MAZZEI, LORENZO
 Distribuzione geografica
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Continente #
NA - Nord America 7.135
EU - Europa 3.891
AS - Asia 2.893
SA - Sud America 386
Continente sconosciuto - Info sul continente non disponibili 124
AF - Africa 71
OC - Oceania 35
Totale 14.535
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Nazione #
US - Stati Uniti d'America 7.047
RU - Federazione Russa 1.391
IT - Italia 1.045
CN - Cina 806
SG - Singapore 758
HK - Hong Kong 406
PL - Polonia 358
BR - Brasile 305
IE - Irlanda 280
VN - Vietnam 269
KR - Corea 234
SE - Svezia 224
DE - Germania 132
FR - Francia 130
IN - India 105
FI - Finlandia 97
GB - Regno Unito 73
JO - Giordania 68
CA - Canada 58
AT - Austria 49
JP - Giappone 42
ES - Italia 37
TR - Turchia 35
AU - Australia 34
BD - Bangladesh 33
ID - Indonesia 28
IQ - Iraq 28
AR - Argentina 27
UA - Ucraina 24
NL - Olanda 23
ZA - Sudafrica 14
CI - Costa d'Avorio 13
EC - Ecuador 12
CO - Colombia 11
NG - Nigeria 10
UZ - Uzbekistan 10
VE - Venezuela 10
IR - Iran 9
MX - Messico 9
PK - Pakistan 9
AE - Emirati Arabi Uniti 8
BE - Belgio 8
NP - Nepal 8
CL - Cile 7
MA - Marocco 7
EG - Egitto 6
UY - Uruguay 6
SA - Arabia Saudita 5
DO - Repubblica Dominicana 4
DZ - Algeria 4
IL - Israele 4
JM - Giamaica 4
KE - Kenya 4
MY - Malesia 4
PY - Paraguay 4
TN - Tunisia 4
BG - Bulgaria 3
EU - Europa 3
OM - Oman 3
PE - Perù 3
RO - Romania 3
AZ - Azerbaigian 2
BJ - Benin 2
BW - Botswana 2
CH - Svizzera 2
DK - Danimarca 2
GE - Georgia 2
KZ - Kazakistan 2
LT - Lituania 2
PA - Panama 2
PH - Filippine 2
QA - Qatar 2
SN - Senegal 2
SV - El Salvador 2
TT - Trinidad e Tobago 2
TW - Taiwan 2
AL - Albania 1
AM - Armenia 1
BA - Bosnia-Erzegovina 1
BB - Barbados 1
CG - Congo 1
CR - Costa Rica 1
CZ - Repubblica Ceca 1
DM - Dominica 1
EE - Estonia 1
GH - Ghana 1
GR - Grecia 1
GT - Guatemala 1
HN - Honduras 1
HR - Croazia 1
KG - Kirghizistan 1
KH - Cambogia 1
LA - Repubblica Popolare Democratica del Laos 1
LV - Lettonia 1
LY - Libia 1
MD - Moldavia 1
MO - Macao, regione amministrativa speciale della Cina 1
NZ - Nuova Zelanda 1
PS - Palestinian Territory 1
SR - Suriname 1
Totale 14.409
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Città #
Santa Clara 1.714
Ashburn 752
Fairfield 622
Singapore 592
San Jose 435
Warsaw 355
Hong Kong 345
Dublin 280
Woodbridge 273
Seattle 269
Houston 253
Cambridge 248
Seoul 212
Milan 211
Wilmington 205
Beijing 200
Chandler 191
Florence 181
Altamura 128
Hefei 123
Ann Arbor 99
Lawrence 95
Ho Chi Minh City 90
Princeton 86
Council Bluffs 83
The Dalles 74
Buffalo 72
Los Angeles 71
Moscow 70
Lauterbourg 61
Mumbai 61
New York 57
Munich 55
Rome 55
Hanoi 51
Dearborn 49
Helsinki 48
Vienna 48
Shanghai 43
Clifton 40
Tokyo 39
Boston 38
Kent 37
Medford 37
Melbourne 33
San Diego 27
Barcelona 24
Boardman 24
São Paulo 24
Norwalk 23
Phoenix 23
Dallas 22
Falls Church 22
Haiphong 22
London 20
Chicago 19
Redwood City 19
Jakarta 18
Naples 18
Paris 17
Turin 17
Duncan 16
Figino 16
Falkenstein 15
Frankfurt am Main 14
Guangzhou 14
Abidjan 13
Orem 13
Scandicci 13
Bologna 12
Da Nang 12
Denver 12
Redondo Beach 12
Salerno 12
Toronto 12
Turku 12
Baghdad 11
Chennai 11
Abuja 10
Brasília 10
Dong Ket 10
Hillsboro 10
Istanbul 10
Johannesburg 10
Jinan 9
Madrid 9
Raleigh 9
Salt Lake City 9
Tashkent 9
Amsterdam 8
Ankara 8
Bari 8
Belo Horizonte 8
Chengdu 8
Hangzhou 8
Meudon 8
Rio de Janeiro 8
Shenzhen 8
Spring 8
Yubileyny 8
Totale 9.833
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Nome #
A 3D coupled approach for the thermal design of aero-engine combustor liners 439
Experimental and CFD analyses of a highly-loaded gas turbine blade 425
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 328
Assessment of modelling strategies for film cooling 243
Development of a numerical correlation for the discharge coefficient of round inclined holes with low crossflow 234
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 232
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 230
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 229
A 3d coupled approach for the thermal design of aero-engine combustor liners 228
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 225
ASSESSMENT OF THICKENED FLAME MODEL COUPLED WITH FLAMELET GENERATED MANIFOLD ON A LOW-SWIRL PARTIALLY PREMIXED GASEOUS LIFTED FLAME 224
Hybrid RANS-LES modeling of the aerothermal field in an annular hot streak generator for the study of combustor-turbine interaction 222
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors 222
Uncertainty quantification of film cooling performance of an industrial gas turbine vane 220
Numerical investigation of surface roughness effects on heat transfer in a turbine cascade 216
Effusion cooling system optimization for modern lean burn combustor 216
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 214
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 209
Assessment of Scale-Resolved Computational Fluid Dynamics Methods for the Investigation of Lean Burn Spray Flames 206
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 205
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 199
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 195
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 195
Metal temperature prediction of a Dry Low NOx Class Flame tube by computational fluid dynamics conjugate heat transfer approach 194
