MASSENI, FILIPPO
 Distribuzione geografica
Continente #
EU - Europa 3.492
AS - Asia 2.836
NA - Nord America 2.442
Continente sconosciuto - Info sul continente non disponibili 224
SA - Sud America 210
AF - Africa 41
OC - Oceania 4
Totale 9.249
Nazione #
US - Stati Uniti d'America 2.339
IT - Italia 2.224
VN - Vietnam 723
SG - Singapore 691
CN - Cina 548
RU - Federazione Russa 435
BD - Bangladesh 213
BR - Brasile 180
KR - Corea 166
DE - Germania 147
HK - Hong Kong 138
FR - Francia 134
GB - Regno Unito 113
IN - India 83
IE - Irlanda 80
BE - Belgio 79
NL - Olanda 62
CA - Canada 59
TR - Turchia 54
JP - Giappone 38
SE - Svezia 37
ES - Italia 36
PH - Filippine 27
FI - Finlandia 26
TH - Thailandia 24
ID - Indonesia 22
UA - Ucraina 19
PT - Portogallo 17
PK - Pakistan 16
IQ - Iraq 14
TW - Taiwan 14
BG - Bulgaria 13
AE - Emirati Arabi Uniti 11
AR - Argentina 11
AT - Austria 11
CH - Svizzera 11
PL - Polonia 11
MX - Messico 9
ZA - Sudafrica 9
CR - Costa Rica 8
IR - Iran 8
KZ - Kazakistan 8
NG - Nigeria 8
MY - Malesia 7
EG - Egitto 6
NO - Norvegia 6
HN - Honduras 5
IL - Israele 5
IS - Islanda 5
JM - Giamaica 5
JO - Giordania 5
RO - Romania 5
UZ - Uzbekistan 5
AL - Albania 4
AU - Australia 4
CZ - Repubblica Ceca 4
DZ - Algeria 4
GT - Guatemala 4
PY - Paraguay 4
TT - Trinidad e Tobago 4
BB - Barbados 3
CO - Colombia 3
EC - Ecuador 3
GR - Grecia 3
KE - Kenya 3
NP - Nepal 3
PR - Porto Rico 3
VE - Venezuela 3
BY - Bielorussia 2
CL - Cile 2
ET - Etiopia 2
GE - Georgia 2
LB - Libano 2
LT - Lituania 2
MA - Marocco 2
MG - Madagascar 2
OM - Oman 2
PE - Perù 2
SA - Arabia Saudita 2
SN - Senegal 2
TN - Tunisia 2
AD - Andorra 1
BA - Bosnia-Erzegovina 1
BH - Bahrain 1
BO - Bolivia 1
DK - Danimarca 1
EE - Estonia 1
EU - Europa 1
GA - Gabon 1
GD - Grenada 1
GP - Guadalupe 1
HU - Ungheria 1
KG - Kirghizistan 1
LA - Repubblica Popolare Democratica del Laos 1
MM - Myanmar 1
NI - Nicaragua 1
TL - Timor Orientale 1
UY - Uruguay 1
Totale 9.025
Città #
Turin 716
Singapore 442
San Jose 343
Ashburn 327
Milan 247
Ho Chi Minh City 182
Hanoi 172
Dallas 148
Hefei 139
Rome 131
Seoul 126
Chandler 107
Beijing 104
Hong Kong 103
Council Bluffs 99
Santa Clara 98
Dublin 77
Los Angeles 77
Brussels 73
New York 71
Moscow 70
Torino 65
Southend 55
Chicago 48
Princeton 46
Da Nang 41
Boardman 40
Phoenix 36
Savigliano 35
Ann Arbor 34
Naples 34
Houston 33
Berlin 27
Haiphong 27
Lauterbourg 26
Amsterdam 25
Genoa 25
Nichelino 25
Frankfurt am Main 24
Istanbul 24
Shanghai 23
Vittoria 23
Buffalo 22
Florence 20
The Dalles 20
Figino 19
Woodbridge 19
Bari 17
Montreal 17
Munich 17
Seattle 17
Bologna 15
Fairfield 14
Palermo 14
San Ramon 14
Helsinki 13
Jakarta 13
Tokyo 13
Toronto 13
West Lafayette 13
Cangzhou 12
Manchester 12
Bangkok 11
Orem 11
Washington 11
Arcos de Valdevez 10
Arlington 10
Bern 10
Biên Hòa 10
Chennai 10
Fremont 10
Nuremberg 10
Paris 10
Roccavione 10
San Donato Milanese 10
Sofia 10
São Paulo 10
Wilmington 10
Cambridge 9
Carmagnola 9
Hải Dương 9
Lappeenranta 9
Miami 9
Padua 9
Pescara 9
Taranto 9
Thái Nguyên 9
Bilbao 8
Cagliari 8
Changsha 8
Dearborn 8
Frisco 8
Guangzhou 8
Martina Franca 8
Monza 8
Ankara 7
Camporosso 7
Canelli 7
Denver 7
Johannesburg 7
Totale 5.225
Nome #
Rheological and Mechanical Characterization of 3D Printable Solid Propellant Slurry 409
Solid Rocket Propellant Photo-Polymerization with an In-House LED-UV Prototype 397
Advancements in Photocurable Solid Propellantsfor Additive Manufacturing 368
Optimization Approaches Under Uncertainty for Hybrid Rocket Engines 330
Evaluation of UV-Curable Solid Rocket Propellants’ Properties for Advanced 3D Printing Technologies 297
Multiphysics Modeling for Combustion Instability in Paraffin-Fueled Hybrid Rocket Engines 291
Design Optimization of a Mg/CO2 Hybrid Rocket Engine for Mars Ascent Vehicles 282
Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance 282
Comparison of Robust Design Approaches for Hybrid Rocket Engines 268
Multi physics modelling for a hybrid rocket engine with liquefying fuel: a sensitivity analysis on combustion instability 266
