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

MAGGI, FILIPPO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 7.885
EU - Europa 5.647
AS - Asia 1.175
AF - Africa 33
OC - Oceania 24
SA - Sud America 20
Continente sconosciuto - Info sul continente non disponibili 2
Totale 14.786
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 7.685
IT - Italia 3.260
UA - Ucraina 378
VN - Vietnam 366
DE - Germania 347
SE - Svezia 318
CN - Cina 293
GB - Regno Unito 254
FI - Finlandia 214
CA - Canada 195
ES - Italia 191
FR - Francia 185
IE - Irlanda 170
AT - Austria 101
IN - India 95
JO - Giordania 80
PH - Filippine 70
NL - Olanda 58
KR - Corea 56
CH - Svizzera 48
RU - Federazione Russa 47
JP - Giappone 45
TR - Turchia 45
BE - Belgio 38
IR - Iran 30
HK - Hong Kong 23
IL - Israele 17
BR - Brasile 16
SG - Singapore 16
AU - Australia 13
GR - Grecia 11
NZ - Nuova Zelanda 11
PL - Polonia 11
EG - Egitto 9
CI - Costa d'Avorio 8
TW - Taiwan 8
MU - Mauritius 7
PK - Pakistan 7
AZ - Azerbaigian 6
ID - Indonesia 6
RO - Romania 5
DK - Danimarca 4
DZ - Algeria 4
MX - Messico 4
TH - Thailandia 4
AE - Emirati Arabi Uniti 3
MY - Malesia 3
EU - Europa 2
KE - Kenya 2
PT - Portogallo 2
RS - Serbia 2
AM - Armenia 1
AN - Antille olandesi 1
AR - Argentina 1
BA - Bosnia-Erzegovina 1
BD - Bangladesh 1
BO - Bolivia 1
BW - Botswana 1
CL - Cile 1
CO - Colombia 1
CZ - Repubblica Ceca 1
HU - Ungheria 1
NG - Nigeria 1
SD - Sudan 1
Totale 14.786
Salva come PNG Salva come JPEG
Città #
Milan 1.014
Fairfield 968
Woodbridge 822
Chandler 796
Ashburn 530
Wilmington 498
Ann Arbor 474
Houston 463
Seattle 369
Cambridge 348
Jacksonville 220
Dong Ket 197
Dearborn 195
Lawrence 184
Medford 180
Málaga 179
Ottawa 177
Dublin 163
Beijing 110
Rome 100
Vienna 99
Redwood City 87
Helsinki 80
Amman 79
Des Moines 75
Davao City 69
Ciampino 57
New York 56
Rho 47
San Diego 45
Bern 42
Gavirate 41
Marnate 39
Bovisio Masciago 38
Monza 37
Redmond 35
Brussels 32
Amsterdam 31
Stuttgart 31
Zibido San Giacomo 30
Bresso 29
Norwalk 29
Turin 26
Istanbul 25
Nanjing 23
Bergamo 21
Chennai 21
Washington 21
Tong 20
Fremont 18
Varese 18
Moscow 17
Seoul 17
Southampton 17
Arcene 16
Boardman 16
London 16
Xian 16
Shanghai 14
Katsushika 13
Luft 13
Nave 13
Auburn Hills 12
Mountain View 12
Trezzano Sul Naviglio 12
Omsk 11
Phoenix 11
Segrate 11
Verona 11
Bareggio 10
Baveno 10
Berlin 10
Bologna 10
Genzano Di Roma 10
Parma 10
Rubiera 10
Falls Church 9
Karlsruhe 9
Tokyo 9
Tradate 9
Venegono Superiore 9
Xi'an 9
Aberdeen 8
Abidjan 8
Ankara 8
Central District 8
Frankfurt am Main 8
Giussano 8
Hangzhou 8
Magenta 8
Montreal 8
Taipei 8
Barzanò 7
Cardiff 7
Changsha 7
College Station 7
Lucca 7
Modica 7
Nottingham 7
Novara 7
Totale 9.796
Salva come PNG Salva come JPEG
Nome #
Iron oxide as solid propellant catalyst: A detailed characterization 212
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 205
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 175
Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants 174
Activated Aluminum Powders for Space Propulsion 173
Fragmentation of Ammonium Nitrate Particles under Thermal Cycling 169
Parallel packing code for propellant microstructure analysis 163
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 162
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 156
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 153
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 150
A method for mechanical activation of powders by means of balls 149
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 146
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 145
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 143
Aerospace Propulsion Research Activities at SPlab. Overview and Results 142
Burning Rate Modifiers to Tailor Combustion of ADN/AN-Based Solid Propellants 136
Prospects of Aluminum Modifications as Energetic Fuels in Chemical Rocket Propulsion 135
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 135
Combustion of Metal Agglomerates in a Solid Rocket Core Flow 133
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 131
Trade-Off Analysis of a New Liquid Rocket Engine 131
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 129
Evaluating New Liquid Storable Bipropellants: Safety and Performance Assessments 128
Development of an intrusive technique for particles collection in rockets plume 128
Towards New Hypergolic Hydrogen Peroxide-Based Bipropellants 127
Efficient Solid Rocket Propulsion for Access to Space 127
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 123
Detailed Properties of Iron Oxide Solid Propellant Catalyst 123
Microstructure Effects in Aluminized Solid Rocket Propellants 121
Active Debris Multi-Removal Mission Concept Based on Hybrid Propulsion 118
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 115
Combustion of Metal Agglomerates in Solid Rocket Core Flow 114
Monte Carlo Uncertainty Quantification Using Quasi-1D SRM Ballistic Model 114
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 108
Active Space Debris Removal by a Hybrid Propulsion Module 107
Preliminary Assessments for the Development of a Green Storable Bipropellant Rocket Engine Based on H2O2 107
