MAZZEI, LORENZO
 Distribuzione geografica
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Continente #
NA - Nord America 6.799
EU - Europa 3.874
AS - Asia 2.870
SA - Sud America 370
AF - Africa 70
OC - Oceania 34
Continente sconosciuto - Info sul continente non disponibili 4
Totale 14.021
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Nazione #
US - Stati Uniti d'America 6.748
RU - Federazione Russa 1.391
IT - Italia 1.030
CN - Cina 801
SG - Singapore 755
HK - Hong Kong 405
PL - Polonia 358
BR - Brasile 295
IE - Irlanda 280
VN - Vietnam 266
KR - Corea 231
SE - Svezia 224
DE - Germania 131
FR - Francia 130
IN - India 105
FI - Finlandia 97
GB - Regno Unito 73
JO - Giordania 67
AT - Austria 49
JP - Giappone 42
ES - Italia 37
AU - Australia 33
BD - Bangladesh 32
TR - Turchia 32
CA - Canada 31
ID - Indonesia 28
IQ - Iraq 27
AR - Argentina 26
UA - Ucraina 24
NL - Olanda 23
ZA - Sudafrica 14
CI - Costa d'Avorio 13
EC - Ecuador 11
NG - Nigeria 10
UZ - Uzbekistan 10
IR - Iran 9
MX - Messico 9
PK - Pakistan 9
VE - Venezuela 9
AE - Emirati Arabi Uniti 8
BE - Belgio 8
CO - Colombia 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
KE - Kenya 4
PY - Paraguay 4
TN - Tunisia 4
BG - Bulgaria 3
EU - Europa 3
MY - Malesia 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
PA - Panama 2
QA - Qatar 2
SN - Senegal 2
TW - Taiwan 2
AL - Albania 1
AM - Armenia 1
BA - Bosnia-Erzegovina 1
CG - Congo 1
CZ - Repubblica Ceca 1
DM - Dominica 1
EE - Estonia 1
GH - Ghana 1
GR - Grecia 1
HR - Croazia 1
JM - Giamaica 1
KG - Kirghizistan 1
KH - Cambogia 1
LA - Repubblica Popolare Democratica del Laos 1
LT - Lituania 1
LV - Lettonia 1
MD - Moldavia 1
MO - Macao, regione amministrativa speciale della Cina 1
NZ - Nuova Zelanda 1
PH - Filippine 1
PS - Palestinian Territory 1
SR - Suriname 1
SY - Repubblica araba siriana 1
TH - Thailandia 1
TJ - Tagikistan 1
TT - Trinidad e Tobago 1
VC - Saint Vincent e Grenadine 1
VG - Isole Vergini Britanniche 1
XK - ???statistics.table.value.countryCode.XK??? 1
Totale 14.021
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Città #
Santa Clara 1.699
Ashburn 737
Fairfield 622
Singapore 590
San Jose 372
Warsaw 355
Hong Kong 344
Dublin 280
Woodbridge 273
Seattle 269
Houston 253
Cambridge 248
Seoul 212
Milan 207
Wilmington 205
Beijing 196
Chandler 191
Florence 179
Altamura 128
Hefei 123
Ann Arbor 99
Lawrence 95
Ho Chi Minh City 90
Princeton 86
The Dalles 74
Buffalo 72
Moscow 70
Los Angeles 63
Lauterbourg 61
Mumbai 61
New York 56
Munich 55
Rome 53
Hanoi 50
Dearborn 49
Helsinki 48
Vienna 48
Shanghai 42
Clifton 40
Tokyo 39
Boston 37
Kent 37
Medford 37
Melbourne 33
San Diego 27
Barcelona 24
Boardman 24
São Paulo 24
Norwalk 23
Falls Church 22
Dallas 20
Haiphong 20
London 19
Redwood City 19
Chicago 18
Jakarta 18
Naples 17
Paris 17
Turin 17
Duncan 16
Figino 16
Council Bluffs 15
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
Turku 12
Baghdad 11
Chennai 11
Abuja 10
Dong Ket 10
Hillsboro 10
Johannesburg 10
Jinan 9
Madrid 9
Salt Lake City 9
Tashkent 9
Toronto 9
Amsterdam 8
Bari 8
Belo Horizonte 8
Chengdu 8
Hangzhou 8
Istanbul 8
Meudon 8
Raleigh 8
Rio de Janeiro 8
Shenzhen 8
Spring 8
Yubileyny 8
Ankara 7
Bengaluru 7
Brussels 7
Totale 9.612
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Nome #
A 3D coupled approach for the thermal design of aero-engine combustor liners 426
Experimental and CFD analyses of a highly-loaded gas turbine blade 420
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 325
Assessment of modelling strategies for film cooling 238
Development of a numerical correlation for the discharge coefficient of round inclined holes with low crossflow 228
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 227
A 3d coupled approach for the thermal design of aero-engine combustor liners 225
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 225
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 223
Hybrid RANS-LES modeling of the aerothermal field in an annular hot streak generator for the study of combustor-turbine interaction 219
ASSESSMENT OF THICKENED FLAME MODEL COUPLED WITH FLAMELET GENERATED MANIFOLD ON A LOW-SWIRL PARTIALLY PREMIXED GASEOUS LIFTED FLAME 216
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 214
Uncertainty quantification of film cooling performance of an industrial gas turbine vane 213
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors 213
Effusion cooling system optimization for modern lean burn combustor 209
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 208
Numerical investigation of surface roughness effects on heat transfer in a turbine cascade 203
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 202
Assessment of Scale-Resolved Computational Fluid Dynamics Methods for the Investigation of Lean Burn Spray Flames 202
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 202
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 197
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 192
Metal temperature prediction of a Dry Low NOx Class Flame tube by computational fluid dynamics conjugate heat transfer approach 192
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 191
Assessment of scale resolved CFD methods for the investigation of lean burn spray flames 191
