FACCHINI, BRUNO
 Distribuzione geografica
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Continente #
NA - Nord America 23.171
EU - Europa 17.574
AS - Asia 9.098
SA - Sud America 1.279
AF - Africa 221
OC - Oceania 187
Continente sconosciuto - Info sul continente non disponibili 11
Totale 51.541
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Nazione #
US - Stati Uniti d'America 22.997
RU - Federazione Russa 5.436
IT - Italia 3.861
PL - Polonia 3.395
CN - Cina 2.337
SG - Singapore 2.285
HK - Hong Kong 1.873
IE - Irlanda 1.280
SE - Svezia 1.101
BR - Brasile 1.038
KR - Corea 907
VN - Vietnam 513
DE - Germania 498
FI - Finlandia 443
UA - Ucraina 394
IN - India 362
GB - Regno Unito 344
FR - Francia 320
JO - Giordania 204
AU - Australia 185
TR - Turchia 176
NL - Olanda 126
AT - Austria 111
AR - Argentina 109
CA - Canada 105
ID - Indonesia 80
ES - Italia 74
IR - Iran 73
CI - Costa d'Avorio 64
JP - Giappone 64
BE - Belgio 54
CH - Svizzera 52
BD - Bangladesh 46
IQ - Iraq 45
EC - Ecuador 44
MX - Messico 42
ZA - Sudafrica 41
MA - Marocco 21
VE - Venezuela 20
CL - Cile 19
CO - Colombia 19
DZ - Algeria 18
TN - Tunisia 16
PK - Pakistan 14
SC - Seychelles 14
AE - Emirati Arabi Uniti 13
KE - Kenya 12
RO - Romania 12
UY - Uruguay 12
UZ - Uzbekistan 11
AL - Albania 10
IL - Israele 10
LT - Lituania 10
BJ - Benin 9
EG - Egitto 9
EU - Europa 9
GR - Grecia 9
NP - Nepal 9
AZ - Azerbaigian 8
DO - Repubblica Dominicana 8
PT - Portogallo 8
PY - Paraguay 8
SA - Arabia Saudita 8
MY - Malesia 7
PE - Perù 7
KZ - Kazakistan 6
JM - Giamaica 5
CZ - Repubblica Ceca 4
DK - Danimarca 4
EE - Estonia 4
LB - Libano 4
MU - Mauritius 4
NG - Nigeria 4
PH - Filippine 4
TH - Thailandia 4
TW - Taiwan 4
AM - Armenia 3
BH - Bahrain 3
HU - Ungheria 3
MD - Moldavia 3
OM - Oman 3
PA - Panama 3
PS - Palestinian Territory 3
BA - Bosnia-Erzegovina 2
BG - Bulgaria 2
BW - Botswana 2
BY - Bielorussia 2
CG - Congo 2
CR - Costa Rica 2
GE - Georgia 2
GT - Guatemala 2
HN - Honduras 2
KG - Kirghizistan 2
KH - Cambogia 2
LA - Repubblica Popolare Democratica del Laos 2
LU - Lussemburgo 2
LV - Lettonia 2
NO - Norvegia 2
QA - Qatar 2
RS - Serbia 2
Totale 51.511
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Città #
Santa Clara 6.562
Warsaw 3.379
Fairfield 2.136
Ashburn 1.641
Singapore 1.590
Hong Kong 1.583
Dublin 1.280
Chandler 1.031
Woodbridge 919
Seoul 886
Seattle 881
Florence 869
Houston 814
Cambridge 813
Wilmington 733
Beijing 646
Hefei 503
Altamura 469
Jacksonville 446
Ann Arbor 434
Lawrence 428
Buffalo 399
Princeton 359
Los Angeles 220
Boston 196
Mumbai 196
Moscow 195
Ho Chi Minh City 186
Melbourne 183
Medford 181
Shanghai 178
Dallas 155
Milan 152
Boardman 145
Prato 134
Helsinki 132
Munich 128
Kent 123
Rome 123
New York 117
San Diego 110
Vienna 104
Hanoi 88
Izmir 86
Falls Church 84
São Paulo 84
Clifton 82
The Dalles 76
Norwalk 68
Chicago 66
Abidjan 64
Redondo Beach 64
London 62
Dearborn 59
Turku 58
Redwood City 55
Dong Ket 54
Frankfurt am Main 52
Jakarta 49
Brussels 48
Tokyo 45
Turin 42
Harbin 40
Barcelona 39
Bengaluru 39
Bari 38
Council Bluffs 38
Phoenix 38
Toronto 36
Yubileyny 34
Hillsboro 33
Rio de Janeiro 33
Duncan 32
Scandicci 31
Andover 29
Brooklyn 28
Orem 28
Paris 28
Bologna 27
Johannesburg 27
Montreal 27
Belo Horizonte 24
Carpi 24
Modena 23
Stockholm 23
Chennai 22
Falkenstein 22
Istanbul 22
West Jordan 22
Salt Lake City 21
Haiphong 20
San Jose 20
Tianjin 20
Salvador 19
Ottawa 18
Amsterdam 17
Bern 17
Brasília 17
Denver 17
Guangzhou 17
Totale 34.055
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Nome #
Esercitazioni di sistemi energetici 1.303
Gas Turbines Design and Off-design Performance Analysis with Emissions Evaluation 352
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 336
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 305
A Rotor Blade Cooling Design Method For Heavy Duty Gas Turbine 299
Turbulent flow-field effects in a hybrid CFD-CRN model for the prediction of NOxand CO emissions in aero-engine combustors 298
A Decoupled CHT Procedure: Application and Validation on a Gas Turbine Vane with Different Cooling Configurations 295
Numerical Simulation of Oil Jet Lubrication for High Speed Gears 292
Some Improvements in a Gas Turbine Stator-Rotor Systems Core-Swirl Ratio Correlation 290
CFD Analysis of NOx Emissions of a Natural Gas Lean Premixed Burner for Heavy Duty Gas Turbine 289
