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

MAGGI, FILIPPO
 Distribuzione geografica
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Continente #
NA - Nord America 9.279
EU - Europa 7.438
AS - Asia 2.280
SA - Sud America 536
AF - Africa 128
OC - Oceania 37
Continente sconosciuto - Info sul continente non disponibili 2
Totale 19.700
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Nazione #
US - Stati Uniti d'America 9.056
IT - Italia 4.187
SG - Singapore 857
BR - Brasile 503
DE - Germania 479
UA - Ucraina 382
VN - Vietnam 369
RU - Federazione Russa 357
CN - Cina 353
SE - Svezia 324
GB - Regno Unito 274
FR - Francia 271
FI - Finlandia 246
IE - Irlanda 223
ES - Italia 206
CA - Canada 201
AT - Austria 166
NL - Olanda 130
IN - India 126
JO - Giordania 82
PH - Filippine 80
CI - Costa d'Avorio 68
KR - Corea 59
ID - Indonesia 56
TR - Turchia 56
JP - Giappone 55
CH - Svizzera 51
BE - Belgio 43
HK - Hong Kong 37
IR - Iran 30
NZ - Nuova Zelanda 23
IL - Israele 21
PL - Polonia 20
PT - Portogallo 20
GR - Grecia 18
EG - Egitto 16
PK - Pakistan 16
TW - Taiwan 15
AU - Australia 14
MX - Messico 13
AZ - Azerbaigian 12
BD - Bangladesh 10
EC - Ecuador 10
MA - Marocco 10
AR - Argentina 8
RO - Romania 8
UZ - Uzbekistan 8
MU - Mauritius 7
MY - Malesia 6
ZA - Sudafrica 6
BJ - Benin 5
DK - Danimarca 5
DZ - Algeria 5
IQ - Iraq 5
KE - Kenya 5
AE - Emirati Arabi Uniti 4
BG - Bulgaria 4
CZ - Repubblica Ceca 4
DO - Repubblica Dominicana 4
KZ - Kazakistan 4
TH - Thailandia 4
AL - Albania 3
BO - Bolivia 3
CL - Cile 3
HU - Ungheria 3
LK - Sri Lanka 3
LT - Lituania 3
NP - Nepal 3
PA - Panama 3
AM - Armenia 2
BA - Bosnia-Erzegovina 2
CO - Colombia 2
EU - Europa 2
KG - Kirghizistan 2
NG - Nigeria 2
PE - Perù 2
PY - Paraguay 2
RS - Serbia 2
UY - Uruguay 2
AN - Antille olandesi 1
BN - Brunei Darussalam 1
BW - Botswana 1
BY - Bielorussia 1
CR - Costa Rica 1
EE - Estonia 1
HR - Croazia 1
IS - Islanda 1
LA - Repubblica Popolare Democratica del Laos 1
LU - Lussemburgo 1
LV - Lettonia 1
ML - Mali 1
NO - Norvegia 1
QA - Qatar 1
SA - Arabia Saudita 1
SD - Sudan 1
TG - Togo 1
TM - Turkmenistan 1
VE - Venezuela 1
Totale 19.700
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Città #
Milan 1.596
Fairfield 968
Woodbridge 822
Chandler 796
Ashburn 612
Santa Clara 557
Singapore 515
Wilmington 498
Ann Arbor 474
Houston 463
Seattle 377
Cambridge 348
Boardman 230
Council Bluffs 230
Jacksonville 220
Dublin 214
Dong Ket 197
Dearborn 195
Lawrence 184
Medford 180
Málaga 179
Ottawa 179
Vienna 144
Rome 120
Beijing 116
Helsinki 92
Amsterdam 88
Redwood City 87
Amman 81
Des Moines 75
Davao City 69
Abidjan 68
New York 62
Ciampino 57
Giussano 57
Jakarta 56
Falkenstein 47
Rho 47
San Diego 45
Pedrengo 43
Bern 42
Monza 42
Frankfurt am Main 41
Gavirate 41
Los Angeles 41
Boltiere 40
Marnate 39
Bovisio Masciago 38
Brussels 36
Redmond 35
Turin 32
Stuttgart 31
Parma 30
Zibido San Giacomo 30
Bresso 29
Norwalk 29
São Paulo 29
Chennai 28
The Dalles 28
Istanbul 26
Nanjing 23
Bergamo 22
Moscow 22
Pavia 22
Washington 21
London 20
Tong 20
Mumbai 19
Shanghai 19
Southampton 19
Fremont 18
Hong Kong 18
Varese 18
Lappeenranta 17
Seoul 17
Arcene 16
Xian 16
Belo Horizonte 15
Brescia 15
Nuremberg 15
Phoenix 15
Bologna 13
Katsushika 13
Luft 13
Nave 13
Tokyo 13
Auburn Hills 12
Mountain View 12
Omsk 12
Trezzano Sul Naviglio 12
Auckland 11
Changsha 11
Dallas 11
Segrate 11
Verona 11
Warsaw 11
Ankara 10
Bareggio 10
Baveno 10
Berlin 10
Totale 12.681
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Nome #
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 232
Iron oxide as solid propellant catalyst: A detailed characterization 224
Evaluating New Liquid Storable Bipropellants: Safety and Performance Assessments 209
Activated Aluminum Powders for Space Propulsion 205