Assessment of Aero-Thermal Design Methodology for Effusion Cooled Lean Burn Annular Combustors 193
Assessment of scale resolved CFD methods for the investigation of lean burn spray flames 193
Numerical Analysis of Effusion Plates for Combustor Liners Cooling with Varying Density Ratio 188
Reduced-Order Models for Effusion Modeling in Gas Turbine Combustors 186
LOCAL SOURCE BASED CFD MODELING OF EFFUSION COOLING HOLES: VALIDATION AND APPLICATION TO AN ACTUAL COMBUSTOR TEST CASE 186
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled HPT vanes 186
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and metal temperature 181
External heat transfer on nozzle guide vanes under highly swirled combustor outlet flow 180
Multi-coupled numerical simulations of the DLR Generic Single Sector Combustor 180
Heat transfer enhancement due to coolant extraction on the cold side of effusion cooling plates 180
Hybrid RANS-LES Modeling of a Hot Streak Generator Oriented to the Study of Combustor-Turbine Interaction 179
Design of a Non-Reactive Warm Rig With Real Lean-Premix Combustor Swirlers and Film-Cooled First Stage Nozzles 178
Local source based CFD modeling of effusion cooling holes: Validation and application to an actual combustor test case 176
Scale Adaptive Simulations of a Swirl Stabilized Spray Flame Using Flamelet Generated Manifold 176
Numerical modeling of gaseous partially premixed low-swirl lifted flame at elevated pressure 174
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 172
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 172
Large-Eddy Simulation of a Model Aero-Engine Sooting Flame With a Multiphysics Approach 172
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 172
Modelling strategies for large-eddy simulation of lean burn spray flames 171
Modeling strategies for large eddy simulation of lean burn spray flames 170
Numerical investigation on the effect of rotation and holes arrangement in cold bridge-type impingement cooling systems 170
Hybrid rans-les modeling of the aero-Thermal field in an annular hot streak generator for the study of combustor-Turbine interaction 169
Metal temperature prediction of a DLN1 class flame tube by CFD CHT approach 168
Heat Transfer Enhancement due to Coolant Extraction on the Cold Side of Effusion Cooling Plates 168
Thermofluid Dynamic Analysis of a Gas Turbine Transition-Piece 167
CHT Analyses of an Industrial Gas Turbine Blade: Comparison Between an In-House Developed Decoupled Procedure and CFD Coupled Simulations 167
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 167
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 165
Numerical analyses of a high pressure sooting flame with multiphysics approach 161
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 160
Uncertainty quantification of an aeronautical combustor using a 1-D approach 160
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled high pressure turbine vanes 159
Numerical investigation on the effect of rotation and holes arrangement in cold bridge type impingement cooling systems 159
Numerical Investigation On The Heat Transfer Enhancement Due To Coolant Extraction On The Cold Side Of Film Cooling Holes 158
Methane swirl-stabilized lean burn flames: Assessment of scale-resolving simulations 158
ASSESSMENT OF A CONJUGATE HEAT TRANSFER METHOD ON AN EFFUSION COOLED COMBUSTOR OPERATED WITH A SWIRL STABILIZED PARTIALLY PREMIXED FLAME 156
Impact of Swirl Flow on Combustor Liner Heat Transfer and Cooling: A Numerical Investigation with Hybrid Reynolds-Averaged Navier Stokes-Large Eddy Simulation Models 156
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 155
Multiphysics numerical investigation of an aeronautical lean burn combustor 154
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 153
Numerical investigation of optimized arrangements for effusion cooling in gas turbine combustor applications 153
Investigation on the effect of a realistic flow field on the adiabatic effectiveness of an effusion-cooled combustor 152
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 150
Thermo-fluid dynamic analysis of a gas turbine transition-piece 148
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 144
Application of uncertainty quantification methods to the prediction of effusion cooled combustor liner temperature 144
Prediction of liner metal temperature of an aeroengine combustor with multi-physics scale-resolving CFD 141
Scale resolving CFD investigations of aerothermal field and emissions of a lean burn aeroengine combustor 134
Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame 132
Development of a numerical correlation for heat transfer coefficients in steam turbines inner chambers 129
Impact of swirl flow on combustor liner heat transfer and cooling - A numerical investigation with hybrid rans-les models 127
Reduced-order models for effusion modelling in gas turbine combustors 126
Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame 110
Totale 14.535
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Categoria #
all - tutte 41.421
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 41.421
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022471 0 0 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
2025/20264.322 344 592 323 337 494 177 497 205 422 265 91 575
2026/2027400 113 119 168 0 0 0 0 0 0 0 0 0
Totale 14.535