BETTI, BARBARA
 Distribuzione geografica
Continente #
NA - Nord America 1.147
EU - Europa 518
AS - Asia 132
AF - Africa 32
SA - Sud America 14
OC - Oceania 2
Totale 1.845
Nazione #
US - Stati Uniti d'America 1.131
IT - Italia 266
CN - Cina 64
IN - India 64
SE - Svezia 55
GB - Regno Unito 44
FI - Finlandia 29
TG - Togo 29
GR - Grecia 28
FR - Francia 20
CA - Canada 16
BE - Belgio 15
DE - Germania 14
UA - Ucraina 13
AR - Argentina 12
IE - Irlanda 8
RO - Romania 7
RU - Federazione Russa 7
NL - Olanda 6
AT - Austria 4
AU - Australia 2
BR - Brasile 2
ES - Italia 2
SC - Seychelles 2
TR - Turchia 2
DZ - Algeria 1
KR - Corea 1
PK - Pakistan 1
Totale 1.845
Città #
Fairfield 187
Rome 101
Ashburn 92
Chandler 86
Seattle 82
Ann Arbor 75
Woodbridge 75
Houston 71
Wilmington 68
Cambridge 64
Beijing 43
Southend 35
Princeton 32
Plano 30
Lomé 29
Millbury 25
Dearborn 20
Lawrence 14
San Diego 13
Brussels 11
Federal 11
San Paolo di Civitate 11
Washington 11
Toronto 10
Boston 8
Dublin 8
Orte 8
Andover 7
Des Moines 6
Hefei 6
Bangalore 4
Boardman 4
Jacksonville 4
Moscow 4
New York 4
Norwalk 4
Rovigo 4
Westminster 4
Bregenz 3
Buffalo 3
Delft 3
Escalquens 3
Imola 3
Italy 3
Kunming 3
Los Angeles 3
Nanjing 3
North York 3
Speyer 3
Barcelona 2
Belfast 2
Braunschweig 2
El Paso 2
Indiana 2
Istanbul 2
Lido Di Ostia 2
Mahé 2
Monte 2
Montréal 2
Rho 2
San Mateo 2
São José Dos Campos 2
Terni 2
Torino 2
Acerra 1
Amsterdam 1
Blida 1
Canberra 1
Casamassima 1
Castel Gandolfo 1
Centro 1
Chaoyang 1
Chiswick 1
Corvallis 1
Denver 1
Drunen 1
Fontenay-aux-roses 1
Islamabad 1
Kazan 1
La Plata 1
Le Chesnay 1
Leawood 1
London 1
Mcallen 1
Milan 1
Molinella 1
Moricone 1
Mountain View 1
Nanchang 1
Nanning 1
Ningbo 1
Ottawa 1
Palermo 1
Paris 1
Provo 1
Quzhou 1
Redmond 1
Reichelsheim 1
Ryazan 1
San Cesareo 1
Totale 1.370
Nome #
null 204
Simulation of gaseous oxygen/hydroxyl-terminated polybutadiene hybrid rocket flowfields and comparison with experiments 110
Chemical reaction effects on heat loads of CH4/O2 and H2/O2 rockets 101
Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers 97
Chemical Reaction Effects on Wall Heat Flux in Liquid Rocket Thrust Chambers 91
Convective and radiative contributions to wall heat transfer in liquid rocket Engine thrust chambers 90
Convective and radiative wall heat transfer in liquid rocket thrust chambers 84
Development of Thrust Chamber Components for a System Analysis Tool 81
Cooling Channel Analysis of a LOX/LCH4 Rocket Engine Demonstrator 80
Numerical simulation of hot-gas side heat transfer enhancement in thrust chambers by wall ribs 76
Hydrogen Microthrusters Based on Hydrogen Storage Materials. 72
Numerical study of heat transfer in film cooled thrust chambers 69
Numerical Modeling of GOX/HTPB Hybrid Rocket Flowfields and Comparison with Experiments 66
Separation shock cutoff frequency in dual bell nozzles 66
NUMERICAL EVALUATION OF HEAT TRANSFER ENHANCEMENT IN ROCKET THRUST CHAMBERS BY WALL RIBS 61
Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers 60
Hydrogen storage materials for microthrusters: Basic performance analysis 59
Flow Separation Response to Unsteady External Disturbances in Dual Bell Nozzles 58
Heat Flux Evaluation in Oxygen/Methane Thrust Chambers by RANS Approach 54
CFD analysis of hybrid rocket Flowfields including fuel pyrolysis and nozzle erosion 49
Experimental investigation and CFD simulation of the film cooling in O2/CH4 subscale combustion chamber 40
Plastic cubf.sat for micropropulsion and active debris removal test 36
A parametric study on the role of near wall chemical reactions in O2/CH4 combustion chamber heat flux evaluation 33
Flow field and heat transfer analysis of oxygen/methane liquid rocket engine thrust chambers 32
Coupled analysis of hot-gas and coolant flows in LOX/methane thrust chambers 30
Numerical simulation of hybrid rocket engine flowfields 29
Analytical modeling of self-similar compressible turbulent mixing layers 23
Near wall recombination eects on the prediction of heat flux in O2/CH4 combustion chambers 22
Numerical Study of Film Cooling in Oxygen/Methane Thrust Chambers 19
Numerical Modeling of Combustion Chamber and Nozzle Flow in HTPB/GOX Hybrid Rocket Motors 18
Totale 1.910
Categoria #
all - tutte 3.225
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 3.225


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019205 0 0 0 5 3 2 2 0 0 43 86 64
2019/2020457 56 15 2 17 44 90 63 52 45 43 22 8
2020/2021271 21 11 16 63 19 11 1 35 33 45 10 6
2021/2022335 1 10 44 13 46 12 5 34 26 25 50 69
2022/2023320 70 73 15 40 22 28 3 13 31 3 15 7
2023/202444 12 16 16 0 0 0 0 0 0 0 0 0
Totale 1.910