Assessment of Aero-Thermal Design Methodology for Effusion Cooled Lean Burn Annular Combustors 188
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled HPT vanes 183
Numerical Analysis of Effusion Plates for Combustor Liners Cooling with Varying Density Ratio 181
LOCAL SOURCE BASED CFD MODELING OF EFFUSION COOLING HOLES: VALIDATION AND APPLICATION TO AN ACTUAL COMBUSTOR TEST CASE 179
Multi-coupled numerical simulations of the DLR Generic Single Sector Combustor 177
Heat transfer enhancement due to coolant extraction on the cold side of effusion cooling plates 177
Hybrid RANS-LES Modeling of a Hot Streak Generator Oriented to the Study of Combustor-Turbine Interaction 176
Reduced-Order Models for Effusion Modeling in Gas Turbine Combustors 175
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and metal temperature 175
Local source based CFD modeling of effusion cooling holes: Validation and application to an actual combustor test case 174
Scale Adaptive Simulations of a Swirl Stabilized Spray Flame Using Flamelet Generated Manifold 174
Numerical modeling of gaseous partially premixed low-swirl lifted flame at elevated pressure 174
Design of a Non-Reactive Warm Rig With Real Lean-Premix Combustor Swirlers and Film-Cooled First Stage Nozzles 172
External heat transfer on nozzle guide vanes under highly swirled combustor outlet flow 170
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 169
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 168
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 168
Modelling strategies for large-eddy simulation of lean burn spray flames 167
Modeling strategies for large eddy simulation of lean burn spray flames 167
Thermofluid Dynamic Analysis of a Gas Turbine Transition-Piece 165
Metal temperature prediction of a DLN1 class flame tube by CFD CHT approach 165
Hybrid rans-les modeling of the aero-Thermal field in an annular hot streak generator for the study of combustor-Turbine interaction 165
Heat Transfer Enhancement due to Coolant Extraction on the Cold Side of Effusion Cooling Plates 162
Large-Eddy Simulation of a Model Aero-Engine Sooting Flame With a Multiphysics Approach 161
Numerical investigation on the effect of rotation and holes arrangement in cold bridge-type impingement cooling systems 159
Numerical analyses of a high pressure sooting flame with multiphysics approach 158
CHT Analyses of an Industrial Gas Turbine Blade: Comparison Between an In-House Developed Decoupled Procedure and CFD Coupled Simulations 158
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 157
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled high pressure turbine vanes 157
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 157
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 156
Uncertainty quantification of an aeronautical combustor using a 1-D approach 156
Numerical investigation on the effect of rotation and holes arrangement in cold bridge type impingement cooling systems 155
Numerical Investigation On The Heat Transfer Enhancement Due To Coolant Extraction On The Cold Side Of Film Cooling Holes 155
Methane swirl-stabilized lean burn flames: Assessment of scale-resolving simulations 154
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 153
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 152
ASSESSMENT OF A CONJUGATE HEAT TRANSFER METHOD ON AN EFFUSION COOLED COMBUSTOR OPERATED WITH A SWIRL STABILIZED PARTIALLY PREMIXED FLAME 152
Impact of Swirl Flow on Combustor Liner Heat Transfer and Cooling: A Numerical Investigation with Hybrid Reynolds-Averaged Navier Stokes-Large Eddy Simulation Models 152
Numerical investigation of optimized arrangements for effusion cooling in gas turbine combustor applications 150
Multiphysics numerical investigation of an aeronautical lean burn combustor 149
Investigation on the effect of a realistic flow field on the adiabatic effectiveness of an effusion-cooled combustor 149
Thermo-fluid dynamic analysis of a gas turbine transition-piece 146
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 145
Application of uncertainty quantification methods to the prediction of effusion cooled combustor liner temperature 140
Prediction of liner metal temperature of an aeroengine combustor with multi-physics scale-resolving CFD 138
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 136
Scale resolving CFD investigations of aerothermal field and emissions of a lean burn aeroengine combustor 132
Development of a numerical correlation for heat transfer coefficients in steam turbines inner chambers 125
Reduced-order models for effusion modelling in gas turbine combustors 124
Impact of swirl flow on combustor liner heat transfer and cooling - A numerical investigation with hybrid rans-les models 123
Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame 117
Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame 102
Totale 14.140
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Categoria #
all - tutte 39.308
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 39.308
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
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
2025/20264.322 344 592 323 337 494 177 497 205 422 265 91 575
2026/20275 5 0 0 0 0 0 0 0 0 0 0 0
Totale 14.140