TARCHI, LORENZO
 Distribuzione geografica
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Continente #
NA - Nord America 1.824
EU - Europa 1.254
AS - Asia 243
AF - Africa 2
Continente sconosciuto - Info sul continente non disponibili 1
Totale 3.324
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Nazione #
US - Stati Uniti d'America 1.820
PL - Polonia 593
IT - Italia 200
IE - Irlanda 171
SE - Svezia 147
HK - Hong Kong 99
CN - Cina 69
GB - Regno Unito 41
FI - Finlandia 34
JO - Giordania 22
DE - Germania 20
UA - Ucraina 16
BE - Belgio 14
TR - Turchia 13
IN - India 10
VN - Vietnam 10
SG - Singapore 9
IR - Iran 7
FR - Francia 6
CA - Canada 4
NL - Olanda 4
AT - Austria 3
ES - Italia 3
KR - Corea 2
RU - Federazione Russa 2
EU - Europa 1
JP - Giappone 1
MU - Mauritius 1
SC - Seychelles 1
TH - Thailandia 1
Totale 3.324
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Città #
Warsaw 592
Fairfield 270
Chandler 206
Dublin 171
Cambridge 129
Woodbridge 129
Seattle 123
Ashburn 121
Ann Arbor 102
Houston 101
Wilmington 101
Florence 85
Altamura 66
Lawrence 61
Hong Kong 60
Princeton 45
Buffalo 42
Beijing 30
Medford 30
Jacksonville 27
Boardman 24
Boston 22
Shanghai 20
Kent 17
Brussels 13
Izmir 13
San Diego 11
Dong Ket 10
Prato 8
Singapore 8
Falls Church 7
Harbin 6
Norwalk 6
Redwood City 6
London 5
Phoenix 5
Carpi 4
Duncan 4
New York 4
Tehran 4
Falkensee 3
Hounslow 3
Meudon 3
Scandicci 3
Toronto 3
Vienna 3
Andover 2
Changsha 2
Chiswick 2
Hangzhou 2
Hillsboro 2
Los Angeles 2
Luft 2
Madrid 2
Mugnano di Napoli 2
Nanjing 2
Pordenone 2
San Casciano Val Di Pesa 2
Stonehaven 2
Storrs Mansfield 2
Tong 2
Wigan 2
Auburn Hills 1
Bergamo 1
Boltenhagen 1
Campomorone 1
Capannori 1
Cedar Knolls 1
Chicago 1
Cranfield 1
Deux-montagnes 1
Frankfurt Am Main 1
Frankfurt am Main 1
Gdansk 1
Genova 1
Kilburn 1
La Verriere 1
Laurel 1
Leawood 1
Marseille 1
Milan 1
Montepulciano 1
Rignano Sull'arno 1
Rotterdam 1
Salerno 1
Saronno 1
Sesto Fiorentino 1
Songkhla 1
Stabroek 1
Tappahannock 1
Torino 1
Zhengzhou 1
Totale 2.768
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Nome #
Experimental Evaluation of the Density Ratio Effects on the Cooling Performance of a Combined Slot/Effusion Combustor Cooling System 210
DENSITY RATIO EFFECTS ON THE COOLING PERFORMANCES OF A COMBUSTOR LINER COOLED BY A COMBINED SLOT/ EFFUSION SYSTEM 209
Experimental Investigation of Innovative Internal Trailing Edge Cooling Configurations with Pentagonal Arrangement and Elliptic Pin Fin 208
Heat Transfer and Pressure Loss Measurements of Matrix Cooling Geometries for Gas Turbine Airfoils 186
Experimental investigation of a leading edge cooling system with optimized inclined racetrack holes 175
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON WINDAGE POWER LOSSES IN HIGH SPEED GEARS 117
Experimental and Numerical Analysis of Multiple Impingement Jet Arrays for an Active Clearance Control System 111
Experimental and numerical investigation on windage power losses in high speed gears 106
Heat Transfer Measurements in a Leading Edge Geometry With Racetrack Holes and Film Cooling Extraction 98
Full aerothermal combustor turbine interaction research 93
Numerical and Experimental Investigation of Turning Flow Effects on Innovative Pin Fin Arrangements for Trailing Edge Cooling Configurations 92
Experimental and Theoretical Investigation of Thermal Effectiveness in Multiperforated Plates for Combustor Liner Effusion Cooling 85
Experimental Survey on Heat Transfer In A Trailing Edge Cooling System: Effects of Rotation In Internal Cooling Ducts 84
Correlative Analysis Of Effusion Cooling Systems 82
