FACCHINI, BRUNO
 Distribuzione geografica
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Continente #
NA - Nord America 26.474
EU - Europa 20.469
AS - Asia 11.955
SA - Sud America 1.422
AF - Africa 312
OC - Oceania 189
Continente sconosciuto - Info sul continente non disponibili 11
Totale 60.832
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Nazione #
US - Stati Uniti d'America 26.214
IT - Italia 6.193
RU - Federazione Russa 5.453
PL - Polonia 3.399
SG - Singapore 3.208
CN - Cina 2.979
HK - Hong Kong 1.929
IE - Irlanda 1.283
VN - Vietnam 1.207
BR - Brasile 1.122
SE - Svezia 1.103
KR - Corea 919
FR - Francia 639
DE - Germania 554
FI - Finlandia 486
IN - India 426
UA - Ucraina 400
GB - Regno Unito 391
BD - Bangladesh 228
JO - Giordania 210
TR - Turchia 193
AU - Australia 186
CA - Canada 154
JP - Giappone 150
NL - Olanda 147
AR - Argentina 129
AT - Austria 115
ID - Indonesia 86
IQ - Iraq 85
ES - Italia 83
IR - Iran 73
CI - Costa d'Avorio 66
MX - Messico 63
BE - Belgio 61
CH - Svizzera 54
EC - Ecuador 51
ZA - Sudafrica 45
NG - Nigeria 41
PK - Pakistan 33
MA - Marocco 28
CO - Colombia 27
TN - Tunisia 27
VE - Venezuela 27
DZ - Algeria 26
CL - Cile 25
UZ - Uzbekistan 24
PH - Filippine 23
AZ - Azerbaigian 21
KE - Kenya 20
SA - Arabia Saudita 19
AE - Emirati Arabi Uniti 17
RO - Romania 16
EG - Egitto 15
NP - Nepal 15
TH - Thailandia 15
MY - Malesia 14
SC - Seychelles 14
GR - Grecia 12
PY - Paraguay 12
UY - Uruguay 12
IL - Israele 11
PE - Perù 11
AL - Albania 10
DO - Repubblica Dominicana 10
LT - Lituania 10
PT - Portogallo 10
BJ - Benin 9
EU - Europa 9
JM - Giamaica 9
TW - Taiwan 8
BA - Bosnia-Erzegovina 6
BH - Bahrain 6
KZ - Kazakistan 6
LB - Libano 6
OM - Oman 6
EE - Estonia 5
NO - Norvegia 5
AM - Armenia 4
BO - Bolivia 4
CZ - Repubblica Ceca 4
DK - Danimarca 4
GE - Georgia 4
HU - Ungheria 4
KG - Kirghizistan 4
KH - Cambogia 4
MD - Moldavia 4
MU - Mauritius 4
QA - Qatar 4
RS - Serbia 4
TT - Trinidad e Tobago 4
BG - Bulgaria 3
CR - Costa Rica 3
ET - Etiopia 3
LA - Repubblica Popolare Democratica del Laos 3
PA - Panama 3
PR - Porto Rico 3
PS - Palestinian Territory 3
SN - Senegal 3
SV - El Salvador 3
SY - Repubblica araba siriana 3
Totale 60.786
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Città #
Santa Clara 6.614
Warsaw 3.380
Ashburn 2.607
Singapore 2.447
Fairfield 2.136
Hong Kong 1.625
San Jose 1.375
Dublin 1.283
Chandler 1.031
Florence 992
Woodbridge 920
Seoul 886
Seattle 884
Milan 862
Houston 822
Cambridge 813
Wilmington 735
Beijing 690
Hefei 503
Altamura 470
Jacksonville 448
Ann Arbor 436
Lawrence 428
Buffalo 414
Ho Chi Minh City 385
Rome 377
Princeton 359
Lauterbourg 295
Hanoi 269
Los Angeles 263
The Dalles 248
Boston 199
Mumbai 199
Moscow 196
Shanghai 192
Medford 183
Melbourne 183
Dallas 175
Helsinki 173
New York 170
Boardman 160
Prato 137
Munich 128
Kent 123
Tokyo 121
Turin 113
San Diego 110
Vienna 104
São Paulo 93
Council Bluffs 89
Izmir 86
Bologna 85
Falls Church 84
Clifton 82
Naples 78
Chicago 73
Frankfurt am Main 73
Figino 72
Norwalk 68
London 67
Orem 67
Abidjan 66
Redondo Beach 64
Dearborn 59
Turku 58
Bari 56
Da Nang 56
Redwood City 55
Dong Ket 54
Jakarta 51
Haiphong 50
Brussels 48
Toronto 48
Phoenix 45
Guangzhou 43
Harbin 41
Bengaluru 40
Barcelona 39
Abuja 38
Miano 38
Hillsboro 37
Paris 37
Modena 36
Verona 36
Montreal 34
Rio de Janeiro 34
Yubileyny 34
Genoa 33
Chennai 32
Duncan 32
Scandicci 31
Tianjin 31
Andover 29
Brooklyn 29
Johannesburg 29
Shenzhen 29
Palermo 28
Brescia 26
Carpi 26
San Francisco 26
Totale 40.258
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Nome #
Esercitazioni di sistemi energetici 1.384
Gas Turbines Design and Off-design Performance Analysis with Emissions Evaluation 393
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 361
A Rotor Blade Cooling Design Method For Heavy Duty Gas Turbine 350
Turbulent flow-field effects in a hybrid CFD-CRN model for the prediction of NOxand CO emissions in aero-engine combustors 334
DENSITY RATIO EFFECTS ON THE COOLING PERFORMANCES OF A COMBUSTOR LINER COOLED BY A COMBINED SLOT/ EFFUSION SYSTEM 331
Film-cooling adiabatic effectiveness measurements on a real high pressure turbine blade 330
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 321
Experimental Evaluation of the Density Ratio Effects on the Cooling Performance of a Combined Slot/Effusion Combustor Cooling System 318
