PICCHI, ALESSIO
 Distribuzione geografica
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Continente #
NA - Nord America 5.184
EU - Europa 3.665
AS - Asia 3.163
SA - Sud America 475
AF - Africa 67
OC - Oceania 51
Continente sconosciuto - Info sul continente non disponibili 3
Totale 12.608
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Nazione #
US - Stati Uniti d'America 5.129
RU - Federazione Russa 1.393
CN - Cina 951
SG - Singapore 773
IT - Italia 736
HK - Hong Kong 592
PL - Polonia 576
BR - Brasile 396
KR - Corea 319
IE - Irlanda 252
SE - Svezia 207
VN - Vietnam 195
DE - Germania 121
FI - Finlandia 116
IN - India 108
GB - Regno Unito 65
JO - Giordania 60
FR - Francia 51
AU - Australia 50
AR - Argentina 38
ID - Indonesia 34
NL - Olanda 34
AT - Austria 33
CA - Canada 30
JP - Giappone 21
TR - Turchia 19
BD - Bangladesh 17
ES - Italia 17
IQ - Iraq 17
UA - Ucraina 17
BE - Belgio 14
IR - Iran 14
MX - Messico 14
ZA - Sudafrica 14
EC - Ecuador 12
MA - Marocco 11
CH - Svizzera 10
CO - Colombia 9
PK - Pakistan 8
CI - Costa d'Avorio 7
DZ - Algeria 7
BJ - Benin 6
KE - Kenya 6
DO - Repubblica Dominicana 5
PY - Paraguay 5
UZ - Uzbekistan 5
VE - Venezuela 5
AE - Emirati Arabi Uniti 4
CL - Cile 4
EG - Egitto 4
PH - Filippine 4
RS - Serbia 4
TN - Tunisia 4
EU - Europa 3
NP - Nepal 3
PE - Perù 3
PT - Portogallo 3
RO - Romania 3
SA - Arabia Saudita 3
TW - Taiwan 3
AZ - Azerbaigian 2
GT - Guatemala 2
HU - Ungheria 2
KZ - Kazakistan 2
LT - Lituania 2
LU - Lussemburgo 2
LV - Lettonia 2
MD - Moldavia 2
NG - Nigeria 2
SN - Senegal 2
TH - Thailandia 2
UY - Uruguay 2
AL - Albania 1
AM - Armenia 1
BH - Bahrain 1
BO - Bolivia 1
BW - Botswana 1
CG - Congo 1
CR - Costa Rica 1
EE - Estonia 1
GR - Grecia 1
HN - Honduras 1
KH - Cambogia 1
KN - Saint Kitts e Nevis 1
LA - Repubblica Popolare Democratica del Laos 1
MU - Mauritius 1
MY - Malesia 1
OM - Oman 1
PA - Panama 1
QA - Qatar 1
TG - Togo 1
TO - Tonga 1
Totale 12.608
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Città #
Santa Clara 1.779
Singapore 618
Warsaw 570
Hong Kong 522
Ashburn 457
Fairfield 359
Hefei 315
Seoul 303
Dublin 252
Florence 215
Woodbridge 195
Beijing 189
Seattle 168
Chandler 156
Houston 151
Cambridge 150
Wilmington 137
San Jose 94
Ann Arbor 83
Altamura 81
Buffalo 81
Lawrence 72
Ho Chi Minh City 70
Moscow 67
Helsinki 62
Princeton 57
Kent 56
Prato 55
Los Angeles 54
Munich 51
Melbourne 46
Shanghai 45
Milan 42
Mumbai 41
Hanoi 36
Boston 33
Medford 33
Vienna 31
New York 30
Dallas 29
Chicago 28
Turku 27
São Paulo 24
Paris 23
Bengaluru 22
Falls Church 21
San Diego 21
Jakarta 18
Boardman 16
Clifton 16
Dong Ket 16
Frankfurt am Main 16
Redwood City 16
Rio de Janeiro 16
Scandicci 16
London 14
Tokyo 14
Dearborn 13
Redondo Beach 13
Tong 13
Brussels 11
Falkenstein 11
Chennai 10
Haiphong 10
Rome 10
The Dalles 10
Belo Horizonte 9
Genova 9
Guangzhou 9
Jacksonville 9
Modena 9
Montreal 9
Norwalk 9
Ottawa 9
Porto Alegre 9
Stockholm 9
Barcelona 8
Brasília 8
Johannesburg 8
Lappeenranta 8
Orem 8
Phoenix 8
Pune 8
Salvador 8
West Jordan 8
Yubileyny 8
Abidjan 7
Bergamo 7
Brooklyn 7
Comun Nuovo 7
Council Bluffs 7
Curitiba 7
Denver 7
Toulouse 7
Xi'an 7
Andover 6
Biên Hòa 6
Changsha 6
Cotonou 6
Da Nang 6
Totale 8.473
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 384
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 337
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 311
Experimental Investigations of Effusion Cooling Systems for Lean Burn Aero-Engine Combustors 309
Film-cooling adiabatic effectiveness measurements on a real high pressure turbine blade 274
Aero-thermal flow characterization downstream of an NGV cascade by five-hole probe and filtered Rayleigh scattering measurements 209
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 192
Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 190
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 187
Effusion cooling system optimization for modern lean burn combustor 185
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 184
Adiabatic effectiveness on high-pressure turbine nozzle guide vanes under realistic swirling conditions 183
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 182
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 180
Experimental Investigation of Swirl and Flow Structure Inside a Rotor-Stator Cavity 180
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 179
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 179
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 178
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 177
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 177
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 176
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 174
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 167
Improving emission and blow-out characteristics of novel natural gas low NOx burners for heavy duty gas turbine 165
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 164
Effect of slot injection and effusion array on the liner heat transfer coefficient of a scaled lean burn combustor with representative swirling flow 163
Performance Improvement of a Heavy Duty GT: Adiabatic Effectiveness Measurements on First Stage Vanes in Representative Engine Conditions 161
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 160
