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

DE LUCA, LUIGI
 Distribuzione geografica
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Continente #
NA - Nord America 13.082
EU - Europa 6.091
AS - Asia 1.902
AF - Africa 100
SA - Sud America 30
OC - Oceania 23
Continente sconosciuto - Info sul continente non disponibili 12
Totale 21.240
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Nazione #
US - Stati Uniti d'America 12.732
IT - Italia 1.692
UA - Ucraina 1.076
SE - Svezia 722
DE - Germania 692
VN - Vietnam 462
CN - Cina 447
FI - Finlandia 415
GB - Regno Unito 412
CA - Canada 341
SG - Singapore 332
IE - Irlanda 216
ES - Italia 213
FR - Francia 187
IN - India 162
AT - Austria 148
KR - Corea 123
JO - Giordania 93
NL - Olanda 86
RU - Federazione Russa 78
CI - Costa d'Avorio 74
TR - Turchia 74
IR - Iran 57
BE - Belgio 49
GR - Grecia 38
JP - Giappone 32
BR - Brasile 22
IL - Israele 22
PK - Pakistan 21
HK - Hong Kong 17
PL - Polonia 15
RO - Romania 15
CH - Svizzera 13
EU - Europa 12
NZ - Nuova Zelanda 12
TW - Taiwan 12
AU - Australia 11
AE - Emirati Arabi Uniti 9
PH - Filippine 9
MU - Mauritius 8
MX - Messico 8
PT - Portogallo 7
MY - Malesia 6
NG - Nigeria 6
EG - Egitto 5
ID - Indonesia 5
KG - Kirghizistan 5
TH - Thailandia 5
DK - Danimarca 4
DZ - Algeria 4
LB - Libano 3
LV - Lettonia 3
RS - Serbia 3
SY - Repubblica araba siriana 3
CL - Cile 2
CO - Colombia 2
CZ - Repubblica Ceca 2
MA - Marocco 2
NO - Norvegia 2
PE - Perù 2
AN - Antille olandesi 1
AR - Argentina 1
AZ - Azerbaigian 1
EC - Ecuador 1
EE - Estonia 1
ET - Etiopia 1
HU - Ungheria 1
LA - Repubblica Popolare Democratica del Laos 1
LK - Sri Lanka 1
LT - Lituania 1
Totale 21.240
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Città #
Fairfield 1.357
Woodbridge 1.310
Chandler 1.227
Ann Arbor 885
Ashburn 861
Wilmington 853
Houston 728
Jacksonville 638
Seattle 545
Milan 523
Cambridge 502
Dearborn 427
Boardman 321
Lawrence 303
Santa Clara 295
Ottawa 289
Dong Ket 282
Medford 271
Dublin 212
Singapore 211
Málaga 206
Beijing 167
Vienna 140
Helsinki 112
Des Moines 102
Amman 93
Abidjan 74
Redwood City 68
San Diego 63
Giussano 60
Washington 59
Bovisio Masciago 49
Brussels 47
Norwalk 46
Amsterdam 45
New York 45
Rome 45
Seoul 44
Munich 34
Nanjing 33
Chennai 30
Princeton 30
Mcallen 28
Shanghai 27
Verona 26
West Lafayette 26
North York 25
Auburn Hills 24
Riverside 24
Ankara 22
Segrate 21
Tong 21
Xian 21
College Station 19
Seongnam 19
Zibido San Giacomo 18
Delft 17
London 17
Zhengzhou 17
Los Angeles 16
Montréal 16
Mountain View 16
Kunming 15
Clifton 14
Gavirate 14
Hefei 14
Ciampino 13
Seregno 13
Omsk 11
Tehran 11
Imam 10
Istanbul 10
Padova 10
Tokyo 10
Tomsk 10
Torre Del Greco 10
Changsha 9
Gangnam-gu 9
Izmir 9
Moscow 9
Nave 9
Falkenstein 8
Karlsruhe 8
Kharagpur 8
Auckland 7
Castellanza 7
Chengdu 7
Delhi 7
Dronten 7
Guangzhou 7
Long Beach 7
Luft 7
Meudon 7
Taipei 7
Tel Aviv 7
Berlin 6
Bern 6
Central 6
Como 6
Duncan 6
Totale 14.393
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Nome #
Advanced Hybrid Solid Fuels 317
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 212
Macro- vs Microcrystalline Wax: Interplay of Evaporation and Decomposition under Pressure Variation 188
Activated Aluminum Powders for Space Propulsion 185
Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants 181
Fracture Mechanics of Composite Solid Rocket Propellant Grains: Material Testing 174
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 168
Intrinsic Burning Stability of Solid Propellants with Variable Thermal Properties 167
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 163
Dynamic Effects on Ignitability Limits of Solid PropellantsSubjected to Radiative Heating 150
Adiabatic Pyrolysis of Solid Propellants 147
Combustion of Metal Agglomerates in a Solid Rocket Core Flow 140
Efficient Solid Rocket Propulsion for Access to Space 133
Gas Phase Velocity Measurements in Solid Rocket Propellants by Laser Doppler Anemometry 130
Nonsteady Burning and Combustion Stability of Solid Propellants 130
Evaluation of paraffin-based fuels for hybrid rocket engines 129
Viscosity and regression rate of liquefying hybrid rocket fuels 129
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 129
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner 128
Analysis of Quasi-Steady and Transient Burning of Hybrid Fuels in a Laboratory-Scale Burner by an Optical Technique 128
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 128
Theory of Nonsteady Burning and Combustion Stability of Solid Propellants by Flame Models 126
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons 126
Microstructure Effects in Aluminized Solid Rocket Propellants 125
Active Debris Multi-Removal Mission Concept Based on Hybrid Propulsion 123
Measuring Thermodynamic Properties of Burning Propellants 122
Feasibility Study of Paraffin-Based Fuels for Hybrid Rocket Engine Applications 121
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 120
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 119
Combustion of Metal Agglomerates in Solid Rocket Core Flow 119
Nano-Aluminum as Energetic Material for Rocket Propellants 119
Active Space Debris Removal by a Hybrid Propulsion Module 116
Micro and Nano-Sized Metal Additives for Solid Fuels in Hybrid Rocket Lab-Scale Burner 114
