Catalogo dei prodotti della ricerca

BIANCHI, DANIELE
 Distribuzione geografica
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Continente #
NA - Nord America 3.190
EU - Europa 2.064
AS - Asia 476
AF - Africa 58
SA - Sud America 37
OC - Oceania 4
Continente sconosciuto - Info sul continente non disponibili 3
Totale 5.832
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Nazione #
US - Stati Uniti d'America 3.158
IT - Italia 1.357
IN - India 176
CN - Cina 153
SE - Svezia 151
DE - Germania 91
GB - Regno Unito 86
FR - Francia 70
FI - Finlandia 60
JP - Giappone 51
TG - Togo 50
UA - Ucraina 47
GR - Grecia 38
BG - Bulgaria 35
CA - Canada 32
IE - Irlanda 30
AR - Argentina 19
SG - Singapore 19
BR - Brasile 18
PL - Polonia 18
BE - Belgio 16
NL - Olanda 15
TR - Turchia 15
KR - Corea 14
RU - Federazione Russa 14
IR - Iran 10
AZ - Azerbaigian 9
IL - Israele 9
RO - Romania 8
CH - Svizzera 7
ES - Italia 6
AE - Emirati Arabi Uniti 5
PT - Portogallo 5
AU - Australia 4
HK - Hong Kong 4
PK - Pakistan 4
EU - Europa 3
TW - Taiwan 3
ZA - Sudafrica 3
AT - Austria 2
DK - Danimarca 2
DZ - Algeria 2
ET - Etiopia 2
ID - Indonesia 2
SK - Slovacchia (Repubblica Slovacca) 2
CZ - Repubblica Ceca 1
HR - Croazia 1
LT - Lituania 1
MY - Malesia 1
SA - Arabia Saudita 1
SC - Seychelles 1
SI - Slovenia 1
Totale 5.832
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Città #
Rome 517
Fairfield 462
Ashburn 281
Chandler 271
Woodbridge 233
Seattle 207
Houston 184
Cambridge 170
Wilmington 169
Ann Arbor 137
Princeton 108
Dearborn 85
San Paolo di Civitate 69
Milan 66
Plano 64
Lomé 50
Lawrence 49
Millbury 49
Beijing 46
Southend 46
Orte 44
Tokyo 43
San Diego 42
Boston 39
Andover 35
Sofia 35
Turin 30
Dresden 27
New York 24
Dublin 21
Norwalk 20
Federal 18
West Lafayette 18
Toronto 16
Brescia 15
London 15
Naples 15
Bremen 13
Brussels 13
Des Moines 13
Redwood City 13
Hefei 11
Hyderabad 11
Jacksonville 11
Ladispoli 11
Sanluri 11
Boardman 10
Baku 9
Kunming 9
Westminster 9
Castledermot 8
Falls Church 8
Munich 8
Speyer 8
São José dos Campos 8
Bari 7
Catania 7
Le Plessis-Robinson 7
Meudon 7
Monte Porzio Catone 7
Nanjing 7
Rouen 7
San Mateo 7
Ankara 6
Cagliari 6
Haifa 6
Montreuil 6
Moscow 6
North York 6
Palermo 6
São Paulo 6
Velletri 6
Auburn 5
Cankaya 5
Fiumicino 5
Los Angeles 5
Marbella 5
Perugia 5
Seongdong-gu 5
Bern 4
Central 4
Civitavecchia 4
Enschede 4
Frosinone 4
Glane 4
Glen Allen 4
Guangzhou 4
Lido Di Ostia 4
Mede 4
Modena 4
Montesilvano Marina 4
Paris 4
Pisa 4
Prato 4
Priverno 4
Torrita di Siena 4
Varano Borghi 4
Venezia 4
Wenzhou 4
Aprilia 3
Totale 4.132
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Nome #
Numerical estimation of nozzle throat heat flux in oxygen-methane rocket engines 125
Numerical analysis of nozzle material thermochemical erosion in hybrid rocket engines 122
Navier-stokes simulation of graphite nozzle erosion under a wide range of pressure conditions 119
Simulation of gaseous oxygen/hydroxyl-terminated polybutadiene hybrid rocket flowfields and comparison with experiments 108
Multiphase effects on solid rocket nozzle performance 106
Chemical reaction effects on heat loads of CH4/O2 and H2/O2 rockets 105
Convective and radiative contributions to wall heat transfer in liquid rocket Engine thrust chambers 100
Radiation and Roughness Effects on the Thermochemical Erosion of Ablative Materials in Rocket Nozzles 99
CSP-based chemical kinetics mechanisms simplification strategy for non-premixed combustion: An application to hybrid rocket propulsion 97
Modeling and simulation of paraffin–based hybrid rocket internal ballistics 95
Modeling multiphase effects on pressure oscillations in solid propulsion 93
Chemical Reaction Effects on Wall Heat Flux in Liquid Rocket Thrust Chambers 91
Chemical Erosion of Carbon-Phenolic Rocket Nozzles with Finite-Rate Surface Chemistry 89
Convective and radiative wall heat transfer in liquid rocket thrust chambers 88
