ANDREINI, ANTONIO
 Distribuzione geografica
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Continente #
NA - Nord America 15.620
EU - Europa 9.725
AS - Asia 2.222
OC - Oceania 112
AF - Africa 68
SA - Sud America 9
Continente sconosciuto - Info sul continente non disponibili 5
Totale 27.761
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Nazione #
US - Stati Uniti d'America 15.574
RU - Federazione Russa 2.983
PL - Polonia 2.418
IT - Italia 1.703
IE - Irlanda 888
SE - Svezia 752
CN - Cina 681
SG - Singapore 648
HK - Hong Kong 376
FI - Finlandia 264
IN - India 196
DE - Germania 163
JO - Giordania 152
GB - Regno Unito 138
AT - Austria 116
AU - Australia 112
FR - Francia 79
UA - Ucraina 72
CI - Costa d'Avorio 60
TR - Turchia 54
ES - Italia 52
CA - Canada 46
VN - Vietnam 41
BE - Belgio 33
NL - Olanda 24
IR - Iran 22
KR - Corea 19
CH - Svizzera 16
JP - Giappone 14
RO - Romania 10
BR - Brasile 5
EU - Europa 5
NP - Nepal 5
PK - Pakistan 4
PT - Portogallo 4
LT - Lituania 3
NG - Nigeria 3
TW - Taiwan 3
DZ - Algeria 2
EE - Estonia 2
ID - Indonesia 2
BG - Bulgaria 1
CL - Cile 1
CM - Camerun 1
CO - Colombia 1
CZ - Repubblica Ceca 1
DK - Danimarca 1
EC - Ecuador 1
GE - Georgia 1
LU - Lussemburgo 1
MO - Macao, regione amministrativa speciale della Cina 1
MU - Mauritius 1
NO - Norvegia 1
SA - Arabia Saudita 1
SC - Seychelles 1
SY - Repubblica araba siriana 1
TH - Thailandia 1
VE - Venezuela 1
Totale 27.761
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Città #
Santa Clara 5.288
Warsaw 2.417
Fairfield 1.687
Dublin 882
Ashburn 795
Woodbridge 758
Seattle 726
Houston 678
Cambridge 622
Chandler 595
Singapore 554
Wilmington 552
Florence 490
Altamura 371
Lawrence 323
Ann Arbor 312
Princeton 253
Beijing 237
Hong Kong 199
Mumbai 149
Boston 137
Buffalo 137
Shanghai 126
Helsinki 123
Moscow 121
Vienna 114
Melbourne 110
Medford 102
Prato 92
Boardman 84
San Diego 84
Falls Church 74
Dearborn 73
Jacksonville 73
Kent 62
Abidjan 60
New York 54
Norwalk 50
Milan 46
Redwood City 45
Barcelona 41
Duncan 40
Dong Ket 39
Brussels 33
Rome 31
Falkenstein 30
Yubileyny 28
Hillsboro 26
Toronto 26
Los Angeles 23
London 21
Izmir 19
Salerno 17
Carpi 16
Phoenix 16
Andover 15
Harbin 15
Scandicci 15
Ottawa 13
Perugia 13
Chicago 12
Munich 12
West Jordan 12
Xian 12
Cranfield 11
Istanbul 11
Tappahannock 11
Tong 11
Turin 11
Gaggiano 10
Guangzhou 10
Lappeenranta 10
Prad am Stilfser Joch 10
Torino 10
Bari 9
Chennai 9
Genova 9
Meudon 9
Redmond 9
Bologna 8
Dallas 8
Frankfurt am Main 8
Hachenburg 8
Sesto Fiorentino 8
Changsha 7
Chengdu 7
Doruk 7
Jinan 7
Laurel 7
Nanchang 7
Nanjing 7
Raleigh 7
Seoul 7
Berlin 6
Cagliari 6
Fuzhou 6
Genoa 6
Hangzhou 6
Karlsruhe 6
Livorno 6
Totale 20.475
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 342
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 303
Gas Turbines Design and Off-design Performance Analysis with Emissions Evaluation 302
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 276
Turbulent flow-field effects in a hybrid CFD-CRN model for the prediction of NOxand CO emissions in aero-engine combustors 269
Aerothermal Analysis of a Turbine Casing Impingement Cooling System 261
CFD Analysis of NOx Emissions of a Natural Gas Lean Premixed Burner for Heavy Duty Gas Turbine 261
A Decoupled CHT Procedure: Application and Validation on a Gas Turbine Vane with Different Cooling Configurations 258
Numerical analysis of the dynamic flame response of a spray flame for aero-engine applications 256
Numerical Simulation of Oil Jet Lubrication for High Speed Gears 254
Numerical Identification of a Premixed Flame Transfer Function and Stability Analysis of a Lean Burn Combustor 254
Experimental Evaluation of the Density Ratio Effects on the Cooling Performance of a Combined Slot/Effusion Combustor Cooling System 251
DENSITY RATIO EFFECTS ON THE COOLING PERFORMANCES OF A COMBUSTOR LINER COOLED BY A COMBINED SLOT/ EFFUSION SYSTEM 249
Large Eddy Simulation of a Bluff Body Stabilized Lean Premixed Flame 248
PYROLYSIS MODELING AND NUMERICAL SIMULATION OF RAIL CARRIAGE FIRE SCENARIOS FOR THE SAFE DESIGN OF A PASSENGER TRAIN 246
SVILUPPO DI MODELLI NUMERICI PER L’ANALISI DELLA COMBUSTIONE TURBOLENTA PREMISCELATA NELLE TURBINE A GAS 244