Nanoaluminum as a Solid Propellant Fuel 113
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 113
Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum 113
Pocket Model for Aluminum Agglomeration Based on Propellant Microstructure 111
Time-resolved burning of solid fuels for hybrid rocket propulsion 111
Solid-Fuel Regression Rate Modeling for Hybrid Rockets 111
Experimental Investigation of the Condensed Combustion Products of Micro Aluminized Solid Rocket Propellants 109
Ballistic effectiveness of Zr-containing composite solid propellants as a function of binder nature and mass fraction 109
Burning of Aluminized Solid Rocket Propellants: from Micrometric to Nanometric Fuel Size 108
Agglomeration of Aluminized Solid Rocket Propellants 108
Pure Paraffin Waxes Analysis for Hybrid Rocket Solid Fuels: Rheological, Thermal and Mechanical Characterization 108
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 108
Combustion Mechanism of Ammonium-Nitrate-Based Propellants 108
Burn-Rate Measurement on Small-Scale Rocket Motors 107
Nano-Composites for Rocket Solid Propellants 107
Burning Rate Measurements on Damaged Propellant Samples Under Mechanical Loads 105
Physical and Ballistic Characterization of AlH3-Based Space Propellants 104
Experimental Investigation and Numerical Modeling of the Condensed Combustion Products of Micro and Nano-Aluminized Solid Propellants 103
Experimental Investigations on Transient Burning of Nano-Aluminized Solid Rocket Propellants 101
Ignition and Extinction of Solid Rocket Propellants 101
Extinction Theories and Experiments 101
Nonlinear Burning Stability Theory of Heterogeneous Thin Flames 101
Intrinsic Stability of Energetic Solids Burning under Thermal Radiation 98
Agglomeration and Pocket Structures in Composite Solid Rocket Propellants 98
Thermal behavior and decomposition kinetics of composite solid propellants in the presence of amide burning rate suppressants 98
Acoustic Emission of Underwater Burning Solid Rocket Propellants 97
Agglomeration in Solid Rocket Propellants: Novel Experimental and Modeling Methods 97
Progress in Propulsion Physics – Volume 8 96
Radiation-Driven Burning of Energetic Solid Materials with Phase Transition 95
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 94
Burning Rate Fundamentals 93
PDL of Micro and Nanoaluminized Laboratory Propellants for Space Applications 92
Micro and Nano Aluminized Solid Propellants Behavior Under Transient Burning Conditions 91
Limit cycles for solid propellant burning rate at constant pressure 91
Time-resolved regression rate of innovative hybrid solid fuel formulations 90
Self-Sustained Oscillatory Combustion of Solid Rocket Propellants 89
Burning of Nano-Aluminized Composite Rocket Propellants 89
Characterization of nAl powders for rocket propulsion 89
Mechanical Characterization of Composite Solid Propellants 88
Comparison Between Nano-Sized Aluminum Powders with Different Coatings: Physical Analyses and Performance Test 88
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 88
Experimental Verification of the Recoil Force Versus Burning-Rate Dependence 88
Burning Rate Data Reduction of Small-Scale Test Motors 86
Surface Pyrolysis of High Energy Materials 86
A Critical Review of Solid Rocket Propellant Transient Flame Models 86
Nanoparticles for Solid Rocket Propulsion 85
Active Space Debris Removal by Hybrid Engine Module 85
Aluminized Gels or Clouds for Low Trust Applications 84
Innovative Metal Fuels for Solid Rocket Propulsion 84
Grain Processing Effects on Steady Burning Rate in Small Scale Test Motors 83
Aluminized Solid Propellant Combustion Under Vibratory Conditions 83
Unstable Burning of Thin Solid Propellant Flames 83
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 83
Burning Rate Data Reduction from Small-Scale Test Motors 82
Linear Stability and Pressure-Driven Response Function of Solid Propellants with Phase Transition 82
Combustion Modeling and Stability of Double-Base Solid Rocket Propellants 81
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 81
Theoretical Analysis of Hydrides in Solid and Hybrid Rocket Propulsion 81
In-Space Propulsion 80
Burning of Hydroxylammonium Nitrate 80
Ballistic Characterization of AlH3-Based Propellants for Solid and Hybrid Rocket Propulsion 80
An Hybrid Microcombustor for Regression Rate Measurements 79
Intrinsic Stability of Pressure-Driven Solid Propellant Burning with Variable Thermal Properties 78
Condensed combustion products from burning of nanoaluminum-based propellants: properties and formation mechanism 78
Dual-Oxidizer Metallized Solid Propellants for Low-Cost Space Access 78
Condensed Combustion Products from Burning of Nanoaluminum Based Propellants: Properties and Formation Mechanism 77
Experimental Investigation of Metallized Hybrid Rocket Fuels 76
Totale 11.056
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Categoria #
all - tutte 59.318
article - articoli 16.033
book - libri 0
conference - conferenze 37.454
curatela - curatele 2.324
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 3.507
Totale 118.636
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20203.485 0 0 0 0 555 557 565 319 528 190 588 183
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
2024/20251.146 143 85 136 107 675 0 0 0 0 0 0 0
Totale 21.415