PICCHI, ALESSIO
 Distribuzione geografica
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Continente #
NA - Nord America 6.387
EU - Europa 4.503
AS - Asia 3.991
SA - Sud America 517
AF - Africa 93
OC - Oceania 54
Continente sconosciuto - Info sul continente non disponibili 3
Totale 15.548
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Nazione #
US - Stati Uniti d'America 6.257
RU - Federazione Russa 1.401
IT - Italia 1.390
CN - Cina 1.121
SG - Singapore 979
HK - Hong Kong 618
PL - Polonia 582
BR - Brasile 419
VN - Vietnam 348
KR - Corea 327
IE - Irlanda 254
SE - Svezia 208
BD - Bangladesh 153
DE - Germania 133
FR - Francia 132
IN - India 126
FI - Finlandia 121
GB - Regno Unito 90
CA - Canada 83
JP - Giappone 71
JO - Giordania 61
AU - Australia 52
NL - Olanda 45
AR - Argentina 44
ID - Indonesia 37
AT - Austria 34
IQ - Iraq 28
TR - Turchia 28
MX - Messico 24
ES - Italia 23
BE - Belgio 21
UA - Ucraina 20
EC - Ecuador 15
NG - Nigeria 15
PK - Pakistan 15
ZA - Sudafrica 15
IR - Iran 14
CH - Svizzera 13
CO - Colombia 12
MA - Marocco 12
DZ - Algeria 10
KE - Kenya 10
UZ - Uzbekistan 8
VE - Venezuela 8
CI - Costa d'Avorio 7
TH - Thailandia 7
AE - Emirati Arabi Uniti 6
AZ - Azerbaigian 6
BJ - Benin 6
DO - Repubblica Dominicana 6
PH - Filippine 6
PY - Paraguay 6
RO - Romania 6
RS - Serbia 6
TN - Tunisia 6
CL - Cile 5
NP - Nepal 5
PE - Perù 5
EG - Egitto 4
MY - Malesia 4
PT - Portogallo 4
SA - Arabia Saudita 4
SV - El Salvador 4
EU - Europa 3
JM - Giamaica 3
MD - Moldavia 3
TW - Taiwan 3
AM - Armenia 2
BH - Bahrain 2
ET - Etiopia 2
GT - Guatemala 2
HN - Honduras 2
HU - Ungheria 2
KH - Cambogia 2
KZ - Kazakistan 2
LT - Lituania 2
LU - Lussemburgo 2
LV - Lettonia 2
NO - Norvegia 2
SN - Senegal 2
SY - Repubblica araba siriana 2
TT - Trinidad e Tobago 2
UY - Uruguay 2
AL - Albania 1
BA - Bosnia-Erzegovina 1
BG - Bulgaria 1
BO - Bolivia 1
BW - Botswana 1
CG - Congo 1
CR - Costa Rica 1
DK - Danimarca 1
EE - Estonia 1
FJ - Figi 1
GE - Georgia 1
GR - Grecia 1
IL - Israele 1
KN - Saint Kitts e Nevis 1
LA - Repubblica Popolare Democratica del Laos 1
LB - Libano 1
MU - Mauritius 1
Totale 15.541
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Città #
Santa Clara 1.809
Singapore 790
Ashburn 783
Warsaw 570
Hong Kong 544
San Jose 439
Fairfield 359
Hefei 315
Seoul 303
Florence 273
Dublin 254
Milan 232
Beijing 205
Woodbridge 195
Seattle 174
Chandler 156
Houston 155
Cambridge 150
Wilmington 142
Ho Chi Minh City 117
Buffalo 96
Los Angeles 86
Ann Arbor 83
Altamura 81
Hanoi 80
Lauterbourg 73
Lawrence 72
Helsinki 67
Moscow 67
New York 67
Rome 67
Prato 58
Tokyo 58
Princeton 57
Kent 56
Shanghai 55
Munich 51
Dallas 47
The Dalles 47
Melbourne 46
Mumbai 43
Boston 34
Chicago 33
Medford 33
Council Bluffs 31
Vienna 31
São Paulo 27
Turku 27
Naples 26
Boardman 25
Paris 24
Figino 23
Bengaluru 22
Falls Church 22
Frankfurt am Main 22
London 21
San Diego 21
Turin 21
Guangzhou 20
Toronto 20
Bologna 19
Da Nang 18
Jakarta 18
Orem 18
Bari 17
Montreal 17
Clifton 16
Denver 16
Dong Ket 16
Redwood City 16
Rio de Janeiro 16
Scandicci 16
Haiphong 15
Miano 14
Abuja 13
Dearborn 13
Redondo Beach 13
Tong 13
Modena 12
Phoenix 12
Belo Horizonte 11
Brussels 11
Chennai 11
Falkenstein 11
Charlotte 10
Ottawa 10
Biên Hòa 9
Brasília 9
Brooklyn 9
Genova 9
Jacksonville 9
Johannesburg 9
Nairobi 9
Norwalk 9
Porto Alegre 9
Stockholm 9
Amsterdam 8
Baghdad 8
Barcelona 8
Genoa 8
Totale 10.299
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 420
Experimental Investigations of Effusion Cooling Systems for Lean Burn Aero-Engine Combustors 366
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 363
Film-cooling adiabatic effectiveness measurements on a real high pressure turbine blade 341
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 325
Improving emission and blow-out characteristics of novel natural gas low NOx burners for heavy duty gas turbine 239
Aero-thermal flow characterization downstream of an NGV cascade by five-hole probe and filtered Rayleigh scattering measurements 236
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 228
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 223
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 216
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 214
