PICCHI, ALESSIO
 Distribuzione geografica
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Continente #
NA - Nord America 6.120
EU - Europa 4.010
AS - Asia 3.881
SA - Sud America 517
AF - Africa 93
OC - Oceania 53
Continente sconosciuto - Info sul continente non disponibili 3
Totale 14.677
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Nazione #
US - Stati Uniti d'America 6.035
RU - Federazione Russa 1.401
CN - Cina 1.108
SG - Singapore 973
IT - Italia 912
HK - Hong Kong 615
PL - Polonia 580
BR - Brasile 419
VN - Vietnam 348
KR - Corea 327
IE - Irlanda 254
SE - Svezia 208
DE - Germania 131
FR - Francia 131
IN - India 125
FI - Finlandia 121
GB - Regno Unito 87
BD - Bangladesh 71
JP - Giappone 66
JO - Giordania 61
AU - Australia 51
CA - Canada 45
AR - Argentina 44
NL - Olanda 44
ID - Indonesia 37
AT - Austria 34
IQ - Iraq 28
TR - Turchia 28
MX - Messico 22
BE - Belgio 21
ES - Italia 21
UA - Ucraina 20
EC - Ecuador 15
NG - Nigeria 15
PK - Pakistan 15
ZA - Sudafrica 15
IR - Iran 14
CH - Svizzera 12
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
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
EU - Europa 3
JM - Giamaica 3
MD - Moldavia 3
RO - Romania 3
TW - Taiwan 3
AM - Armenia 2
BH - Bahrain 2
ET - Etiopia 2
GT - Guatemala 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
HN - Honduras 1
IL - Israele 1
KN - Saint Kitts e Nevis 1
LA - Repubblica Popolare Democratica del Laos 1
LB - Libano 1
MU - Mauritius 1
OM - Oman 1
Totale 14.671
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Città #
Santa Clara 1.795
Singapore 788
Ashburn 752
Warsaw 570
Hong Kong 541
San Jose 424
Fairfield 359
Hefei 315
Seoul 303
Dublin 254
Florence 252
Beijing 201
Woodbridge 195
Seattle 170
Chandler 156
Houston 153
Cambridge 150
Wilmington 141
Ho Chi Minh City 117
Buffalo 89
Ann Arbor 83
Altamura 81
Hanoi 80
Lauterbourg 73
Lawrence 72
Milan 71
Helsinki 67
Moscow 67
Los Angeles 62
Tokyo 58
Prato 57
Princeton 57
Kent 56
New York 54
Munich 51
Shanghai 50
The Dalles 47
Melbourne 46
Mumbai 42
Dallas 36
Boston 33
Medford 33
Vienna 31
Chicago 30
Council Bluffs 29
São Paulo 27
Turku 27
Boardman 25
Paris 24
Bengaluru 22
Falls Church 21
San Diego 21
Frankfurt am Main 20
Guangzhou 20
Da Nang 18
Jakarta 18
London 17
Orem 17
Clifton 16
Dong Ket 16
Redwood City 16
Rio de Janeiro 16
Scandicci 16
Haiphong 15
Abuja 13
Dearborn 13
Redondo Beach 13
Tong 13
Denver 12
Miano 12
Montreal 12
Phoenix 12
Rome 12
Belo Horizonte 11
Bologna 11
Brussels 11
Chennai 11
Falkenstein 11
Turin 11
Modena 10
Toronto 10
Biên Hòa 9
Brasília 9
Genova 9
Jacksonville 9
Johannesburg 9
Nairobi 9
Norwalk 9
Ottawa 9
Porto Alegre 9
Stockholm 9
Amsterdam 8
Baghdad 8
Barcelona 8
Brooklyn 8
Grammichele 8
Hillsboro 8
Lappeenranta 8
Pune 8
Salvador 8
Totale 9.823
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 399
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 353
Experimental Investigations of Effusion Cooling Systems for Lean Burn Aero-Engine Combustors 350
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 325
Film-cooling adiabatic effectiveness measurements on a real high pressure turbine blade 313
Aero-thermal flow characterization downstream of an NGV cascade by five-hole probe and filtered Rayleigh scattering measurements 226
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 217
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 212
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 209
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 206
Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 202
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 200
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 200
Experimental Investigation of Swirl and Flow Structure Inside a Rotor-Stator Cavity 199
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 198
Adiabatic effectiveness on high-pressure turbine nozzle guide vanes under realistic swirling conditions 198
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 198
Effusion cooling system optimization for modern lean burn combustor 197
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 193
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 192
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 191
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 190
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 190
Commissioning of a Newly Designed Experimental Facility for Hot Gas Ingestion Investigation 189
Improving emission and blow-out characteristics of novel natural gas low NOx burners for heavy duty gas turbine 188
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 184
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 183
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 183
Experimental and Theoretical Investigation of Thermal Effectiveness in Multiperforated Plates for Combustor Liner Effusion Cooling 182
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 181
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 181
Effect of slot injection and effusion array on the liner heat transfer coefficient of a scaled lean burn combustor with representative swirling flow 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
Development and Application of a Concentration Probe for Mixing Flows Tracking in Turbomachinery Applications 179
Performance Improvement of a Heavy Duty GT: Adiabatic Effectiveness Measurements on First Stage Vanes in Representative Engine Conditions 179
Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow 176
A new test facility for investigating thermal behaviour of effusion cooling test plates for rql combustors 175
On the Use of PSP to Determine the Rim Sealing Effectiveness 174
Heat Transfer Coefficient and Adiabatic Effectiveness on a Film-Cooled Pressure Side: Results and Assessment of the IR-Based Measurement Technique Reliability 174
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 173
Comparison of psp and tlc steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 173
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 171
