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

MAGGI, FILIPPO
 Distribuzione geografica
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Continente #
NA - Nord America 16.230
EU - Europa 15.361
AS - Asia 7.571
SA - Sud America 1.347
AF - Africa 335
Continente sconosciuto - Info sul continente non disponibili 244
OC - Oceania 51
Totale 41.139
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Nazione #
US - Stati Uniti d'America 15.709
IT - Italia 5.793
RU - Federazione Russa 5.327
SG - Singapore 2.232
CN - Cina 2.183
BR - Brasile 1.132
VN - Vietnam 990
FR - Francia 669
DE - Germania 652
KR - Corea 494
GB - Regno Unito 441
UA - Ucraina 391
SE - Svezia 359
JP - Giappone 355
CA - Canada 349
FI - Finlandia 336
NL - Olanda 321
IE - Irlanda 280
ES - Italia 240
IN - India 233
AT - Austria 227
BD - Bangladesh 164
HK - Hong Kong 133
MA - Marocco 101
PH - Filippine 96
JO - Giordania 91
TR - Turchia 87
ID - Indonesia 85
CI - Costa d'Avorio 84
PL - Polonia 79
AR - Argentina 71
CH - Svizzera 65
MX - Messico 63
TW - Taiwan 59
ZA - Sudafrica 55
BE - Belgio 53
IQ - Iraq 52
IR - Iran 38
PK - Pakistan 37
EC - Ecuador 36
SA - Arabia Saudita 34
IL - Israele 31
MY - Malesia 28
NZ - Nuova Zelanda 27
CO - Colombia 25
AU - Australia 24
VE - Venezuela 24
KZ - Kazakistan 23
PT - Portogallo 23
GR - Grecia 22
CR - Costa Rica 20
EG - Egitto 20
UZ - Uzbekistan 19
CL - Cile 18
AZ - Azerbaigian 17
KE - Kenya 17
AE - Emirati Arabi Uniti 16
DZ - Algeria 16
JM - Giamaica 16
PY - Paraguay 15
NP - Nepal 14
TH - Thailandia 13
BG - Bulgaria 12
BO - Bolivia 11
LT - Lituania 11
GT - Guatemala 10
DO - Repubblica Dominicana 9
TT - Trinidad e Tobago 9
CZ - Repubblica Ceca 8
PE - Perù 8
RO - Romania 8
HN - Honduras 7
MU - Mauritius 7
TN - Tunisia 7
AL - Albania 6
BB - Barbados 6
ET - Etiopia 6
NI - Nicaragua 6
BJ - Benin 5
DK - Danimarca 5
KG - Kirghizistan 5
OM - Oman 5
PA - Panama 5
QA - Qatar 5
UY - Uruguay 5
AM - Armenia 4
LB - Libano 4
LV - Lettonia 4
SN - Senegal 4
SV - El Salvador 4
XK - ???statistics.table.value.countryCode.XK??? 4
AO - Angola 3
BA - Bosnia-Erzegovina 3
BH - Bahrain 3
BN - Brunei Darussalam 3
GD - Grenada 3
HR - Croazia 3
HU - Ungheria 3
LK - Sri Lanka 3
LU - Lussemburgo 3
Totale 40.841
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Città #
Milan 2.306
Ashburn 2.035
San Jose 1.591
Singapore 1.252
Fairfield 968
Woodbridge 824
Chandler 796
Santa Clara 684
Moscow 681
Council Bluffs 542
Wilmington 502
Hefei 487
Houston 482
Ann Arbor 474
Seoul 434
Seattle 387
The Dalles 371
Beijing 354
Cambridge 350
Boardman 335
Dallas 331
Tokyo 298
Dublin 269
Rome 257
Jacksonville 229
Los Angeles 227
Lauterbourg 204
Dearborn 199
Ho Chi Minh City 199
Dong Ket 197
Vienna 195
Lawrence 184
Ottawa 183
Medford 182
Málaga 180
New York 168
Helsinki 158
Hanoi 151
Buffalo 137
Amsterdam 135
North Charleston 131
Phoenix 114
Hong Kong 102
Amman 90
Redwood City 87
Frankfurt am Main 86
São Paulo 85
Abidjan 82
Des Moines 81
Turin 76
Chicago 70
Orem 70
Davao City 69
Kent 65
Jakarta 61
Warsaw 58
Ciampino 57
Giussano 57
Las Vegas 57
Chennai 54
London 53
Rho 53
Changsha 51
San Diego 49
Monza 48
Falkenstein 47
Naples 46
Shanghai 46
Montreal 44
Casablanca 43
Pedrengo 43
Bern 42
Bologna 42
Brussels 42
Kenitra 42
Denver 41
Gavirate 41
Boltiere 40
Marnate 39
Taipei 39
Bovisio Masciago 38
Mumbai 37
Stuttgart 37
Brooklyn 36
Parma 36
Stockholm 36
Redmond 35
Washington 35
Rio de Janeiro 34
Istanbul 33
San Francisco 33
Guangzhou 32
Nanjing 31
Zibido San Giacomo 30
Bresso 29
Da Nang 29
Norwalk 29
Lappeenranta 28
Modena 28
Haiphong 27
Totale 23.034
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Nome #
Evaluating New Liquid Storable Bipropellants: Safety and Performance Assessments 385
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 351
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 331
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 319
