BACCI, TOMMASO
 Distribuzione geografica
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Continente #
NA - Nord America 3.587
AS - Asia 2.675
EU - Europa 2.613
SA - Sud America 377
Continente sconosciuto - Info sul continente non disponibili 95
AF - Africa 70
OC - Oceania 25
Totale 9.442
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Nazione #
US - Stati Uniti d'America 3.519
RU - Federazione Russa 889
CN - Cina 854
IT - Italia 754
SG - Singapore 635
HK - Hong Kong 377
BR - Brasile 296
PL - Polonia 281
VN - Vietnam 221
KR - Corea 203
IE - Irlanda 162
SE - Svezia 130
BD - Bangladesh 98
DE - Germania 83
FI - Finlandia 78
FR - Francia 69
IN - India 66
JP - Giappone 55
GB - Regno Unito 51
JO - Giordania 51
CA - Canada 38
AR - Argentina 31
NL - Olanda 28
AU - Australia 24
ID - Indonesia 24
MX - Messico 23
AT - Austria 20
EC - Ecuador 17
BE - Belgio 16
IQ - Iraq 16
UA - Ucraina 15
TR - Turchia 14
ZA - Sudafrica 14
NG - Nigeria 11
CH - Svizzera 10
PK - Pakistan 10
ES - Italia 9
DZ - Algeria 8
MA - Marocco 8
TN - Tunisia 8
UZ - Uzbekistan 8
CL - Cile 7
CO - Colombia 7
BJ - Benin 6
NP - Nepal 6
PE - Perù 6
PY - Paraguay 6
RO - Romania 6
VE - Venezuela 6
AE - Emirati Arabi Uniti 4
DO - Repubblica Dominicana 4
IR - Iran 4
AZ - Azerbaigian 3
GE - Georgia 3
KE - Kenya 3
PH - Filippine 3
SN - Senegal 3
BW - Botswana 2
CI - Costa d'Avorio 2
EG - Egitto 2
EU - Europa 2
IL - Israele 2
JM - Giamaica 2
KZ - Kazakistan 2
LT - Lituania 2
MD - Moldavia 2
OM - Oman 2
SA - Arabia Saudita 2
SY - Repubblica araba siriana 2
TW - Taiwan 2
AL - Albania 1
AM - Armenia 1
BH - Bahrain 1
CG - Congo 1
DK - Danimarca 1
ET - Etiopia 1
GR - Grecia 1
KH - Cambogia 1
LA - Repubblica Popolare Democratica del Laos 1
LU - Lussemburgo 1
LV - Lettonia 1
MU - Mauritius 1
MY - Malesia 1
PT - Portogallo 1
QA - Qatar 1
RS - Serbia 1
SI - Slovenia 1
TH - Thailandia 1
TJ - Tagikistan 1
TO - Tonga 1
TT - Trinidad e Tobago 1
UY - Uruguay 1
Totale 9.349
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Città #
Santa Clara 1.069
Singapore 525
Ashburn 427
Hong Kong 325
San Jose 283
Warsaw 271
Hefei 236
Seoul 200
Dublin 162
Fairfield 144
Florence 136
Beijing 132
Woodbridge 116
Milan 115
Chandler 82
Houston 82
Seattle 81
Cambridge 78
Wilmington 69
Ho Chi Minh City 67
Council Bluffs 57
Hanoi 55
Los Angeles 54
Moscow 54
Helsinki 52
Ann Arbor 49
Kent 47
Tokyo 43
Buffalo 42
Lauterbourg 42
Prato 42
Altamura 36
Rome 36
Lawrence 35
Shanghai 34
The Dalles 34
New York 33
Munich 31
Princeton 31
Mumbai 27
São Paulo 23
Tong 22
Melbourne 21
Turku 20
Medford 19
Boston 17
Dallas 16
Vienna 16
Bengaluru 15
Redwood City 15
Scandicci 15
Rio de Janeiro 14
Boardman 13
Bologna 13
Dong Ket 13
San Diego 13
Chicago 12
Naples 12
Toronto 12
Abuja 11
Guangzhou 11
Bari 10
Clifton 10
Da Nang 10
Frankfurt am Main 10
London 10
Phoenix 10
Redondo Beach 10
Comun Nuovo 9
Hillsboro 9
Jakarta 9
Johannesburg 9
Modena 9
Orem 9
Amsterdam 8
Brasília 8
Brussels 8
Curitiba 8
Hải Dương 8
Stockholm 8
West Jordan 8
Charlotte 7
Luft 7
Paris 7
Zhengzhou 7
Andover 6
Belo Horizonte 6
Cotonou 6
Guayaquil 6
Kurita 6
Mexico City 6
Miano 6
Porto Alegre 6
Arezzo 5
Bern 5
Biên Hòa 5
Chennai 5
Dearborn 5
Falkenstein 5
Figino 5
Totale 6.048
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Nome #
Experimental investigation on a high pressure NGV cascade in the presence of a representative lean burn aero-engine combustor outflow 454
Experimental and CFD analyses of a highly-loaded gas turbine blade 420
Simulation Model and Experimental Setup for Power Quality Disturbances Methodologies Testing and Validation 243
Aero-thermal flow characterization downstream of an NGV cascade by five-hole probe and filtered Rayleigh scattering measurements 237
Hybrid RANS-LES modeling of the aerothermal field in an annular hot streak generator for the study of combustor-turbine interaction 221
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors 218
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 216
Uncertainty quantification of film cooling performance of an industrial gas turbine vane 216
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
Adiabatic effectiveness on high-pressure turbine nozzle guide vanes under realistic swirling conditions 210
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 206
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
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 186
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled HPT vanes 184
Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow 182
