FACCHINI, BRUNO
 Distribuzione geografica
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Continente #
NA - Nord America 27.472
EU - Europa 20.670
AS - Asia 12.050
SA - Sud America 1.432
Continente sconosciuto - Info sul continente non disponibili 501
AF - Africa 315
OC - Oceania 190
Totale 62.630
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Nazione #
US - Stati Uniti d'America 27.048
IT - Italia 6.355
RU - Federazione Russa 5.453
PL - Polonia 3.401
SG - Singapore 3.229
CN - Cina 3.001
HK - Hong Kong 1.940
IE - Irlanda 1.284
VN - Vietnam 1.208
BR - Brasile 1.125
SE - Svezia 1.117
KR - Corea 922
FR - Francia 642
DE - Germania 555
FI - Finlandia 486
IN - India 430
UA - Ucraina 402
GB - Regno Unito 394
CA - Canada 286
BD - Bangladesh 241
JO - Giordania 211
TR - Turchia 199
AU - Australia 187
JP - Giappone 159
NL - Olanda 153
AR - Argentina 130
AT - Austria 115
ID - Indonesia 86
ES - Italia 85
IQ - Iraq 85
IR - Iran 73
CI - Costa d'Avorio 66
MX - Messico 66
BE - Belgio 61
CH - Svizzera 55
EC - Ecuador 52
ZA - Sudafrica 45
NG - Nigeria 41
PK - Pakistan 33
CO - Colombia 29
VE - Venezuela 29
MA - Marocco 28
TN - Tunisia 27
CL - Cile 26
DZ - Algeria 26
UZ - Uzbekistan 24
PH - Filippine 23
AZ - Azerbaigian 21
KE - Kenya 20
SA - Arabia Saudita 19
AE - Emirati Arabi Uniti 18
RO - Romania 17
SC - Seychelles 17
EG - Egitto 15
MY - Malesia 15
NP - Nepal 15
TH - Thailandia 15
JM - Giamaica 14
GR - Grecia 12
IL - Israele 12
PY - Paraguay 12
UY - Uruguay 12
AL - Albania 11
LT - Lituania 11
PE - Perù 11
DO - Repubblica Dominicana 10
PT - Portogallo 10
BJ - Benin 9
CR - Costa Rica 9
EU - Europa 9
TT - Trinidad e Tobago 9
TW - Taiwan 8
SV - El Salvador 7
BA - Bosnia-Erzegovina 6
BH - Bahrain 6
KZ - Kazakistan 6
LB - Libano 6
OM - Oman 6
AM - Armenia 5
EE - Estonia 5
NO - Norvegia 5
BO - Bolivia 4
CZ - Repubblica Ceca 4
DK - Danimarca 4
GE - Georgia 4
GT - Guatemala 4
HN - Honduras 4
HU - Ungheria 4
KG - Kirghizistan 4
KH - Cambogia 4
MD - Moldavia 4
MU - Mauritius 4
PR - Porto Rico 4
QA - Qatar 4
RS - Serbia 4
BG - Bulgaria 3
ET - Etiopia 3
LA - Repubblica Popolare Democratica del Laos 3
NI - Nicaragua 3
PA - Panama 3
Totale 62.087
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Città #
Santa Clara 6.653
Warsaw 3.381
Ashburn 2.649
Singapore 2.454
Fairfield 2.137
Hong Kong 1.635
San Jose 1.420
Dublin 1.284
Chandler 1.031
Florence 1.007
Woodbridge 923
Seattle 892
Milan 890
Seoul 886
Houston 828
Cambridge 813
Wilmington 739
Beijing 698
Hefei 503
Altamura 470
Jacksonville 449
Ann Arbor 436
Lawrence 428
Council Bluffs 426
Buffalo 418
Rome 393
Ho Chi Minh City 385
Princeton 359
Lauterbourg 295
Los Angeles 281
Hanoi 270
The Dalles 248
Boston 200
Mumbai 200
Shanghai 199
Moscow 196
Dallas 188
Medford 183
Melbourne 183
New York 182
Helsinki 173
Boardman 160
Prato 137
Munich 128
Kent 123
Tokyo 121
Turin 116
San Diego 112
Vienna 104
São Paulo 94
Naples 88
Bologna 86
Izmir 86
Falls Church 85
Clifton 82
Chicago 78
Figino 74
Frankfurt am Main 73
London 72
Norwalk 69
Orem 69
Abidjan 66
Redondo Beach 64
Toronto 64
Dearborn 59
Bari 58
Turku 58
Da Nang 56
Redwood City 55
Dong Ket 54
Jakarta 51
Haiphong 50
Brussels 48
Phoenix 48
Montreal 47
Guangzhou 43
Harbin 41
Bengaluru 40
Barcelona 39
Abuja 38
Miano 38
Hillsboro 37
Paris 37
Modena 36
Verona 36
Genoa 35
Rio de Janeiro 34
Yubileyny 34
Brooklyn 33
Chennai 32
Duncan 32
San Francisco 32
Istanbul 31
Scandicci 31
Tianjin 31
Andover 29
Johannesburg 29
Palermo 29
Shenzhen 29
Atlanta 28
Totale 40.974
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Nome #
Esercitazioni di sistemi energetici 1.418
Gas Turbines Design and Off-design Performance Analysis with Emissions Evaluation 395
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 364
A Rotor Blade Cooling Design Method For Heavy Duty Gas Turbine 359
Film-cooling adiabatic effectiveness measurements on a real high pressure turbine blade 353
Turbulent flow-field effects in a hybrid CFD-CRN model for the prediction of NOxand CO emissions in aero-engine combustors 346
DENSITY RATIO EFFECTS ON THE COOLING PERFORMANCES OF A COMBUSTOR LINER COOLED BY A COMBINED SLOT/ EFFUSION SYSTEM 344
Esercitazioni di Sistemi Energetici 329
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 325
A Decoupled CHT Procedure: Application and Validation on a Gas Turbine Vane with Different Cooling Configurations 323