DENSITY RATIO EFFECTS ON THE COOLING PERFORMANCES OF A COMBUSTOR LINER COOLED BY A COMBINED SLOT/ EFFUSION SYSTEM 283
Aerothermal Analysis of a Turbine Casing Impingement Cooling System 283
Numerical analysis of the dynamic flame response of a spray flame for aero-engine applications 282
"Design issues and performance of a chemically recuperated aeroderivative gas turbine." 280
Numerical Identification of a Premixed Flame Transfer Function and Stability Analysis of a Lean Burn Combustor 280
Experimental Evaluation of the Density Ratio Effects on the Cooling Performance of a Combined Slot/Effusion Combustor Cooling System 277
LES FOR THE EVALUATION OF ACOUSTIC DAMPING OF EFFUSION PLATES 276
Experimental Investigation of Innovative Internal Trailing Edge Cooling Configurations with Pentagonal Arrangement and Elliptic Pin Fin 275
Film-cooling adiabatic effectiveness measurements on a real high pressure turbine blade 270
COMBUSTOR LINER TEMPERATURE PREDICTION: A PRELIMINARY TOOL DEVELOPMENT AND ITS APPLICATION ON EFFUSION COOLING SYSTEMS 264
Heat Transfer and Pressure Loss Measurements of Matrix Cooling Geometries for Gas Turbine Airfoils 263
CONJUGATE HEAT TRANSFER ANALYSIS OF AN INTERNALLY COOLED TURBINE BLADES WITH AN OBJECT ORIENTED CFD CODE 262
Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation 255
A Comparison between Two Gas Turbine Solutions to Increase Combined Power Plant Efficiency 253
A Numerical Procedure To Design Internal Cooling Of Gas Turbines Stator Blades 253
Experimental investigation of a leading edge cooling system with optimized inclined racetrack holes 243
L'UTILIZZO DEI PROMOTORI DI TURBOLENZA IN GEOMETRIE DI TURBOMACCHINA: VALUTAZIONI GLOBALI DI SCAMBIO TERMICO E PERDITE DI CARICO 241
NUMERICAL HEAT TRANSFER ANALYSIS OF AN INNOVATIVE GAS TURBINE COMBUSTOR: COUPLED STUDY OF RADIATION AND COOLING IN THE UPPER PART OF THE LINER 241
Design and Off-Design Analysis of a CRGT Cycle Based on the LM2500-STIG Gas Turbine 241
Film cooling modeling for gas turbine nozzles and blades: Validation and application 240
Heat transfer investigation in new cooling schemes of a stationary blade trailing edge 237
Esercitazioni di Sistemi Energetici 237
HEAT TRANSFERT AND PRESSURE DROP EVALUATION IN THIN WEDGE-SHAPED TRAILING EDGE 224
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON WINDAGE POWER LOSSES IN HIGH SPEED GEARS 217
Heat Transfer Measurements in a Leading Edge Geometry With Racetrack Holes and Film Cooling Extraction 216
Refroidissement des turbines à gaz. Chambre de combustion 209
Correlative Analysis Of Effusion Cooling Systems 205
Assessment of modelling strategies for film cooling 203
Experimental Investigation on Impingement Array Cooling Systems Through IR Thermography 203
A Simplified Approach To Off-Design Performance Evaluation Of Single Shaft Heavy Duty Gas Turbines 200
INFLUENCE OF AMBIENT CONDITIONS ON AN AERODERIVATIVE GAS TURBINE BASED COGENERATION PLANT. A COMPARISON OF NUMERICAL SIMULATION WITH FIEL PERFORMANCE DATA 199
Modular approach to analysis of chemically recuperated gas turbine cycles 198
Volume Of Fluid (VOF) Analysis of Oil-Jet Lubrication for High-Speed Spur Gears Using an Adaptive Meshing Approach 198
A Rotor Blade Cooling improvement for Heavy Duty Gas Turbine Using Steam and Mixed Steam/Air Cooling 195
ASSESSMENT OF A SET OF NUMERICAL TOOLS FOR THE DESIGN OF AERO ENGINES COMBUSTORS: STUDY OF A TUBULAR TEST RIG 194
Experimental and numerical investigation on windage power losses in high speed gears 194
A 3d coupled approach for the thermal design of aero-engine combustor liners 194
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 189
Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 189
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 189
Transient thermal modelling of whole gt engine with a partly coupled fem-fluid network approach 186
Effusion cooling system optimization for modern lean burn combustor 184
Investigation on low-pressure steam turbine exhaust hood modelling through computational fluid dynamic simulations 183
Heat transfer investigation on an internal cooling system of a gas turbine leading edge model 183
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 182
Numerical Simulation of Dam-Break Problem Using an Adaptive Meshing Approach 182
Adiabatic effectiveness on high-pressure turbine nozzle guide vanes under realistic swirling conditions 181
