COLOMBO, GIOVANNI
 Distribuzione geografica
Continente #
NA - Nord America 5.909
EU - Europa 4.127
AS - Asia 2.353
SA - Sud America 411
AF - Africa 113
OC - Oceania 6
Continente sconosciuto - Info sul continente non disponibili 4
Totale 12.923
Nazione #
US - Stati Uniti d'America 5.728
RU - Federazione Russa 1.332
IT - Italia 1.202
SG - Singapore 730
CN - Cina 691
VN - Vietnam 352
BR - Brasile 350
UA - Ucraina 271
DE - Germania 224
FR - Francia 217
SE - Svezia 184
FI - Finlandia 153
CA - Canada 137
ES - Italia 130
GB - Regno Unito 129
KR - Corea 113
IN - India 93
NL - Olanda 87
JP - Giappone 79
AT - Austria 66
IE - Irlanda 65
HK - Hong Kong 43
JO - Giordania 40
MA - Marocco 40
CI - Costa d'Avorio 32
BD - Bangladesh 26
AR - Argentina 24
IQ - Iraq 23
IR - Iran 23
MX - Messico 23
TR - Turchia 19
PL - Polonia 16
ZA - Sudafrica 16
BE - Belgio 15
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
HN - Honduras 5
AE - Emirati Arabi Uniti 4
AZ - Azerbaigian 4
CL - Cile 4
CR - Costa Rica 4
PE - Perù 4
PY - Paraguay 4
AU - Australia 3
CO - Colombia 3
CZ - Repubblica Ceca 3
EG - Egitto 3
EU - Europa 3
MY - Malesia 3
NZ - Nuova Zelanda 3
TN - Tunisia 3
AL - Albania 2
AO - Angola 2
BO - Bolivia 2
DM - Dominica 2
DO - Repubblica Dominicana 2
GT - Guatemala 2
HU - Ungheria 2
LK - Sri Lanka 2
LT - Lituania 2
PT - Portogallo 2
QA - Qatar 2
TT - Trinidad e Tobago 2
AI - Anguilla 1
BG - Bulgaria 1
BH - Bahrain 1
BN - Brunei Darussalam 1
BY - Bielorussia 1
BZ - Belize 1
DK - Danimarca 1
EE - Estonia 1
GA - Gabon 1
HR - Croazia 1
IS - Islanda 1
JM - Giamaica 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
Totale 12.916
Città #
Ashburn 624
San Jose 475
Singapore 393
Milan 381
Chandler 379
Fairfield 360
Woodbridge 345
Santa Clara 263
Ann Arbor 244
Wilmington 220
Houston 205
Moscow 169
Jacksonville 157
Seattle 144
The Dalles 143
Beijing 137
Dallas 137
Council Bluffs 134
Boardman 124
Cambridge 122
Hefei 119
Málaga 119
Dearborn 112
Ottawa 92
Seoul 91
Los Angeles 83
Lawrence 82
Medford 81
Dong Ket 77
Lauterbourg 74
Helsinki 73
Dublin 64
Tokyo 64
North Charleston 62
Vienna 61
New York 58
Hanoi 55
Ho Chi Minh City 55
Rome 48
Buffalo 41
Amman 40
Ciampino 37
Des Moines 33
Abidjan 32
Hong Kong 30
São Paulo 30
Chennai 25
Gavirate 25
Kenitra 25
Orem 24
Frankfurt am Main 23
Amsterdam 22
Redwood City 21
Nanjing 19
Washington 19
Bologna 18
Redmond 18
Montreal 17
Changsha 15
Denver 15
Las Vegas 15
London 15
Warsaw 15
Atlanta 14
Brussels 14
Da Nang 13
Nave 13
Norwalk 13
Rio de Janeiro 13
Shanghai 13
Bovisio Masciago 12
Chicago 12
Johannesburg 12
Palakkad 12
Brooklyn 11
Casablanca 11
San Francisco 11
Verona 11
Baveno 10
Genzano Di Roma 10
Giussano 10
Monza 10
Naples 10
Phoenix 10
Belo Horizonte 9
Boston 9
Guangzhou 9
Legnano 9
Mumbai 9
Porto Alegre 9
Shenzhen 9
Turin 9
Auburn Hills 8
Falkenstein 8
Haiphong 8
Hải Dương 8
Long Beach 8
Mountain View 8
Parma 8
San Diego 8
Totale 7.581
Nome #
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 320
A method for mechanical activation of powders by means of balls 300
Adiabatic Pyrolysis of Solid Propellants 297
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 294
Aerospace Propulsion Research Activities at SPlab. Overview and Results 290
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 275
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 266
Aluminum Particle Size Influence on Ignition and Combustion of AP/HTPB/Al Solid Rocket Propellants 258
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 250
A Survey of Pressure-Driven Burning of Energetic Solids with Arrhenius Surface Pyrolysis 244
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 239
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 236
Microstructure Effects in Aluminized Solid Rocket Propellants 213
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 208
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 205
Time-resolved burning of solid fuels for hybrid rocket propulsion 198
Particulate Phase Evolution Inside Solid Rocket Motors: Preliminary Results 198
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 197
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 188
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 186
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 186
An Hybrid Microcombustor for Regression Rate Measurements 174
Aggregation Vs. Agglomeration in Metallized Solid Rocket Propellants 169
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 169
Ballistic Properties of Nano-Aluminized High-Energy Materials (HEM) 163
