PICCHI, ALESSIO
 Distribuzione geografica
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Continente #
NA - Nord America 6.943
EU - Europa 4.613
AS - Asia 4.058
SA - Sud America 544
Continente sconosciuto - Info sul continente non disponibili 177
AF - Africa 96
OC - Oceania 54
Totale 16.485
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Nazione #
US - Stati Uniti d'America 6.782
IT - Italia 1.471
RU - Federazione Russa 1.402
CN - Cina 1.133
SG - Singapore 992
HK - Hong Kong 625
PL - Polonia 582
BR - Brasile 428
VN - Vietnam 352
KR - Corea 330
IE - Irlanda 254
SE - Svezia 219
BD - Bangladesh 156
DE - Germania 134
FR - Francia 133
IN - India 131
FI - Finlandia 121
CA - Canada 100
GB - Regno Unito 96
JP - Giappone 73
JO - Giordania 61
AU - Australia 52
NL - Olanda 49
AR - Argentina 44
ID - Indonesia 37
TR - Turchia 35
AT - Austria 34
IQ - Iraq 30
MX - Messico 25
ES - Italia 23
BE - Belgio 21
UA - Ucraina 21
CO - Colombia 19
EC - Ecuador 19
CH - Svizzera 15
NG - Nigeria 15
PK - Pakistan 15
ZA - Sudafrica 15
IR - Iran 14
VE - Venezuela 14
MA - Marocco 12
KE - Kenya 11
DZ - Algeria 10
CI - Costa d'Avorio 8
PH - Filippine 8
TH - Thailandia 8
UZ - Uzbekistan 8
AE - Emirati Arabi Uniti 7
AZ - Azerbaigian 6
BJ - Benin 6
CL - Cile 6
DO - Repubblica Dominicana 6
PY - Paraguay 6
RO - Romania 6
RS - Serbia 6
SA - Arabia Saudita 6
TN - Tunisia 6
CR - Costa Rica 5
MY - Malesia 5
NP - Nepal 5
PE - Perù 5
EG - Egitto 4
HN - Honduras 4
JM - Giamaica 4
PT - Portogallo 4
SV - El Salvador 4
TT - Trinidad e Tobago 4
AM - Armenia 3
EE - Estonia 3
EU - Europa 3
MD - Moldavia 3
TW - Taiwan 3
BH - Bahrain 2
ET - Etiopia 2
GT - Guatemala 2
HU - Ungheria 2
KH - Cambogia 2
KZ - Kazakistan 2
LB - Libano 2
LT - Lituania 2
LU - Lussemburgo 2
LV - Lettonia 2
NI - Nicaragua 2
NO - Norvegia 2
PA - Panama 2
PR - Porto Rico 2
SN - Senegal 2
SY - Repubblica araba siriana 2
UY - Uruguay 2
AL - Albania 1
BA - Bosnia-Erzegovina 1
BG - Bulgaria 1
BO - Bolivia 1
BW - Botswana 1
CG - Congo 1
DK - Danimarca 1
FJ - Figi 1
GE - Georgia 1
GR - Grecia 1
IL - Israele 1
Totale 16.302
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Città #
Santa Clara 1.829
Ashburn 821
Singapore 796
Warsaw 571
Hong Kong 551
San Jose 521
Fairfield 359
Hefei 315
Florence 307
Seoul 303
Dublin 254
Milan 243
Beijing 209
Woodbridge 196
Seattle 179
Chandler 156
Houston 156
Cambridge 151
Wilmington 143
Council Bluffs 139
Ho Chi Minh City 117
Buffalo 97
Los Angeles 93
Ann Arbor 83
Hanoi 82
Altamura 81
Lauterbourg 73
Lawrence 72
New York 71
Rome 71
Helsinki 67
Moscow 67
Shanghai 61
Tokyo 60
Prato 58
Princeton 57
Kent 56
Phoenix 54
Dallas 52
Munich 51
The Dalles 47
Melbourne 46
Mumbai 43
Boston 34
Chicago 34
Medford 33
Vienna 31
Naples 30
Bengaluru 27
São Paulo 27
Turku 27
Boardman 25
Figino 25
Paris 24
Falls Church 22
Frankfurt am Main 22
San Diego 22
Turin 22
London 21
Toronto 21
Bologna 20
Guangzhou 20
Montreal 20
Bari 18
Da Nang 18
Jakarta 18
Orem 18
Clifton 17
Denver 16
Dong Ket 16
Haiphong 16
Redwood City 16
Rio de Janeiro 16
Scandicci 16
Miano 14
Orlando 14
Abuja 13
Dearborn 13
Redondo Beach 13
St Louis 13
Tong 13
Brasília 12
Brooklyn 12
Istanbul 12
Modena 12
Amsterdam 11
Belo Horizonte 11
Brussels 11
Chennai 11
Falkenstein 11
Charlotte 10
Jacksonville 10
Nairobi 10
Ottawa 10
Biên Hòa 9
Genova 9
Hillsboro 9
Johannesburg 9
Newark 9
Norwalk 9
Totale 10.740
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 425
Experimental Investigations of Effusion Cooling Systems for Lean Burn Aero-Engine Combustors 376
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 370
Film-cooling adiabatic effectiveness measurements on a real high pressure turbine blade 367
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 328
Improving emission and blow-out characteristics of novel natural gas low NOx burners for heavy duty gas turbine 242
Aero-thermal flow characterization downstream of an NGV cascade by five-hole probe and filtered Rayleigh scattering measurements 238
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 232
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 230
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 227
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 222
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 220
Effusion cooling system optimization for modern lean burn combustor 216
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 214
Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 214
Adiabatic effectiveness on high-pressure turbine nozzle guide vanes under realistic swirling conditions 212
Experimental Investigation of Swirl and Flow Structure Inside a Rotor-Stator Cavity 211
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 210
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 209
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 209
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 209
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 207
Experimental and Theoretical Investigation of Thermal Effectiveness in Multiperforated Plates for Combustor Liner Effusion Cooling 207
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 206
Commissioning of a Newly Designed Experimental Facility for Hot Gas Ingestion Investigation 202
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 199
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 197
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 196
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 194
On the Use of PSP to Determine the Rim Sealing Effectiveness 193
A new test facility for investigating thermal behaviour of effusion cooling test plates for rql combustors 192
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 192
Performance Improvement of a Heavy Duty GT: Adiabatic Effectiveness Measurements on First Stage Vanes in Representative Engine Conditions 190
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 188
Effect of slot injection and effusion array on the liner heat transfer coefficient of a scaled lean burn combustor with representative swirling flow 187
Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow 186
Heat Transfer Coefficient and Adiabatic Effectiveness on a Film-Cooled Pressure Side: Results and Assessment of the IR-Based Measurement Technique Reliability 186
Development and Application of a Concentration Probe for Mixing Flows Tracking in Turbomachinery Applications 185
Comparison of psp and tlc steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 185
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 184
Evaluation of Cooling Requirements for Rotating Detonation Combustors 183
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 182
Experimental Characterization of a Micro-Turbine Generator for Energy Recovery Applications 182
Development of experimental and numerical methods for the analysis of active clearance control systems 180
Film cooling adiabatic effectiveness measurements of pressure side trailing edge cooling configurations 180
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 179
Adiabatic effectiveness on high pressure turbine nozzle guide vanes under realistic swirling conditions 178
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 176
Measurement of internal heat transfer distributions using transient infrared thermography 175
DEVELOPMENT AND APPLICATION OF A CONCENTRATION PROBE FOR MIXING FLOWS TRACKING IN TURBOMACHINERY APPLICATIONS 173
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 172
Experimental Assessment of Correlative Approaches for the Prediction of Leakage Flow through Labyrinth Seals 170
Turbulence intensity measurements across a NGV cooled cascade with representative lean burn combustor outflow 170
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness 168
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 167
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 167
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 165
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 164
Swirling main flow effects on film cooling: Time resolved adiabatic effectiveness measurements in a gas turbine combustor model 162
Analysis of Swirl Number Effects on Effusion Flow Behavior Using Time-Resolved Particle Image Velocimetry 162
Assessment of Additive Manufactured Micro-Channel Characteristics: Impact of Hydraulic Diameter Evaluation 161
Effect of Coolant Extraction on Cold Side Heat Transfer Enhancement of an Effusion Cooling Plate 161
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 160
Experimental and theoretical investigation of thermal effectiveness in multi-perforated plates for combustor liner effusion cooling 160
Combustion Diagnostics and Emissions Measurements of a Novel Low NOx Burner for Industrial Gas Turbine Operated With CO2 Diluted Methane/Air Mixtures 156
