MAZZEI, LORENZO
 Distribuzione geografica
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Continente #
NA - Nord America 5.903
EU - Europa 3.267
AS - Asia 2.262
SA - Sud America 317
AF - Africa 46
OC - Oceania 34
Continente sconosciuto - Info sul continente non disponibili 4
Totale 11.833
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Nazione #
US - Stati Uniti d'America 5.863
RU - Federazione Russa 1.389
CN - Cina 661
SG - Singapore 556
IT - Italia 545
HK - Hong Kong 392
PL - Polonia 358
IE - Irlanda 279
BR - Brasile 259
KR - Corea 224
SE - Svezia 224
DE - Germania 115
VN - Vietnam 114
FI - Finlandia 92
IN - India 92
GB - Regno Unito 65
JO - Giordania 65
FR - Francia 56
AT - Austria 48
ES - Italia 35
AU - Australia 33
TR - Turchia 31
ID - Indonesia 27
CA - Canada 25
AR - Argentina 22
JP - Giappone 22
UA - Ucraina 22
NL - Olanda 16
IQ - Iraq 13
CI - Costa d'Avorio 12
BD - Bangladesh 11
ZA - Sudafrica 11
EC - Ecuador 10
BE - Belgio 8
IR - Iran 8
AE - Emirati Arabi Uniti 7
MA - Marocco 6
MX - Messico 6
NP - Nepal 6
PK - Pakistan 6
UY - Uruguay 6
UZ - Uzbekistan 6
CO - Colombia 5
VE - Venezuela 5
CL - Cile 4
DO - Repubblica Dominicana 3
EG - Egitto 3
EU - Europa 3
PY - Paraguay 3
RO - Romania 3
SA - Arabia Saudita 3
BJ - Benin 2
BW - Botswana 2
CH - Svizzera 2
DK - Danimarca 2
DZ - Algeria 2
IL - Israele 2
KE - Kenya 2
KZ - Kazakistan 2
PA - Panama 2
PE - Perù 2
SN - Senegal 2
AL - Albania 1
AM - Armenia 1
AZ - Azerbaigian 1
BG - Bulgaria 1
CG - Congo 1
CZ - Repubblica Ceca 1
DM - Dominica 1
EE - Estonia 1
GE - Georgia 1
GH - Ghana 1
GR - Grecia 1
HR - Croazia 1
JM - Giamaica 1
KG - Kirghizistan 1
KH - Cambogia 1
LT - Lituania 1
LV - Lettonia 1
MO - Macao, regione amministrativa speciale della Cina 1
MY - Malesia 1
NG - Nigeria 1
NZ - Nuova Zelanda 1
OM - Oman 1
PH - Filippine 1
PS - Palestinian Territory 1
QA - Qatar 1
SR - Suriname 1
TH - Thailandia 1
TJ - Tagikistan 1
TN - Tunisia 1
TT - Trinidad e Tobago 1
TW - Taiwan 1
VG - Isole Vergini Britanniche 1
XK - ???statistics.table.value.countryCode.XK??? 1
Totale 11.833
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Città #
Santa Clara 1.692
Fairfield 622
Ashburn 439
Singapore 403
Warsaw 355
Hong Kong 335
Dublin 279
Woodbridge 273
Seattle 268
Cambridge 248
Houston 247
Seoul 212
Wilmington 202
Chandler 191
Beijing 184
Florence 154
Altamura 128
Hefei 123
Ann Arbor 99
Lawrence 95
Princeton 86
Buffalo 71
Moscow 70
Los Angeles 60
Mumbai 59
Munich 51
New York 50
Dearborn 49
Vienna 48
Helsinki 44
Ho Chi Minh City 43
Clifton 40
Shanghai 39
Kent 37
Medford 37
Boston 36
Melbourne 33
San Diego 27
Barcelona 24
Boardman 23
Norwalk 23
São Paulo 23
Falls Church 22
Milan 22
London 19
Redwood City 19
The Dalles 19
Tokyo 19
Jakarta 18
Dallas 17
Duncan 16
Hanoi 16
Falkenstein 14
Chicago 13
Scandicci 13
Abidjan 12
Redondo Beach 12
Turku 12
Frankfurt am Main 11
Dong Ket 10
Haiphong 10
Hillsboro 10
Salerno 10
Chennai 9
Paris 9
Rome 9
Toronto 9
Belo Horizonte 8
Denver 8
Istanbul 8
Johannesburg 8
Madrid 8
Meudon 8
Raleigh 8
Yubileyny 8
Ankara 7
Bengaluru 7
Brussels 7
Genova 7
Jinan 7
Tong 7
Xian 7
Curitiba 6
Monsummano Terme 6
Montevideo 6
Orem 6
Phoenix 6
Prato 6
Rio de Janeiro 6
Salt Lake City 6
Stuttgart 6
Tashkent 6
Brasília 5
Brooklyn 5
Carpi 5
Chengdu 5
Guangzhou 5
Hangzhou 5
Montreal 5
Nanchang 5
Totale 8.085
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 381
A 3D coupled approach for the thermal design of aero-engine combustor liners 358
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 304
Assessment of modelling strategies for film cooling 203
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors 198
A 3d coupled approach for the thermal design of aero-engine combustor liners 193
Hybrid RANS-LES modeling of the aerothermal field in an annular hot streak generator for the study of combustor-turbine interaction 189
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 189
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 188
Uncertainty quantification of film cooling performance of an industrial gas turbine vane 184
Effusion cooling system optimization for modern lean burn combustor 184
ASSESSMENT OF THICKENED FLAME MODEL COUPLED WITH FLAMELET GENERATED MANIFOLD ON A LOW-SWIRL PARTIALLY PREMIXED GASEOUS LIFTED FLAME 180
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 178
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 176
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 174
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 174
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 171
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 171
Numerical investigation of surface roughness effects on heat transfer in a turbine cascade 170
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 168
Assessment of Scale-Resolved Computational Fluid Dynamics Methods for the Investigation of Lean Burn Spray Flames 167
Development of a numerical correlation for the discharge coefficient of round inclined holes with low crossflow 166
Metal temperature prediction of a Dry Low NOx Class Flame tube by computational fluid dynamics conjugate heat transfer approach 165
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 163
Assessment of Aero-Thermal Design Methodology for Effusion Cooled Lean Burn Annular Combustors 163
