MARTELLI, EMANUELE
 Distribuzione geografica
Continente #
EU - Europa 482
NA - Nord America 233
AS - Asia 170
AF - Africa 6
OC - Oceania 2
Totale 893
Nazione #
BE - Belgio 240
US - Stati Uniti d'America 233
IT - Italia 171
SG - Singapore 115
CN - Cina 25
IE - Irlanda 23
DE - Germania 15
KR - Corea 10
FI - Finlandia 7
CH - Svizzera 6
DZ - Algeria 6
HK - Hong Kong 6
GB - Regno Unito 5
NL - Olanda 4
FR - Francia 3
IN - India 3
JO - Giordania 3
TR - Turchia 3
AU - Australia 2
MY - Malesia 2
RO - Romania 2
RU - Federazione Russa 2
SA - Arabia Saudita 2
CZ - Repubblica Ceca 1
ES - Italia 1
IL - Israele 1
PL - Polonia 1
SE - Svezia 1
Totale 893
Città #
Brussels 240
Singapore 84
Seattle 55
Council Bluffs 54
Turin 39
Chandler 26
Dublin 23
Rome 18
Milan 17
Beijing 14
Torino 14
Santa Clara 12
Houston 10
Seoul 9
Changsha 7
Princeton 7
Helsinki 6
Lausanne 6
Naples 6
Algiers 5
Ashburn 5
Amsterdam 4
Berlin 4
Wilmington 4
Bresso 3
Macerata 3
Cinisello Balsamo 2
Dresden 2
Falls Church 2
Guangzhou 2
Hong Kong 2
Iasi 2
Istanbul 2
Jeddah 2
Malappuram 2
Menlo Park 2
Moscow 2
Rivoli 2
Salerno 2
Saluzzo 2
Valdagno 2
Arezzo 1
Arzano 1
Atlanta 1
Barcelona 1
Bari 1
Binasco 1
Brno 1
Busan 1
Cattolica 1
Central District 1
Crema 1
Ernakulam 1
Florence 1
Frosinone 1
Gorgonzola 1
Isernia 1
Kuala Lumpur 1
Lappeenranta 1
Miami 1
Mountain View 1
New York 1
Nichelino 1
Novara 1
Orléans 1
Perth 1
Piscataway 1
Prineville 1
Redmond 1
Rho 1
Rzeszów 1
San Giuliano Milanese 1
Santa Rosa 1
Shenzhen 1
Southend 1
Springfield 1
Sydney 1
Tel Aviv 1
Varese 1
Woodbridge 1
Xi'an 1
Totale 745
Nome #
Dual-bell nozzle with fluidic control of transition for space launchers 124
Fluidic control of transition in a dual-bell nozzle 78
Numerical Study of Heat Transfer in Film Cooled Thrust Chambers 38
Dual-bell nozzle for space launchers with fluidic control of transition 37
High-fidelity simulations of the aeroacoustic environment of the VEGA launch vehicle at lift-off 28
A Numerical Study on Carbon-Fiber-Reinforced Composite Cylindrical Skirts for Solid Propeller Rockets 26
Boundary Conditions for Inhomogeneous Combustion Simulation in Solid Rocket Motors 25
Unsteadiness characterisation of shock wave/turbulent boundary-layer interaction at moderate Reynolds number 24
Numerical analysis of laser-pulse transient ignition of oxygen/methane mixtures in rocket-like combustion chamber 23
Parametric study of transition fluidic control in a dual-bell nozzle 23
Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method 20
Characterization of unsteadiness in an overexpanded planar nozzle 19
Numerical Analysis of Side-loads Reduction in a Sub-scale Dual-bell Rocket Nozzle 19
COUPLED ANALYSIS OF FLOW AND SURFACE ABLATION IN CARBON-CARBON ROCKET NOZZLES, AIAA Paper 2008-3912 19
Numerical calculation of FSS/RSS transition in highly overexpanded rocket nozzle flows 18
Flow dynamics and wall-pressure signatures in a high-Reynolds-number overexpanded nozzle with free shock separation 18
Secondary gas injection effect on Dual-Bell nozzle flow transition 18
Film Cooling in Dual-Bell Nozzles 17
Film Cooling Effect on Dual-Bell Nozzle Flow Transition 17
Large-Eddy Simulation of Vortex Shedding and Pressure Oscillations in Solid Rocket Motors 16
Navier-stokes computations of reentry flowfields with coupled surface ablation 16
A NUMERICAL APPROACH FOR HIGH-TEMPERATURES FLOWS OVER ABLATING SURFACES, AIAA Paper 2007-4537 14
Numerical analysis of flow separation structures in rocket nozzles, AIAA Paper 2007-5473 14
Numerical Analysis of Film Cooling in Advanced Rocket Nozzles 14
