ANDREINI, ANTONIO
 Distribuzione geografica
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Continente #
NA - Nord America 18.143
EU - Europa 11.572
AS - Asia 7.229
SA - Sud America 1.035
AF - Africa 185
OC - Oceania 118
Continente sconosciuto - Info sul continente non disponibili 9
Totale 38.291
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Nazione #
US - Stati Uniti d'America 17.988
RU - Federazione Russa 4.009
PL - Polonia 2.445
SG - Singapore 1.983
IT - Italia 1.950
CN - Cina 1.935
HK - Hong Kong 1.278
IE - Irlanda 893
BR - Brasile 838
SE - Svezia 769
KR - Corea 699
VN - Vietnam 414
DE - Germania 331
FI - Finlandia 328
IN - India 293
GB - Regno Unito 203
FR - Francia 165
JO - Giordania 155
AT - Austria 122
AU - Australia 116
CA - Canada 94
UA - Ucraina 94
AR - Argentina 91
ID - Indonesia 83
TR - Turchia 82
ES - Italia 73
NL - Olanda 71
CI - Costa d'Avorio 61
JP - Giappone 52
BD - Bangladesh 42
MX - Messico 38
IQ - Iraq 37
ZA - Sudafrica 37
EC - Ecuador 35
BE - Belgio 34
IR - Iran 26
MA - Marocco 24
CH - Svizzera 21
PK - Pakistan 19
CO - Colombia 17
AE - Emirati Arabi Uniti 16
KE - Kenya 15
SA - Arabia Saudita 14
NP - Nepal 13
VE - Venezuela 13
EG - Egitto 12
RO - Romania 12
UY - Uruguay 12
AZ - Azerbaigian 11
CL - Cile 10
PY - Paraguay 10
DZ - Algeria 9
LT - Lituania 9
UZ - Uzbekistan 9
IL - Israele 8
BJ - Benin 7
DO - Repubblica Dominicana 7
KZ - Kazakistan 7
PE - Perù 7
PT - Portogallo 7
GR - Grecia 6
EU - Europa 5
KG - Kirghizistan 5
MY - Malesia 5
TN - Tunisia 5
CZ - Repubblica Ceca 4
EE - Estonia 4
HN - Honduras 4
OM - Oman 4
QA - Qatar 4
XK - ???statistics.table.value.countryCode.XK??? 4
AL - Albania 3
BG - Bulgaria 3
BH - Bahrain 3
BY - Bielorussia 3
JM - Giamaica 3
LA - Repubblica Popolare Democratica del Laos 3
LB - Libano 3
NG - Nigeria 3
NO - Norvegia 3
PA - Panama 3
PH - Filippine 3
PS - Palestinian Territory 3
TW - Taiwan 3
AM - Armenia 2
BW - Botswana 2
DK - Danimarca 2
GE - Georgia 2
KH - Cambogia 2
KW - Kuwait 2
LK - Sri Lanka 2
LU - Lussemburgo 2
NZ - Nuova Zelanda 2
RS - Serbia 2
SN - Senegal 2
TH - Thailandia 2
AO - Angola 1
BO - Bolivia 1
BZ - Belize 1
CG - Congo 1
Totale 38.270
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Città #
Santa Clara 5.326
Warsaw 2.437
Fairfield 1.687
Singapore 1.475
Ashburn 1.351
Hong Kong 1.091
Dublin 887
Woodbridge 758
Seattle 726
Houston 689
Seoul 679
Cambridge 622
Chandler 595
Florence 563
Wilmington 554
Beijing 532
Hefei 409
San Jose 390
Altamura 371
Lawrence 323
Ann Arbor 312
Princeton 253
Buffalo 249
Los Angeles 178
Moscow 175
Ho Chi Minh City 167
Mumbai 165
Boston 146
Shanghai 130
Helsinki 126
Munich 117
Melbourne 115
Vienna 115
New York 107
Medford 102
Dallas 100
The Dalles 100
Kent 99
Prato 95
Milan 88
San Diego 85
Boardman 84
Clifton 81
Falls Church 74
Dearborn 73
Jacksonville 73
São Paulo 69
Hanoi 66
Abidjan 61
Chicago 58
Jakarta 55
Norwalk 50
Redondo Beach 49
Turku 49
Redwood City 45
London 42
Barcelona 41
Duncan 40
Dong Ket 39
Rome 39
Tokyo 37
Brussels 34
Frankfurt am Main 34
Bengaluru 33
Paris 33
Toronto 33
Falkenstein 32
Council Bluffs 30
Rio de Janeiro 29
Yubileyny 28
Hillsboro 26
Phoenix 26
Johannesburg 24
Montreal 24
Brooklyn 23
Lappeenranta 22
Salt Lake City 20
Turin 20
Haiphong 19
Istanbul 19
Izmir 19
Belo Horizonte 18
Orem 18
Carpi 17
Chennai 17
Salerno 17
Harbin 16
Madrid 16
San Francisco 16
Tampa 16
Andover 15
Brasília 15
Denver 15
Scandicci 15
Stockholm 14
Chengdu 13
Guangzhou 13
Nairobi 13
Ottawa 13
Perugia 13
Totale 26.432
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 385
Gas Turbines Design and Off-design Performance Analysis with Emissions Evaluation 368
The effect of effusion holes inclination angle on the adiabatic film cooling effectiveness in a three-sector gas turbine combustor rig with a realistic swirling flow 338
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 312
SVILUPPO DI MODELLI NUMERICI PER L’ANALISI DELLA COMBUSTIONE TURBOLENTA PREMISCELATA NELLE TURBINE A GAS 302
Turbulent flow-field effects in a hybrid CFD-CRN model for the prediction of NOxand CO emissions in aero-engine combustors 302
A Decoupled CHT Procedure: Application and Validation on a Gas Turbine Vane with Different Cooling Configurations 301
Numerical Simulation of Oil Jet Lubrication for High Speed Gears 296
CFD Analysis of NOx Emissions of a Natural Gas Lean Premixed Burner for Heavy Duty Gas Turbine 294
Numerical Characterization of Pressure Drop Across the Manifold of Turbine Casing Cooling System 290
PYROLYSIS MODELING AND NUMERICAL SIMULATION OF RAIL CARRIAGE FIRE SCENARIOS FOR THE SAFE DESIGN OF A PASSENGER TRAIN 285
