FACCHINI, BRUNO
 Distribuzione geografica
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Continente #
NA - Nord America 4.066
EU - Europa 3.746
AS - Asia 2.479
AF - Africa 188
SA - Sud America 84
Continente sconosciuto - Info sul continente non disponibili 28
OC - Oceania 23
Totale 10.614
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Nazione #
US - Stati Uniti d'America 3.914
IT - Italia 1.240
FR - Francia 707
DE - Germania 535
CN - Cina 481
IN - India 417
GB - Regno Unito 301
IR - Iran 297
TR - Turchia 270
KR - Corea 202
JP - Giappone 135
RU - Federazione Russa 134
IE - Irlanda 130
UA - Ucraina 115
TW - Taiwan 113
CA - Canada 112
VN - Vietnam 99
PL - Polonia 92
IQ - Iraq 89
NL - Olanda 88
ID - Indonesia 64
DZ - Algeria 49
TH - Thailandia 49
RO - Romania 48
ES - Italia 46
CH - Svizzera 45
HK - Hong Kong 41
CZ - Repubblica Ceca 40
SG - Singapore 39
MX - Messico 35
ZA - Sudafrica 35
BE - Belgio 34
PK - Pakistan 33
EG - Egitto 30
GR - Grecia 30
BR - Brasile 28
MY - Malesia 27
AT - Austria 25
EU - Europa 23
FI - Finlandia 23
AE - Emirati Arabi Uniti 21
CL - Cile 20
NO - Norvegia 20
SA - Arabia Saudita 20
AU - Australia 19
NG - Nigeria 18
SE - Svezia 18
CO - Colombia 14
IL - Israele 14
AR - Argentina 12
BG - Bulgaria 12
BD - Bangladesh 11
HU - Ungheria 11
DK - Danimarca 10
KE - Kenya 10
RS - Serbia 10
LY - Libia 9
NP - Nepal 9
TN - Tunisia 9
GH - Ghana 8
MA - Marocco 8
PH - Filippine 8
PT - Portogallo 8
LT - Lituania 7
LV - Lettonia 7
JO - Giordania 6
LK - Sri Lanka 6
SY - Repubblica araba siriana 6
EC - Ecuador 5
OM - Oman 5
AP - ???statistics.table.value.countryCode.AP??? 4
NZ - Nuova Zelanda 4
CM - Camerun 3
MM - Myanmar 3
TT - Trinidad e Tobago 3
BN - Brunei Darussalam 2
EE - Estonia 2
ET - Etiopia 2
KZ - Kazakistan 2
LB - Libano 2
MO - Macao, regione amministrativa speciale della Cina 2
MZ - Mozambico 2
PE - Perù 2
PR - Porto Rico 2
SC - Seychelles 2
SI - Slovenia 2
SK - Slovacchia (Repubblica Slovacca) 2
VE - Venezuela 2
A1 - Anonimo 1
BA - Bosnia-Erzegovina 1
BH - Bahrain 1
GE - Georgia 1
HR - Croazia 1
KG - Kirghizistan 1
LU - Lussemburgo 1
MT - Malta 1
QA - Qatar 1
TZ - Tanzania 1
UY - Uruguay 1
UZ - Uzbekistan 1
Totale 10.611
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Città #
Houston 405
Fairfield 297
Santa Cruz 228
Buffalo 220
Florence 214
Ann Arbor 204
Seattle 197
Woodbridge 175
Ashburn 163
Beijing 129
Dublin 116
Cambridge 102
Duncan 89
Milan 87
Wilmington 87
Taipei 78
Warsaw 71
Dong Ket 60
Shanghai 60
Chicago 55
Hangzhou 54
Wuhan 49
Mountain View 45
University Park 45
Dearborn 43
Ankara 42
Rome 42
Seoul 42
Bangalore 41
Jakarta 41
Kharkov 40
Boardman 39
London 38
Bengaluru 37
Istanbul 36
Las Vegas 33
Nürnberg 33
Tehran 32
Torino 32
Los Angeles 31
Cranfield 30
Singapore 30
Phoenix 29
Dallas 28
Redmond 28
Severna Park 28
Paris 27
San Diego 27
Hanoi 26
Izmir 26
Tokyo 26
Chennai 25
Hyderabad 25
Changsha 24
Toronto 23
Baghdad 22
Clearwater 22
Nanjing 21
San Jose 21
Turin 21
Berlin 19
Harbin 19
Meudon 19
Fremont 18
Islamabad 18
Norwalk 18
Bari 17
Council Bluffs 17
Hamilton 17
Muizenberg 17
New York 17
Prato 17
Gostar 16
Henderson 16
Leawood 16
Madison 16
New Delhi 16
Ottawa 16
Oxford 16
Poggiomarino 16
Zurich 16
Bangkok 15
Scranton 15
Genova 14
Mumbai 14
Surabaya 14
Atlanta 13
Boulder 13
Cincinnati 13
Gurgaon 13
Helsinki 13
Madrid 13
Pardis 13
Toulouse 13
Athens 12
Coimbatore 12
Darmstadt 12
Palermo 12
Ferrara 11
Munich 11
Totale 4.944
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Nome #
Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation, file e398c37d-0959-179a-e053-3705fe0a4cff 955
A Comparison between Two Gas Turbine Solutions to Increase Combined Power Plant Efficiency, file e398c37d-574a-179a-e053-3705fe0a4cff 848
A Decoupled CHT Procedure: Application and Validation on a Gas Turbine Vane with Different Cooling Configurations, file e398c378-fc67-179a-e053-3705fe0a4cff 798