Numerical Identification of a Premixed Flame Transfer Function and Stability Analysis of a Lean Burn Combustor 320
Experimental Evaluation of the Density Ratio Effects on the Cooling Performance of a Combined Slot/Effusion Combustor Cooling System 319
CFD Analysis of NOx Emissions of a Natural Gas Lean Premixed Burner for Heavy Duty Gas Turbine 319
Some Improvements in a Gas Turbine Stator-Rotor Systems Core-Swirl Ratio Correlation 314
"Design issues and performance of a chemically recuperated aeroderivative gas turbine." 312
COMBUSTOR LINER TEMPERATURE PREDICTION: A PRELIMINARY TOOL DEVELOPMENT AND ITS APPLICATION ON EFFUSION COOLING SYSTEMS 312
Numerical Simulation of Oil Jet Lubrication for High Speed Gears 311
Experimental Investigation of Innovative Internal Trailing Edge Cooling Configurations with Pentagonal Arrangement and Elliptic Pin Fin 310
LES FOR THE EVALUATION OF ACOUSTIC DAMPING OF EFFUSION PLATES 309
A Numerical Procedure To Design Internal Cooling Of Gas Turbines Stator Blades 307
Numerical analysis of the dynamic flame response of a spray flame for aero-engine applications 305
Aerothermal Analysis of a Turbine Casing Impingement Cooling System 300
CONJUGATE HEAT TRANSFER ANALYSIS OF AN INTERNALLY COOLED TURBINE BLADES WITH AN OBJECT ORIENTED CFD CODE 298
Heat Transfer and Pressure Loss Measurements of Matrix Cooling Geometries for Gas Turbine Airfoils 293
A Comparison between Two Gas Turbine Solutions to Increase Combined Power Plant Efficiency 292
NUMERICAL HEAT TRANSFER ANALYSIS OF AN INNOVATIVE GAS TURBINE COMBUSTOR: COUPLED STUDY OF RADIATION AND COOLING IN THE UPPER PART OF THE LINER 279
Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation 277
Design and Off-Design Analysis of a CRGT Cycle Based on the LM2500-STIG Gas Turbine 275
Experimental investigation of a leading edge cooling system with optimized inclined racetrack holes 275
Film cooling modeling for gas turbine nozzles and blades: Validation and application 272
Heat transfer investigation in new cooling schemes of a stationary blade trailing edge 266
L'UTILIZZO DEI PROMOTORI DI TURBOLENZA IN GEOMETRIE DI TURBOMACCHINA: VALUTAZIONI GLOBALI DI SCAMBIO TERMICO E PERDITE DI CARICO 256
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON WINDAGE POWER LOSSES IN HIGH SPEED GEARS 254
HEAT TRANSFERT AND PRESSURE DROP EVALUATION IN THIN WEDGE-SHAPED TRAILING EDGE 251
Heat Transfer Measurements in a Leading Edge Geometry With Racetrack Holes and Film Cooling Extraction 247
Experimental and numerical investigation on windage power losses in high speed gears 245
INFLUENCE OF AMBIENT CONDITIONS ON AN AERODERIVATIVE GAS TURBINE BASED COGENERATION PLANT. A COMPARISON OF NUMERICAL SIMULATION WITH FIEL PERFORMANCE DATA 241
Assessment of modelling strategies for film cooling 240
Improving emission and blow-out characteristics of novel natural gas low NOx burners for heavy duty gas turbine 240
A Rotor Blade Cooling improvement for Heavy Duty Gas Turbine Using Steam and Mixed Steam/Air Cooling 234
Experimental Investigation on Impingement Array Cooling Systems Through IR Thermography 229
Refroidissement des turbines à gaz. Chambre de combustion 228
Correlative Analysis Of Effusion Cooling Systems 227
Numerical Simulation of Dam-Break Problem Using an Adaptive Meshing Approach 227
A 3d coupled approach for the thermal design of aero-engine combustor liners 227
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 227
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 226
A Simplified Approach To Off-Design Performance Evaluation Of Single Shaft Heavy Duty Gas Turbines 225
Modular approach to analysis of chemically recuperated gas turbine cycles 223
Volume Of Fluid (VOF) Analysis of Oil-Jet Lubrication for High-Speed Spur Gears Using an Adaptive Meshing Approach 221
Investigation on low-pressure steam turbine exhaust hood modelling through computational fluid dynamic simulations 220
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 219
Numerical Investigation On the Aerodynamic Performance of a Low-Pressure Steam Turbine Exhaust Hood Using Doe Analysis 219
ASSESSMENT OF A SET OF NUMERICAL TOOLS FOR THE DESIGN OF AERO ENGINES COMBUSTORS: STUDY OF A TUBULAR TEST RIG 218
Heat transfer investigation on an internal cooling system of a gas turbine leading edge model 218
