Catalogo dei prodotti della ricerca

NASUTI, Francesco
 Distribuzione geografica
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Continente #
NA - Nord America 8.709
EU - Europa 4.005
AS - Asia 1.183
AF - Africa 118
SA - Sud America 103
OC - Oceania 20
Continente sconosciuto - Info sul continente non disponibili 7
Totale 14.145
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Nazione #
US - Stati Uniti d'America 8.631
IT - Italia 2.337
IN - India 464
CN - Cina 437
SE - Svezia 293
GB - Regno Unito 234
UA - Ucraina 224
FI - Finlandia 184
DE - Germania 183
FR - Francia 128
TG - Togo 104
GR - Grecia 90
SG - Singapore 80
AR - Argentina 76
CA - Canada 73
BG - Bulgaria 71
IE - Irlanda 59
JP - Giappone 50
BE - Belgio 45
NL - Olanda 41
KR - Corea 34
TR - Turchia 29
BR - Brasile 22
ES - Italia 21
RO - Romania 21
RU - Federazione Russa 21
AU - Australia 16
AE - Emirati Arabi Uniti 14
IR - Iran 14
CH - Svizzera 12
PL - Polonia 11
PK - Pakistan 10
AT - Austria 9
AZ - Azerbaigian 9
ID - Indonesia 9
IL - Israele 9
DZ - Algeria 7
EU - Europa 7
SA - Arabia Saudita 7
CL - Cile 5
MX - Messico 5
HK - Hong Kong 4
NP - Nepal 4
NZ - Nuova Zelanda 4
PT - Portogallo 4
DK - Danimarca 3
TW - Taiwan 3
ZA - Sudafrica 3
CZ - Repubblica Ceca 2
ET - Etiopia 2
HR - Croazia 2
HU - Ungheria 2
MY - Malesia 2
NO - Norvegia 2
SC - Seychelles 2
SK - Slovacchia (Repubblica Slovacca) 2
BY - Bielorussia 1
IQ - Iraq 1
KZ - Kazakistan 1
LU - Lussemburgo 1
MO - Macao, regione amministrativa speciale della Cina 1
RS - Serbia 1
SI - Slovenia 1
VN - Vietnam 1
Totale 14.145
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Città #
Fairfield 1.504
Rome 764
Ashburn 727
Woodbridge 714
Chandler 622
Seattle 555
Houston 544
Wilmington 526
Cambridge 456
Ann Arbor 382
Beijing 283
Princeton 253
Plano 201
Southend 163
Milan 154
Dearborn 150
Lawrence 136
Millbury 126
San Paolo di Civitate 124
Boston 110
Lomé 104
San Diego 91
Jacksonville 88
Andover 73
Sofia 71
Federal 70
Boardman 57
Venezia 55
Dublin 51
Turin 42
Toronto 41
Orte 38
Singapore 37
Brussels 34
Des Moines 34
Norwalk 34
San Mateo 34
West Lafayette 33
Tokyo 32
Naples 31
Dresden 29
Los Angeles 28
New York 28
Paris 27
Falls Church 26
Brescia 25
Palermo 22
Munich 21
Westminster 21
Hefei 20
Bremen 18
Indiana 18
Enschede 16
Luft 16
Nanjing 15
London 14
Redwood City 14
Chicago 13
Istanbul 13
Ladispoli 13
Al Ain City 12
Barcelona 11
Bühl 11
Genoa 11
Kunming 11
Mcallen 11
North York 11
Le Plessis-Robinson 10
Napoli 10
Rovigo 10
Sydney 10
Washington 10
Baku 9
Bengaluru 9
Florence 9
Italy 9
Tappahannock 9
Bari 8
Castledermot 8
Gurgaon 8
Jakarta 8
Montreuil 8
Moscow 8
Ottawa 8
Buffalo 7
Karlsruhe 7
Lahore 7
Livorno 7
Rouen 7
Shanghai 7
São Paulo 7
Xi'an 7
Afragola 6
Ankara 6
Cagliari 6
Haifa 6
Helsinki 6
Madrid 6
Meda 6
Meudon 6
Totale 10.274
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Nome #
Dispense del Corso di Propulsione Aerospaziale 406
null 204
Numerical estimation of nozzle throat heat flux in oxygen-methane rocket engines 127
Numerical analysis of nozzle material thermochemical erosion in hybrid rocket engines 122
Numerical issues in modeling combustion instability by quasi-1D Euler equations 122
Navier-stokes simulation of graphite nozzle erosion under a wide range of pressure conditions 121
Simulation of a single-element GCH4/GOx rocket combustor using a non-adiabatic flamelet method 110
Evaluation of Turbulence Modeling in Supersonic Afterbody Computations 109
Effect of Wall Shape and Real Gas Properties on Dual Bell Nozzle Flowfields 108
Simulation of gaseous oxygen/hydroxyl-terminated polybutadiene hybrid rocket flowfields and comparison with experiments 108
