MAZZEI, LORENZO
 Distribuzione geografica
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Continente #
NA - Nord America 4.470
EU - Europa 2.633
AS - Asia 789
AF - Africa 14
Continente sconosciuto - Info sul continente non disponibili 3
SA - Sud America 3
Totale 7.912
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Nazione #
US - Stati Uniti d'America 4.462
RU - Federazione Russa 1.036
IT - Italia 509
PL - Polonia 346
IE - Irlanda 277
CN - Cina 259
SE - Svezia 219
SG - Singapore 215
HK - Hong Kong 122
IN - India 69
JO - Giordania 64
AT - Austria 47
GB - Regno Unito 43
FI - Finlandia 42
DE - Germania 28
FR - Francia 27
ES - Italia 26
TR - Turchia 17
UA - Ucraina 16
CI - Costa d'Avorio 12
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
PK - Pakistan 2
BG - Bulgaria 1
BR - Brasile 1
DK - Danimarca 1
GE - Georgia 1
MO - Macao, regione amministrativa speciale della Cina 1
NG - Nigeria 1
TN - Tunisia 1
TW - Taiwan 1
Totale 7.912
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Città #
Santa Clara 843
Fairfield 622
Warsaw 345
Ashburn 305
Dublin 277
Woodbridge 273
Seattle 267
Cambridge 248
Houston 241
Wilmington 202
Chandler 191
Singapore 185
Florence 149
Altamura 128
Ann Arbor 99
Lawrence 95
Princeton 86
Beijing 81
Hong Kong 65
Mumbai 56
Moscow 50
Dearborn 49
Vienna 47
Shanghai 38
Medford 37
Boston 34
Buffalo 32
New York 30
San Diego 27
Kent 26
Barcelona 24
Boardman 23
Norwalk 23
Falls Church 22
Redwood City 19
Milan 18
Duncan 16
Los Angeles 13
Scandicci 13
Abidjan 12
Dong Ket 10
Hillsboro 10
London 10
Salerno 10
Helsinki 8
Meudon 8
Toronto 8
Yubileyny 8
Genova 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
Shenzhen 4
Stuttgart 4
Tappahannock 4
West Jordan 4
Zhengzhou 4
Berlin 3
Brasov 3
Chicago 3
Comun Nuovo 3
Cranfield 3
Dongguan 3
Doruk 3
Fucecchio 3
Genoa 3
Harbin 3
Hefei 3
Jacksonville 3
Kunming 3
Leawood 3
Nanjing 3
Naples 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
Totale 5.587
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 329
A 3D coupled approach for the thermal design of aero-engine combustor liners 283
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 265
Assessment of modelling strategies for film cooling 156
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 148
A 3d coupled approach for the thermal design of aero-engine combustor liners 148
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 145
Hybrid RANS-LES modeling of the aerothermal field in an annular hot streak generator for the study of combustor-turbine interaction 143
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 137
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 136
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors 133
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 132
Assessment of Aero-Thermal Design Methodology for Effusion Cooled Lean Burn Annular Combustors 128
Metal temperature prediction of a Dry Low NOx Class Flame tube by computational fluid dynamics conjugate heat transfer approach 128
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 127
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 126
Assessment of Scale-Resolved Computational Fluid Dynamics Methods for the Investigation of Lean Burn Spray Flames 125
Assessment of scale resolved CFD methods for the investigation of lean burn spray flames 125
Development of a numerical correlation for the discharge coefficient of round inclined holes with low crossflow 125
LOCAL SOURCE BASED CFD MODELING OF EFFUSION COOLING HOLES: VALIDATION AND APPLICATION TO AN ACTUAL COMBUSTOR TEST CASE 122
Effusion cooling system optimization for modern lean burn combustor 121
Numerical Analysis of Effusion Plates for Combustor Liners Cooling with Varying Density Ratio 116
Thermofluid Dynamic Analysis of a Gas Turbine Transition-Piece 113
Scale Adaptive Simulations of a Swirl Stabilized Spray Flame Using Flamelet Generated Manifold 113
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled HPT vanes 111
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 109
Metal temperature prediction of a DLN1 class flame tube by CFD CHT approach 109
Uncertainty quantification of film cooling performance of an industrial gas turbine vane 109
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 108
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and metal temperature 107
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 107
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 106
