FACCHINI, BRUNO
 Distribuzione geografica
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Continente #
NA - Nord America 17.673
EU - Europa 14.749
AS - Asia 2.961
AF - Africa 99
SA - Sud America 25
Continente sconosciuto - Info sul continente non disponibili 9
OC - Oceania 4
Totale 35.520
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Nazione #
US - Stati Uniti d'America 17.634
RU - Federazione Russa 4.030
PL - Polonia 3.361
IT - Italia 3.301
IE - Irlanda 1.275
SE - Svezia 1.077
SG - Singapore 840
CN - Cina 808
HK - Hong Kong 512
UA - Ucraina 368
DE - Germania 294
FI - Finlandia 284
IN - India 261
GB - Regno Unito 231
FR - Francia 216
JO - Giordania 201
TR - Turchia 149
AT - Austria 104
CI - Costa d'Avorio 63
VN - Vietnam 63
IR - Iran 61
CH - Svizzera 49
BE - Belgio 44
ES - Italia 42
CA - Canada 39
NL - Olanda 30
KR - Corea 26
JP - Giappone 23
SC - Seychelles 14
RO - Romania 10
EU - Europa 9
BR - Brasile 8
DZ - Algeria 8
CL - Cile 6
GR - Grecia 6
AR - Argentina 5
AL - Albania 4
AU - Australia 4
DK - Danimarca 4
EG - Egitto 4
MU - Mauritius 4
NG - Nigeria 4
PK - Pakistan 4
CZ - Repubblica Ceca 3
PT - Portogallo 3
TW - Taiwan 3
BA - Bosnia-Erzegovina 2
CO - Colombia 2
EC - Ecuador 2
EE - Estonia 2
IL - Israele 2
MD - Moldavia 2
MY - Malesia 2
TH - Thailandia 2
VE - Venezuela 2
BG - Bulgaria 1
CM - Camerun 1
GE - Georgia 1
HU - Ungheria 1
LB - Libano 1
LT - Lituania 1
LU - Lussemburgo 1
MO - Macao, regione amministrativa speciale della Cina 1
NO - Norvegia 1
SI - Slovenia 1
SM - San Marino 1
SY - Repubblica araba siriana 1
ZA - Sudafrica 1
Totale 35.520
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Città #
Santa Clara 3.576
Warsaw 3.356
Fairfield 2.136
Dublin 1.275
Chandler 1.031
Ashburn 1.006
Woodbridge 919
Seattle 879
Cambridge 813
Houston 799
Wilmington 732
Florence 720
Singapore 693
Altamura 469
Jacksonville 442
Ann Arbor 434
Lawrence 428
Princeton 359
Beijing 298
Buffalo 241
Hong Kong 240
Mumbai 185
Boston 184
Medford 181
Shanghai 169
Boardman 145
Moscow 129
Prato 121
Milan 113
San Diego 109
Vienna 103
Rome 93
Izmir 86
Falls Church 84
Kent 79
Norwalk 68
Abidjan 63
Dearborn 59
Redwood City 55
Dong Ket 54
New York 53
Brussels 40
Harbin 37
Barcelona 36
Helsinki 34
Yubileyny 34
Hillsboro 33
Duncan 32
London 30
Andover 29
Scandicci 29
Bari 26
Toronto 26
Los Angeles 25
Carpi 24
Turin 24
Phoenix 22
Bologna 20
West Jordan 20
Munich 19
Bern 17
Tong 16
Modena 15
Siena 15
Cranfield 14
Istanbul 14
Empoli 13
Gaggiano 13
Genova 13
Salerno 13
Taranto 13
Guangzhou 12
Nanjing 12
Tehran 12
Xian 12
Dallas 11
Lappeenranta 11
Livorno 11
Saint Petersburg 11
Chennai 10
Pune 10
Tappahannock 10
Comun Nuovo 9
Genoa 9
Laurel 9
Monsummano Terme 9
Padova 9
Perugia 9
Pisa 9
Prad am Stilfser Joch 9
Redmond 9
Seoul 9
Zurich 9
Arezzo 8
Frankfurt Am Main 8
Hachenburg 8
Naples 8
Torino 8
Bergamo 7
Berlin 7
Totale 23.950
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Nome #
Esercitazioni di sistemi energetici 1.082
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 289
Gas Turbines Design and Off-design Performance Analysis with Emissions Evaluation 288
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 265
Turbulent flow-field effects in a hybrid CFD-CRN model for the prediction of NOxand CO emissions in aero-engine combustors 255
Aerothermal Analysis of a Turbine Casing Impingement Cooling System 255
CFD Analysis of NOx Emissions of a Natural Gas Lean Premixed Burner for Heavy Duty Gas Turbine 253
Some Improvements in a Gas Turbine Stator-Rotor Systems Core-Swirl Ratio Correlation 252
A Decoupled CHT Procedure: Application and Validation on a Gas Turbine Vane with Different Cooling Configurations 250
Numerical analysis of the dynamic flame response of a spray flame for aero-engine applications 249
Numerical Identification of a Premixed Flame Transfer Function and Stability Analysis of a Lean Burn Combustor 246
Numerical Simulation of Oil Jet Lubrication for High Speed Gears 243
Experimental Evaluation of the Density Ratio Effects on the Cooling Performance of a Combined Slot/Effusion Combustor Cooling System 238
DENSITY RATIO EFFECTS ON THE COOLING PERFORMANCES OF A COMBUSTOR LINER COOLED BY A COMBINED SLOT/ EFFUSION SYSTEM 238
Experimental Investigation of Innovative Internal Trailing Edge Cooling Configurations with Pentagonal Arrangement and Elliptic Pin Fin 237