LES FOR THE EVALUATION OF ACOUSTIC DAMPING OF EFFUSION PLATES 239
Numerical Characterization of Pressure Drop Across the Manifold of Turbine Casing Cooling System 236
COMBUSTOR LINER TEMPERATURE PREDICTION: A PRELIMINARY TOOL DEVELOPMENT AND ITS APPLICATION ON EFFUSION COOLING SYSTEMS 223
NUMERICAL HEAT TRANSFER ANALYSIS OF AN INNOVATIVE GAS TURBINE COMBUSTOR: COUPLED STUDY OF RADIATION AND COOLING IN THE UPPER PART OF THE LINER 210
Film cooling modeling for gas turbine nozzles and blades: Validation and application 194
Development of a turbulent liquid flux model for Eulerian-Eulerian multiphase flow simulations 175
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON WINDAGE POWER LOSSES IN HIGH SPEED GEARS 174
ASSESSMENT OF A SET OF NUMERICAL TOOLS FOR THE DESIGN OF AERO ENGINES COMBUSTORS: STUDY OF A TUBULAR TEST RIG 168
Assessment of modelling strategies for film cooling 163
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 159
Volume Of Fluid (VOF) Analysis of Oil-Jet Lubrication for High-Speed Spur Gears Using an Adaptive Meshing Approach 159
Hybrid RANS-LES modeling of the aerothermal field in an annular hot streak generator for the study of combustor-turbine interaction 158
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 158
A 3d coupled approach for the thermal design of aero-engine combustor liners 157
Numerical Analysis of a Low NOx Partially Premixed Burner for Industrial Gas Turbine Applications 155
Experimental and Numerical Analysis of Multiple Impingement Jet Arrays for an Active Clearance Control System 151
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 150
Experimental and numerical investigation on windage power losses in high speed gears 150
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 147
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 144
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 144
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors 144
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 142
ASSESSMENT OF NUMERICAL TOOLS FOR THE EVALUATION OF THE ACOUSTICIMPEDANCE OF MULTI-PERFORATED PLATES. 140
Assessment of Flame Transfer Function Formulations for the Thermoacoustic Analysis of Lean Burn Aero-engine Combustors 140
Heat transfer investigation on an internal cooling system of a gas turbine leading edge model 140
Development of a numerical correlation for the discharge coefficient of round inclined holes with low crossflow 140
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 140
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 140
Metal temperature prediction of a Dry Low NOx Class Flame tube by computational fluid dynamics conjugate heat transfer approach 139
Heat transfer in internal channel of a blade: effects of rotation in a trailing edge cooling system 137
Assessment of Aero-Thermal Design Methodology for Effusion Cooled Lean Burn Annular Combustors 137
Assessment of Scale-Resolved Computational Fluid Dynamics Methods for the Investigation of Lean Burn Spray Flames 136
Numerical predictions of pollutant emissions of novel natural gas low nox burners for heavy duty gas turbine 136
Film Cooling Modelling for Gas Turbine Nozzles and Blades: Validation and Application 135
Numerical study of aerodynamic losses of effusion cooling holes in aero-engine combustor liners 135
Assessment of scale resolved CFD methods for the investigation of lean burn spray flames 134
LOCAL SOURCE BASED CFD MODELING OF EFFUSION COOLING HOLES: VALIDATION AND APPLICATION TO AN ACTUAL COMBUSTOR TEST CASE 133
Numerical Study of Aerodynamic Losses of Effusion Cooling Holes in Aero-Engine Combustor Liners 133
Numerical Characterization of Aerodynamic Losses of Jet Arrays for Gas Turbine Applications 132
CFD simulations of a meshing gear pair 132
Effect of slot injection and effusion array on the liner heat transfer coefficient of a scaled lean burn combustor with representative swirling flow 131
Effusion cooling system optimization for modern lean burn combustor 131
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 130