Impact of Swirl Flow on Combustor Liner Heat Transfer and Cooling: A Numerical Investigation with Hybrid Reynolds-Averaged Navier Stokes-Large Eddy Simulation Models 105
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 105
Local source based CFD modeling of effusion cooling holes: Validation and application to an actual combustor test case 104
Heat Transfer Enhancement due to Coolant Extraction on the Cold Side of Effusion Cooling Plates 104
Heat transfer enhancement due to coolant extraction on the cold side of effusion cooling plates 104
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 102
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 102
Hybrid rans-les modeling of the aero-Thermal field in an annular hot streak generator for the study of combustor-Turbine interaction 101
Multi-coupled numerical simulations of the DLR Generic Single Sector Combustor 99
Investigation on the effect of a realistic flow field on the adiabatic effectiveness of an effusion-cooled combustor 99
Methane swirl-stabilized lean burn flames: Assessment of scale-resolving simulations 97
Hybrid RANS-LES Modeling of a Hot Streak Generator Oriented to the Study of Combustor-Turbine Interaction 96
Modelling strategies for large-eddy simulation of lean burn spray flames 95
Numerical Investigation On The Heat Transfer Enhancement Due To Coolant Extraction On The Cold Side Of Film Cooling Holes 95
Thermo-fluid dynamic analysis of a gas turbine transition-piece 94
Numerical investigation of optimized arrangements for effusion cooling in gas turbine combustor applications 94
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled high pressure turbine vanes 94
Design of a Non-Reactive Warm Rig With Real Lean-Premix Combustor Swirlers and Film-Cooled First Stage Nozzles 92
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 88
Large-Eddy Simulation of a Model Aero-Engine Sooting Flame With a Multiphysics Approach 88
Numerical investigation on the effect of rotation and holes arrangement in cold bridge-type impingement cooling systems 88
ASSESSMENT OF THICKENED FLAME MODEL COUPLED WITH FLAMELET GENERATED MANIFOLD ON A LOW-SWIRL PARTIALLY PREMIXED GASEOUS LIFTED FLAME 87
Numerical modeling of gaseous partially premixed low-swirl lifted flame at elevated pressure 87
Modeling strategies for large eddy simulation of lean burn spray flames 86
Impact of swirl flow on combustor liner heat transfer and cooling - A numerical investigation with hybrid rans-les models 85
Numerical investigation on the effect of rotation and holes arrangement in cold bridge type impingement cooling systems 84
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 82
CHT Analyses of an Industrial Gas Turbine Blade: Comparison Between an In-House Developed Decoupled Procedure and CFD Coupled Simulations 81
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 77
Numerical investigation of surface roughness effects on heat transfer in a turbine cascade 65
Prediction of liner metal temperature of an aeroengine combustor with multi-physics scale-resolving CFD 63
Reduced-Order Models for Effusion Modeling in Gas Turbine Combustors 59
Scale resolving CFD investigations of aerothermal field and emissions of a lean burn aeroengine combustor 59
Application of uncertainty quantification methods to the prediction of effusion cooled combustor liner temperature 58
Development of a numerical correlation for heat transfer coefficients in steam turbines inner chambers 57
Uncertainty quantification of an aeronautical combustor using a 1-D approach 56
Reduced-order models for effusion modelling in gas turbine combustors 55
External heat transfer on nozzle guide vanes under highly swirled combustor outlet flow 51
Numerical analyses of a high pressure sooting flame with multiphysics approach 51
Multiphysics numerical investigation of an aeronautical lean burn combustor 51
ASSESSMENT OF A CONJUGATE HEAT TRANSFER METHOD ON AN EFFUSION COOLED COMBUSTOR OPERATED WITH A SWIRL STABILIZED PARTIALLY PREMIXED FLAME 49
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 45
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 41
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 38
Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame 22
Totale 8.025
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Categoria #
all - tutte 23.949
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 23.949
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.079 0 0 0 0 147 187 208 165 159 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
2024/20252.466 151 407 276 604 1.028 0 0 0 0 0 0 0
Totale 8.025