Dynamical system analysis of ignition phenomena using the Tangential Stretching Rate concept 14
Role of Wall Shape on the Transition in Axisymmetric Dual Bell Nozzles 14
Immersed Boundary Simulations of Aeroacoustics Phenomena in Solid Rocket Motors 13
Navier-Stokes Simulations with Graphite Surface Ablation for Atmospheric Entry 13
Chemical reaction effects on heat loads of CH4/O2 and H2/O2 rockets 13
Enhancements of the G-Scheme Framework 13
Numerical Simulation of Hot-Gas Side Heat Transfer Enhancement in Thrust Chambers by Wall Ribs 13
Heat Flux Evaluation in Oxygen/Methane Thrust Chambers by RANS Approach 13
Transition Between Open and Closed Wake in 3D Linear Aerospike Nozzles 13
Comparison of Different CH4-Air Combustion Mechanisms in a Perfectly Stirred Reactor with Oscillating Residence Times Close to Extinction 13
Non-linear perturbation response of methane-air global and detailed kinetics in premixed reactors 13
Large Eddy Simulation on the Effects of Pressure on Syngas/Air Turbulent Nonpremixed Jet Flames 13
Numerical simulation of edge flames initiation and propagation using an adaptive wavelet collocation method 13
Separation Shock Cutoff Frequency in Dual Bell Nozzles 12
Flow Separation Response to Unsteady External Disturbances in Dual Bell Nozzles 12
Role of wall shape on the transition in dual-bell nozzles”, AIAA Paper 2003-4911 , 12
Near wall recombination effects on the prediction of heat flux in O2/CH4 combustion chambers 12
Effect of Wall Shape and Real Gas Properties on Dual Bell Nozzle Flowfield, AIAA Paper 2005-3943 12
Analytical modeling of self-similar compressible turbulent mixing layers 12
Non-linear response to periodic forcing of methane-air global and detailed kinetics in continuous stirred tank reactors close to extinction conditions 12
Thermochemical erosion analysis for carbon-carbon rocket nozzles 12
Enhanced delayed DES of shock wave/boundary layer interaction in a planar transonic nozzle 12
Forced Ignition Study Based on Wavelet Method 11
Size effects on the transition in Dual-Bell Nozzles, AIAA Paper 2004-3999 11
Practical Navier-Stokes computation of flowfields with ablation products injection 11
Numerical Parametric Analysis of Dual-Bell Nozzle Flows 10
Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles 10
Delayed Detached Eddy simulation of separated flows in a planar nozzle 10
Numerical Study of Film Cooling in Oxygen/Methane Thrust Chambers 10
Thermochemical erosion analysis for graphite/carbon-carbon rocket nozzles 10
Numerical Evaluation of Heat Transfer Enhancement in Rocket Thrust Chambers by Wall Ribs 10
Detached-eddy simulation of shock unsteadiness in an overexpanded planar nozzle 10
Thermo-Fluid-Dynamics Analysis of Film Cooling in Overexpanded Rocket Nozzles, AIAA Paper 2006-5207 9
CFD STUDY OF ISOTHERMAL ABLATION 9
Chemical Reaction Effects on Wall Heat Flux in Liquid Rocket Thrust Chambers 9
Numerical study of transition between the two operating modes of dual bell nozzles, AIAA Paper 2002-3989 9
Navier-Stokes Simulations of Hypersonic Flows with Coupled Graphite Ablation 9
Assessment of detached eddy simulation of a separated flow in a planar nozzle 9
Totale 1.101
Categoria #
all - tutte 6.996
article - articoli 3.394
book - libri 0
conference - conferenze 3.602
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 13.992


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202119 0 0 0 0 0 6 0 1 1 9 2 0
2021/202291 0 0 4 0 1 5 9 5 29 5 13 20
2022/202391 10 9 3 11 9 12 4 13 6 1 4 9
2023/2024804 321 171 24 32 14 7 22 78 9 10 58 58
2024/202596 4 92 0 0 0 0 0 0 0 0 0 0
Totale 1.101