Design and Off-Design Analysis of a CRGT Cycle Based on the LM2500-STIG Gas Turbine, file e398c37d-4335-179a-e053-3705fe0a4cff 584
COMBUSTOR LINER TEMPERATURE PREDICTION: A PRELIMINARY TOOL DEVELOPMENT AND ITS APPLICATION ON EFFUSION COOLING SYSTEMS, file e398c378-d17a-179a-e053-3705fe0a4cff 567
Turbulent flow-field effects in a hybrid CFD-CRN model for the prediction of NOxand CO emissions in aero-engine combustors, file e398c37c-8d07-179a-e053-3705fe0a4cff 502
CONJUGATE HEAT TRANSFER ANALYSIS OF AN INTERNALLY COOLED TURBINE BLADES WITH AN OBJECT ORIENTED CFD CODE, file e398c378-afa0-179a-e053-3705fe0a4cff 464
Numerical Simulation of Oil Jet Lubrication for High Speed Gears, file e398c37a-599c-179a-e053-3705fe0a4cff 440
"Design issues and performance of a chemically recuperated aeroderivative gas turbine.", file e398c37d-4eef-179a-e053-3705fe0a4cff 419
Experimental investigation of a leading edge cooling system with optimized inclined racetrack holes, file e398c37d-0768-179a-e053-3705fe0a4cff 405
DENSITY RATIO EFFECTS ON THE COOLING PERFORMANCES OF A COMBUSTOR LINER COOLED BY A COMBINED SLOT/ EFFUSION SYSTEM, file e398c378-e426-179a-e053-3705fe0a4cff 380
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio, file e398c378-fc68-179a-e053-3705fe0a4cff 349
Numerical analysis of the dynamic flame response of a spray flame for aero-engine applications, file e398c37c-c37b-179a-e053-3705fe0a4cff 293
A Numerical Procedure To Design Internal Cooling Of Gas Turbines Stator Blades, file e398c37d-025c-179a-e053-3705fe0a4cff 291
Modular approach to analysis of chemically recuperated gas turbine cycles, file e398c37d-50b6-179a-e053-3705fe0a4cff 283
Heat Transfer and Pressure Loss Measurements of Matrix Cooling Geometries for Gas Turbine Airfoils, file e398c37d-12c1-179a-e053-3705fe0a4cff 264
A Rotor Blade Cooling Design Method For Heavy Duty Gas Turbine, file e398c37d-4326-179a-e053-3705fe0a4cff 263
CFD Analysis of NOx Emissions of a Natural Gas Lean Premixed Burner for Heavy Duty Gas Turbine, file e398c379-ba91-179a-e053-3705fe0a4cff 259
Experimental Investigation of Innovative Internal Trailing Edge Cooling Configurations with Pentagonal Arrangement and Elliptic Pin Fin, file e398c378-bc2e-179a-e053-3705fe0a4cff 258
Numerical Identification of a Premixed Flame Transfer Function and Stability Analysis of a Lean Burn Combustor, file e398c379-bd73-179a-e053-3705fe0a4cff 256
NUMERICAL HEAT TRANSFER ANALYSIS OF AN INNOVATIVE GAS TURBINE COMBUSTOR: COUPLED STUDY OF RADIATION AND COOLING IN THE UPPER PART OF THE LINER, file e398c37d-01ef-179a-e053-3705fe0a4cff 246
HEAT TRANSFERT AND PRESSURE DROP EVALUATION IN THIN WEDGE-SHAPED TRAILING EDGE, file e398c37d-113d-179a-e053-3705fe0a4cff 245
LES FOR THE EVALUATION OF ACOUSTIC DAMPING OF EFFUSION PLATES, file e398c378-e9de-179a-e053-3705fe0a4cff 213
Heat transfer investigation in new cooling schemes of a stationary blade trailing edge, file e398c37d-1467-179a-e053-3705fe0a4cff 200
Aerothermal Analysis of a Turbine Casing Impingement Cooling System, file e398c37a-5a71-179a-e053-3705fe0a4cff 166
Experimental Evaluation of the Density Ratio Effects on the Cooling Performance of a Combined Slot/Effusion Combustor Cooling System, file e398c378-df68-179a-e053-3705fe0a4cff 156
NUMERICAL INVESTIGATION OF POTENTIAL FLOW INDUCED VIBRATIONS OF STEAM TURBINE LAST STAGE ROTOR AT LOW LOAD OPERATION - PART 2: ROTATING INSTABILITIES DETECTION, file dedab734-6c68-48f6-9840-a85c7e17eb3e 146
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes, file e398c380-ddbb-179a-e053-3705fe0a4cff 118
Flat plate and turbine vane film-cooling performance with laid-back fan-shaped holes, file e398c380-7522-179a-e053-3705fe0a4cff 110
Some Improvements in a Gas Turbine Stator-Rotor Systems Core-Swirl Ratio Correlation, file e398c378-d843-179a-e053-3705fe0a4cff 108
