engines 134
Combustion of Metal Agglomerates in Solid Rocket Core Flow 131
Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by Flame Models 129
Measuring Thermodynamic Properties of Burning Propellants 129
Feasibility Study of Paraffin-Based Fuels for Hybrid Rocket Engine Applications 129
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 128
Nano-Aluminum as Energetic Material for Rocket Propellants 128
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 127
Active Space Debris Removal by a Hybrid Propulsion Module 126
Micro and Nano-Sized Metal Additives for Solid Fuels in Hybrid Rocket Lab-Scale Burner 122
Nanoaluminum as a Solid Propellant Fuel 120
Time-resolved burning of solid fuels for hybrid rocket propulsion 120
Solid-Fuel Regression Rate Modeling for Hybrid Rockets 119
Pocket Model for Aluminum Agglomeration Based on Propellant Microstructure 118
Pure Paraffin Waxes Analysis for Hybrid Rocket Solid Fuels: Rheological, Thermal and Mechanical Characterization 118
Experimental Investigations on Transient Burning of Nano-Aluminized Solid Rocket Propellants 117
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 117
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 117
Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum 117
Burning Rate Measurements on Damaged Propellant Samples Under Mechanical Loads 117
Experimental Investigation of the Condensed Combustion Products of Micro Aluminized Solid Rocket Propellants 116
Agglomeration of Aluminized Solid Rocket Propellants 116
Burn-Rate Measurement on Small-Scale Rocket Motors 114
Nano-Composites for Rocket Solid Propellants 114
Burning of Aluminized Solid Rocket Propellants: from Micrometric to Nanometric Fuel Size 113
Ballistic effectiveness of Zr-containing composite solid propellants as a function of binder nature and mass fraction 113
Combustion Mechanism of Ammonium-Nitrate-Based Propellants 113
Physical and Ballistic Characterization of AlH3-Based Space Propellants 111
Experimental Investigation and Numerical Modeling of the Condensed Combustion Products of Micro and Nano-Aluminized Solid Propellants 109
Agglomeration and Pocket Structures in Composite Solid Rocket Propellants 108
Nonlinear Burning Stability Theory of Heterogeneous Thin Flames 108
Ignition and Extinction of Solid Rocket Propellants 105
Extinction Theories and Experiments 105
Agglomeration in Solid Rocket Propellants: Novel Experimental and Modeling Methods 105
Thermal behavior and decomposition kinetics of composite solid propellants in the presence of amide burning rate suppressants 105
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 104
Intrinsic Stability of Energetic Solids Burning under Thermal Radiation 103
Acoustic Emission of Underwater Burning Solid Rocket Propellants 102
Progress in Propulsion Physics – Volume 8 101
Comparison Between Nano-Sized Aluminum Powders with Different Coatings: Physical Analyses and Performance Test 100
PDL of Micro and Nanoaluminized Laboratory Propellants for Space Applications 99
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 99
Micro and Nano Aluminized Solid Propellants Behavior Under Transient Burning Conditions 98
Radiation-Driven Burning of Energetic Solid Materials with Phase Transition 98
Limit cycles for solid propellant burning rate at constant pressure 98
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 98
Burning Rate Fundamentals 97
Time-resolved regression rate of innovative hybrid solid fuel formulations 96
Mechanical Characterization of Composite Solid Propellants 95
Aluminized Gels or Clouds for Low Trust Applications 95
Characterization of nAl powders for rocket propulsion 95
Active Space Debris Removal by Hybrid Engine Module 95
Aluminized Solid Propellant Combustion Under Vibratory Conditions 94
Self-Sustained Oscillatory Combustion of Solid Rocket Propellants 94
Innovative Metal Fuels for Solid Rocket Propulsion 94
Burning Rate Data Reduction of Small-Scale Test Motors 93
Nanoparticles for Solid Rocket Propulsion 93
Burning of Nano-Aluminized Composite Rocket Propellants 92
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 92
Experimental Verification of the Recoil Force Versus Burning-Rate Dependence 92
Grain Processing Effects on Steady Burning Rate in Small Scale Test Motors 91
Surface Pyrolysis of High Energy Materials 91
A Critical Review of Solid Rocket Propellant Transient Flame Models 91
Theoretical Analysis of Hydrides in Solid and Hybrid Rocket Propulsion 90
Unstable Burning of Thin Solid Propellant Flames 88
Ballistic Characterization of AlH3-Based Propellants for Solid and Hybrid Rocket Propulsion 88
Advanced Aluminum Powders for Solid Propellants 87
Comparing AP- and AN-based Propellants with Low Aluminum Content 86
High-Energy Metal Fuels for Rocket Propulsion: Characterization and Performance 86
In-Space Propulsion 85
An Hybrid Microcombustor for Regression Rate Measurements 85
Intrinsic Stability of Pressure-Driven Solid Propellant Burning with Variable Thermal Properties 85
Burning Rate Data Reduction from Small-Scale Test Motors 85
Burning of Hydroxylammonium Nitrate 85
Linear Stability and Pressure-Driven Response Function of Solid Propellants with Phase Transition 85
Combustion Modeling and Stability of Double-Base Solid Rocket Propellants 84
A Wide Characterization of Aluminum Powders for Propellants 84
Totale 11.875
Salva come PNG Salva come JPEG
Categoria #
all - tutte 68.084
article - articoli 17.869
book - libri 0
conference - conferenze 43.564
curatela - curatele 2.725
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 3.926
Totale 136.168
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020961 0 0 0 0 0 0 0 0 0 190 588 183
2020/20213.092 300 82 286 171 337 183 298 285 171 285 155 539
2021/20222.365 112 302 188 117 416 79 87 121 86 165 157 535
2022/20233.027 433 287 92 256 327 370 15 196 470 268 186 127
2023/20241.375 124 254 66 129 82 195 108 77 17 125 69 129
2024/20253.176 143 85 136 107 901 266 145 583 741 69 0 0
Totale 23.445