MAZZEI, LORENZO
 Distribuzione geografica
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Continente #
NA - Nord America 3.471
EU - Europa 2.016
AS - Asia 690
Continente sconosciuto - Info sul continente non disponibili 3
SA - Sud America 3
AF - Africa 1
Totale 6.184
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Nazione #
US - Stati Uniti d'America 3.463
IT - Italia 500
RU - Federazione Russa 433
PL - Polonia 345
IE - Irlanda 277
CN - Cina 237
SE - Svezia 219
SG - Singapore 142
HK - Hong Kong 120
IN - India 69
JO - Giordania 64
AT - Austria 47
GB - Regno Unito 43
FI - Finlandia 41
DE - Germania 26
ES - Italia 26
FR - Francia 26
TR - Turchia 17
UA - Ucraina 16
VN - Vietnam 12
CA - Canada 8
IR - Iran 8
KR - Corea 7
BE - Belgio 6
JP - Giappone 6
NP - Nepal 5
NL - Olanda 4
EU - Europa 3
RO - Romania 3
CH - Svizzera 2
CO - Colombia 2
BG - Bulgaria 1
BR - Brasile 1
DK - Danimarca 1
GE - Georgia 1
MO - Macao, regione amministrativa speciale della Cina 1
TN - Tunisia 1
TW - Taiwan 1
Totale 6.184
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Città #
Fairfield 622
Warsaw 344
Ashburn 305
Dublin 277
Woodbridge 273
Seattle 267
Cambridge 248
Houston 241
Wilmington 202
Chandler 191
Florence 147
Altamura 128
Singapore 117
Ann Arbor 99
Lawrence 95
Princeton 86
Beijing 81
Hong Kong 65
Mumbai 56
Dearborn 49
Vienna 47
Medford 37
Shanghai 36
Boston 34
Buffalo 32
New York 30
Moscow 28
San Diego 27
Kent 26
Barcelona 24
Boardman 23
Norwalk 23
Falls Church 22
Redwood City 19
Milan 17
Duncan 16
Santa Clara 15
Los Angeles 13
Scandicci 13
Dong Ket 10
Hillsboro 10
London 10
Salerno 10
Meudon 8
Toronto 8
Genova 7
Helsinki 7
Raleigh 7
Tong 7
Xian 7
Ankara 6
Brussels 6
Monsummano Terme 6
Prato 6
Rome 6
Chennai 5
Hangzhou 5
Jinan 5
Nanchang 5
Redmond 5
Triggiano 5
Andover 4
Cagliari 4
Carpi 4
Guangzhou 4
Seodaemun-gu 4
Stuttgart 4
Tappahannock 4
West Jordan 4
Zhengzhou 4
Berlin 3
Brasov 3
Chicago 3
Comun Nuovo 3
Cranfield 3
Doruk 3
Fucecchio 3
Genoa 3
Harbin 3
Hefei 3
Jacksonville 3
Kunming 3
Leawood 3
Nanjing 3
Paris 3
Perugia 3
Phoenix 3
Prescot 3
Pune 3
Tokyo 3
Bogotá 2
Bologna 2
Cedar Knolls 2
Chengdu 2
Châtenay-malabry 2
Citta 2
Frankfurt am Main 2
Fuzhou 2
Höst 2
Istanbul 2
Totale 4.642
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 304
A 3D coupled approach for the thermal design of aero-engine combustor liners 261
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 243
Assessment of modelling strategies for film cooling 138
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 125
A 3d coupled approach for the thermal design of aero-engine combustor liners 125
Hybrid RANS-LES modeling of the aerothermal field in an annular hot streak generator for the study of combustor-turbine interaction 122
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 122
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 121
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 112
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 111
Assessment of Aero-Thermal Design Methodology for Effusion Cooled Lean Burn Annular Combustors 109
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors 109
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 106
Metal temperature prediction of a Dry Low NOx Class Flame tube by computational fluid dynamics conjugate heat transfer approach 105
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 104
Assessment of Scale-Resolved Computational Fluid Dynamics Methods for the Investigation of Lean Burn Spray Flames 102
Assessment of scale resolved CFD methods for the investigation of lean burn spray flames 102
LOCAL SOURCE BASED CFD MODELING OF EFFUSION COOLING HOLES: VALIDATION AND APPLICATION TO AN ACTUAL COMBUSTOR TEST CASE 101
Development of a numerical correlation for the discharge coefficient of round inclined holes with low crossflow 99
Effusion cooling system optimization for modern lean burn combustor 98
Thermofluid Dynamic Analysis of a Gas Turbine Transition-Piece 94
Numerical Analysis of Effusion Plates for Combustor Liners Cooling with Varying Density Ratio 93
Scale Adaptive Simulations of a Swirl Stabilized Spray Flame Using Flamelet Generated Manifold 93
Metal temperature prediction of a DLN1 class flame tube by CFD CHT approach 90
Impact of Swirl Flow on Combustor Liner Heat Transfer and Cooling: A Numerical Investigation with Hybrid Reynolds-Averaged Navier Stokes-Large Eddy Simulation Models 89
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 89
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 88
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 87
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 85