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 317
Activated Aluminum Powders for Space Propulsion 308
A method for mechanical activation of powders by means of balls 304
Experimental investigation of paraffin-based fuels for hybrid rocket propulsion 300
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 297
Aerospace Propulsion Research Activities at SPlab. Overview and Results 295
Iron oxide as solid propellant catalyst: A detailed characterization 289
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 283
Characterization of SRM plumes with alumina particulate in subscale testing 273
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 270
A parametric study of electrodes geometries for atmospheric electrohydrodynamic propulsion 269
Development of an intrusive technique for particles collection in rockets plume 266
Towards New Hypergolic Hydrogen Peroxide-Based Bipropellants 265
An Experimental Assessment of Soil Contamination by Composite Solid Rocket Propellants 264
A Two-Phase Mass Flow Rate Model for Nitrous Oxide Based on Void Fraction 259
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 258
Effects of Different Nano-Sized Metal Oxide Catalysts on the Properties of Composite Solid Propellants 251
Rheology and Stability of Hydrocarbon-Based Gelled Fuels for Airbreathing Applications 247
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 245
Detailed Properties of Iron Oxide Solid Propellant Catalyst 244
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 243
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 240
Free and Forced Oscillations of Magnetic Liquids Under Low-Gravity Conditions 240
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 240
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 238
Overview of Additive Manufacturing and Quality Assurance of Powders for Space Propulsive Components 237
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 237
Combustion of Metal Agglomerates in a Solid Rocket Core Flow 235
Experimental techniques for characterization of particles in plumes of sub-scale solid rocket motors 235
Thermite-for-demise (T4D): experiments and numerical modelling on solar array drive mechanism mock-ups containing thermite in an arc-heated wind tunnel 233
Active Space Debris Removal by a Hybrid Propulsion Module 233
Active Debris Multi-Removal Mission Concept Based on Hybrid Propulsion 233
Prospects of Aluminum Modifications as Energetic Fuels in Chemical Rocket Propulsion 232
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 231
Trade-Off Analysis of a New Liquid Rocket Engine 231
Fragmentation of Ammonium Nitrate Particles under Thermal Cycling 230
Parallel packing code for propellant microstructure analysis 224
Burning Rate Modifiers to Tailor Combustion of ADN/AN-Based Solid Propellants 219
Burning Rate Measurements on Damaged Propellant Samples Under Mechanical Loads 217
Numerical Simulation of HTPB Combustion in a 2D Hybrid Slab Combustor 216
Microstructure Effects in Aluminized Solid Rocket Propellants 215
Thermite-for-Demise (T4D): Experimental analysis of heat transfer principles and preliminary sizing of an application 213
Efficient Solid Rocket Propulsion for Access to Space 213
Burn-Rate Measurement on Small-Scale Rocket Motors 212
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 211
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 211
Collecting Data on Aluminum Combustion and Its Oxides in Solid Rocket Motors 211
2D Numerical Simulation of Combustion Processes in a Slab Hybrid Rocket Motor 208
Preliminary Assessments for the Development of a Green Storable Bipropellant Rocket Engine Based on H2O2 208
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 207
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 206
Burning Behavior of ADN-Based Propellants Loaded with Al-Mg Mechanically Activated Powders 206
Aluminized Gels or Clouds for Low Trust Applications 205
Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel 204
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Conceptual and Detailed Design 203
Particulate Phase Evolution Inside Solid Rocket Motors: Preliminary Results 203
Monoethanolamine-Based Fuels Hypergolic with Rocket-Grade Hydrogen Peroxide 202
Aging Effects on Nano-Sized Aluminum Reactivity 202
Time-resolved burning of solid fuels for hybrid rocket propulsion 201
Monte Carlo Uncertainty Quantification Using Quasi-1D SRM Ballistic Model 201
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 201
Quantification of HCl in Solid Propellant Combustion Products 200
Photo-polymerization for additive manufacturing of composite solid propellants 200
Solid Rocket Propellant Photo-Polymerization with an In-House LED-UV Prototype 198
Combustion of Metal Agglomerates in Solid Rocket Core Flow 198
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 198
Environmental impact of propulsion systems and green alternatives 197
Agglomeration of Aluminized Solid Rocket Propellants 196
Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion 196
Overview of a supersonic probe for solid propellant rocket CCP collection 195
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 195
Mechanical Characterization of Composite Solid Propellants 194
Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Application of Quasi-1D Engineering Model and 2D Axisymmetric CFD 189
Agglomeration and Pocket Structures in Composite Solid Rocket Propellants 188
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 187
Active Space Debris Removal by Hybrid Engine Module 186
Thermite-for-Demise: Preliminary on-Ground Heat Transfer Experimental Testing 185
Pocket Model for Aluminum Agglomeration Based on Propellant Microstructure 185
Ignition of Mechanically Activated Aluminum Powders Doped with Metal Oxides 185
Advancements in Photocurable Solid Propellants for Additive Manufacturing 182
Particle Size in SRM Plume: Assessment of Collection Method 182
Activation of Micrometric Aluminum - Metal Oxide Mixtures by Mechanical Milling 181
Thermite-for-Demise (T4D): Preliminary Assessment on the Effects of a Thermite Charge in Arc-Heated Wind Tunnel Experiments 180
Advanced Aluminum Powders for Solid Propellants 180
Experimental and Numerical Investigation of the Condensed Combustion Products of AP-based Rocket Propellants 180
Thermal behavior and decomposition kinetics of composite solid propellants in the presence of amide burning rate suppressants 180
Experimental Characterization of Al/Mg Dual Metal Neutralizing Propellants 179
An Hybrid Microcombustor for Regression Rate Measurements 179
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 178
Monte Carlo Analysis of a LEO Reentry Mission by Solid Rocket Propulsion 178
Reduction of Solid Propellants Environmental Impact: Al-Mg Mechanically Activated Fuels and AP-PSAN Blends 178
Current Environmental Concerns About Space and Suborbital Launch Activities 177
Caratterizzazione meccanica e applicazione di modelli iperelastici ad un materiale plastico a base di legante per uso propulsivo spaziale 176
Innovative Metal Fuels for Solid Rocket Propulsion 176
Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 176
Aggregation Vs. Agglomeration in Metallized Solid Rocket Propellants 174
Totale 22.385
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Categoria #
all - tutte 104.736
article - articoli 31.248
book - libri 0
conference - conferenze 66.411
curatela - curatele 0
other - altro 0
patent - brevetti 2.090
selected - selezionate 0
volume - volumi 4.987
Totale 209.472
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.540 0 0 222 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
2024/20256.366 318 96 194 280 1.094 372 224 574 743 290 684 1.497
2025/202618.027 3.718 2.607 937 1.129 875 939 2.397 1.053 956 1.507 510 1.399
2026/20271.459 544 483 432 0 0 0 0 0 0 0 0 0
Totale 41.139