Numerical analysis of the dynamic flame response of a spray flame for aero-engine applications 285
DENSITY RATIO EFFECTS ON THE COOLING PERFORMANCES OF A COMBUSTOR LINER COOLED BY A COMBINED SLOT/ EFFUSION SYSTEM 285
Aerothermal Analysis of a Turbine Casing Impingement Cooling System 285
Numerical Identification of a Premixed Flame Transfer Function and Stability Analysis of a Lean Burn Combustor 282
LES FOR THE EVALUATION OF ACOUSTIC DAMPING OF EFFUSION PLATES 281
Experimental Evaluation of the Density Ratio Effects on the Cooling Performance of a Combined Slot/Effusion Combustor Cooling System 281
Large Eddy Simulation of a Bluff Body Stabilized Lean Premixed Flame 277
COMBUSTOR LINER TEMPERATURE PREDICTION: A PRELIMINARY TOOL DEVELOPMENT AND ITS APPLICATION ON EFFUSION COOLING SYSTEMS 272
NUMERICAL HEAT TRANSFER ANALYSIS OF AN INNOVATIVE GAS TURBINE COMBUSTOR: COUPLED STUDY OF RADIATION AND COOLING IN THE UPPER PART OF THE LINER 249
Film cooling modeling for gas turbine nozzles and blades: Validation and application 240
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON WINDAGE POWER LOSSES IN HIGH SPEED GEARS 221
Development of a turbulent liquid flux model for Eulerian-Eulerian multiphase flow simulations 216
Assessment of modelling strategies for film cooling 211
Volume Of Fluid (VOF) Analysis of Oil-Jet Lubrication for High-Speed Spur Gears Using an Adaptive Meshing Approach 202
A 3d coupled approach for the thermal design of aero-engine combustor liners 200
Experimental and numerical investigation on windage power losses in high speed gears 199
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors 198
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 197
Hybrid RANS-LES modeling of the aerothermal field in an annular hot streak generator for the study of combustor-turbine interaction 196
ASSESSMENT OF A SET OF NUMERICAL TOOLS FOR THE DESIGN OF AERO ENGINES COMBUSTORS: STUDY OF A TUBULAR TEST RIG 194
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 192
Uncertainty quantification of film cooling performance of an industrial gas turbine vane 188
Heat transfer investigation on an internal cooling system of a gas turbine leading edge model 188
Transient thermal modelling of whole gt engine with a partly coupled fem-fluid network approach 188
ASSESSMENT OF THICKENED FLAME MODEL COUPLED WITH FLAMELET GENERATED MANIFOLD ON A LOW-SWIRL PARTIALLY PREMIXED GASEOUS LIFTED FLAME 187
Investigation on low-pressure steam turbine exhaust hood modelling through computational fluid dynamic simulations 187
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 186
Numerical Analysis of a Low NOx Partially Premixed Burner for Industrial Gas Turbine Applications 185
Effusion cooling system optimization for modern lean burn combustor 185
Numerical predictions of pollutant emissions of novel natural gas low nox burners for heavy duty gas turbine 185
Numerical Simulation of Dam-Break Problem Using an Adaptive Meshing Approach 182
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 182
CFD simulations of a meshing gear pair 181
Experimental and Numerical Analysis of Multiple Impingement Jet Arrays for an Active Clearance Control System 181
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 180
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 179
Cooling system optimization of combustor liners 179
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 179
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 178
Development of a numerical correlation for the discharge coefficient of round inclined holes with low crossflow 178
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 177
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 177
Heat transfer in internal channel of a blade: effects of rotation in a trailing edge cooling system 176
ASSESSMENT OF NUMERICAL TOOLS FOR THE EVALUATION OF THE ACOUSTICIMPEDANCE OF MULTI-PERFORATED PLATES. 175
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 175
Assessment of Flame Transfer Function Formulations for the Thermoacoustic Analysis of Lean Burn Aero-engine Combustors 174
Numerical Investigation On the Aerodynamic Performance of a Low-Pressure Steam Turbine Exhaust Hood Using Doe Analysis 173
Assessment of Scale-Resolved Computational Fluid Dynamics Methods for the Investigation of Lean Burn Spray Flames 172
Numerical investigation of surface roughness effects on heat transfer in a turbine cascade 171
Metal temperature prediction of a Dry Low NOx Class Flame tube by computational fluid dynamics conjugate heat transfer approach 170
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 169