On the onset of heat transfer deterioration in supercritical coolant flow channels 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 100
Numerical Analysis of Heated Channel Flows by a Space-Marching Finite-Volume Technique 98
Parametric analysis of cooling properties of candidate expander cycle fuels 97
CSP-based chemical kinetics mechanisms simplification strategy for non-premixed combustion: An application to hybrid rocket propulsion 97
Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers 97
Modeling and simulation of paraffin–based hybrid rocket internal ballistics 95
Experimental Investigation on Methane in Transcritical Conditions 94
Chemical Reaction Effects on Wall Heat Flux in Liquid Rocket Thrust Chambers 91
Development of Thrust Chamber Components for a System Analysis Tool 90
Chemical Erosion of Carbon-Phenolic Rocket Nozzles with Finite-Rate Surface Chemistry 90
Experimental investigation of transcritical methane flow in rocket engine cooling channel 89
Characterization of unsteadiness in an overexpanded planar nozzle 89
Detached-Eddy simulation of shock unsteadiness in an overexpanded planar nozzle 88
Convective and radiative wall heat transfer in liquid rocket thrust chambers 88
A Multi-Block Shock-Fitting Technique to Solve Steady and Unsteady Compressible Flows 87
Validation of conjugate heat transfer model for rocket cooling with supercritical methane 87
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
Parametric analysis of heat transfer to supercritical pressure methane 85
The accuracy of reconstruction techniques for determining hybrid rocket fuel regression rate 84
Flowfield analysis of a linear clustered plug nozzle with round-to-square modules 83
Ablative material behavior in oxygen/methane thruster environment 83
Low-order model studies of combustion instabilities in a DVRC combustor 83
Radius of curvature effects on throat thermochemical erosion in solid rocket motors 83
Cooling Channel Analysis of a LOX/LCH4 Rocket Engine Demonstrator 83
Numerical Study of Unsteady Compressible Flows by a Shock-Fitting Technique 82
Numerical analysis of nozzle flows with finite-rate surface ablation and pyrolysis-gas injection 80
Analysis of thermal stratification impact on the design of cooling channels for liquid rocket engines 80
Analysis of Three-dimensional Flow Generated by a Linear Aerospike 79
Numerical Study of Transition Between the Two Operating Modes of Dual-Bell Nozzles 79
Experimental and Numerical Analysis of Linear Plug Nozzles 78
Hybrid rockets with axial injector: port diameter effect on fuel regression rate 78
Coupled numerical simulation of wall heat conduction and coolant flow in liquid rocket engines 78
An Italian network to improve hybrid rocket performance: The strategy, the program, the results 77
Coupled CFD analysis of thermochemical erosion and unsteady heat conduction in solid rocket nozzles 77
Driving mechanisms in low order modeling of longitudinal combustion instability 77
Numerical simulation of hot-gas side heat transfer enhancement in thrust chambers by wall ribs 77
A Numerical Study of Wake Behavior in Plug Nozzles 77
Hydrogen Microthrusters Based on Hydrogen Storage Materials. 76
Supercritical methane heat transfer modeling in rocket engine cooling channels 76
Quasi-1D modeling of heat release for the study of longitudinal combustion instability 76
Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles 76
Assessment of a conjugate heat transfer model for rocket engine cooling channels fed with supercritical methane 75
Assessment of detached eddy simulation of a separated flow in a planar nozzle 75