A Rotor Blade Cooling Design Method For Heavy Duty Gas Turbine 227
CONJUGATE HEAT TRANSFER ANALYSIS OF AN INTERNALLY COOLED TURBINE BLADES WITH AN OBJECT ORIENTED CFD CODE 226
LES FOR THE EVALUATION OF ACOUSTIC DAMPING OF EFFUSION PLATES 226
Heat Transfer and Pressure Loss Measurements of Matrix Cooling Geometries for Gas Turbine Airfoils 219
"Design issues and performance of a chemically recuperated aeroderivative gas turbine." 211
A Comparison between Two Gas Turbine Solutions to Increase Combined Power Plant Efficiency 211
COMBUSTOR LINER TEMPERATURE PREDICTION: A PRELIMINARY TOOL DEVELOPMENT AND ITS APPLICATION ON EFFUSION COOLING SYSTEMS 210
Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation 210
Design and Off-Design Analysis of a CRGT Cycle Based on the LM2500-STIG Gas Turbine 209
Heat transfer investigation in new cooling schemes of a stationary blade trailing edge 207
NUMERICAL HEAT TRANSFER ANALYSIS OF AN INNOVATIVE GAS TURBINE COMBUSTOR: COUPLED STUDY OF RADIATION AND COOLING IN THE UPPER PART OF THE LINER 203
Experimental investigation of a leading edge cooling system with optimized inclined racetrack holes 201
L'UTILIZZO DEI PROMOTORI DI TURBOLENZA IN GEOMETRIE DI TURBOMACCHINA: VALUTAZIONI GLOBALI DI SCAMBIO TERMICO E PERDITE DI CARICO 199
Film-cooling adiabatic effectiveness measurements on a real high pressure turbine blade 195
Refroidissement des turbines à gaz. Chambre de combustion 193
A Numerical Procedure To Design Internal Cooling Of Gas Turbines Stator Blades 193
HEAT TRANSFERT AND PRESSURE DROP EVALUATION IN THIN WEDGE-SHAPED TRAILING EDGE 185
Film cooling modeling for gas turbine nozzles and blades: Validation and application 181
Modular approach to analysis of chemically recuperated gas turbine cycles 172
INFLUENCE OF AMBIENT CONDITIONS ON AN AERODERIVATIVE GAS TURBINE BASED COGENERATION PLANT. A COMPARISON OF NUMERICAL SIMULATION WITH FIEL PERFORMANCE DATA 165
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON WINDAGE POWER LOSSES IN HIGH SPEED GEARS 163
Assessment of modelling strategies for film cooling 156
ASSESSMENT OF A SET OF NUMERICAL TOOLS FOR THE DESIGN OF AERO ENGINES COMBUSTORS: STUDY OF A TUBULAR TEST RIG 155
A Simplified Approach To Off-Design Performance Evaluation Of Single Shaft Heavy Duty Gas Turbines 152
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 148
A 3d coupled approach for the thermal design of aero-engine combustor liners 148
Numerical Analysis of a Low NOx Partially Premixed Burner for Industrial Gas Turbine Applications 148
Volume Of Fluid (VOF) Analysis of Oil-Jet Lubrication for High-Speed Spur Gears Using an Adaptive Meshing Approach 146
Esercitazioni di Sistemi Energetici 145
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 145
Experimental Investigation on Impingement Array Cooling Systems Through IR Thermography 144
Experimental and Numerical Analysis of Multiple Impingement Jet Arrays for an Active Clearance Control System 140
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 138
Experimental and numerical investigation on windage power losses in high speed gears 138
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 137
Impingement Cooling Experimental Investigation Using Different Heating Elements 136
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 136
HEAVY DUTY GAS TURBINE SIMULATION: GLOBAL PERFORMANCES ESTIMATION AND SECONDARY AIR SYSTEM MODIFICATIONS 135
A Rotor Blade Cooling improvement for Heavy Duty Gas Turbine Using Steam and Mixed Steam/Air Cooling 132
Heat Transfer Measurements in a Leading Edge Geometry With Racetrack Holes and Film Cooling Extraction 132
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 132
Effect of rotation on a gas turbine blade internal cooling system: Experimental investigation 132
Modeling and experimental study of power losses in a rolling bearing 130
ASSESSMENT OF NUMERICAL TOOLS FOR THE EVALUATION OF THE ACOUSTICIMPEDANCE OF MULTI-PERFORATED PLATES. 128
Assessment of Flame Transfer Function Formulations for the Thermoacoustic Analysis of Lean Burn Aero-engine Combustors 128
Assessment of Aero-Thermal Design Methodology for Effusion Cooled Lean Burn Annular Combustors 128
"DESIGN CRITERIA FOR RIBBED CHANNELS: EXPERIMENTAL INVESTIGATION AND THEORETICAL ANALYSIS", 127