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 168
Adiabatic effectiveness on high pressure turbine nozzle guide vanes under realistic swirling conditions 168
DEVELOPMENT AND APPLICATION OF A CONCENTRATION PROBE FOR MIXING FLOWS TRACKING IN TURBOMACHINERY APPLICATIONS 168
Experimental Assessment of Correlative Approaches for the Prediction of Leakage Flow through Labyrinth Seals 167
Experimental Characterization of a Micro-Turbine Generator for Energy Recovery Applications 167
Evaluation of Cooling Requirements for Rotating Detonation Combustors 162
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness 160
Film cooling adiabatic effectiveness measurements of pressure side trailing edge cooling configurations 160
Development of experimental and numerical methods for the analysis of active clearance control systems 159
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 159
Turbulence intensity measurements across a NGV cooled cascade with representative lean burn combustor outflow 158
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 157
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 157
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 156
Measurement of internal heat transfer distributions using transient infrared thermography 154
Swirling main flow effects on film cooling: Time resolved adiabatic effectiveness measurements in a gas turbine combustor model 151
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 151
Flat plate and turbine vane film-cooling performance with laid-back fan-shaped holes 151
Experimental and theoretical investigation of thermal effectiveness in multi-perforated plates for combustor liner effusion cooling 150
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 150
Analysis of Swirl Number Effects on Effusion Flow Behavior Using Time-Resolved Particle Image Velocimetry 150
Effect of Coolant Extraction on Cold Side Heat Transfer Enhancement of an Effusion Cooling Plate 149
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 143
Combustion Diagnostics and Emissions Measurements of a Novel Low NOx Burner for Industrial Gas Turbine Operated With CO2 Diluted Methane/Air Mixtures 143
Effect of rotation and hole arrangement in cold bridge-type impingement cooling systems 142
Heat Transfer Coefficient and Adiabatic Effectiveness Measurements on a Nozzle Guide Vane With a Single Row of Cylindrical Holes 141
Comparison of Rim Sealing Effectiveness in Different Geometrical Configurations 141
Heat transfer measurements in leading-edge cooling geometry under rotating conditions 139
Analysis of swirl number effects on effusion flow behaviour using time resolved PIV 138
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 137
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 133
ASSESSMENT OF ADDITIVE MANUFACTURED MICRO-CHANNEL CHARACTERISTICS: IMPACT OF HYDRAULIC DIAMETER EVALUATION 132
APPLICATION OF INTERNAL HEAT TRANSFER INVERSE PROBLEM SOLUTION METHOD TO JET ARRAY IMPINGEMENT COOLING SYSTEM 132
TURBULENCE FIELD MEASUREMENTS AT THE EXIT OF A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION 126
Effect of Jet-to-Jet Distance and Pipe Position on Flow and Heat Transfer Features of Active Clearance Control Systems 125
Heat transfer measurements in a leading edge cooling geometry under rotating conditions 124
Assessment of Additive Manufactured Micro-Channel Characteristics: Impact of Hydraulic Diameter Evaluation 113
Impact of Target Surface Building Direction on the Heat Transfer Characteristics of Additive Manufactured Impingement Systems 97
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 40
Experimental Analysis on Microchannels with Different Cross-Sectional Shapes for Internal Cooling Applications 38
High-Fidelity Simulation for the Lean Blow-Out Analysis of an Industrial Burner Operated With Artificial Exhaust Gas Recirculation 38
INTERNAL CONVECTIVE HEAT TRANSFER IN A REAL ENGINE COMPONENT: A COMPARISON BETWEEN PIN-FINS AND KAGOME LATTICE 21
Thickened Flame Model Extension for Dual Gas Turbine Combustion: Validation Against Single Cup Atmospheric Test 20
Impact of Fuel Injection System on the Performance of an Industrial Burner With Hydrogen Piloting Operated With Simulated Exhaust Gas Recirculation 20
Investigation of the Flow Field Morphology of Film Cooling in Supersonic Flow 17
Internal Convective Heat Transfer in a Real Engine Component: A Comparison Between Pin-Fins and Kagome Lattice 13
EXPERIMENTAL STUDY ON STABILITY ENHANCEMENT OF A NATURAL GAS GT BURNER WITH HYDROGEN FLAME PILOTING OPERATED WITH SIMULATED EXHAUST GAS RECIRCULATION 12
EXPERIMENTAL ANALYSIS ON MICRO-CHANNELS WITH DIFFERENT CROSS-SECTIONAL SHAPES FOR INTERNAL COOLING APPLICATIONS 12
Development and Application of an Internal Heat-Transfer Measurement Technique for Cooled Real Engine Components 12
Development of Experimental and Numerical Methods for the Analysis of Active Clearance Control Systems 8
A NEW TEST FACILITY FOR INVESTIGATING LEAF-SEAL CAVITY INGESTION AT COMBUSTOR-TURBINE INTERFACE 8
Effect of Jet-to-Plate Temperature Ratio on Flow and Heat Transfer Features of Active Clearance Control Systems 8
Effect of Jet-to-Jet Distance and Pipe Position on Flow and Heat Transfer Features of Active Clearance Control Systems 7
Flow Check and Adiabatic Effectiveness Measurements on Traditionally Versus Additively Manufactured Film-Cooling Holes 7
Integration of Film Cooling in a Micro Rotating Detonation Combustor 6
Experimental Measurements of Ingress in a Turbine Stator-Rotor Cavity 6
Measurement of Internal Heat Transfer Distribution of Highly-Loaded Gas Turbine Blade by Combined Experimental/Numerical Method 6
Totale 14.783
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Categoria #
all - tutte 38.946
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 38.946
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202135 0 0 0 0 0 0 0 0 0 0 0 35
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
2025/20265.510 452 812 671 566 563 204 557 315 541 438 320 71
Totale 14.849