Effusion cooling system optimization for modern lean burn combustor 212
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 212
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 211
Adiabatic effectiveness on high-pressure turbine nozzle guide vanes under realistic swirling conditions 209
Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 208
Experimental Investigation of Swirl and Flow Structure Inside a Rotor-Stator Cavity 207
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 207
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 205
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 205
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 204
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 202
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 201
Experimental and Theoretical Investigation of Thermal Effectiveness in Multiperforated Plates for Combustor Liner Effusion Cooling 198
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 198
Commissioning of a Newly Designed Experimental Facility for Hot Gas Ingestion Investigation 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 190
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 190
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 189
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 186
Effect of slot injection and effusion array on the liner heat transfer coefficient of a scaled lean burn combustor with representative swirling flow 186
Performance Improvement of a Heavy Duty GT: Adiabatic Effectiveness Measurements on First Stage Vanes in Representative Engine Conditions 185
On the Use of PSP to Determine the Rim Sealing Effectiveness 183
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 182
A new test facility for investigating thermal behaviour of effusion cooling test plates for rql combustors 180
Development and Application of a Concentration Probe for Mixing Flows Tracking in Turbomachinery Applications 180
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 179
Heat Transfer Coefficient and Adiabatic Effectiveness on a Film-Cooled Pressure Side: Results and Assessment of the IR-Based Measurement Technique Reliability 178
Comparison of psp and tlc steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 178
Experimental Characterization of a Micro-Turbine Generator for Energy Recovery Applications 178
Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow 176
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 175
Adiabatic effectiveness on high pressure turbine nozzle guide vanes under realistic swirling conditions 175
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 174
Evaluation of Cooling Requirements for Rotating Detonation Combustors 173
Film cooling adiabatic effectiveness measurements of pressure side trailing edge cooling configurations 171
DEVELOPMENT AND APPLICATION OF A CONCENTRATION PROBE FOR MIXING FLOWS TRACKING IN TURBOMACHINERY APPLICATIONS 169
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 168
Experimental Assessment of Correlative Approaches for the Prediction of Leakage Flow through Labyrinth Seals 168
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 168
Measurement of internal heat transfer distributions using transient infrared thermography 168
Turbulence intensity measurements across a NGV cooled cascade with representative lean burn combustor outflow 167
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 165
Development of experimental and numerical methods for the analysis of active clearance control systems 161
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness 160
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 159
Analysis of Swirl Number Effects on Effusion Flow Behavior Using Time-Resolved Particle Image Velocimetry 159
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 158
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 157
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 157
Effect of Coolant Extraction on Cold Side Heat Transfer Enhancement of an Effusion Cooling Plate 156
Experimental and theoretical investigation of thermal effectiveness in multi-perforated plates for combustor liner effusion cooling 154
Flat plate and turbine vane film-cooling performance with laid-back fan-shaped holes 154