Large-Eddy Simulation of a turbulent spray flame using the flamelet generated manifold approach 130
Design improvement survey for NOx emissions reduction of a heavy-duty gas turbine partially premixed fuel nozzle operating with natural gas: Numerical assessment 129
Numerical Simulation of Dam-Break Problem Using an Adaptive Meshing Approach 129
Numerical investigations of pollutant emissions from novel heavy duty gas turbine burners operated with natural gas 129
INVESTIGATION OF CIRCULAR AND SHAPED EFFUSION COOLING ARRAYS FOR COMBUSTOR LINER APPLICATION - PART 2: NUMERICAL ANALYSIS 129
EXPERIMENTAL INVESTIGATION ON EFFUSION LINER GEOMETRIES FOR AERO-ENGINE COMBUSTORS: EVALUATION OF GLOBAL ACOUSTIC PARAMETERS. 129
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 129
Thermoacoustic analysis of a full annular lean burn aero-engine combustor 128
Cooling system optimization of combustor liners 128
Numerical Analysis of Effusion Plates for Combustor Liners Cooling with Varying Density Ratio 128
Transient thermal modelling of whole gt engine with a partly coupled fem-fluid network approach 128
Numerical Investigation On the Aerodynamic Performance of a Low-Pressure Steam Turbine Exhaust Hood Using Doe Analysis 128
Turbine stator well CFD studies: Effects of coolant supply geometry on cavity sealing performance 127
Multi-Coupled Numerical Analysis of Advanced Lean Burn Injection Systems 127
Flowfield and heat transfer numerical analysis of a stator vane endwall with high freestream turbulence 126
Scale Adaptive Simulations of a Swirl Stabilized Spray Flame Using Flamelet Generated Manifold 126
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled HPT vanes 126
Conjugate heat transfer methodology for thermal design and verification of gas turbine cooled components 126
Thermofluid Dynamic Analysis of a Gas Turbine Transition-Piece 125
Three-dimensional cfd analysis of meshing losses in a spur gear pair 125
Investigation on low-pressure steam turbine exhaust hood modelling through computational fluid dynamic simulations 125
Uncertainty quantification of film cooling performance of an industrial gas turbine vane 124
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 123
Numerical investigation on windage losses of high-speed gears in enclosed configuration 123
Flow Field Analysis of a Trailing Edge Internal Cooling Channel 122
NUMERICAL BENCHMARK OF NON-CONVENTIONAL RANS TURBULENCE MODELS FOR FILM AND EFFUSION COOLING 122
Numerical Investigations of NOx Emissions of a Partially Premixed Burner for Natural Gas Operations in Industrial Gas Turbine 122
Numerical Benchmark of Nonconventional RANS Turbulence Models for Film and Effusion Cooling 122
Numerical Characterization of Swirl Brakes for High Pressure Centrifugal Compressors 122
Numerical Benchmark of Turbulence Modeling in Gas Turbine Rotor-Stator System 121
Metal temperature prediction of a DLN1 class flame tube by CFD CHT approach 121
Combined Effect of Slot Injection, Effusion Array and Dilution Hole on the Heat Transfer Coefficient of a Real Combustor Liner: Part 2: Numerical Analysis 120
NUMERICAL CHARACTERIZATION OF PRESSURE DROP ACROSS THE MANIFOLD OF TURBINE CASING COOLING SYSTEM 120
Numerical Analysis of Heat Transfer in a Leading Edge Geometry With Racetrack Holes and Film Cooling Extraction 120
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and metal temperature 120
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 120
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 120
Film Cooling System Numerical Design: Adiabatic and Conjugate Analysis 120
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 120
Heat transfer augmentation due to coolant extraction on the cold side of active clearance control manifolds 120
Totale 16.004
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Categoria #
all - tutte 76.879
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 76.879
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20202.555 0 0 0 0 0 482 510 476 424 266 307 90
2020/20212.208 180 197 89 289 201 182 120 209 243 248 151 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
2024/202510.391 442 1.202 763 1.753 4.058 2.173 0 0 0 0 0 0
Totale 28.077