Assessment of scale resolved CFD methods for the investigation of lean burn spray flames 162
LOCAL SOURCE BASED CFD MODELING OF EFFUSION COOLING HOLES: VALIDATION AND APPLICATION TO AN ACTUAL COMBUSTOR TEST CASE 161
Numerical Analysis of Effusion Plates for Combustor Liners Cooling with Varying Density Ratio 159
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled HPT vanes 159
Hybrid RANS-LES Modeling of a Hot Streak Generator Oriented to the Study of Combustor-Turbine Interaction 158
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and metal temperature 152
Multi-coupled numerical simulations of the DLR Generic Single Sector Combustor 152
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 151
Scale Adaptive Simulations of a Swirl Stabilized Spray Flame Using Flamelet Generated Manifold 150
Metal temperature prediction of a DLN1 class flame tube by CFD CHT approach 148
Local source based CFD modeling of effusion cooling holes: Validation and application to an actual combustor test case 146
Hybrid rans-les modeling of the aero-Thermal field in an annular hot streak generator for the study of combustor-Turbine interaction 146
Heat transfer enhancement due to coolant extraction on the cold side of effusion cooling plates 144
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 143
Reduced-Order Models for Effusion Modeling in Gas Turbine Combustors 142
Thermofluid Dynamic Analysis of a Gas Turbine Transition-Piece 142
Heat Transfer Enhancement due to Coolant Extraction on the Cold Side of Effusion Cooling Plates 140
Numerical Investigation On The Heat Transfer Enhancement Due To Coolant Extraction On The Cold Side Of Film Cooling Holes 139
Numerical modeling of gaseous partially premixed low-swirl lifted flame at elevated pressure 139
Design of a Non-Reactive Warm Rig With Real Lean-Premix Combustor Swirlers and Film-Cooled First Stage Nozzles 138
Modelling strategies for large-eddy simulation of lean burn spray flames 137
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled high pressure turbine vanes 137
Numerical analyses of a high pressure sooting flame with multiphysics approach 136
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 136
Modeling strategies for large eddy simulation of lean burn spray flames 136
External heat transfer on nozzle guide vanes under highly swirled combustor outlet flow 135
Large-Eddy Simulation of a Model Aero-Engine Sooting Flame With a Multiphysics Approach 135
Methane swirl-stabilized lean burn flames: Assessment of scale-resolving simulations 134
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 133
Impact of Swirl Flow on Combustor Liner Heat Transfer and Cooling: A Numerical Investigation with Hybrid Reynolds-Averaged Navier Stokes-Large Eddy Simulation Models 133
Multiphysics numerical investigation of an aeronautical lean burn combustor 132
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 132
Investigation on the effect of a realistic flow field on the adiabatic effectiveness of an effusion-cooled combustor 130
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 130
Numerical investigation of optimized arrangements for effusion cooling in gas turbine combustor applications 129
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 126
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 126
Numerical investigation on the effect of rotation and holes arrangement in cold bridge-type impingement cooling systems 126
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 125
Numerical investigation on the effect of rotation and holes arrangement in cold bridge type impingement cooling systems 125
CHT Analyses of an Industrial Gas Turbine Blade: Comparison Between an In-House Developed Decoupled Procedure and CFD Coupled Simulations 125
ASSESSMENT OF A CONJUGATE HEAT TRANSFER METHOD ON AN EFFUSION COOLED COMBUSTOR OPERATED WITH A SWIRL STABILIZED PARTIALLY PREMIXED FLAME 124
Thermo-fluid dynamic analysis of a gas turbine transition-piece 124
Uncertainty quantification of an aeronautical combustor using a 1-D approach 118
Impact of swirl flow on combustor liner heat transfer and cooling - A numerical investigation with hybrid rans-les models 110
Scale resolving CFD investigations of aerothermal field and emissions of a lean burn aeroengine combustor 109
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 108
Application of uncertainty quantification methods to the prediction of effusion cooled combustor liner temperature 108
Prediction of liner metal temperature of an aeroengine combustor with multi-physics scale-resolving CFD 106
Development of a numerical correlation for heat transfer coefficients in steam turbines inner chambers 102
Reduced-order models for effusion modelling in gas turbine combustors 98
Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame 86
Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame 68
Totale 11.947
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Categoria #
all - tutte 34.065
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 34.065
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021364 0 0 0 0 0 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
2024/20254.254 151 407 276 604 1.262 788 37 214 140 81 132 162
2025/20262.134 344 592 323 337 494 44 0 0 0 0 0 0
Totale 11.947