Heat transfer investigation on an internal cooling system of a gas turbine leading edge model 127
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 127
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 126
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 126
Numerical and Experimental Investigation of Turning Flow Effects on Innovative Pin Fin Arrangements for Trailing Edge Cooling Configurations 125
Heat transfer in internal channel of a blade: effects of rotation in a trailing edge cooling system 125
Experimental Investigation of Swirl and Flow Structure Inside a Rotor-Stator Cavity 125
A semi analytical Approach to emissions prediction in gas Turbine Combustors 124
Film Cooling Modelling for Gas Turbine Nozzles and Blades: Validation and Application 123
EVALUATION AND COMPARISON OF DIFFERENT BLADE COOLING SOLUTIONS TO IMPROVE COOLING EFFICIENCY AND GAS TURBINE PERFORMANCES 122
LOCAL SOURCE BASED CFD MODELING OF EFFUSION COOLING HOLES: VALIDATION AND APPLICATION TO AN ACTUAL COMBUSTOR TEST CASE 122
Numerical study of aerodynamic losses of effusion cooling holes in aero-engine combustor liners 122
Numerical Study of Aerodynamic Losses of Effusion Cooling Holes in Aero-Engine Combustor Liners 122
The 701fd gas turbine design process: upgrade and innovations of blade cooling system 121
Effusion cooling system optimization for modern lean burn combustor 121
Heat transfer and pressure drop measurements on rotating matrix cooling geometries for airfoil trailing edges 120
CFD simulations of a meshing gear pair 119
BLADE COOLING IMPROVEMENT FOR HEAVY DUTY GAS TURBINE: THE AIR COOLANT TEMPERATURE REDUCTION AND THE INTRODUCTION OF STEAM AND MIXED/AIR COOLING 119
Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 119
Effect of slot injection and effusion array on the liner heat transfer coefficient of a scaled lean burn combustor with representative swirling flow 119
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 118
Design improvement survey for NOx emissions reduction of a heavy-duty gas turbine partially premixed fuel nozzle operating with natural gas: Numerical assessment 118
Large-Eddy Simulation of a turbulent spray flame using the flamelet generated manifold approach 118
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 118
Blade cooling improvement for heavy duty gas turbine: the air coolant temperature reduction and the introduction of steam and mixed steam/air cooling 117
Analysis of flat plate honeycomb seals aerodynamic losses: effects of clearance 117
EXPERIMENTAL INVESTIGATION ON EFFUSION LINER GEOMETRIES FOR AERO-ENGINE COMBUSTORS: EVALUATION OF GLOBAL ACOUSTIC PARAMETERS. 117
Transient thermal modelling of whole gt engine with a partly coupled fem-fluid network approach 117
Numerical Investigation On the Aerodynamic Performance of a Low-Pressure Steam Turbine Exhaust Hood Using Doe Analysis 117
Numerical Simulation of Dam-Break Problem Using an Adaptive Meshing Approach 116
Cooling system optimization of combustor liners 116
Numerical investigations of pollutant emissions from novel heavy duty gas turbine burners operated with natural gas 116
INVESTIGATION OF CIRCULAR AND SHAPED EFFUSION COOLING ARRAYS FOR COMBUSTOR LINER APPLICATION - PART 2: NUMERICAL ANALYSIS 116
Numerical Analysis of Effusion Plates for Combustor Liners Cooling with Varying Density Ratio 116
Experimental Survey on Heat Transfer In A Trailing Edge Cooling System: Effects of Rotation In Internal Cooling Ducts 116
Flat Plate Honeycomb Seals Friction Factor Analysis 116
Multi-Coupled Numerical Analysis of Advanced Lean Burn Injection Systems 116
Turbine stator well CFD studies: Effects of coolant supply geometry on cavity sealing performance 115
Totale 17.016
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Categoria #
all - tutte 96.629
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 96.629
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20203.983 0 0 0 0 558 619 648 670 537 381 459 111
2020/20213.416 282 283 195 430 256 314 187 319 342 393 184 231
2021/20222.683 114 220 165 109 135 193 108 199 106 89 600 645
2022/20235.946 573 1.077 301 373 423 1.073 807 293 662 65 209 90
2023/20242.514 123 310 380 141 157 273 168 380 87 135 239 121
2024/20259.885 621 1.591 1.077 2.326 4.270 0 0 0 0 0 0 0
Totale 35.940