PICCHI, ALESSIO
 Distribuzione geografica
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Continente #
NA - Nord America 2.372
EU - Europa 1.835
AS - Asia 524
AF - Africa 6
Continente sconosciuto - Info sul continente non disponibili 3
OC - Oceania 2
Totale 4.742
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Nazione #
US - Stati Uniti d'America 2.364
PL - Polonia 563
IT - Italia 539
IE - Irlanda 252
CN - Cina 204
SE - Svezia 198
HK - Hong Kong 128
RU - Federazione Russa 114
JO - Giordania 59
SG - Singapore 58
GB - Regno Unito 33
AT - Austria 31
DE - Germania 28
IN - India 26
FI - Finlandia 22
VN - Vietnam 19
CH - Svizzera 10
FR - Francia 10
ES - Italia 9
TR - Turchia 9
BE - Belgio 8
CA - Canada 8
IR - Iran 7
UA - Ucraina 7
JP - Giappone 6
KR - Corea 5
EU - Europa 3
NL - Olanda 3
TW - Taiwan 3
AU - Australia 2
DZ - Algeria 2
MD - Moldavia 2
NG - Nigeria 2
RO - Romania 2
RS - Serbia 2
LT - Lituania 1
LU - Lussemburgo 1
MU - Mauritius 1
ZA - Sudafrica 1
Totale 4.742
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Città #
Warsaw 562
Fairfield 359
Dublin 252
Ashburn 220
Woodbridge 195
Seattle 167
Florence 165
Chandler 156
Cambridge 150
Houston 144
Wilmington 137
Beijing 86
Ann Arbor 83
Altamura 81
Hong Kong 72
Lawrence 72
Princeton 57
Buffalo 47
Prato 47
Singapore 46
Shanghai 41
Medford 33
Moscow 31
Vienna 31
Boston 30
Kent 28
Milan 28
Falls Church 21
San Diego 20
Boardman 16
Dong Ket 16
Redwood City 16
New York 14
Scandicci 14
Dearborn 13
Tong 13
Genova 9
Norwalk 9
Barcelona 8
West Jordan 8
Brussels 7
Comun Nuovo 7
London 7
Pune 7
Andover 6
Guangzhou 6
Hillsboro 6
Jacksonville 6
Bergamo 5
Carpi 5
Duncan 5
Montreal 5
Bari 4
Bern 4
Bristol 4
Cagliari 4
Chennai 4
Chicago 4
Harbin 4
Lappeenranta 4
Los Angeles 4
Modena 4
Nanjing 4
Osimo 4
Ponte San Pietro 4
Prad am Stilfser Joch 4
Rome 4
Salerno 4
Assemini 3
Kurita 3
Parma 3
Phoenix 3
Raleigh 3
Remetschwil 3
Sanayi 3
Saronno 3
Southfield 3
Toronto 3
Anglet 2
Anguillara Sabazia 2
Arezzo 2
Baesweiler 2
Barletta 2
Bengaluru 2
Berlin 2
Bremen 2
Capannori 2
Castelleone 2
Changsha 2
Correggio 2
Höst 2
Isfahan 2
Kochi 2
Laurel 2
Luft 2
Melbourne 2
Oxford 2
Pisa 2
Pontedera 2
Reggio Emilia 2
Totale 3.707
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Nome #
Experimental and CFD analyses of a highly-loaded gas turbine blade 295
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 258
Effusion Cooling Plates for Combustor Liners: Experimental and Numerical Investigations on the Effect of Density Ratio 237
Experimental Investigations of Effusion Cooling Systems for Lean Burn Aero-Engine Combustors 228
Film-cooling adiabatic effectiveness measurements on a real high pressure turbine blade 158
Adiabatic Effectiveness and Flow Field Measurements in a Realistic Effusion Cooled Lean Burn Combustor 117
Unsteady computational fluid dynamics investigation of effusion cooling process in a lean burn aero-engine combustor 114
Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor with Representative Swirling Flow 112
Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor 106
Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes 105
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 99
Experimental Investigation of Swirl and Flow Structure Inside a Rotor-Stator Cavity 98
Aero-thermal flow characterization downstream of an NGV cascade by five-hole probe and filtered Rayleigh scattering measurements 97
Effect of slot injection and effusion array on the liner heat transfer coefficient of a scaled lean burn combustor with representative swirling flow 93
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 89
Unsteady flow field characterization of effusion cooling systems with swirling main flow: Comparison between cylindrical and shaped holes 88
Effusion cooling system optimization for modern lean burn combustor 88
Unsteady cfd investigation of effusion cooling process in a lean burn aero-engine combustor 87
Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 87
Experimental and Theoretical Investigation of Thermal Effectiveness in Multiperforated Plates for Combustor Liner Effusion Cooling 86
Performance Improvement of a Heavy Duty GT: Adiabatic Effectiveness Measurements on First Stage Vanes in Representative Engine Conditions 81
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 81
Experimental and numerical investigations of novel natural gas low NOx burners for heavy duty gas turbine 78
Time-Resolved flow field analysis of effusion cooling system with representative swirling main flow 76
Adiabatic effectiveness on high-pressure turbine nozzle guide vanes under realistic swirling conditions 75
Experimental Characterization of a Micro-Turbine Generator for Energy Recovery Applications 74