Experimental and numerical methods for radiative wall heat flux predictions in paraffin–based hybrid rocket engines 87
Modeling of high density polyethylene regression rate in the simulation of hybrid rocket flowfields 86
Aerothermodynamic analysis of reentry flows with coupled ablation 85
Systematic strategies for thermochemical model reduction in rocket propulsion applications 85
The accuracy of reconstruction techniques for determining hybrid rocket fuel regression rate 84
Ablative material behavior in oxygen/methane thruster environment 83
Radius of curvature effects on throat thermochemical erosion in solid rocket motors 83
Numerical analysis of nozzle flows with finite-rate surface ablation and pyrolysis-gas injection 80
Aerothermoacoustics Q1D Modeling for Solid Rocket Motors Instabilities 79
Hybrid rockets with axial injector: port diameter effect on fuel regression rate 78
Coupled CFD analysis of thermochemical erosion and unsteady heat conduction in solid rocket nozzles 77
Static firing ballistic reconstruction modelling and performance extrapolation to flight in srms 76
Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles 76
Analysis and reconstruction of Zefiro 40 solid rocket motor static firing tests and extrapolation to flight 76
Numerical investigation on radiative heat loads in liquid rocket thrust chambers 75
Numerical simulation of chemical erosion in Vega solid-rocket-motor nozzles 74
A Numerical Approach for High-Temperature Flows over Ablating Surfaces 71
Modeling of paraffin-based fuels in the simulation of hybrid rocket flowfields 71
Simulations of paraffin-based hybrid rocket motors and comparison with experiments 69
Numerical simulation of hypersonic flows past three-dimensional blunt bodies through a unstructured shock-fitting solver 69
Propellant trade-off analysis for upper stage solid rocket motors performance 68
Numerical Modeling of GOX/HTPB Hybrid Rocket Flowfields and Comparison with Experiments 67
Radiation and Roughness Effects on Nozzle Thermochemical Erosion in Solid Rocket Motors 65
Numerical Analysis of Nozzle Material Thermochemical Erosion in Hybrid Rocket Engines 65
Navier-stokes simulations of hypersonic flows with coupled graphite ablation 64
Thermochemical Erosion Analysis of Carbon-Carbon Nozzles in Solid-Propellant Rocket Motors 64
A numerical approach for the study of the gas-surface interaction in carbon-phenolic solid rocket nozzles 64
Numerical simulation of chemical erosion in VEGA launcher solid-propellant rocket motor nozzles 64
Navier–Stokes simulation of graphite nozzle erosion at different pressure conditions 63
Numerical analysis of port diameter effect on hybrid rocket fuel regression rate with axial injection 63
Numerical and experimental investigation of nozzle thermochemical erosion in hybrid rockets 62
Numerical analysis of paraffin-wax/oxygen hybrid rocket engines 62
Cooling system design for an upper-stage aerospike 60
Internal ballistics modeling of high performance SRMs with coupled nozzle erosion characterization 60
Thermochemical erosion analysis for carbon-carbon rocket nozzles 59
Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles 59
Thermochemical erosion analysis for graphite/carbon-carbon rocket nozzles 55
Radius of curvature effects on throat thermochemical erosion in solid rocket motors 52
Carbon-carbon nozzle erosion and shape change in full-scale solid-rocket motors 52
CFD analysis of hybrid rocket Flowfields including fuel pyrolysis and nozzle erosion 52
Numerical Simulations of a Paraffin-Hydrogen Peroxide Hybrid Rocket with Swirl Injection 49
null 49
A family of skeletal mechanisms for methane oxidation at high pressure 48
Numerical and experimental investigation of a lab-scale paraffin motor with swirled injection of gaseous oxygen 46
Design and evaluation of aerospike nozzles for an upper stage application. 46
Modeling of ablation phenomena in space applications 42