Flat plate and turbine vane film-cooling performance with laid-back fan-shaped holes 155
Comparison of Rim Sealing Effectiveness in Different Geometrical Configurations 154
Experimental characterization of an industrial burner operated with simulated EGR 153
Flow Field and Hot Streak Migration Through High Pressure Cooled Vanes With Representative Lean Burn Combustor Outflow 151
Analysis of swirl number effects on effusion flow behaviour using time resolved PIV 151
Heat Transfer Coefficient and Adiabatic Effectiveness Measurements on a Nozzle Guide Vane With a Single Row of Cylindrical Holes 150
Heat transfer measurements in leading-edge cooling geometry under rotating conditions 150
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 150
Effect of rotation and hole arrangement in cold bridge-type impingement cooling systems 148
APPLICATION OF INTERNAL HEAT TRANSFER INVERSE PROBLEM SOLUTION METHOD TO JET ARRAY IMPINGEMENT COOLING SYSTEM 146
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 142
ASSESSMENT OF ADDITIVE MANUFACTURED MICRO-CHANNEL CHARACTERISTICS: IMPACT OF HYDRAULIC DIAMETER EVALUATION 140
Heat transfer measurements in a leading edge cooling geometry under rotating conditions 135
Effect of Jet-to-Jet Distance and Pipe Position on Flow and Heat Transfer Features of Active Clearance Control Systems 134
TURBULENCE FIELD MEASUREMENTS AT THE EXIT OF A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION 132
Impact of Target Surface Building Direction on the Heat Transfer Characteristics of Additive Manufactured Impingement Systems 108
INTERNAL CONVECTIVE HEAT TRANSFER IN A REAL ENGINE COMPONENT: A COMPARISON BETWEEN PIN-FINS AND KAGOME LATTICE 85
High-Fidelity Simulation for the Lean Blow-Out Analysis of an Industrial Burner Operated With Artificial Exhaust Gas Recirculation 79
Prediction of the Flame Characteristics of an Industrial Gas Turbine Operated with CO2-Diluted Air Through a High-Fidelity Numerical Analysis: A Comparison between Flamelet Generated Manifolds and Artificially Thickened Flame 71
EXPERIMENTAL STUDY ON STABILITY ENHANCEMENT OF A NATURAL GAS GT BURNER WITH HYDROGEN FLAME PILOTING OPERATED WITH SIMULATED EXHAUST GAS RECIRCULATION 60
Experimental Analysis on Microchannels with Different Cross-Sectional Shapes for Internal Cooling Applications 55
Investigation of the Flow Field Morphology of Film Cooling in Supersonic Flow 42
Thickened Flame Model Extension for Dual Gas Turbine Combustion: Validation Against Single Cup Atmospheric Test 37
Impact of Fuel Injection System on the Performance of an Industrial Burner With Hydrogen Piloting Operated With Simulated Exhaust Gas Recirculation 33
A NEW TEST FACILITY FOR INVESTIGATING LEAF-SEAL CAVITY INGESTION AT COMBUSTOR-TURBINE INTERFACE 26
ADIABATIC EFFECTIVENESS MEASUREMENTS OF FILM COOLING IN SUPERSONIC FLOW 24
Effect of Jet-to-Jet Distance and Pipe Position on Flow and Heat Transfer Features of Active Clearance Control Systems 23
Internal Convective Heat Transfer in a Real Engine Component: A Comparison Between Pin-Fins and Kagome Lattice 23
EXPERIMENTAL ANALYSIS ON MICRO-CHANNELS WITH DIFFERENT CROSS-SECTIONAL SHAPES FOR INTERNAL COOLING APPLICATIONS 21
Measurement of Internal Heat Transfer Distribution of Highly-Loaded Gas Turbine Blade by Combined Experimental/Numerical Method 21
Development and Application of an Internal Heat-Transfer Measurement Technique for Cooled Real Engine Components 21
Experimental Analysis of Additively Manufactured Latticework Coupons 20
Film Cooling in Supersonic Flow: Experiment Design and CFD Investigatio 20
Comparison of Rim Sealing Effectiveness in Different Geometrical Configurations 16
On the Proper Use of Pressure-Sensitive Paint for the Investigation of Film Cooling Adiabatic Effectiveness in Supersonic Flow 16
Totale 16.302
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Categoria #
all - tutte 44.408
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 44.408
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022468 0 0 26 29 22 75 9 56 23 29 93 106
2022/20231.110 93 203 72 54 65 189 201 43 133 5 31 21
2023/2024691 18 58 75 40 42 76 61 114 35 47 92 33
2024/20254.676 136 389 259 611 1.357 784 97 376 109 131 177 250
2025/20266.169 452 812 671 566 563 204 557 315 541 438 320 730
2026/2027977 312 258 407 0 0 0 0 0 0 0 0 0
Totale 16.485