COLOMBO, GIOVANNI
 Distribuzione geografica
Continente #
NA - Nord America 4.776
EU - Europa 3.777
AS - Asia 1.812
SA - Sud America 390
AF - Africa 105
OC - Oceania 6
Continente sconosciuto - Info sul continente non disponibili 4
Totale 10.870
Nazione #
US - Stati Uniti d'America 4.627
RU - Federazione Russa 1.332
IT - Italia 997
SG - Singapore 675
CN - Cina 575
BR - Brasile 340
UA - Ucraina 271
DE - Germania 209
VN - Vietnam 199
SE - Svezia 184
FR - Francia 133
FI - Finlandia 132
ES - Italia 129
CA - Canada 121
GB - Regno Unito 117
NL - Olanda 84
IN - India 82
AT - Austria 66
IE - Irlanda 62
MA - Marocco 40
JO - Giordania 39
CI - Costa d'Avorio 32
JP - Giappone 29
KR - Corea 26
HK - Hong Kong 25
BD - Bangladesh 23
IR - Iran 23
AR - Argentina 21
IQ - Iraq 19
TR - Turchia 19
MX - Messico 17
BE - Belgio 14
ZA - Sudafrica 14
PL - Polonia 12
PK - Pakistan 10
EC - Ecuador 9
PH - Filippine 9
CH - Svizzera 8
ID - Indonesia 8
IL - Israele 8
KE - Kenya 6
KG - Kirghizistan 6
RO - Romania 6
UZ - Uzbekistan 6
VE - Venezuela 6
SA - Arabia Saudita 5
NP - Nepal 4
PE - Perù 4
PY - Paraguay 4
TH - Thailandia 4
TW - Taiwan 4
AU - Australia 3
AZ - Azerbaigian 3
CR - Costa Rica 3
CZ - Repubblica Ceca 3
DZ - Algeria 3
EG - Egitto 3
EU - Europa 3
NZ - Nuova Zelanda 3
AL - Albania 2
CO - Colombia 2
DO - Repubblica Dominicana 2
HN - Honduras 2
HU - Ungheria 2
LK - Sri Lanka 2
LT - Lituania 2
TN - Tunisia 2
AE - Emirati Arabi Uniti 1
AO - Angola 1
BG - Bulgaria 1
BH - Bahrain 1
BN - Brunei Darussalam 1
BO - Bolivia 1
BY - Bielorussia 1
BZ - Belize 1
CL - Cile 1
DK - Danimarca 1
DM - Dominica 1
EE - Estonia 1
GT - Guatemala 1
HR - Croazia 1
IS - Islanda 1
KZ - Kazakistan 1
LA - Repubblica Popolare Democratica del Laos 1
LB - Libano 1
LU - Lussemburgo 1
MC - Monaco 1
MU - Mauritius 1
MY - Malesia 1
NG - Nigeria 1
NO - Norvegia 1
PS - Palestinian Territory 1
PT - Portogallo 1
QA - Qatar 1
RS - Serbia 1
SD - Sudan 1
SK - Slovacchia (Repubblica Slovacca) 1
SN - Senegal 1
SR - Suriname 1
TT - Trinidad e Tobago 1
Totale 10.868
Città #
Ashburn 523
Chandler 379
Singapore 362
Fairfield 360
Woodbridge 345
Milan 313
Santa Clara 250
Ann Arbor 244
Wilmington 220
Houston 203
Moscow 169
Jacksonville 157
Seattle 143
Beijing 127
Cambridge 122
Málaga 119
Hefei 118
Dearborn 110
Council Bluffs 100
Ottawa 92
Boardman 87
Lawrence 82
Medford 81
Dong Ket 77
Los Angeles 71
Dallas 68
Dublin 61
Vienna 61
San Jose 57
New York 53
Helsinki 52
Amman 39
Buffalo 39
Ciampino 37
Des Moines 33
Abidjan 32
São Paulo 28
Gavirate 25
Kenitra 25
Chennai 21
Redwood City 21
Amsterdam 20
Rome 20
Tokyo 20
The Dalles 19
Redmond 18
Hong Kong 17
Ho Chi Minh City 16
Nanjing 16
Washington 16
London 15
Brussels 14
Changsha 14
Hanoi 14
Montreal 13
Nave 13
Norwalk 13
Rio de Janeiro 13
Bovisio Masciago 12
Bologna 11
Casablanca 11
Frankfurt am Main 11
Palakkad 11
Warsaw 11
Baveno 10
Chicago 10
Denver 10
Genzano Di Roma 10
Giussano 10
Johannesburg 10
Monza 10
Atlanta 9
Belo Horizonte 9
Legnano 9
Porto Alegre 9
Seoul 9
Shanghai 9
Verona 9
Auburn Hills 8
Falkenstein 8
Mountain View 8
Phoenix 8
San Diego 8
Boston 7
College Station 7
Dhaka 7
Jinan 7
Munich 7
San Francisco 7
Tianjin 7
Baghdad 6
Brooklyn 6
Columbus 6
Istanbul 6
Jakarta 6
Mumbai 6
Nairobi 6
Parma 6
Stockholm 6
Tashkent 6
Totale 6.126
Nome #
Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants 284
A method for mechanical activation of powders by means of balls 259
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 255
Aerospace Propulsion Research Activities at SPlab. Overview and Results 254
Adiabatic Pyrolysis of Solid Propellants 251
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 236
Aluminum Particle Size Influence on Ignition and Combustion of AP/HTPB/Al Solid Rocket Propellants 224
A Survey of Pressure-Driven Burning of Energetic Solids with Arrhenius Surface Pyrolysis 213
Evaluation of a Ramjet Model in a Supersonic High-Enthalpy Tunnel 212
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 210
Characterization and Combustion of Aluminum Nanopowders in Energetic Systems 206
Hybrid Combustion Studies on Regression Rate Enhancement and Transient Ballistic Response 205
Aggregation Versus Agglomeration in Metallized Solid Rocket Propellants 184
Time-resolved burning of solid fuels for hybrid rocket propulsion 173
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 173
Microstructure Effects in Aluminized Solid Rocket Propellants 168
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 168
Particulate Phase Evolution Inside Solid Rocket Motors: Preliminary Results 162
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 158
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 158
Innovative Metallized Formulations for Solid or Hybrid Rocket Propulsion 153
An Hybrid Microcombustor for Regression Rate Measurements 148