Numerical Analysis of a Low NOx Partially Premixed Burner for Industrial Gas Turbine Applications 180
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 180
"DESIGN CRITERIA FOR RIBBED CHANNELS: EXPERIMENTAL INVESTIGATION AND THEORETICAL ANALYSIS", 179
CFD simulations of a meshing gear pair 178
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 178
Experimental and Numerical Analysis of Multiple Impingement Jet Arrays for an Active Clearance Control System 178
Analysis of gas turbine rotating cavities by a one-dimensional model: Definition of a new discs fiction coefficients correlations set 178
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 177
Experimental Investigation of Swirl and Flow Structure Inside a Rotor-Stator Cavity 177
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 177
Impingement Cooling Experimental Investigation Using Different Heating Elements 176
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 176
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 176
Cooling system optimization of combustor liners 176
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 175
HEAVY DUTY GAS TURBINE SIMULATION: GLOBAL PERFORMANCES ESTIMATION AND SECONDARY AIR SYSTEM MODIFICATIONS 175
Modeling and experimental study of power losses in a rolling bearing 174
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 174
Effect of rotation on a gas turbine blade internal cooling system: Experimental investigation 174
Assessment of Flame Transfer Function Formulations for the Thermoacoustic Analysis of Lean Burn Aero-engine Combustors 173
ASSESSMENT OF NUMERICAL TOOLS FOR THE EVALUATION OF THE ACOUSTICIMPEDANCE OF MULTI-PERFORATED PLATES. 172
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 172
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 171
Numerical Investigation On the Aerodynamic Performance of a Low-Pressure Steam Turbine Exhaust Hood Using Doe Analysis 171
A semi analytical Approach to emissions prediction in gas Turbine Combustors 168
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 168
EVALUATION AND COMPARISON OF DIFFERENT BLADE COOLING SOLUTIONS TO IMPROVE COOLING EFFICIENCY AND GAS TURBINE PERFORMANCES 167
Heat transfer in internal channel of a blade: effects of rotation in a trailing edge cooling system 167
Numerical study of aerodynamic losses of effusion cooling holes in aero-engine combustor liners 167
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 166
BLADE COOLING IMPROVEMENT FOR HEAVY DUTY GAS TURBINE: THE AIR COOLANT TEMPERATURE REDUCTION AND THE INTRODUCTION OF STEAM AND MIXED/AIR COOLING 166
“A 1-D Model Of The “Coldbridge” Cooling Technique Applied To Gas Turbine Blades” International Journal of Heat and Technology Vol. 22 n. 1 June 2004, pag. 113, ETS Edition. . 165
Assessment of turbulent models for a low-pressure turbine guide vane heat transfer with high free-stream turbulence 165
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 164
Assessment of Aero-Thermal Design Methodology for Effusion Cooled Lean Burn Annular Combustors 164
Film Cooling Modelling for Gas Turbine Nozzles and Blades: Validation and Application 164
Improving emission and blow-out characteristics of novel natural gas low NOx burners for heavy duty gas turbine 164
Numerical investigation on windage losses of high-speed gears in enclosed configuration 164
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 163
Experimental validation of an innovative metallic tile holder system for a ceramic combustor liner 163
Numerical Study of Aerodynamic Losses of Effusion Cooling Holes in Aero-Engine Combustor Liners 162
LOCAL SOURCE BASED CFD MODELING OF EFFUSION COOLING HOLES: VALIDATION AND APPLICATION TO AN ACTUAL COMBUSTOR TEST CASE 161
Numerical investigations of pollutant emissions from novel heavy duty gas turbine burners operated with natural gas 161
Totale 22.038
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Categoria #
all - tutte 138.029
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 138.029
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.970 0 0 0 0 0 314 187 319 342 393 184 231
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
2024/202516.806 621 1.591 1.077 2.326 5.108 2.796 224 1.072 567 315 537 572
2025/20269.119 1.434 2.469 1.447 1.339 1.987 443 0 0 0 0 0 0
Totale 51.980