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

COLOMBO, GIOVANNI
 Distribuzione geografica
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Continente #
NA - Nord America 5.636
EU - Europa 3.926
AS - Asia 2.319
SA - Sud America 403
AF - Africa 113
OC - Oceania 6
Continente sconosciuto - Info sul continente non disponibili 4
Totale 12.407
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Nazione #
US - Stati Uniti d'America 5.472
RU - Federazione Russa 1.332
IT - Italia 1.007
SG - Singapore 728
CN - Cina 684
BR - Brasile 344
VN - Vietnam 330
UA - Ucraina 271
DE - Germania 224
FR - Francia 215
SE - Svezia 184
FI - Finlandia 153
CA - Canada 129
ES - Italia 129
GB - Regno Unito 129
KR - Corea 113
IN - India 93
NL - Olanda 86
JP - Giappone 79
AT - Austria 66
IE - Irlanda 65
HK - Hong Kong 41
JO - Giordania 40
MA - Marocco 40
CI - Costa d'Avorio 32
BD - Bangladesh 26
AR - Argentina 23
IQ - Iraq 23
IR - Iran 23
MX - Messico 22
TR - Turchia 19
ZA - Sudafrica 16
PL - Polonia 15
BE - Belgio 14
PH - Filippine 13
PK - Pakistan 13
EC - Ecuador 12
KZ - Kazakistan 11
ID - Indonesia 10
TW - Taiwan 10
CH - Svizzera 8
IL - Israele 8
NP - Nepal 8
SA - Arabia Saudita 8
KE - Kenya 7
TH - Thailandia 7
KG - Kirghizistan 6
RO - Romania 6
UZ - Uzbekistan 6
VE - Venezuela 6
DZ - Algeria 5
AZ - Azerbaigian 4
CL - Cile 4
CR - Costa Rica 4
PE - Perù 4
PY - Paraguay 4
AE - Emirati Arabi Uniti 3
AU - Australia 3
CZ - Repubblica Ceca 3
EG - Egitto 3
EU - Europa 3
HN - Honduras 3
MY - Malesia 3
NZ - Nuova Zelanda 3
TN - Tunisia 3
AL - Albania 2
AO - Angola 2
BO - Bolivia 2
CO - Colombia 2
DO - Repubblica Dominicana 2
HU - Ungheria 2
LK - Sri Lanka 2
LT - Lituania 2
PT - Portogallo 2
QA - Qatar 2
BG - Bulgaria 1
BH - Bahrain 1
BN - Brunei Darussalam 1
BY - Bielorussia 1
BZ - Belize 1
DK - Danimarca 1
DM - Dominica 1
EE - Estonia 1
GA - Gabon 1
GT - Guatemala 1
HR - Croazia 1
IS - Islanda 1
LA - Repubblica Popolare Democratica del Laos 1
LB - Libano 1
LU - Lussemburgo 1
MC - Monaco 1
MU - Mauritius 1
NG - Nigeria 1
NO - Norvegia 1
PS - Palestinian Territory 1
RS - Serbia 1
SD - Sudan 1
SK - Slovacchia (Repubblica Slovacca) 1
SN - Senegal 1
SR - Suriname 1
Totale 12.403
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Città #
Ashburn 612
San Jose 451
Singapore 392
Chandler 379
Fairfield 360
Woodbridge 345
Milan 315
Santa Clara 257
Ann Arbor 244
Wilmington 220
Houston 204
Moscow 169
Jacksonville 157
Seattle 144
The Dalles 143
Dallas 135
Beijing 133
Cambridge 122
Hefei 119
Málaga 119
Dearborn 110
Council Bluffs 108
Ottawa 92
Seoul 91
Boardman 87
Lawrence 82
Medford 81
Los Angeles 78
Dong Ket 77
Lauterbourg 74
Helsinki 73
Dublin 64
Tokyo 64
North Charleston 62
Vienna 61
New York 57
Hanoi 53
Ho Chi Minh City 51
Amman 40
Buffalo 40
Ciampino 37
Des Moines 33
Abidjan 32
Hong Kong 29
São Paulo 28
Chennai 25
Gavirate 25
Kenitra 25
Orem 24
Frankfurt am Main 23
Rome 22
Amsterdam 21
Redwood City 21
Nanjing 19
Redmond 18
Washington 17
Montreal 16
Changsha 15
Las Vegas 15
London 15
Brussels 14
Warsaw 14
Nave 13
Norwalk 13
Rio de Janeiro 13
Shanghai 13
Bologna 12
Bovisio Masciago 12
Denver 12
Johannesburg 12
Palakkad 12
Atlanta 11
Casablanca 11
Chicago 11
Da Nang 11
Baveno 10
Genzano Di Roma 10
Giussano 10
Monza 10
San Francisco 10
Belo Horizonte 9
Guangzhou 9
Legnano 9
Mumbai 9
Porto Alegre 9
Shenzhen 9
Verona 9
Auburn Hills 8
Falkenstein 8
Haiphong 8
Hải Dương 8
Mountain View 8
Phoenix 8
San Diego 8
Taipei 8
Almaty 7
Boston 7
Brooklyn 7
College Station 7
Dhaka 7
Totale 7.321
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Nome #
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 309
A method for mechanical activation of powders by means of balls 286
Adiabatic Pyrolysis of Solid Propellants 281
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 281
Aerospace Propulsion Research Activities at SPlab. Overview and Results 280
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 268
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 257
Aluminum Particle Size Influence on Ignition and Combustion of AP/HTPB/Al Solid Rocket Propellants 253
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 235
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 235
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 234
A Survey of Pressure-Driven Burning of Energetic Solids with Arrhenius Surface Pyrolysis 232
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 204
Microstructure Effects in Aluminized Solid Rocket Propellants 198
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 198
Time-resolved burning of solid fuels for hybrid rocket propulsion 195
Particulate Phase Evolution Inside Solid Rocket Motors: Preliminary Results 190
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 186
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 183
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 179
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 177
An Hybrid Microcombustor for Regression Rate Measurements 171
