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

PARAVAN, CHRISTIAN
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
EU - Europa 8.662
NA - Nord America 7.317
AS - Asia 4.171
SA - Sud America 757
AF - Africa 179
OC - Oceania 33
Continente sconosciuto - Info sul continente non disponibili 4
Totale 21.123
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 7.111
IT - Italia 3.410
RU - Federazione Russa 3.359
CN - Cina 1.189
SG - Singapore 1.181
BR - Brasile 638
VN - Vietnam 465
KR - Corea 359
FR - Francia 295
DE - Germania 256
JP - Giappone 224
SE - Svezia 194
NL - Olanda 180
GB - Regno Unito 176
FI - Finlandia 175
IE - Irlanda 156
CA - Canada 150
IN - India 126
AT - Austria 109
ES - Italia 108
HK - Hong Kong 72
PH - Filippine 71
TR - Turchia 65
BD - Bangladesh 62
UA - Ucraina 62
ID - Indonesia 60
CH - Svizzera 52
CI - Costa d'Avorio 50
MA - Marocco 47
AR - Argentina 45
JO - Giordania 38
TW - Taiwan 38
PL - Polonia 36
IQ - Iraq 34
BE - Belgio 30
ZA - Sudafrica 30
MX - Messico 28
TH - Thailandia 26
IR - Iran 25
SA - Arabia Saudita 24
EC - Ecuador 19
PK - Pakistan 19
AU - Australia 17
AE - Emirati Arabi Uniti 16
CL - Cile 16
NZ - Nuova Zelanda 16
EG - Egitto 12
CO - Colombia 11
UZ - Uzbekistan 11
GR - Grecia 10
KZ - Kazakistan 10
AZ - Azerbaigian 9
BJ - Benin 9
IL - Israele 9
MY - Malesia 9
VE - Venezuela 9
BO - Bolivia 8
DO - Repubblica Dominicana 8
KE - Kenya 8
CZ - Repubblica Ceca 6
LT - Lituania 6
NP - Nepal 6
PY - Paraguay 6
TT - Trinidad e Tobago 6
HU - Ungheria 5
PT - Portogallo 5
AL - Albania 4
DZ - Algeria 4
HN - Honduras 4
OM - Oman 4
PE - Perù 4
RO - Romania 4
TN - Tunisia 4
BG - Bulgaria 3
CR - Costa Rica 3
ET - Etiopia 3
MT - Malta 3
NO - Norvegia 3
PS - Palestinian Territory 3
QA - Qatar 3
RS - Serbia 3
SI - Slovenia 3
XK - ???statistics.table.value.countryCode.XK??? 3
BB - Barbados 2
BN - Brunei Darussalam 2
DK - Danimarca 2
GA - Gabon 2
JM - Giamaica 2
KG - Kirghizistan 2
KW - Kuwait 2
LB - Libano 2
LV - Lettonia 2
MK - Macedonia 2
MU - Mauritius 2
NG - Nigeria 2
SN - Senegal 2
SY - Repubblica araba siriana 2
AO - Angola 1
BA - Bosnia-Erzegovina 1
BH - Bahrain 1
Totale 21.111
Salva come PNG Salva come JPEG
Città #
Milan 1.302
Ashburn 996
Singapore 704
San Jose 703
Fairfield 483
Moscow 427
Chandler 376
Woodbridge 371
Seoul 306
Santa Clara 304
Hefei 279
Wilmington 241
Seattle 227
Council Bluffs 216
Houston 212
The Dalles 209
Beijing 205
Tokyo 193
Cambridge 183
Ann Arbor 174
Dallas 169
Dublin 147
Boardman 119
Lauterbourg 104
Helsinki 102
Los Angeles 100
Rome 95
Vienna 92
Ho Chi Minh City 91
Dearborn 87
Dong Ket 87
Ottawa 85
Amsterdam 84
Málaga 83
Lawrence 82
Medford 81
Redwood City 78
New York 76
Hanoi 68
Redmond 61
Davao City 58
Buffalo 57
São Paulo 56
Frankfurt am Main 55
North Charleston 53
Hong Kong 52
Abidjan 49
Ciampino 49
Bern 46
Monza 46
Jakarta 43
Gavirate 41
Orem 41
Jacksonville 40
Amman 38
Bovisio Masciago 38
Turin 37
Kent 34
Des Moines 31
Taipei 31
Las Vegas 29
Chennai 26
Nanjing 26
Segrate 26
Shanghai 26
Parma 25
Stockholm 25
Busto Arsizio 24
Kenitra 24
Rio de Janeiro 24
Riverside 24
Istanbul 23
London 23
Marnate 23
Redondo Beach 23
Giussano 22
Pedrengo 22
Brussels 21
Chicago 21
Phoenix 21
San Diego 21
Warsaw 21
Boltiere 20
Changsha 20
Islington 20
Trezzano Sul Naviglio 20
Arcene 19
Basingstoke 19
Bergamo 19
Lappeenranta 17
Washington 17
Brooklyn 16
Fremont 16
Montreal 15
Belo Horizonte 14
Berlin 14
Dhaka 14
Guangzhou 14
Johannesburg 14
Mumbai 14
Totale 11.719
Salva come PNG Salva come JPEG
Nome #
Accelerated ageing of micron- and nano-sized aluminum powders: Metal content, composition and non-isothermal oxidation reactivity 333
Aluminum powders: aging effects on metal content and thermogravimetry reactivity 296
A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion 295
Activated Aluminum Powders for Space Propulsion 293
Combustion Processes in Hybrid Rockets 289
A method for mechanical activation of powders by means of balls 286
Iron oxide as solid propellant catalyst: A detailed characterization 282
Characterization of HTPB-based Solid Fuel Formulations: Performance, Mechanical Properties, and Pollution 281
Aerospace Propulsion Research Activities at SPlab. Overview and Results 280