Swirling main flow effects on film cooling: Time resolved adiabatic effectiveness measurements in a gas turbine combustor model 151
Assessment of Additive Manufactured Micro-Channel Characteristics: Impact of Hydraulic Diameter Evaluation 150
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 148
Combustion Diagnostics and Emissions Measurements of a Novel Low NOx Burner for Industrial Gas Turbine Operated With CO2 Diluted Methane/Air Mixtures 147
Analysis of swirl number effects on effusion flow behaviour using time resolved PIV 147
Comparison of Rim Sealing Effectiveness in Different Geometrical Configurations 147
Heat transfer measurements in leading-edge cooling geometry under rotating conditions 146
Flow Field and Hot Streak Migration Through High Pressure Cooled Vanes With Representative Lean Burn Combustor Outflow 144
Experimental characterization of an industrial burner operated with simulated EGR 144
Heat Transfer Coefficient and Adiabatic Effectiveness Measurements on a Nozzle Guide Vane With a Single Row of Cylindrical Holes 143
Effect of rotation and hole arrangement in cold bridge-type impingement cooling systems 143
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 140
APPLICATION OF INTERNAL HEAT TRANSFER INVERSE PROBLEM SOLUTION METHOD TO JET ARRAY IMPINGEMENT COOLING SYSTEM 138
ASSESSMENT OF ADDITIVE MANUFACTURED MICRO-CHANNEL CHARACTERISTICS: IMPACT OF HYDRAULIC DIAMETER EVALUATION 135
Effect of Jet-to-Jet Distance and Pipe Position on Flow and Heat Transfer Features of Active Clearance Control Systems 131
Heat transfer measurements in a leading edge cooling geometry under rotating conditions 131
TURBULENCE FIELD MEASUREMENTS AT THE EXIT OF A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION 129
Impact of Target Surface Building Direction on the Heat Transfer Characteristics of Additive Manufactured Impingement Systems 97
INTERNAL CONVECTIVE HEAT TRANSFER IN A REAL ENGINE COMPONENT: A COMPARISON BETWEEN PIN-FINS AND KAGOME LATTICE 82
High-Fidelity Simulation for the Lean Blow-Out Analysis of an Industrial Burner Operated With Artificial Exhaust Gas Recirculation 62
Experimental Analysis on Microchannels with Different Cross-Sectional Shapes for Internal Cooling Applications 50
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 42
EXPERIMENTAL STUDY ON STABILITY ENHANCEMENT OF A NATURAL GAS GT BURNER WITH HYDROGEN FLAME PILOTING OPERATED WITH SIMULATED EXHAUST GAS RECIRCULATION 41
Investigation of the Flow Field Morphology of Film Cooling in Supersonic Flow 31
Thickened Flame Model Extension for Dual Gas Turbine Combustion: Validation Against Single Cup Atmospheric Test 22
Impact of Fuel Injection System on the Performance of an Industrial Burner With Hydrogen Piloting Operated With Simulated Exhaust Gas Recirculation 21
A NEW TEST FACILITY FOR INVESTIGATING LEAF-SEAL CAVITY INGESTION AT COMBUSTOR-TURBINE INTERFACE 20
Development and Application of an Internal Heat-Transfer Measurement Technique for Cooled Real Engine Components 19
EXPERIMENTAL ANALYSIS ON MICRO-CHANNELS WITH DIFFERENT CROSS-SECTIONAL SHAPES FOR INTERNAL COOLING APPLICATIONS 17
Effect of Jet-to-Jet Distance and Pipe Position on Flow and Heat Transfer Features of Active Clearance Control Systems 17
Measurement of Internal Heat Transfer Distribution of Highly-Loaded Gas Turbine Blade by Combined Experimental/Numerical Method 16
Internal Convective Heat Transfer in a Real Engine Component: A Comparison Between Pin-Fins and Kagome Lattice 16
Flow Check and Adiabatic Effectiveness Measurements on Traditionally Versus Additively Manufactured Film-Cooling Holes 14
Film Cooling in Supersonic Flow: Experiment Design and CFD Investigatio 13
Experimental Analysis of Additive Manufactured Latticework Coupons 10
Experimental Analysis of Additively Manufactured Latticework Coupons 10
ADIABATIC EFFECTIVENESS MEASUREMENTS OF FILM COOLING IN SUPERSONIC FLOW 10
Totale 15.626
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Categoria #
all - tutte 41.432
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 41.432
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022501 17 16 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
2026/2027212 212 0 0 0 0 0 0 0 0 0 0 0
Totale 15.720