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 201
Free and Forced Oscillations of Magnetic Liquids Under Low-Gravity Conditions 191
Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants 188
A method for mechanical activation of powders by means of balls 184
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 178
Fragmentation of Ammonium Nitrate Particles under Thermal Cycling 178
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 177
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 177
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 177
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 176
Aerospace Propulsion Research Activities at SPlab. Overview and Results 175
Parallel packing code for propellant microstructure analysis 173
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 161
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 160
Combustion of Metal Agglomerates in a Solid Rocket Core Flow 157
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 155
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 152
Trade-Off Analysis of a New Liquid Rocket Engine 152
Towards New Hypergolic Hydrogen Peroxide-Based Bipropellants 151
Prospects of Aluminum Modifications as Energetic Fuels in Chemical Rocket Propulsion 151
Development of an intrusive technique for particles collection in rockets plume 148
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 147
Detailed Properties of Iron Oxide Solid Propellant Catalyst 146
Burning Rate Modifiers to Tailor Combustion of ADN/AN-Based Solid Propellants 145
A parametric study of electrodes geometries for atmospheric electrohydrodynamic propulsion 145
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 142
Efficient Solid Rocket Propulsion for Access to Space 140
Microstructure Effects in Aluminized Solid Rocket Propellants 139
Monte Carlo Uncertainty Quantification Using Quasi-1D SRM Ballistic Model 139
Active Debris Multi-Removal Mission Concept Based on Hybrid Propulsion 138
Characterization of SRM plumes with alumina particulate in subscale testing 137
Experimental techniques for characterization of particles in plumes of sub-scale solid rocket motors 136
Burning Behavior of ADN-Based Propellants Loaded with Al-Mg Mechanically Activated Powders 135
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 135
Combustion of Metal Agglomerates in Solid Rocket Core Flow 132
Numerical Simulation of HTPB Combustion in a 2D Hybrid Slab Combustor 132
Active Space Debris Removal by a Hybrid Propulsion Module 131
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 129
Preliminary Assessments for the Development of a Green Storable Bipropellant Rocket Engine Based on H2O2 126
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 125
Time-resolved burning of solid fuels for hybrid rocket propulsion 124
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 121
Burn-Rate Measurement on Small-Scale Rocket Motors 120
Particulate Phase Evolution Inside Solid Rocket Motors: Preliminary Results 120
Agglomeration of Aluminized Solid Rocket Propellants 119
Pocket Model for Aluminum Agglomeration Based on Propellant Microstructure 119
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 119
Burning Rate Measurements on Damaged Propellant Samples Under Mechanical Loads 119
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 117
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 117
Overview of a supersonic probe for solid propellant rocket CCP collection 116
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 115
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Conceptual and Detailed Design 114
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 113
Nature of Packs Used in Propellant Modeling 112