CFD Boundary Conditions for the Interaction of Rocket Nozzle Flows with Ablating Walls 41
Cfd analysis of paraffin-based hybrid rockets with coupled nozzle erosion characterization 41
Numerical and experimental analysis of capsules ablation and shape change including heating transient effects 41
Student firing tests and launches with commercial and self-made solid rocket motors 41
Performance reconstruction of VEGA solid rocket motors: VERTA flights experience 40
Numerical analysis of nozzle heating and erosion in hybrid rockets and comparison with experiments 40
Navier-Stokes Analysis of Scale Effects on Ablation in Carbon-Carbon Rocket Nozzles 39
Cooling system analysis of a clustered module aerospike for upper-stage applications 38
Computational Analysis of Hypersonic Flows Including Finite Rate Ablation Thermochemistry 38
Parametric Numerical Study of Erosion in Solid Rocket Motor Nozzles 37
Review and implementation of engineering models of rocket film cooling and nozzle erosion 36
Propellant effects on SRM upper stage internal ballistics and performance with nozzle erosion characterization 36
Graphite nozzle erosion trends in paraffin/oxygen hybrid rockets 36
Hypersonic Flow Analysis Including Finite Rate Ablation Thermochemistry 35
A parametric study on the role of near wall chemical reactions in O2/CH4 combustion chamber heat flux evaluation 35
ASCenSIon: An innovative network to train the space access leaders of tomorrow 35
Navier-Stokes Analysis of Scale Effects on Ablation in Carbon-Carbon Rocket Nozzles 34
Modeling of swirl injection effects in a H2O2-HDPE hybrid rocket 33
A Gas-Surface Interaction Model for the Numerical Study of High Temperature Flows Over Pyrolyzing Ablative Materials 33
A sensitivity study on a cfd model for paraffin-based hybrid rockets 33
Numerical analysis of nozzle erosion in hybrid rockets and comparison with experiments 33
Practical Navier-Stokes Computations of Flowfields with Ablation Products Injection 32
Thermoacoustics Q1D Modeling in Solid Rocket Motors 31
Best Paper Certificate of Merit for the purpose of promoting technical and scientific excellence in Solid Rockets 30
Numerical simulation of hybrid rocket engine flowfields 30
Machine learning techniques for flight performance prediction of hybrid rocket engines 30
Numerical Analysis of Film Cooling and Mixture Ratio Bias in Oxygen-Methane Liquid Rocket Engines 29
A computational tool for the design of hybrid rockets 29
Ablative and catalytic behavior of carbon-based porous thermal protection materials in nitrogen plasmas 28
Solid Rocket Motor Internal Ballistics Simulation Using Eulerian Multiphase Models 28
Internal Ballistic Model with Erosion Characterization for High Performance SRMs 27
Numerical investigation on the role of thermal radiation in hybrid rocket fuel pyrolysis 27
Modeling of wall heat flux in oxygen-methane liquid rocket thrust chambers 27
Multi-disciplinary Optimization of Single-stage Hybrid Rocket with Swirl Injection for Lunar Ascent 26
CFD Study of Isothermal Ablation 26
Near wall recombination eects on the prediction of heat flux in O2/CH4 combustion chambers 26
Navier-Stokes Computations of Reentry Flowfields with Coupled Surface Ablation 25
null 24
Navier-Stokes Solutions with Surface Ablation under Reentry Conditions 22
Predictive cfd model for internal ballistics of hybrid rocket engines using supercritical paraffin-wax and oxygen 21
Totale 5.794
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Categoria #
all - tutte 16.810
article - articoli 0
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 16.810
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019364 0 0 0 0 0 0 0 0 0 75 174 115
2019/20201.128 121 30 13 44 119 223 174 134 132 70 38 30
2020/2021882 36 34 50 172 151 32 16 116 86 108 49 32
2021/2022951 13 47 86 33 120 34 18 89 99 55 128 229
2022/20231.393 230 254 97 112 104 175 56 125 116 27 40 57
2023/20241.038 79 129 88 129 151 155 101 72 69 65 0 0
Totale 6.152