Burning Behavior Investigation of a Vortex Flow Pancake Hybrid Rocket Engine 273
Paraffin-Based Fuels and Energetic Additives for Hybrid Rocket Propulsion 267
Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-Based Formulations 263
Experimental data from ramjet/scramjet combustion and numerical validation perspectives 257
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization 254
Experimental evaluation of HTPB/paraffin fuel blends for hybrid rocket applications 253
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Ballistic characterization 248
A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain - Mechanical characterization 248
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
Detailed Properties of Iron Oxide Solid Propellant Catalyst 231
Nickel acetylacetonate as decomposition catalyst for HTPB-based fuels: Regression rate enhancement effects 230
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 228
Enhancing Micrometric Aluminum Reactivity by Mechanical Activation 227
A Comparative Study of the Aging Behavior of Different Nano-Sized Aluminum Powders 226
Hybrid Propulsion System for Future Rocket Applications 222
Activated and Nano-Sized Aluminum as Metal Fuels in Solid Rocket Propellants 221
Cellular Structures for Solid Fuel Grain Reinforcement: Mechanical and Combustion Performance in Conventional and Non-Conventional Hybrid Rocket Engines 220
Role of Pressure and Aluminum Size in Solid Propellant CCP Generation 219
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 219
Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine 217
Trade-Off Analysis of a New Liquid Rocket Engine 216
Prospects of Aluminum Modifications as Energetic Fuels in Chemical Rocket Propulsion 215
Analysis of Quasi-Steady and Transient Burning of Hybrid Fuels in a Laboratory-Scale Burner by an Optical Technique 210
Thermite-For-Demise (T4D): Material Selection for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 204
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 202
Diagnostics for Entrainment Characterization in Liquefying Fuel Formulations 200
Pre-burning Characterization of Nanosized Aluminum in Condensed Energetic Systems 198
Time-resolved burning of solid fuels for hybrid rocket propulsion 195
An Innovative Strategy for Paraffin-Based Fuels Reinforcement: Part II, Ballistic Characterization 195
Aging Effects on Nano-Sized Aluminum Reactivity 193
Towards High-Performing Paraffin-Based Fuels Exploiting the Armored Grain Concept 191
Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel 190
Liquid Film Cooling: Advanced Modeling and Efforts Towards Validation 187
Exploratory Investigations on Metal-Based Fuels for Airbreathing Propulsion 187
Regression Rate and Combustion Efficiency in a Vortex-Flow Hybrid Rocket Engine 185
Micro and Nano-Sized Metal Additives for Solid Fuels in Hybrid Rocket Lab-Scale Burner 184
Non-Isothermal Oxidation of Aluminum Nanopowder Coated by Hydrocarbons and Fluorohydrocarbons 184
Combustion in a Lab-Scale Vortex Flow Hybrid Rocket Engine 184
Effect of Fluorides Coated Nano-Aluminum Powder on Combustion Properties of HTPB Based Fuels 183
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner 182
Lab-Scale Investigation of Metal Hydrides as Solid Fuel Additives for Hybrid Rocket Propulsion 181
An Optical Time-Resolved Technique of Solid Fuels Burning for Hybrid Rocket Propulsion 179
Strategies for Paraffin-based Fuels Reinforcement: 3D Printing and Blending with Polymers 178
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection 177
Liquefying Fuel Combustion in a Lab-scale Vortex Flow Pancake Hybrid Rocket Engine 176
Development of Paraffin-Based Fuels for a Vortex Combustion Hybrid Rocket Engine 175
Thermite-for-Demise (T4D): Preliminary Assessment on the Effects of a Thermite Charge in Arc-Heated Wind Tunnel Experiments 171
Combustion in a Non-Conventional Hybrid Rocket Engine: Lab-Scale Testing of a Vortex Flow Pancake 171
Monte Carlo Analysis of a LEO Reentry Mission by Solid Rocket Propulsion 171
Thermite-for-Demise: Preliminary on-Ground Heat Transfer Experimental Testing 170
Thermite-for-demise (T4D): experiments and numerical modelling on solar array drive mechanism mock-ups containing thermite in an arc-heated wind tunnel 170