Numerical study of aerodynamic losses of effusion cooling holes in aero-engine combustor liners 168
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 168
Thermoacoustic analysis of a full annular lean burn aero-engine combustor 167
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 167
Assessment of Aero-Thermal Design Methodology for Effusion Cooled Lean Burn Annular Combustors 167
Film Cooling Modelling for Gas Turbine Nozzles and Blades: Validation and Application 167
Numerical investigations of pollutant emissions from novel heavy duty gas turbine burners operated with natural gas 167
Assessment of turbulent models for a low-pressure turbine guide vane heat transfer with high free-stream turbulence 166
Assessment of scale resolved CFD methods for the investigation of lean burn spray flames 166
Numerical investigation on windage losses of high-speed gears in enclosed configuration 166
NUMERICAL STUDY OF COMBUSTOR-TURBINE INTERACTION BY USING HYBRID RANS-LES APPROACH 165
Experimental Investigation of the Flow Field and the Heat Transfer on a Scaled Cooled Combustor Liner With Realistic Swirling Flow Generated by a Lean-Burn Injection System 165
Large-Eddy Simulation of a turbulent spray flame using the flamelet generated manifold approach 165
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled HPT vanes 165
Numerical Study of Aerodynamic Losses of Effusion Cooling Holes in Aero-Engine Combustor Liners 163
Conjugate Heat Transfer Calculations on GT Rotor Blade for Industrial Applications. Part I: Equivalent Internal Fluid Network Setup and Procedure Description 163
Effect of slot injection and effusion array on the liner heat transfer coefficient of a scaled lean burn combustor with representative swirling flow 163
LOCAL SOURCE BASED CFD MODELING OF EFFUSION COOLING HOLES: VALIDATION AND APPLICATION TO AN ACTUAL COMBUSTOR TEST CASE 162
Numerical Analysis of Effusion Plates for Combustor Liners Cooling with Varying Density Ratio 162
Hybrid RANS-LES Modeling of a Hot Streak Generator Oriented to the Study of Combustor-Turbine Interaction 162
Multi-Coupled Numerical Analysis of Advanced Lean Burn Injection Systems 162
Design improvement survey for NOx emissions reduction of a heavy-duty gas turbine partially premixed fuel nozzle operating with natural gas: Numerical assessment 161
Multi-coupled numerical simulations of the DLR Generic Single Sector Combustor 158
INVESTIGATION OF CIRCULAR AND SHAPED EFFUSION COOLING ARRAYS FOR COMBUSTOR LINER APPLICATION - PART 2: NUMERICAL ANALYSIS 158
Experimental Investigation of the Flow Field and the Heat Transfer on a Scaled Cooled Combustor Liner With Realistic Swirling Flow Generated by a Lean-Burn Injection System 158
Combined Effect of Slot Injection, Effusion Array and Dilution Hole on the Heat Transfer Coefficient of a Real Combustor Liner: Part 2: Numerical Analysis 157
EXPERIMENTAL INVESTIGATION ON EFFUSION LINER GEOMETRIES FOR AERO-ENGINE COMBUSTORS: EVALUATION OF GLOBAL ACOUSTIC PARAMETERS. 156
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and metal temperature 155
Flowfield and heat transfer numerical analysis of a stator vane endwall with high freestream turbulence 155
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 155
Conjugate heat transfer methodology for thermal design and verification of gas turbine cooled components 155
Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow 154
Flow Field Analysis of a Trailing Edge Internal Cooling Channel 154
Numerical Benchmark of Nonconventional RANS Turbulence Models for Film and Effusion Cooling 154
A multi-coupled Eulerian-Lagrangian solver for airblast injectors including liquid film evolution and primary breakup - Application 154
Three-dimensional cfd analysis of meshing losses in a spur gear pair 153
Scale Adaptive Simulations of a Swirl Stabilized Spray Flame Using Flamelet Generated Manifold 153
Numerical Analysis of Heat Transfer in a Leading Edge Geometry With Racetrack Holes and Film Cooling Extraction 152
Totale 19.931
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Categoria #
all - tutte 107.198
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 107.198
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.070 0 0 0 0 0 0 120 209 243 248 151 99
2021/20221.790 92 109 130 75 88 137 72 154 67 70 337 459
2022/20234.157 400 819 219 237 264 763 593 214 449 46 108 45
2023/20241.683 78 186 253 94 97 162 95 318 70 103 160 67
2024/202513.071 442 1.202 763 1.753 4.058 2.312 152 730 461 266 420 512
2025/20267.869 1.111 1.796 1.135 1.008 1.585 613 621 0 0 0 0 0
Totale 38.626