Advances in Hybrid Propulsion 162
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 160
PDL of Micro and Nanoaluminized Laboratory Propellants for Space Applications 158
Ballistic Properties of Nano-Aluminized High-Energy Materials (HEM) 157
Aggregation Vs. Agglomeration in Metallized Solid Rocket Propellants 157
Experimental Laboratory Characterization of Charring Thermal Insulators 156
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 151
Characterization of nAl powders for rocket propulsion 150
Experimental Investigation of Metallized Hybrid Rocket Fuels 148
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 148
Advances in Hybrid Rocket Propulsion 146
Micro and Nano Aluminized Solid Propellants Behavior Under Transient Burning Conditions 144
Burning of Metallized Composite Solid Rocket Propellants: Toward Nanometric Fuel Size 144
Burning Stability of Double Base Propellants 143
Experimental Study of Solid-Propellant Ignition Transient and Flame Spreading Under Convective Flows 142
Advances in Hybrid Propulsion at the Space Propulsion Laboratory of Politecnico di Milano 141
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 140
Surface Pyrolysis of High Energy Materials 140
The Measurement of Emissivity of Charring Ablative Materials 139
Magnesium and Aluminum Ignition in CO2 Atmosphere 139
Effects of Metal Oxides on the Burning Rate of Ammonium Nitrate Based Solid Rocket Propellants 138
Nano-Ingredients for Rocket Propulsion: Performance Evaluation and Diagnostics 138
Nano Vs. Micro Iron Oxide Catalysts for Composite Solid Rocket Propellants 137
Influence of Additives on the Ballistic Behavior of Natural and Syntetic Elastomers/AN Based Solid Propellants 136
Regression Rate Measurements in Lab-Scale Hybrid Burners 136
Steady and Transient Burning of Microaluminized Solid Rocket Propellants 134
Degradation of a Thermal Insulator Under Vibration and Acceleration 133
Effect of Metallized Powders as Fuel Additives in AP/HTPB-Based Solid Rocket Propellants 133
Iron Oxide Catalysis: Comparison of Micro and Nano Sized Particles 132
Burning Rate Visualization with Digital High-Speed Color Camera 130
Anomalous Burning of Ammonium Perchlorate-Based Nonmetallized Solid Rocket Propellants 127
Iron Oxide Catalysts for Composite Solid Rocket Propellants 126
Modeling of Diffusive and Premixed Flame of AP/HTPB Laminate Propellant 125
Experimental Investigation of Transient Combustion in a Hybrid 2D Lab-Scale Burner by a Wire-Cut Transducer Technique 125
Agglomeration Effects in Metallized Solid Rocket Propellants 124
Ignition and combustion of hydroxyl-terminated polybutadiene (HTPB)-based solid fuels loaded with innovative micrometer-sized metals 119
Regression Rate Measurements of Hybrid Rocket Metallized Solid Fuels: Influence of Oxidizer Mass Flux and Pressure 116
Nanometric Powders Dispersion in a Polymeric Matrix 116
Sensore di ablazione e velocità di combustione per materiali solidi 115
Combustion Behaviour Investigation of Solid Fuels Using a Micro-Sized Hybrid Rocket Motor 114
Modeling of diffusion and premixed flame of AP/HTPB laminate propellant 110
Coating Nano-sized Aluminum to Improve Solid Rocket Propellant Performance 110
Chemical and Physical Characterization of Nano-Aluminum Powders 109
Setting up an Hybrid Microcombustor 108
The FP7 Spartan Program Status and Achievements 107
Ignition and Combustion of HTPB-based Solid Fuels Loaded with Micron-sized Metals 105
Transient Modeling of Spacewise Thick Flames for Rocket Propulsion 101
Characterization of Ablative Thermal Protections Used in Space Propulsion Systems 100
Magnesium and Aluminum Ignition in CO2 Atmosphere 99
Transient Burning of Nanoaluminized Solid Propellants 98
Thermal Protections Degradation Under Mechanical Loads 97
End-To-end Flight Test for Planetary Landing, an Unprecedented Approach in Europe 96
Nano Energetics for Aerospace Propulsion 94
Radiative Heat Feedback in Aluminized Hybrid Fuel Combustion 92
Combustion Response to Laser Radiation of Composite AP/HTPB Propellants 92
Mechanical Behavior of Aluminized Solid Fuels for Hybrid Rockets 86
Nano vs. Micro Catalyst Effects on Solid Rocket Propellants 83
Low Temperature Gas Generators Propellants 78
Oscillatory Burning of Composite Propellants Near Pressure Deflagration Limit 77
Low Temperature Gas Generator Propellants 72
Totale 12.465
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Categoria #
all - tutte 31.411
article - articoli 6.106
book - libri 0
conference - conferenze 22.071
curatela - curatele 0
other - altro 0
patent - brevetti 1.247
selected - selezionate 0
volume - volumi 1.987
Totale 62.822
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021283 0 0 0 0 0 0 0 0 0 83 46 154
2021/2022699 36 82 44 33 111 39 25 55 20 53 57 144
2022/20231.081 158 110 45 97 102 104 7 65 140 142 55 56
2023/2024462 32 75 28 39 19 97 44 20 2 34 18 54
2024/20251.644 26 31 57 39 334 137 59 158 253 91 201 258
2025/20264.694 1.049 830 296 335 252 276 745 233 218 460 0 0
Totale 12.465