Processo di produzione di propellente composito tramite deposizione e polimerizzazione foto-attivata per endoreattori a propellente solidi 112
Ignition of Mechanically Activated Aluminum Powders Doped with Metal Oxides 111
Agglomeration and Pocket Structures in Composite Solid Rocket Propellants 110
Agglomeration in Solid Rocket Propellants: Novel Experimental and Modeling Methods 108
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 108
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 108
Photo-polymerization for additive manufacturing of composite solid propellants 107
Vortex combustion in a hybrid rocket motor 107
Thermal behavior and decomposition kinetics of composite solid propellants in the presence of amide burning rate suppressants 106
Curing Viscosity of HTPB-Based Binder Embedding Micro and Nano-Aluminum Particles 105
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Application of Quasi-1D Engineering Model and 2D Axisymmetric CFD 105
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 104
StELIUM: A student experiment to investigate the sloshing of magnetic liquids in microgravity 104
Collecting Data on Aluminum Combustion and Its Oxides in Solid Rocket Motors 103
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 102
2D Numerical Simulation of Combustion Processes in a Slab Hybrid Rocket Motor 101
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 100
A Two-Phase Mass Flow Rate Model for Nitrous Oxide Based on Void Fraction 100
Micro and Nano Aluminized Solid Propellants Behavior Under Transient Burning Conditions 99
Caratterizzazione meccanica e applicazione di modelli iperelastici ad un materiale plastico a base di legante per uso propulsivo spaziale 99
Aluminized Gels or Clouds for Low Trust Applications 99
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 99
Aging Effects on Nano-Sized Aluminum Reactivity 99
Active Space Debris Removal by Hybrid Engine Module 99
Mechanical Characterization of Composite Solid Propellants 98
Monte Carlo Analysis of a LEO Reentry Mission by Solid Rocket Propulsion 98
Innovative Metal Fuels for Solid Rocket Propulsion 96
Particle Size in SRM Plume: Assessment of Collection Method 96
Feature Extraction from Micro-Tomography Analysis of Solid Propellants 95
Grain Processing Effects on Steady Burning Rate in Small Scale Test Motors 93
Overview of Additive Manufacturing and Quality Assurance of Powders for Space Propulsive Components 91
Theoretical Analysis of Hydrides in Solid and Hybrid Rocket Propulsion 91
Rheological and Mechanical Characterization of Hybrid Rocket Solid Fuels 90
Activation of Micrometric Aluminum - Metal Oxide Mixtures by Mechanical Milling 89
Advanced Aluminum Powders for Solid Propellants 89
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 88
Simulation Code for Hybrid Rocket Combustion 88
Magnesium and Aluminum Ignition in CO2 Atmosphere 87
An Hybrid Microcombustor for Regression Rate Measurements 86
High-Energy Metal Fuels for Rocket Propulsion: Characterization and Performance 86
Combustion Synthesis of AlN (Al3O3N), BN, ZrN, and TiN in Air and Ceramic Application 86
Totale 12.838
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Categoria #
all - tutte 59.488
article - articoli 18.836
book - libri 0
conference - conferenze 36.143
curatela - curatele 0
other - altro 0
patent - brevetti 1.316
selected - selezionate 0
volume - volumi 3.193
Totale 118.976
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020607 0 0 0 0 0 0 0 0 0 0 418 189
2020/20212.252 204 118 180 115 219 201 127 185 116 179 161 447
2021/20221.866 115 211 222 76 225 102 120 135 58 118 174 310
2022/20232.515 325 227 84 176 238 251 40 165 363 346 165 135
2023/20241.586 92 195 84 158 87 190 256 79 50 163 79 153
2024/20254.631 318 96 194 280 1.094 372 224 574 743 290 446 0
Totale 19.918