Numerical investigation on radiative heat loads in liquid rocket thrust chambers 75
Heat transfer modeling for supercritical methane flowing in rocket engine cooling channels 75
Shock-Generated Vortices in Rocket Nozzles 74
Transition between open and closed wake in 3D linear aerospike nozzles 74
Quasi-2D modeling of high-aspect-ratio-cooling-channel flows 74
Evolution of cooling-channel properties for varying aspect ratio 74
Analysis of Curved-Cooling-Channel Flow and Heat Transfer in Rocket Engines 73
Size Effects on the Transition in Dual-Bell Nozzles 72
CFD analysis of transcritical methane in rocket engine cooling channels 72
A Numerical Approach for High-Temperature Flows over Ablating Surfaces 72
Numerical Analysis of Flow Separation Structures in Rocket Nozzles 71
CFD Analysis of Curved Cooling Channel Flow and Heat Transfer in Rocket Engines 71
Flow Analysis and Methods of Design for Dual-Bell Nozzles 71
Modeling of paraffin-based fuels in the simulation of hybrid rocket flowfields 71
Numerical study of heat transfer in film cooled thrust chambers 70
Moretti's shock-fitting methods on structured and unstructured meshes 70
A numerical methodology to predict exhaust plumes of propulsion nozzles 69
Three Dimensional Features of Clustered Plug Nozzle Flows 69
An approximate Riemann solver for real gas parabolized Navier-Stokes equations 69
Numerical Analysis of Heated Channel Flows by a Space-Marching Finite Volume Technique 69
Simulations of paraffin-based hybrid rocket motors and comparison with experiments 69
Modeling liquid rocket engine coolant flow and heat transfer in high roughness channels 69
Heat transfer prediction in rough cooling channels for liquid rocket engines 69
Analysis of In-Flight Behavior of Truncated Plug Nozzles 67
Numerical Modeling of GOX/HTPB Hybrid Rocket Flowfields and Comparison with Experiments 67
Separation shock cutoff frequency in dual bell nozzles 67
A low order modeling approach to transverse combustion instability 67
Cooling system design for an upper-stage aerospike 66
The influence of nozzle shape on the shock structure in separated flows 66
Methodology to solve flowfields of plug nozzles for future launchers 66
Size Effects on the Performance of Liquid Rocket Engines Fed with LH/LOX, LCH4/LOX and Kerosene/LOX 66
A numerical approach for the study of the gas-surface interaction in carbon-phenolic solid rocket nozzles 66
Analysis on the effect of channel aspect ratio on rocket thermal behavior 66
Shock structure in separated nozzle flows 66
Navier-stokes simulations of hypersonic flows with coupled graphite ablation 65
Numerical analysis of deterioration in heat transfer to near-critical rocket propellants 65
Radiation and Roughness Effects on Nozzle Thermochemical Erosion in Solid Rocket Motors 65
NUMERICAL EVALUATION OF HEAT TRANSFER ENHANCEMENT IN ROCKET THRUST CHAMBERS BY WALL RIBS 65
Conditions for the occurrence of heat transfer deterioration in light hydrocarbons flows 65
Material-dependent catalytic recombination modeling for hypersonic flows 65
Numerical Analysis of Nozzle Material Thermochemical Erosion in Hybrid Rocket Engines 65
Totale 8.552
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Categoria #
all - tutte 35.185
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 35.185
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/20191.057 0 0 0 0 0 0 0 0 0 0 633 424
2019/20203.328 402 92 43 146 344 537 450 390 346 301 206 71
2020/20211.733 111 121 62 416 135 62 15 220 235 233 92 31
2021/20222.550 21 128 256 74 356 95 56 256 196 185 378 549
2022/20232.626 495 535 120 250 285 273 52 155 194 63 118 86
2023/20241.826 127 191 197 161 245 247 195 149 89 225 0 0
Totale 14.756