Local source based CFD modeling of effusion cooling holes: Validation and application to an actual combustor test case 85
Heat transfer enhancement due to coolant extraction on the cold side of effusion cooling plates 85
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and metal temperature 83
Hybrid rans-les modeling of the aero-Thermal field in an annular hot streak generator for the study of combustor-Turbine interaction 83
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 82
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 82
Uncertainty quantification of film cooling performance of an industrial gas turbine vane 82
Heat Transfer Enhancement due to Coolant Extraction on the Cold Side of Effusion Cooling Plates 82
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled HPT vanes 82
Multi-coupled numerical simulations of the DLR Generic Single Sector Combustor 80
Methane swirl-stabilized lean burn flames: Assessment of scale-resolving simulations 80
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 79
Numerical Investigation On The Heat Transfer Enhancement Due To Coolant Extraction On The Cold Side Of Film Cooling Holes 76
Hybrid RANS-LES Modeling of a Hot Streak Generator Oriented to the Study of Combustor-Turbine Interaction 76
Modelling strategies for large-eddy simulation of lean burn spray flames 75
Investigation on the effect of a realistic flow field on the adiabatic effectiveness of an effusion-cooled combustor 75
Thermo-fluid dynamic analysis of a gas turbine transition-piece 74
Numerical investigation of optimized arrangements for effusion cooling in gas turbine combustor applications 71
Impact of swirl flow on combustor liner heat transfer and cooling - A numerical investigation with hybrid rans-les models 70
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled high pressure turbine vanes 68
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 66
Large-Eddy Simulation of a Model Aero-Engine Sooting Flame With a Multiphysics Approach 66
Modeling strategies for large eddy simulation of lean burn spray flames 66
Design of a Non-Reactive Warm Rig With Real Lean-Premix Combustor Swirlers and Film-Cooled First Stage Nozzles 64
Numerical modeling of gaseous partially premixed low-swirl lifted flame at elevated pressure 63
Numerical investigation on the effect of rotation and holes arrangement in cold bridge-type impingement cooling systems 63
ASSESSMENT OF THICKENED FLAME MODEL COUPLED WITH FLAMELET GENERATED MANIFOLD ON A LOW-SWIRL PARTIALLY PREMIXED GASEOUS LIFTED FLAME 60
CHT Analyses of an Industrial Gas Turbine Blade: Comparison Between an In-House Developed Decoupled Procedure and CFD Coupled Simulations 59
Numerical investigation on the effect of rotation and holes arrangement in cold bridge type impingement cooling systems 58
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 58
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 56
Numerical investigation of surface roughness effects on heat transfer in a turbine cascade 41
Prediction of liner metal temperature of an aeroengine combustor with multi-physics scale-resolving CFD 40
Scale resolving CFD investigations of aerothermal field and emissions of a lean burn aeroengine combustor 35
Application of uncertainty quantification methods to the prediction of effusion cooled combustor liner temperature 34
Reduced-order models for effusion modelling in gas turbine combustors 32
Development of a numerical correlation for heat transfer coefficients in steam turbines inner chambers 31
Reduced-Order Models for Effusion Modeling in Gas Turbine Combustors 30
Uncertainty quantification of an aeronautical combustor using a 1-D approach 28
Numerical analyses of a high pressure sooting flame with multiphysics approach 27
External heat transfer on nozzle guide vanes under highly swirled combustor outlet flow 26
Multiphysics numerical investigation of an aeronautical lean burn combustor 25
ASSESSMENT OF A CONJUGATE HEAT TRANSFER METHOD ON AN EFFUSION COOLED COMBUSTOR OPERATED WITH A SWIRL STABILIZED PARTIALLY PREMIXED FLAME 24
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 17
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 15
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 14
Totale 6.295
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Categoria #
all - tutte 21.021
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 21.021
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.210 0 0 27 104 147 187 208 165 159 89 81 43
2020/2021657 45 61 23 73 91 57 32 48 73 73 51 30
2021/2022528 38 19 37 38 20 55 14 54 21 22 73 137
2022/20231.365 130 272 84 55 81 251 201 66 160 20 36 9
2023/2024566 16 63 83 33 36 75 24 113 29 27 49 18
2024/2025736 151 407 178 0 0 0 0 0 0 0 0 0
Totale 6.295