Experimental and theoretical investigation of thermal effectiveness in multi-perforated plates for combustor liner effusion cooling 74
Adiabatic effectiveness on high pressure turbine nozzle guide vanes under realistic swirling conditions 74
Effect of holes arrangement on heat transfer in impingement/effusion cooling double wall schemes 72
Improving emission and blow-out characteristics of novel natural gas low NOx burners for heavy duty gas turbine 71
Comparison of psp and tlc steady state techniques for adiabatic effectiveness measurement on a multiperforated plate 67
Effect of rotation and hole arrangement in cold bridge-type impingement cooling systems 67
Flat plate and turbine vane film-cooling performance with laid-back fan-shaped holes 65
Film cooling adiabatic effectiveness measurements of pressure side trailing edge cooling configurations 64
Turbulence intensity measurements across a NGV cooled cascade with representative lean burn combustor outflow 63
Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio 59
DEVELOPMENT AND APPLICATION OF A CONCENTRATION PROBE FOR MIXING FLOWS TRACKING IN TURBOMACHINERY APPLICATIONS 56
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 52
Heat transfer measurements in leading-edge cooling geometry under rotating conditions 50
Experimental & numerical investigation of the mutual interaction between liner film cooling & combustor swirl flow 49
Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes with Representative Lean Burn Combustor Outflow 48
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 47
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 47
Analysis of swirl number effects on effusion flow behaviour using time resolved PIV 46
Heat transfer measurements in a leading edge cooling geometry under rotating conditions 45
Effect of Coolant Extraction on Cold Side Heat Transfer Enhancement of an Effusion Cooling Plate 45
Measurement of internal heat transfer distributions using transient infrared thermography 45
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 43
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 38
Analysis of Swirl Number Effects on Effusion Flow Behavior Using Time-Resolved Particle Image Velocimetry 38
TURBULENCE FIELD MEASUREMENTS AT THE EXIT OF A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION 32
Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow 31
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 30
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 28
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 27
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 26
Experimental Assessment of Correlative Approaches for the Prediction of Leakage Flow through Labyrinth Seals 26
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 24
A new test facility for investigating thermal behaviour of effusion cooling test plates for rql combustors 23
Development and Application of a Concentration Probe for Mixing Flows Tracking in Turbomachinery Applications 23
Swirling main flow effects on film cooling: Time resolved adiabatic effectiveness measurements in a gas turbine combustor model 22
Heat Transfer Coefficient and Adiabatic Effectiveness on a Film-Cooled Pressure Side: Results and Assessment of the IR-Based Measurement Technique Reliability 19
Development of experimental and numerical methods for the analysis of active clearance control systems 18
Effect of Jet-to-Jet Distance and Pipe Position on Flow and Heat Transfer Features of Active Clearance Control Systems 18
Flow Field and Hot Streak Migration Through High Pressure Cooled Vanes With Representative Lean Burn Combustor Outflow 13
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 9
Heat Transfer Coefficient and Adiabatic Effectiveness Measurements on a Nozzle Guide Vane With a Single Row of Cylindrical Holes 9
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness 9
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 7
On the Use of PSP to Determine the Rim Sealing Effectiveness 5
Design Procedure of a Rotating Cavity Rig for Hot Gas Ingestion Investigation 5
Commissioning of a Newly Designed Experimental Facility for Hot Gas Ingestion Investigation 4
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 1
Totale 4.841
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Categoria #
all - tutte 16.277
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 16.277
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020810 0 43 19 51 86 84 144 113 100 65 75 30
2020/2021693 31 52 14 72 130 58 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
2024/2025178 136 42 0 0 0 0 0 0 0 0 0 0
Totale 4.841