PDL of Micro and Nanoaluminized Laboratory Propellants for Space Applications 163
Advances in Hybrid Propulsion 163
Experimental Laboratory Characterization of Charring Thermal Insulators 161
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 158
Characterization of nAl powders for rocket propulsion 153
Experimental Study of Solid-Propellant Ignition Transient and Flame Spreading Under Convective Flows 152
Experimental Investigation of Metallized Hybrid Rocket Fuels 151
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 151
Burning of Metallized Composite Solid Rocket Propellants: Toward Nanometric Fuel Size 150
Advances in Hybrid Rocket Propulsion 149
Micro and Nano Aluminized Solid Propellants Behavior Under Transient Burning Conditions 147
Advances in Hybrid Propulsion at the Space Propulsion Laboratory of Politecnico di Milano 147
Burning Stability of Double Base Propellants 145
Effects of Metal Oxides on the Burning Rate of Ammonium Nitrate Based Solid Rocket Propellants 145
Surface Pyrolysis of High Energy Materials 144
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 143
The Measurement of Emissivity of Charring Ablative Materials 142
Influence of Additives on the Ballistic Behavior of Natural and Syntetic Elastomers/AN Based Solid Propellants 142
Effect of Metallized Powders as Fuel Additives in AP/HTPB-Based Solid Rocket Propellants 142
Nano-Ingredients for Rocket Propulsion: Performance Evaluation and Diagnostics 142
Steady and Transient Burning of Microaluminized Solid Rocket Propellants 141
Iron Oxide Catalysis: Comparison of Micro and Nano Sized Particles 141
Nano Vs. Micro Iron Oxide Catalysts for Composite Solid Rocket Propellants 141
Regression Rate Measurements in Lab-Scale Hybrid Burners 141
Magnesium and Aluminum Ignition in CO2 Atmosphere 139
Burning Rate Visualization with Digital High-Speed Color Camera 138
Iron Oxide Catalysts for Composite Solid Rocket Propellants 134
Degradation of a Thermal Insulator Under Vibration and Acceleration 133
Experimental Investigation of Transient Combustion in a Hybrid 2D Lab-Scale Burner by a Wire-Cut Transducer Technique 132
Modeling of Diffusive and Premixed Flame of AP/HTPB Laminate Propellant 130
Anomalous Burning of Ammonium Perchlorate-Based Nonmetallized Solid Rocket Propellants 129
Agglomeration Effects in Metallized Solid Rocket Propellants 128
Nanometric Powders Dispersion in a Polymeric Matrix 126
Regression Rate Measurements of Hybrid Rocket Metallized Solid Fuels: Influence of Oxidizer Mass Flux and Pressure 124
Ignition and combustion of hydroxyl-terminated polybutadiene (HTPB)-based solid fuels loaded with innovative micrometer-sized metals 123
Sensore di ablazione e velocità di combustione per materiali solidi 120
Combustion Behaviour Investigation of Solid Fuels Using a Micro-Sized Hybrid Rocket Motor 118
Setting up an Hybrid Microcombustor 115
Coating Nano-sized Aluminum to Improve Solid Rocket Propellant Performance 115
Modeling of diffusion and premixed flame of AP/HTPB laminate propellant 114
Chemical and Physical Characterization of Nano-Aluminum Powders 112
The FP7 Spartan Program Status and Achievements 111
Ignition and Combustion of HTPB-based Solid Fuels Loaded with Micron-sized Metals 109
Characterization of Ablative Thermal Protections Used in Space Propulsion Systems 108
Thermal Protections Degradation Under Mechanical Loads 106
End-To-end Flight Test for Planetary Landing, an Unprecedented Approach in Europe 106
Nano Energetics for Aerospace Propulsion 104
Transient Modeling of Spacewise Thick Flames for Rocket Propulsion 104
Transient Burning of Nanoaluminized Solid Propellants 104
Magnesium and Aluminum Ignition in CO2 Atmosphere 104
Radiative Heat Feedback in Aluminized Hybrid Fuel Combustion 99
Combustion Response to Laser Radiation of Composite AP/HTPB Propellants 95
Mechanical Behavior of Aluminized Solid Fuels for Hybrid Rockets 89
Nano vs. Micro Catalyst Effects on Solid Rocket Propellants 86
Low Temperature Gas Generators Propellants 86
Oscillatory Burning of Composite Propellants Near Pressure Deflagration Limit 83
Low Temperature Gas Generator Propellants 80
Totale 12.981
Categoria #
all - tutte 33.694
article - articoli 6.482
book - libri 0
conference - conferenze 23.797
curatela - curatele 0
other - altro 0
patent - brevetti 1.328
selected - selezionate 0
volume - volumi 2.087
Totale 67.388


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
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
2025/20265.140 1.049 830 296 335 252 276 745 233 218 477 101 328
2026/202770 70 0 0 0 0 0 0 0 0 0 0 0
Totale 12.981