Catalogo dei prodotti della ricerca

BRUNO, Claudio
 Distribuzione geografica
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Continente #
NA - Nord America 1.415
EU - Europa 325
AS - Asia 163
AF - Africa 26
SA - Sud America 16
Totale 1.945
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Nazione #
US - Stati Uniti d'America 1.403
IN - India 100
UA - Ucraina 86
SE - Svezia 68
IT - Italia 65
FI - Finlandia 48
CN - Cina 41
TG - Togo 21
GB - Regno Unito 19
SG - Singapore 18
AR - Argentina 15
DE - Germania 14
BE - Belgio 10
CA - Canada 9
IE - Irlanda 7
ZA - Sudafrica 4
CH - Svizzera 3
FR - Francia 3
KR - Corea 3
BG - Bulgaria 2
MX - Messico 2
CL - Cile 1
JM - Giamaica 1
PH - Filippine 1
SC - Seychelles 1
Totale 1.945
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Città #
Fairfield 214
Chandler 119
Ann Arbor 109
Seattle 86
Woodbridge 86
Wilmington 84
Ashburn 79
Cambridge 73
Houston 65
Princeton 58
Plano 45
Des Moines 38
Boston 36
San Paolo di Civitate 30
Jacksonville 27
Beijing 25
Rome 24
Lomé 21
Lawrence 20
San Diego 18
Federal 14
Andover 12
Millbury 12
Brussels 10
Singapore 9
Boardman 8
Falls Church 8
Norwalk 8
Dearborn 7
Dublin 7
Southend 7
Toronto 5
Hefei 4
Auburn Hills 3
Bühl 3
Gurgaon 3
Pune 3
Bern 2
Centurion 2
Changsha 2
Gwanak-gu 2
Indiana 2
Kunming 2
Mexico City 2
Montréal 2
Muizenberg 2
Munich 2
Ottawa 2
San Gregorio da Sassola 2
Santa Maria La Carita 2
Simi Valley 2
Sofia 2
Tappahannock 2
Wuhan 2
Benevento 1
Bourg-la-reine 1
Buenos Aires 1
Dallas 1
El Paso 1
Helsinki 1
Huzhou 1
Kilburn 1
Lappeenranta 1
Laurel 1
London 1
Los Angeles 1
Manila 1
Milan 1
Paris 1
Redwood City 1
Romanel-sur-Lausanne 1
San Francisco 1
San Jose 1
San Mateo 1
Santa Maria Capua Vetere 1
Staten Island 1
Turku 1
Wenzhou 1
Totale 1.438
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Nome #
Satellite de-orbiting by means of electrodynamic tethers - Part I: General concepts and requirements 100
Satellite de-orbiting by means of electrodynamic tethers - Part II: System configuration and performance 100
Feasibility of high speed atmospheric flight on Venus 74
LAPCAT-II: Conceptual design of a mach 8 TBCC civil aircraft, enforced by full navier-stokes 3D nose-to-tail computation 72
Using aluminum for space propulsion 70
Aeronautical approach and support to mars exploration 70
Mixing and turbulent kinetic energy scaling in compressible reacting flows 69
Material-dependent catalytic recombination modeling for hypersonic flows 66
Exergy analyis of hypersonic propulsion systems: performance comparison of two different scramjet configurations at cruise conditions 63
Flame temperatures in non-premixed flames 62
Hydrogen/air supersonic combustion for future hypersonic vehicles 62
LES of a Supersonic Combustor with Variable Turbulent Prandtl and Schmidt Numbers 61
Fractal Modeling of Turbulent Combustion 59
LES of a CH4/air Mesocombustor at 3 atm: EDC and Laminar-rate models 57
Supersonic Mixing And Combustion: Advance In LES Modeling 56
Fractal modeling of turbulent Mixing 53
Supersonic mixing and combustion: advance in LES modeling 51
Non premixed Supersonic flames: Combustion models 50
Sizing of a Fully Integrated Hypersonic Commercial Airliner 49
Mixing and combustion in supersonic reactive flows 47
Preliminary Sizing of Hypersonic Airbreathing Airliner 45
Satellite deorbiting by means of electrodynamic tethers: general concepts and requirements 42
Advances in Supersonic Combustion: Modeling and Simulation 35
A Spectrometric Device To Measure Species Concentrations Close to the Surface During Re-entry 34
comparison between supercrtical combustion modelling for LO2-CH4 rocket engines at 15MPa using real and ideal gas properties 34
The role of the baroclinic term in fuel/air mixing enhancement 34
Theoretical and Numerical analysis of the Turbulence scaling in Supersonic Flows 32
A model for steady state flameless combustion in homogeneous isotropic turbulence 31
Comparison between Real and Ideal Sub and Supercritical Combustion Simulations for LO2-CH4 LRE at 15MPa 31
Comparison Between Simulations of Real and Ideal LRE Combustion of LO2-CH4 30
Comparison between Supercritical Combustion Modelling for LO2-CH4 Rocket Engines at 15MPa and 16.5MPa using Real and Ideal gas properties 29
Numerical Simulation of a Micro-Combustor Chamber 27
Mixing and flame anchoring in a supersonic combustor 26
LES Simulation of CH4/air Microcombustor with Detailed Chemistry”, Combustion Science and Technology 25
SubTrans and Supercritical Properties for LO2-CH4 at 15MPa 24
LAPCAT II : conceptual design of a Mach 8 TBCC civil aircraft 24
Cracking of Methanol for Microrocket Applications and Scaling Analysis 23
Turbulence Scaling in Supersonic Flows 22
Invited paper at 47th JPC Conference, 2 Augut 2011, San Diego, CA 22
Comparison between Subcritical Cobustion modelling for LO2-CH4 rocket engines at 15MPa using Real and Ideal gas properties 22
6 minute walk test in Duchenne MD patients with different mutations: 12 month changes 19
Micro-Combustor Chamber: Comparison between LES and Experiments 18
Turbulent Combustion Modelling In Supersonic Flows for Applications To Future RBCC Vehicles 17
Prediction of SCRJ flame anchoring 14
Numerical and Theoretical Study of Supersonic Turbulent Non premixed flames 14
Sizing of a Scramjet Vehicle 13
Mars One-Year Mission Craft 9
Totale 1.987
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Categoria #
all - tutte 4.932
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 4.932
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019152 0 0 0 0 0 0 0 0 0 0 87 65
2019/2020446 80 22 11 17 37 48 47 45 41 65 21 12
2020/2021150 19 25 1 22 4 6 5 15 20 16 14 3
2021/2022404 2 24 34 8 60 8 12 40 33 34 52 97
2022/2023456 89 90 23 40 50 85 1 18 35 9 12 4
2023/2024138 16 41 4 14 13 7 7 1 1 21 13 0
Totale 1.987