Adiabatic And Overall Effectiveness Measurements Of An Effusion Cooling Array For Turbine Endwall Application 81
Performance Improvement of a Heavy Duty GT: Adiabatic Effectiveness Measurements on First Stage Vanes in Representative Engine Conditions 80
Heat transfer and pressure drop measurements on rotating matrix cooling geometries for airfoil trailing edges 78
Application of the inverse analysis for boundary condition retrieval 77
EXPERIMENTAL AND NUMERICAL ANALYSIS OF MULTIPLE IMPINGEMENT JET ARRAYS FOR AN ACTIVE CLEARANCE CONTROL SYSTEM 74
Heat Transfer Measurements in a leading Edge Geometry with racetrack Holes and Film Cooling Extraction 70
Experimental Investigation on the Effects of a Large Recirculating Area on the Performance of an Effusion Cooled Combustor Liner 69
Investigation of innovative trailing edge cooling configurations with enlarged pedestals and square or semicircular ribs. part 1 - experimental results 67
HEAT TRANSFER PERFORMANCE OF FAN-SHAPED FILM COOLING HOLES.PART I: EXPERIMENTAL ANALYSIS 67
Development of an engine representative combustor simulator dedicated to hot streak generation 66
Combined use of turbulators and enlarged pedestals in trailing edge cooling systems: an experimental and numerical analysis 60
Heat transfer and friction in circular ducts with shaped ribs 56
Flowfield and heat transfer analysis of a gas turbine trailing edgecooling configuration 55
INVESTIGATION OF CIRCULAR AND SHAPED EFFUSION COOLING ARRAYS FOR COMBUSTOR LINER APPLICATION - PART 1: EXPERIMENTAL ANALYSIS 54
Experimental and Numerical Calculation of Turbulent Timescales at the Exit of an Engine Representative Combustor Simulator 50
HEAT TRANSFER MEASUREMENTS AND EFFECTS OF ROTATION IN A TRAILING EDGE COOLING SYSTEM 48
Experimental Investigation Of Turning Flow Effects On Innovative Trailing Edge Cooling Configurations Based On Circular And Oblong Pin Fins 46
Experimental Investigation Of Turning Flow Effects On Innovative Trailing Edge Cooling Configurations With Enlarged Pedestals And Square Or Semicircular Ribs”. 45
MEASUREMENTS OF THE COOLING PERFORMANCES OF A REAL COMBUSTOR LINER WITH AIR AND CO2 INJECTION THROUGH A SLOT AND AN ARRAY OF EFFUSION COOLING HOLES 42
FLOWFIELD AND TEMPERATURE PROFILES MEASUREMENTS ON A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION 41
Hole spacing effect on adiabatic effectiveness of effusion cooling arrays for turbine endwall application: Experimental and numerical analysis 40
Experimental Investigation on Power Losses due to Oil Jet Lubrication in High Speed Gearing Systems 40
Windage Losses of a Meshing Gear Pair Measured at Different Working Conditions 40
EXPERIMENTAL SURVEY ON HEAT TRANSFER IN AN INTERNAL CHANNEL OF A TRAILING EDGE COOLING SYSTEM 39
Endwall Effusion Cooling System Behaviour Within a High-Pressure Turbine Cascade: Part 2—Heat Transfer and Effectiveness Measurements 37
Experimental investigation on the effects of shaped ribs in circular ducts 33
TURBULENCE FIELD MEASUREMENTS AT THE EXIT OF A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION 29
Numerical and experimental investigation of a combustor simulator dedicated to hot streak generation 27
Totale 3.367
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Categoria #
all - tutte 9.791
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 9.791
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020702 65 56 16 65 83 82 72 84 68 45 56 10
2020/2021408 44 44 20 43 33 30 21 38 40 44 29 22
2021/2022339 17 27 36 8 14 12 10 29 10 4 89 83
2022/2023814 70 168 36 71 65 140 95 48 94 8 17 2
2023/2024263 18 31 47 7 10 23 12 66 6 1 29 13
2024/202518 18 0 0 0 0 0 0 0 0 0 0 0
Totale 3.367