Numerical Identification of a Premixed Flame Transfer Function and Stability Analysis of a Lean Burn Combustor 318
CFD Analysis of NOx Emissions of a Natural Gas Lean Premixed Burner for Heavy Duty Gas Turbine 318
Esercitazioni di Sistemi Energetici 315
Some Improvements in a Gas Turbine Stator-Rotor Systems Core-Swirl Ratio Correlation 310
"Design issues and performance of a chemically recuperated aeroderivative gas turbine." 309
COMBUSTOR LINER TEMPERATURE PREDICTION: A PRELIMINARY TOOL DEVELOPMENT AND ITS APPLICATION ON EFFUSION COOLING SYSTEMS 309
Numerical Simulation of Oil Jet Lubrication for High Speed Gears 309
Experimental Investigation of Innovative Internal Trailing Edge Cooling Configurations with Pentagonal Arrangement and Elliptic Pin Fin 306
Numerical analysis of the dynamic flame response of a spray flame for aero-engine applications 304
LES FOR THE EVALUATION OF ACOUSTIC DAMPING OF EFFUSION PLATES 303
A Numerical Procedure To Design Internal Cooling Of Gas Turbines Stator Blades 299
Aerothermal Analysis of a Turbine Casing Impingement Cooling System 298
CONJUGATE HEAT TRANSFER ANALYSIS OF AN INTERNALLY COOLED TURBINE BLADES WITH AN OBJECT ORIENTED CFD CODE 297
Heat Transfer and Pressure Loss Measurements of Matrix Cooling Geometries for Gas Turbine Airfoils 291
A Comparison between Two Gas Turbine Solutions to Increase Combined Power Plant Efficiency 286
NUMERICAL HEAT TRANSFER ANALYSIS OF AN INNOVATIVE GAS TURBINE COMBUSTOR: COUPLED STUDY OF RADIATION AND COOLING IN THE UPPER PART OF THE LINER 275
Design and Off-Design Analysis of a CRGT Cycle Based on the LM2500-STIG Gas Turbine 275
Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation 275
Experimental investigation of a leading edge cooling system with optimized inclined racetrack holes 274
Film cooling modeling for gas turbine nozzles and blades: Validation and application 264
Heat transfer investigation in new cooling schemes of a stationary blade trailing edge 264
L'UTILIZZO DEI PROMOTORI DI TURBOLENZA IN GEOMETRIE DI TURBOMACCHINA: VALUTAZIONI GLOBALI DI SCAMBIO TERMICO E PERDITE DI CARICO 255
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON WINDAGE POWER LOSSES IN HIGH SPEED GEARS 249
HEAT TRANSFERT AND PRESSURE DROP EVALUATION IN THIN WEDGE-SHAPED TRAILING EDGE 248
Heat Transfer Measurements in a Leading Edge Geometry With Racetrack Holes and Film Cooling Extraction 245
Assessment of modelling strategies for film cooling 238
Experimental and numerical investigation on windage power losses in high speed gears 237
INFLUENCE OF AMBIENT CONDITIONS ON AN AERODERIVATIVE GAS TURBINE BASED COGENERATION PLANT. A COMPARISON OF NUMERICAL SIMULATION WITH FIEL PERFORMANCE DATA 236
A Rotor Blade Cooling improvement for Heavy Duty Gas Turbine Using Steam and Mixed Steam/Air Cooling 232
Experimental Investigation on Impingement Array Cooling Systems Through IR Thermography 228
Refroidissement des turbines à gaz. Chambre de combustion 227
A 3d coupled approach for the thermal design of aero-engine combustor liners 225
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 225
Correlative Analysis Of Effusion Cooling Systems 224
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 223
A Simplified Approach To Off-Design Performance Evaluation Of Single Shaft Heavy Duty Gas Turbines 223
Modular approach to analysis of chemically recuperated gas turbine cycles 221
Volume Of Fluid (VOF) Analysis of Oil-Jet Lubrication for High-Speed Spur Gears Using an Adaptive Meshing Approach 220
Investigation on low-pressure steam turbine exhaust hood modelling through computational fluid dynamic simulations 219
Heat transfer investigation on an internal cooling system of a gas turbine leading edge model 216
ASSESSMENT OF A SET OF NUMERICAL TOOLS FOR THE DESIGN OF AERO ENGINES COMBUSTORS: STUDY OF A TUBULAR TEST RIG 215
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 214
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 214
Effect of rotation on a gas turbine blade internal cooling system: Experimental investigation 212
CFD simulations of a meshing gear pair 210
BLADE COOLING IMPROVEMENT FOR HEAVY DUTY GAS TURBINE: THE AIR COOLANT TEMPERATURE REDUCTION AND THE INTRODUCTION OF STEAM AND MIXED/AIR COOLING 209