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 216
Effect of rotation on a gas turbine blade internal cooling system: Experimental investigation 214
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 214
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 213
Effusion cooling system optimization for modern lean burn combustor 213
Transient thermal modelling of whole gt engine with a partly coupled fem-fluid network approach 213
CFD simulations of a meshing gear pair 212
BLADE COOLING IMPROVEMENT FOR HEAVY DUTY GAS TURBINE: THE AIR COOLANT TEMPERATURE REDUCTION AND THE INTRODUCTION OF STEAM AND MIXED/AIR COOLING 212
HEAVY DUTY GAS TURBINE SIMULATION: GLOBAL PERFORMANCES ESTIMATION AND SECONDARY AIR SYSTEM MODIFICATIONS 211
Adiabatic effectiveness on high-pressure turbine nozzle guide vanes under realistic swirling conditions 210
Numerical Analysis of a Low NOx Partially Premixed Burner for Industrial Gas Turbine Applications 210
Experimental Investigation of Swirl and Flow Structure Inside a Rotor-Stator Cavity 210
Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 209
“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. . 208
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 208
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 207
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 207
"DESIGN CRITERIA FOR RIBBED CHANNELS: EXPERIMENTAL INVESTIGATION AND THEORETICAL ANALYSIS", 206
Heat transfer in internal channel of a blade: effects of rotation in a trailing edge cooling system 206
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 206
Modeling and experimental study of power losses in a rolling bearing 204
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 203
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 203
Experimental and Theoretical Investigation of Thermal Effectiveness in Multiperforated Plates for Combustor Liner Effusion Cooling 203
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 203
Cooling system optimization of combustor liners 202
Numerical study of aerodynamic losses of effusion cooling holes in aero-engine combustor liners 201
ASSESSMENT OF NUMERICAL TOOLS FOR THE EVALUATION OF THE ACOUSTICIMPEDANCE OF MULTI-PERFORATED PLATES. 200
Impingement Cooling Experimental Investigation Using Different Heating Elements 200
Experimental and Numerical Analysis of Multiple Impingement Jet Arrays for an Active Clearance Control System 200
Analysis of gas turbine rotating cavities by a one-dimensional model: Definition of a new discs fiction coefficients correlations set 200
Commissioning of a Newly Designed Experimental Facility for Hot Gas Ingestion Investigation 199
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 199
A semi analytical Approach to emissions prediction in gas Turbine Combustors 198
Assessment of turbulent models for a low-pressure turbine guide vane heat transfer with high free-stream turbulence 198
Conjugate Heat Transfer Calculations on GT Rotor Blade for Industrial Applications. Part I: Equivalent Internal Fluid Network Setup and Procedure Description 197
Flat Plate Honeycomb Seals Friction Factor Analysis 197
Large-Eddy Simulation of a turbulent spray flame using the flamelet generated manifold approach 195
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 194
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 194
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 194
Conjugate heat transfer methodology for thermal design and verification of gas turbine cooled components 194
EVALUATION AND COMPARISON OF DIFFERENT BLADE COOLING SOLUTIONS TO IMPROVE COOLING EFFICIENCY AND GAS TURBINE PERFORMANCES 192
Experimental validation of an innovative metallic tile holder system for a ceramic combustor liner 192
Analysis of flat plate honeycomb seals aerodynamic losses: effects of clearance 192
Totale 25.542
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Categoria #
all - tutte 167.692
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 167.692
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20222.569 0 220 165 109 135 193 108 199 106 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
2025/202618.480 1.434 2.469 1.447 1.339 1.987 813 2.013 975 1.708 1.150 591 2.554
2026/20271.289 751 538 0 0 0 0 0 0 0 0 0 0
Totale 62.630