Development and Application of a Concentration Probe for Mixing Flows Tracking in Turbomachinery Applications 182
Heat Transfer Coefficient and Adiabatic Effectiveness on a Film-Cooled Pressure Side: Results and Assessment of the IR-Based Measurement Technique Reliability 182
Non-reactive test rig for combustor-turbine interaction studies in industrial gas turbines 181
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 180
Experimental Characterization of a Micro-Turbine Generator for Energy Recovery Applications 180
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 178
Adiabatic effectiveness on high pressure turbine nozzle guide vanes under realistic swirling conditions 177
Design of a Non-Reactive Warm Rig With Real Lean-Premix Combustor Swirlers and Film-Cooled First Stage Nozzles 176
NUMERICAL PREDICTION OF HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS ON A NOZZLE GUIDE VANE WITH REPRESENTATIVE COMBUSTOR OUTFLOW 171
DEVELOPMENT AND APPLICATION OF A CONCENTRATION PROBE FOR MIXING FLOWS TRACKING IN TURBOMACHINERY APPLICATIONS 170
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 169
Experimental Assessment of Correlative Approaches for the Prediction of Leakage Flow through Labyrinth Seals 169
Turbulence intensity measurements across a NGV cooled cascade with representative lean burn combustor outflow 168
Hybrid rans-les modeling of the aero-Thermal field in an annular hot streak generator for the study of combustor-Turbine interaction 166
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 166
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 162
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 159
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled high pressure turbine vanes 158
Assessment of Additive Manufactured Micro-Channel Characteristics: Impact of Hydraulic Diameter Evaluation 157
Long-term evaluation of corneal sub-basal nerve recovery after photorefractive keratectomy and influence of pars plana vitrectomy 154
Flat plate and turbine vane film-cooling performance with laid-back fan-shaped holes 154
NUMERICAL PREDICTION OF THE HEAT LOADS ON A NON-REACTIVE TEST RIG FOR COMBUSTOR-TURBINE INTERACTION BY USING HYBRID RANS-LES APPROACH 151
FLOWFIELD AND TEMPERATURE PROFILES MEASUREMENTS ON A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION 151
Flow Field and Hot Streak Migration Through High Pressure Cooled Vanes With Representative Lean Burn Combustor Outflow 145
Heat Transfer Coefficient and Adiabatic Effectiveness Measurements on a Nozzle Guide Vane With a Single Row of Cylindrical Holes 144
APPLICATION OF INTERNAL HEAT TRANSFER INVERSE PROBLEM SOLUTION METHOD TO JET ARRAY IMPINGEMENT COOLING SYSTEM 142
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 141
Clocking and Potential Effects in Combustor–Turbine Stator Interactions 138
ASSESSMENT OF ADDITIVE MANUFACTURED MICRO-CHANNEL CHARACTERISTICS: IMPACT OF HYDRAULIC DIAMETER EVALUATION 136
TURBULENCE FIELD MEASUREMENTS AT THE EXIT OF A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION 131
Numerical modeling and exergetic analysis of efficiency improving solutions for a micro-CAES system 126
NUMERICAL MODELING AND DESIGN OPTIMIZATION OF A MICRO-CAES SYSTEM 117
Impact of Target Surface Building Direction on the Heat Transfer Characteristics of Additive Manufactured Impingement Systems 98
INTERNAL CONVECTIVE HEAT TRANSFER IN A REAL ENGINE COMPONENT: A COMPARISON BETWEEN PIN-FINS AND KAGOME LATTICE 84
Experimental Analysis on Microchannels with Different Cross-Sectional Shapes for Internal Cooling Applications 52
NUMERICAL PREDICTION OF THE HEAT LOADS ON A TURBINE VANE TEST CASE 38
Hybrid micro-compressed air energy storage with photovoltaic and diesel generation for off-grid applications: A parametric life cycle and techno-economic study 25
EXPERIMENTAL ANALYSIS ON MICRO-CHANNELS WITH DIFFERENT CROSS-SECTIONAL SHAPES FOR INTERNAL COOLING APPLICATIONS 19
Internal Convective Heat Transfer in a Real Engine Component: A Comparison Between Pin-Fins and Kagome Lattice 19
Totale 9.442
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Categoria #
all - tutte 26.093
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 26.093
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022314 0 9 11 39 22 52 9 43 10 16 40 63
2022/2023691 53 106 50 24 31 113 130 23 101 9 29 22
2023/2024505 14 42 49 27 24 47 39 112 26 36 68 21
2024/20252.844 77 247 147 395 810 437 61 220 74 67 140 169
2025/20263.780 307 547 457 423 374 120 357 147 305 233 134 376
2026/2027191 108 83 0 0 0 0 0 0 0 0 0 0
Totale 9.442