Multi-objective Optimization of Electric Pumps for Hybrid Rocket Engines 264
Hybrid rocket engine design optimization at politecnico di torino: A review 258
Optimal Design of Hybrid Rocket Small Satellite Launchers: Ground Versus Airborne Launch 256
Emission-Driven Hybrid Rocket Engine Optimization for Small Launchers 255
Viability of an Electrically Driven Pump-Fed Hybrid Rocket for Small Launcher Upper Stages 247
Deterministic and Robust Optimization of Hybrid Rocket Engines for Small Satellite Launchers 243
Numerical investigation of different configurations for hydrogen fuelled jet engine combustors 241
Robust Design Approaches for Hybrid Rocket Upper Stage 239
Swirl Injection Modeling for Paraffin-Based Hybrid Rocket Engines Combustion Instabilities 227
Optimal Design of Electrically Fed Hybrid Mars Ascent Vehicle 220
Comparison of Methods for Thermodynamic Modelling of Cryogenic Storage Systems for Aerospace Applications 208
Integrated Numerical Modeling of a Hydrogen Turbofan Engine and Fuel System With Alternative Thermodynamic Cycles 208
Numerical Validation of a Swirl Injection Model for a Paraffin-Based Hybrid Rocket Engine 206
Pintle Injector Spray Study via Physics-Based Spray Model and Generative Adversarial Networks 195
NOx Emission Prediction of a Lean Premixed Hydrogen Combustor via Reactor Network Analysis 177
Low-Order Models for Low-Frequency Combustion Instability in Hybrid Rocket Engines 175
Chemical Reactor Network for Hybrid Rocket Engines Optimization 171
A Numerical Method for Burnback Analysis of UV-cured Solid Rocket Propellant Grains 171
Multiphysics Modelling of a Hybrid Rocket Engine 169
Towards the Integration of Surrogate Models in the Robust Optimization of Hybrid Rocket Engines 143
Optimal Design Comparison of Hybrid Rocket for Small Satellite Launchers 138
Generalizable Graph Neural Operators for Field Inversion Based RANS Corrections 138
Optimization of Hybrid Rocket Engines for Small Satellite Launchers 133
Uncertainty Analysis and Robust Design for a Hybrid Rocket Upper Stage 133
Inverse Design of Additive Manufactured Rocket Propellant Grains with Non-Uniform Properties 123
Reduction of Chemical Kinetic Mechanisms for Oxygen/Methane Liquid Rocket Engines 123
Uncertainty Analysis and Robust Design for Hybrid Rocket Engines 119
Robust Design of Hybrid Rocket Engine for Small Satellite Launchers 119
Optimization of Solid Rocket Motor Grains Exploiting Non-Uniform Ballistic Properties of 3D-Printed Propellants 117
Multi-Fidelity Modeling of a Lean Premixed Swirl-Stabilized Hydrogen Burner with Axial Air Injection 113
Optimal battery selection for hybrid rocket engine 112
A Chemical Reactor Network methodology for estimating NOx emissions under non-premixed lean hydrogen combustion with water injection 99
Uncertainty analysis and robust design for hybrid rocket engines 91
Optimal battery selection for hybrid rocket engine 90
Reduced-Order Modeling and Active Subspace to Support Shape Optimization of Centrifugal Pumps 46
Experimental investigation of cryogenic tank chilldown and boil-off phenomena using liquid nitrogen 32
FIELD-INVERSION-GUIDED GENE EXPRESSION PROGRAMMING FOR RANS 20
Chemical Reactor Network for Hybrid Rocket Engine Optimization 16
Use of Convolutional Neural Networks for Multifidelity CFD Problems 9
Numerical Simulation of NOx Emissions in a Lean Premixed Hydrogen Combustor Using Different Levels of Fidelity 8
Uncertainty Quantification and Computational Cost Reduction of a Chemical Reactor Network for a Hydrogen Combustor 7
Totale 9.249
Categoria #
all - tutte 24.523
article - articoli 10.442
book - libri 0
conference - conferenze 13.346
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 48.311


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022282 0 0 0 31 25 19 42 22 22 37 39 45
2022/2023577 21 55 24 36 43 63 43 97 92 28 26 49
2023/2024814 28 45 38 66 48 133 97 169 38 46 66 40
2024/20251.499 24 82 55 121 103 85 146 140 170 113 198 262
2025/20264.599 213 188 288 288 188 195 600 442 1.009 432 285 471
2026/2027834 203 159 267 205 0 0 0 0 0 0 0 0
Totale 9.249