Commissioning of a Newly Designed Experimental Facility for Hot Gas Ingestion Investigation 159
Adiabatic effectiveness on high pressure turbine nozzle guide vanes under realistic swirling conditions 158
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 157
Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow 154
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 152
Development and Application of a Concentration Probe for Mixing Flows Tracking in Turbomachinery Applications 152
Experimental Characterization of a Micro-Turbine Generator for Energy Recovery Applications 152
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 151
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 151
Experimental and Theoretical Investigation of Thermal Effectiveness in Multiperforated Plates for Combustor Liner Effusion Cooling 151
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 151
A new test facility for investigating thermal behaviour of effusion cooling test plates for rql combustors 149
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 147
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 147
Comparison of psp and tlc steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 146
DEVELOPMENT AND APPLICATION OF A CONCENTRATION PROBE FOR MIXING FLOWS TRACKING IN TURBOMACHINERY APPLICATIONS 145
Experimental Assessment of Correlative Approaches for the Prediction of Leakage Flow through Labyrinth Seals 143
Film cooling adiabatic effectiveness measurements of pressure side trailing edge cooling configurations 143
Development of experimental and numerical methods for the analysis of active clearance control systems 142
On the Use of PSP to Determine the Rim Sealing Effectiveness 142
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness 140
Flat plate and turbine vane film-cooling performance with laid-back fan-shaped holes 140
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 138
Heat Transfer Coefficient and Adiabatic Effectiveness on a Film-Cooled Pressure Side: Results and Assessment of the IR-Based Measurement Technique Reliability 136
Experimental and theoretical investigation of thermal effectiveness in multi-perforated plates for combustor liner effusion cooling 136
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 135
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 135
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 132
Measurement of internal heat transfer distributions using transient infrared thermography 131
Turbulence intensity measurements across a NGV cooled cascade with representative lean burn combustor outflow 130
Heat Transfer Coefficient and Adiabatic Effectiveness Measurements on a Nozzle Guide Vane With a Single Row of Cylindrical Holes 129
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 129
Effect of rotation and hole arrangement in cold bridge-type impingement cooling systems 129
Effect of Coolant Extraction on Cold Side Heat Transfer Enhancement of an Effusion Cooling Plate 129
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 128
Swirling main flow effects on film cooling: Time resolved adiabatic effectiveness measurements in a gas turbine combustor model 126
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 126
Analysis of swirl number effects on effusion flow behaviour using time resolved PIV 126
Analysis of Swirl Number Effects on Effusion Flow Behavior Using Time-Resolved Particle Image Velocimetry 126
Evaluation of Cooling Requirements for Rotating Detonation Combustors 123
Flow Field and Hot Streak Migration Through High Pressure Cooled Vanes With Representative Lean Burn Combustor Outflow 122
Heat transfer measurements in leading-edge cooling geometry under rotating conditions 120
Experimental characterization of an industrial burner operated with simulated EGR 118
ASSESSMENT OF ADDITIVE MANUFACTURED MICRO-CHANNEL CHARACTERISTICS: IMPACT OF HYDRAULIC DIAMETER EVALUATION 115
APPLICATION OF INTERNAL HEAT TRANSFER INVERSE PROBLEM SOLUTION METHOD TO JET ARRAY IMPINGEMENT COOLING SYSTEM 114
TURBULENCE FIELD MEASUREMENTS AT THE EXIT OF A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION 114
Combustion Diagnostics and Emissions Measurements of a Novel Low NOx Burner for Industrial Gas Turbine Operated With CO2 Diluted Methane/Air Mixtures 112
Comparison of Rim Sealing Effectiveness in Different Geometrical Configurations 112
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 109
Effect of Jet-to-Jet Distance and Pipe Position on Flow and Heat Transfer Features of Active Clearance Control Systems 108
Heat transfer measurements in a leading edge cooling geometry under rotating conditions 108
Assessment of Additive Manufactured Micro-Channel Characteristics: Impact of Hydraulic Diameter Evaluation 83
Impact of Target Surface Building Direction on the Heat Transfer Characteristics of Additive Manufactured Impingement Systems 80
Totale 12.738
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Categoria #
all - tutte 33.875
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 33.875
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021336 0 0 0 0 0 0 55 39 90 74 43 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
2025/20263.399 452 812 671 566 563 204 131 0 0 0 0 0
Totale 12.738