Time-resolved burning of solid fuels for hybrid rocket propulsion 106
Numerical Simulation of HTPB Combustion in a 2D Hybrid Slab Combustor 106
Pocket Model for Aluminum Agglomeration Based on Propellant Microstructure 105
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 105
Agglomeration of Aluminized Solid Rocket Propellants 103
Burn-Rate Measurement on Small-Scale Rocket Motors 102
Nature of Packs Used in Propellant Modeling 101
Overview of a supersonic probe for solid propellant rocket CCP collection 101
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 101
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 100
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 100
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 100
Burning Rate Measurements on Damaged Propellant Samples Under Mechanical Loads 100
Particulate Phase Evolution Inside Solid Rocket Motors: Preliminary Results 99
Curing Viscosity of HTPB-Based Binder Embedding Micro and Nano-Aluminum Particles 97
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Conceptual and Detailed Design 97
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 96
Ignition of Mechanically Activated Aluminum Powders Doped with Metal Oxides 96
Vortex combustion in a hybrid rocket motor 96
Processo di produzione di propellente composito tramite deposizione e polimerizzazione foto-attivata per endoreattori a propellente solidi 95
Free and Forced Oscillations of Magnetic Liquids Under Low-Gravity Conditions 95
Agglomeration in Solid Rocket Propellants: Novel Experimental and Modeling Methods 93
Thermal behavior and decomposition kinetics of composite solid propellants in the presence of amide burning rate suppressants 93
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 92
Burning Behavior of ADN-Based Propellants Loaded with Al-Mg Mechanically Activated Powders 92
Agglomeration and Pocket Structures in Composite Solid Rocket Propellants 91
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 91
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Application of Quasi-1D Engineering Model and 2D Axisymmetric CFD 90
Micro and Nano Aluminized Solid Propellants Behavior Under Transient Burning Conditions 86
Feature Extraction from Micro-Tomography Analysis of Solid Propellants 86
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 84
Characterization of SRM plumes with alumina particulate in subscale testing 84
Monte Carlo Analysis of a LEO Reentry Mission by Solid Rocket Propulsion 81
Aging Effects on Nano-Sized Aluminum Reactivity 81
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 81
Active Space Debris Removal by Hybrid Engine Module 81
Caratterizzazione meccanica e applicazione di modelli iperelastici ad un materiale plastico a base di legante per uso propulsivo spaziale 80
Innovative Metal Fuels for Solid Rocket Propulsion 80
Particle Size in SRM Plume: Assessment of Collection Method 80
Collecting Data on Aluminum Combustion and Its Oxides in Solid Rocket Motors 79
Grain Processing Effects on Steady Burning Rate in Small Scale Test Motors 78
Simulation Code for Hybrid Rocket Combustion 78
Mechanical Characterization of Composite Solid Propellants 77
2D Numerical Simulation of Combustion Processes in a Slab Hybrid Rocket Motor 77
Rheological and Mechanical Characterization of Hybrid Rocket Solid Fuels 77
Theoretical Analysis of Hydrides in Solid and Hybrid Rocket Propulsion 77
Combustion Synthesis of AlN (Al3O3N), BN, ZrN, and TiN in Air and Ceramic Application 76
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 76
An Hybrid Microcombustor for Regression Rate Measurements 74
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 74
Aluminized Gels or Clouds for Low Trust Applications 71
Contact-less Active Debris Removal: the Hybrid Propulsion Alternative 71
Approaching Solid Propellant Heterogeneity for Agglomerate Size Prediction 70
Flame Structure Simulation of Nonaluminized Composite Propellants 68
Aggregation Vs. Agglomeration in Metallized Solid Rocket Propellants 67
Assessment of Rocket Exhaust Pollution Through Thermochemistry 67
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 67
Using Tomography to Characterize Heterogeneous Propellants 67
The FP7 Spartan Program Status and Achievements 67
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 67
Experimental techniques for characterization of particles in plumes of sub-scale solid rocket motors 67
Burning Rate Measurement on Small-Scale Rocket Motors 66
Activation of Micrometric Aluminum - Metal Oxide Mixtures by Mechanical Milling 66
Totale 10.578
Salva come PNG Salva come JPEG
Categoria #
all - tutte 37.803
article - articoli 12.568
book - libri 0
conference - conferenze 22.098
curatela - curatele 0
other - altro 0
patent - brevetti 863
selected - selezionate 0
volume - volumi 2.274
Totale 75.606
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019880 0 0 0 0 0 0 0 0 0 220 316 344
2019/20203.502 230 220 156 229 524 392 360 276 338 170 418 189
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
2023/20241.275 92 195 84 158 87 190 256 79 50 84 0 0
Totale 14.976