Ballistic Properties of Nano-Aluminized High-Energy Materials (HEM) 143
PDL of Micro and Nanoaluminized Laboratory Propellants for Space Applications 142
Experimental Laboratory Characterization of Charring Thermal Insulators 140
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 139
Aggregation Vs. Agglomeration in Metallized Solid Rocket Propellants 138
Characterization of nAl powders for rocket propulsion 135
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 133
Micro and Nano Aluminized Solid Propellants Behavior Under Transient Burning Conditions 132
Experimental Investigation of Metallized Hybrid Rocket Fuels 131
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 131
Burning Stability of Double Base Propellants 129
Burning of Metallized Composite Solid Rocket Propellants: Toward Nanometric Fuel Size 129
Degradation of a Thermal Insulator Under Vibration and Acceleration 125
Surface Pyrolysis of High Energy Materials 125
Advances in Hybrid Rocket Propulsion 125
The Measurement of Emissivity of Charring Ablative Materials 124
Nano-Ingredients for Rocket Propulsion: Performance Evaluation and Diagnostics 124
Magnesium and Aluminum Ignition in CO2 Atmosphere 123
Advances in Hybrid Propulsion 123
Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants 122
Effect of Metallized Powders as Fuel Additives in AP/HTPB-Based Solid Rocket Propellants 122
Advances in Hybrid Propulsion at the Space Propulsion Laboratory of Politecnico di Milano 121
Experimental Study of Solid-Propellant Ignition Transient and Flame Spreading Under Convective Flows 121
Nano Vs. Micro Iron Oxide Catalysts for Composite Solid Rocket Propellants 120
Influence of Additives on the Ballistic Behavior of Natural and Syntetic Elastomers/AN Based Solid Propellants 119
Iron Oxide Catalysis: Comparison of Micro and Nano Sized Particles 117
Regression Rate Measurements in Lab-Scale Hybrid Burners 117
Steady and Transient Burning of Microaluminized Solid Rocket Propellants 116
Effects of Metal Oxides on the Burning Rate of Ammonium Nitrate Based Solid Rocket Propellants 115
Modeling of Diffusive and Premixed Flame of AP/HTPB Laminate Propellant 115
Burning Rate Visualization with Digital High-Speed Color Camera 114
Anomalous Burning of Ammonium Perchlorate-Based Nonmetallized Solid Rocket Propellants 114
Experimental Investigation of Transient Combustion in a Hybrid 2D Lab-Scale Burner by a Wire-Cut Transducer Technique 107
Iron Oxide Catalysts for Composite Solid Rocket Propellants 105
Agglomeration Effects in Metallized Solid Rocket Propellants 105
Combustion Behaviour Investigation of Solid Fuels Using a Micro-Sized Hybrid Rocket Motor 103
Regression Rate Measurements of Hybrid Rocket Metallized Solid Fuels: Influence of Oxidizer Mass Flux and Pressure 103
Nanometric Powders Dispersion in a Polymeric Matrix 100
The FP7 Spartan Program Status and Achievements 98
Sensore di ablazione e velocità di combustione per materiali solidi 98
Chemical and Physical Characterization of Nano-Aluminum Powders 97
Modeling of diffusion and premixed flame of AP/HTPB laminate propellant 96
Coating Nano-sized Aluminum to Improve Solid Rocket Propellant Performance 96
Ignition and combustion of hydroxyl-terminated polybutadiene (HTPB)-based solid fuels loaded with innovative micrometer-sized metals 96
Ignition and Combustion of HTPB-based Solid Fuels Loaded with Micron-sized Metals 92
Characterization of Ablative Thermal Protections Used in Space Propulsion Systems 84
Transient Modeling of Spacewise Thick Flames for Rocket Propulsion 84
Setting up an Hybrid Microcombustor 84
Magnesium and Aluminum Ignition in CO2 Atmosphere 84
Thermal Protections Degradation Under Mechanical Loads 81
End-To-end Flight Test for Planetary Landing, an Unprecedented Approach in Europe 81
Radiative Heat Feedback in Aluminized Hybrid Fuel Combustion 80
Nano Energetics for Aerospace Propulsion 79
Transient Burning of Nanoaluminized Solid Propellants 78
Combustion Response to Laser Radiation of Composite AP/HTPB Propellants 77
Mechanical Behavior of Aluminized Solid Fuels for Hybrid Rockets 74
Nano vs. Micro Catalyst Effects on Solid Rocket Propellants 71
Low Temperature Gas Generators Propellants 69
Low Temperature Gas Generator Propellants 64
Oscillatory Burning of Composite Propellants Near Pressure Deflagration Limit 64
Totale 10.928
Categoria #
all - tutte 28.899
article - articoli 5.690
book - libri 0
conference - conferenze 20.230
curatela - curatele 0
other - altro 0
patent - brevetti 1.149
selected - selezionate 0
volume - volumi 1.830
Totale 57.798


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021476 0 0 0 0 0 0 70 81 42 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
2025/20263.157 1.049 830 296 335 252 276 119 0 0 0 0 0
Totale 10.928