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, file e398c380-b951-179a-e053-3705fe0a4cff 98
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes, file e398c380-84a9-179a-e053-3705fe0a4cff 90
Turbulence intensity measurements across a NGV cooled cascade with representative lean burn combustor outflow, file e398c380-84a0-179a-e053-3705fe0a4cff 64
Effect of rotation and hole arrangement in cold bridge-type impingement cooling systems, file e398c37f-fb13-179a-e053-3705fe0a4cff 61
NUMERICAL PREDICTION OF HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS ON A NOZZLE GUIDE VANE WITH REPRESENTATIVE COMBUSTOR OUTFLOW, file d5058d1c-8b64-4823-aaef-fa839bb3c257 55
Multiphysics numerical investigation of an aeronautical lean burn combustor, file bd0cbc13-c4cc-4174-bed2-1a8e63a7e995 37
A new test facility for investigating thermal behaviour of effusion cooling test plates for rql combustors, file 46f5eb8c-82fc-4440-a923-2bccfc106aa3 28
INFLUENCE OF AMBIENT CONDITIONS ON AN AERODERIVATIVE GAS TURBINE BASED COGENERATION PLANT. A COMPARISON OF NUMERICAL SIMULATION WITH FIEL PERFORMANCE DATA, file e398c37d-3645-179a-e053-3705fe0a4cff 28
Turbulent flow-field effects in a hybrid CFD-CRN model for the prediction of NOxand CO emissions in aero-engine combustors, file e398c381-04b6-179a-e053-3705fe0a4cff 28
Development of a numerical correlation for heat transfer coefficients in steam turbines inner chambers, file 30061644-68cf-4671-b176-603ff7ef2c63 21
Effect of Jet-to-Jet Distance and Pipe Position on Flow and Heat Transfer Features of Active Clearance Control Systems, file 8e985404-27de-444a-b613-dd19af939ab9 19
Development of experimental and numerical methods for the analysis of active clearance control systems, file 3fae5d39-7045-4be7-a93f-b79a5429edc9 16
Numerical analyses of a high pressure sooting flame with multiphysics approach, file 95a58e67-ad1e-40b2-b520-2d9d6fb81cb0 10
Numerical simulation of a swirl stabilized methane-air flame with an automatic meshing CFD solver, file 23b760fa-d890-414f-a28e-36a898dea20c 9
Modeling and experimental study of power losses in a rolling bearing, file e398c37e-b61d-179a-e053-3705fe0a4cff 5
Numerical and experimental investigation on an effusion-cooled lean burn aeronautical combustor: Aerothermal field and emissions, file e398c37e-d9d8-179a-e053-3705fe0a4cff 2
SCGT/CC: An Innovative Cycle with Advanced Environmental and Peakload Shaving Features, file e398c378-883a-179a-e053-3705fe0a4cff 1
Heat Transfer Measurements in a Leading Edge Geometry With Racetrack Holes and Film Cooling Extraction, file e398c378-ebd9-179a-e053-3705fe0a4cff 1
Turbine Stator Well CFD Studies: Effects of Coolant Supply Geometry on Cavity Sealing Performance, file e398c378-ecbe-179a-e053-3705fe0a4cff 1
Aerodynamical Characterization of Swirl Brakes for High Pressure Centrifugal Compressors, file e398c378-f629-179a-e053-3705fe0a4cff 1
Impingement Cooling Experimental Investigation Using Different Heating Elements, file e398c37b-a956-179a-e053-3705fe0a4cff 1
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, file e398c380-b952-179a-e053-3705fe0a4cff 1
Film cooling modeling for gas turbine nozzles and blades: Validation and application, file e398c380-b9f3-179a-e053-3705fe0a4cff 1
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow, file e398c381-c29f-179a-e053-3705fe0a4cff 1
Totale 11.165
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Categoria #
all - tutte 16.680
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 16.680
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019457 0 0 0 0 0 0 0 0 0 0 262 195
2019/20201.861 163 156 126 199 210 194 137 147 143 120 125 141
2020/20211.536 117 135 95 120 171 132 136 113 111 112 144 150
2021/20221.704 146 66 126 296 242 106 99 90 94 68 264 107
2022/20231.495 67 98 206 174 83 119 175 95 130 141 130 77
2023/20241.427 65 106 118 106 125 83 232 317 182 80 13 0
Totale 11.165