Numerical Analysis of a Low NOx Partially Premixed Burner for Industrial Gas Turbine Applications 209
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 208
HEAVY DUTY GAS TURBINE SIMULATION: GLOBAL PERFORMANCES ESTIMATION AND SECONDARY AIR SYSTEM MODIFICATIONS 208
Effusion cooling system optimization for modern lean burn combustor 208
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 208
Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 207
Adiabatic effectiveness on high-pressure turbine nozzle guide vanes under realistic swirling conditions 206
Experimental Investigation of Swirl and Flow Structure Inside a Rotor-Stator Cavity 206
Transient thermal modelling of whole gt engine with a partly coupled fem-fluid network approach 206
Numerical Investigation On the Aerodynamic Performance of a Low-Pressure Steam Turbine Exhaust Hood Using Doe Analysis 206
Numerical Simulation of Dam-Break Problem Using an Adaptive Meshing Approach 205
“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. . 205
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 205
"DESIGN CRITERIA FOR RIBBED CHANNELS: EXPERIMENTAL INVESTIGATION AND THEORETICAL ANALYSIS", 204
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 204
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 203
Heat transfer in internal channel of a blade: effects of rotation in a trailing edge cooling system 202
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 202
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions 202
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 201
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 200
Numerical study of aerodynamic losses of effusion cooling holes in aero-engine combustor liners 199
Analysis of gas turbine rotating cavities by a one-dimensional model: Definition of a new discs fiction coefficients correlations set 199
Impingement Cooling Experimental Investigation Using Different Heating Elements 198
Modeling and experimental study of power losses in a rolling bearing 198
Experimental and Numerical Analysis of Multiple Impingement Jet Arrays for an Active Clearance Control System 198
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 197
A semi analytical Approach to emissions prediction in gas Turbine Combustors 196
ASSESSMENT OF NUMERICAL TOOLS FOR THE EVALUATION OF THE ACOUSTICIMPEDANCE OF MULTI-PERFORATED PLATES. 196
Cooling system optimization of combustor liners 196
Experimental and Theoretical Investigation of Thermal Effectiveness in Multiperforated Plates for Combustor Liner Effusion Cooling 196
Commissioning of a Newly Designed Experimental Facility for Hot Gas Ingestion Investigation 195
Assessment of turbulent models for a low-pressure turbine guide vane heat transfer with high free-stream turbulence 195
Flat Plate Honeycomb Seals Friction Factor Analysis 193
Large-Eddy Simulation of a turbulent spray flame using the flamelet generated manifold approach 193
Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion-Cooled Combustor 192
Conjugate Heat Transfer Calculations on GT Rotor Blade for Industrial Applications. Part I: Equivalent Internal Fluid Network Setup and Procedure Description 191
Effect of rotation on a gas turbine blade internal cooling system: Numerical investigation 191
EVALUATION AND COMPARISON OF DIFFERENT BLADE COOLING SOLUTIONS TO IMPROVE COOLING EFFICIENCY AND GAS TURBINE PERFORMANCES 190
Assessment of Flame Transfer Function Formulations for the Thermoacoustic Analysis of Lean Burn Aero-engine Combustors 190
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 190
Film Cooling Modelling for Gas Turbine Nozzles and Blades: Validation and Application 190
Numerical investigations of pollutant emissions from novel heavy duty gas turbine burners operated with natural gas 190
Analysis of flat plate honeycomb seals aerodynamic losses: effects of clearance 190
Totale 25.079
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Categoria #
all - tutte 161.107
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 161.107
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021231 0 0 0 0 0 0 0 0 0 0 0 231
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
2025/202618.461 1.434 2.469 1.447 1.339 1.987 813 2.013 975 1.708 1.150 591 2.535
Totale 61.322