Impact of 3d-printing on the mechanical reinforcement and the ballistic response of paraffin-based fuels: The armored grain 170
Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum 166
Time-resolved regression rate of innovative hybrid solid fuel formulations 164
Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants 162
Liquid Film Cooling: Open-Literature Review, Modeling and Efforts Towards Validation 161
Hydrogen-Based Thrusters for Supersonic and Hypersonic Flight: Experimental Characterization 160
Thermite-for-Demise (T4D): from Material Selection to Test Campaign 159
Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise During Re-Entry 158
Vortex combustion in a hybrid rocket motor 157
Preparation and Characterization of Al/HTPB Composite for High Energetic Materials 156
Ballistic Characterization of Armored Grains with Vortex Flow Pancake Hybrid Rocket Engine 154
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels 152
Aggregation and Incipient Agglomeration in Metallized Solid Propellants and Solid Fuels for Rocket Propulsion 151
Reduction of Solid Propellants Environmental Impact: Al-Mg Mechanically Activated Fuels and AP-PSAN Blends 151
Boosting Green Propellants: the Sustainable Armored Grain for Hybrid Rocket Propulsion 149
Mechanically Activated Al/Mg Powders for Solid Rocket Propellants 149
Comparison Between Nano-Sized Aluminum Powders with Different Coatings: Physical Analyses and Performance Test 148
METODO PER LA LAVORAZIONE E/O L'ATTIVAZIONE MECCANICA DI POLVERI TRAMITE SFERE 148
Test Activities on Hybrid Rocket Engines: Combustion Analyses and Green Storable Oxidizers - A Short Review 146
Development of a Compact Hybrid Rocket Engine for Low-Cost In-Space Propulsion 144
Nano-Sized and Mechanically Activated Composites: Perspectives for Enhanced Mass Burning Rate in Aluminized Solid Fuels for Hybrid Rocket Propulsion 144
Effects of Vortex Flow Pancake Hybrid Rocket Engine Operating Parameters on Liquefying Fuel Combustion 143
Regression Rate and CCPs Measurement of Metallized Solid Fuels 142
Reconstructed Ballistic Data Versus Wax Regression-Rate Intrusive Measurement in a Hybrid Rocket 141
Regression Rate Measurements in Lab-Scale Hybrid Burners 136
Experimental activities on the paraffin-based fuel MTM in the framework of the PHAEDRA project 134
Paraffin-Based Fuels: Perspectives from Different Reinforcing Strategies and Metal Additives 133
Effects of Aluminum Composites on the Regression Rates of Solid Fuels 133
Mapping of Aluminum Particle Dispersion in Solid Rocket Fuel Formulations 129
Numerical and Experimental Investigation of a Lab-Scale Paraffin Motor with Swirled Injection of Gaseous Oxygen 127
Green Solid Fuels with Enhanced Mechanical Properties: Sustainable Waxes and Scale-Up Analysis of Armored Grains 126
Hydrolytic Space Propulsion: a New Opportunity for CubeSat Missions 125
Mixed-Hybrid Fuel Formulations: Composition, Regression Rate and Condensed Combustion Products 125
Testing Advanced Green Thermoplastic Fuels in a Vortex Hybrid Rocket Engine 123
Diagnostic Techniques for Regression Rate of Paraffin-Based Fuels in a VFP Hybrid Rocket Engine 122
Ignition and combustion of hydroxyl-terminated polybutadiene (HTPB)-based solid fuels loaded with innovative micrometer-sized metals 119
Coated Nano-Sized Aluminum Powders: Physical Analyses and Performance Tests in Hybrid Propulsion 118
Innovative Methodology for Evaluating Combustion Efficiency in Swirled Rocket Engines 117
Totale 19.108
Salva come PNG Salva come JPEG
Categoria #
all - tutte 51.799
article - articoli 13.268
book - libri 0
conference - conferenze 33.881
curatela - curatele 0
other - altro 0
patent - brevetti 974
selected - selezionate 0
volume - volumi 3.676
Totale 103.598
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021408 0 0 0 0 0 0 0 0 0 97 96 215
2021/2022974 57 104 93 48 90 64 70 100 32 71 119 126
2022/20231.417 155 112 64 122 143 130 47 109 212 150 67 106
2023/2024876 72 119 37 98 56 110 111 43 36 66 53 75
2024/20253.830 150 58 141 131 710 164 187 316 336 170 450 1.017
2025/20269.138 2.044 1.423 590 603 397 576 1.370 647 666 822 0 0
Totale 21.294