INNOCENTI, LUCA
 Distribuzione geografica
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Continente #
EU - Europa 1.039
NA - Nord America 972
AS - Asia 200
AF - Africa 1
Continente sconosciuto - Info sul continente non disponibili 1
SA - Sud America 1
Totale 2.214
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Nazione #
US - Stati Uniti d'America 969
PL - Polonia 326
IT - Italia 244
IE - Irlanda 118
SE - Svezia 96
UA - Ucraina 82
CN - Cina 60
RU - Federazione Russa 59
DE - Germania 44
HK - Hong Kong 40
FI - Finlandia 33
SG - Singapore 28
TR - Turchia 28
GB - Regno Unito 26
JO - Giordania 21
IR - Iran 11
VN - Vietnam 6
BE - Belgio 4
CA - Canada 3
FR - Francia 3
KR - Corea 3
CH - Svizzera 2
JP - Giappone 2
NL - Olanda 2
CL - Cile 1
DZ - Algeria 1
EU - Europa 1
IN - India 1
Totale 2.214
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Città #
Warsaw 324
Chandler 128
Dublin 118
Fairfield 109
Jacksonville 91
Wilmington 54
Seattle 52
Ashburn 50
Cambridge 50
Woodbridge 47
Florence 35
Houston 33
Ann Arbor 31
Princeton 31
Altamura 27
Buffalo 27
Lawrence 27
Izmir 26
Beijing 21
Boston 20
Singapore 19
Hong Kong 18
Shanghai 17
Boardman 13
Prato 11
Medford 10
Milan 9
Falls Church 8
Dong Ket 6
Helsinki 6
Kent 6
Rome 6
Norwalk 5
San Diego 5
Turin 5
Brussels 4
Ferrara 4
Harbin 4
Naples 4
Santa Marinella 4
Bologna 3
Comun Nuovo 3
Figline Valdarno 3
London 3
Mozzanica 3
Pavia 3
Saint Petersburg 3
Seodaemun-gu 3
Seriate 3
Southfield 3
Xian 3
Aberdeen 2
Anghiari 2
Belmonte Mezzagno 2
Casavatore 2
Caserta 2
Catania 2
Como 2
Genova 2
Hounslow 2
Issiglio 2
Los Angeles 2
Mikolow 2
Moscow 2
Ozzano dell'Emilia 2
Phoenix 2
Reading 2
Redwood City 2
Rovescala 2
San Giuliano Milanese 2
Toronto 2
Aprilia 1
Arezzo 1
Bari 1
Brescia 1
Chennai 1
Chiari 1
Dalmine 1
Dearborn 1
Delft 1
Duncan 1
Eboli 1
Empoli 1
Eskişehir 1
Foggia 1
Frankfurt Am Main 1
Gatchina 1
Ghedi 1
Guangzhou 1
Guglionesi 1
Hillsboro 1
Lausanne 1
Messina 1
Modena 1
Montalcino 1
Ottawa 1
Pisa 1
Porto Torres 1
Reggio Nell'emilia 1
Remetschwil 1
Totale 1.567
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Nome #
Some Improvements in a Gas Turbine Stator-Rotor Systems Core-Swirl Ratio Correlation 220
Heat Transfer and Pressure Loss Measurements of Matrix Cooling Geometries for Gas Turbine Airfoils 186
L'UTILIZZO DEI PROMOTORI DI TURBOLENZA IN GEOMETRIE DI TURBOMACCHINA: VALUTAZIONI GLOBALI DI SCAMBIO TERMICO E PERDITE DI CARICO 171
HEAT TRANSFERT AND PRESSURE DROP EVALUATION IN THIN WEDGE-SHAPED TRAILING EDGE 157
A Rotor Blade Cooling improvement for Heavy Duty Gas Turbine Using Steam and Mixed Steam/Air Cooling 104
"DESIGN CRITERIA FOR RIBBED CHANNELS: EXPERIMENTAL INVESTIGATION AND THEORETICAL ANALYSIS", 97
EVALUATION AND COMPARISON OF DIFFERENT BLADE COOLING SOLUTIONS TO IMPROVE COOLING EFFICIENCY AND GAS TURBINE PERFORMANCES 92
BLADE COOLING IMPROVEMENT FOR HEAVY DUTY GAS TURBINE: THE AIR COOLANT TEMPERATURE REDUCTION AND THE INTRODUCTION OF STEAM AND MIXED/AIR COOLING 91
Heat transfer and pressure drop measurements on rotating matrix cooling geometries for airfoil trailing edges 81
Analysis of gas turbine rotating cavities by a one-dimensional model: Definition of a new discs fiction coefficients correlations set 78
Flat Plate Honeycomb Seals Friction Factor Analysis 78
Flat Plate Honeycomb Seals Friction Factor Analysis 76
Conjugate Heat Transfer Calculations on GT Rotor Blade for Industrial Applications. Part I: Equivalent Internal Fluid Network Setup and Procedure Description 75
Preliminary Evaluation Of Turbulence Level Influence In Heat Transfer Measurements 70
PNEUMA - PNEUMATIC UNINTERRUPTIBLE MACHINE: UN SISTEMA DI BACKUP AD ARIA COMPRESSA 70
MEASUREMENT AND SIMULATION OF A TRANSONIC INNOVATIVE COOLING SYSTEM (ICS) FOR HIGHT-TEMPERATURE TRANSONIC GAS TURBINE STAGES 59
PNEUMA, PNEUMATIC UNINTERRUPTIBLE MACHINE SYSTEM: AN UNINTERRUPTIBLE PNEUMATIC POWER GENERATOR. PART 1: TECHNICAL ANALYSIS OF A COMPRESSED AIR BASED POWER BACKUP SYSTEM 53
VALUTAZIONE E COMPARAZIONE DI DIFFERENTI SOLUZIONI PER IL MIGLIORAMENTO DELL'EFFICIENZA DEL RAFFREDDAMENTO PALARE E DELLE PRESTAZIONI DI UNA BUONA TURBINA A GAS 48
Flat plate honeycomb seals acoustic analysis 48
L'APPLICAZIONE DEI CRISTALLI LIQUIDI NELLO STUDIO DELLO SCAMBIO TERMICO IN COMPONENTI DI MACCHINE 47
Effetti della riduzione della temperatura dell'aria di raffreddamento nelle palettature refrigerate in turbine a gas heavy-duty 47
INTEGRATION OF ENVIRONMENTAL PARAMETERS INTO DECISION MAKING WITHIN THE PNEUMA PROJECT 47
EXPERIMENTAL STUDIES ON TURBOLENCE BEHIND POROUS FOAMS 46
REFROIDISSEMENT DES TURBINE A GAZ Techniques et efficacitè 44
UTILISATION DES CALODUCS POUR LE REFROIDISSEMENT DES AUBAGES DISTRIBUTEURS DE TURBINES A GAZ 43
HEAT TRANSFERT ANALYSIS IN A MODERN DLN COMBUSTOR 41
EXPERIMENTAL INVESTIGATION ON LEAKAGE LOSS AND HEAT TRANSFER IN ASTRAIGHT THROUGH LABYRINTH SEAL 41
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements 9
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness 9
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 7
On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 5
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 2.255
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Categoria #
all - tutte 6.366
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 6.366
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020363 0 36 11 39 38 47 32 54 28 29 46 3
2020/2021285 28 16 31 36 11 32 10 30 21 27 11 32
2021/2022225 12 12 16 3 20 12 6 16 6 8 68 46
2022/2023538 42 72 28 39 54 101 61 36 79 7 11 8
2023/2024191 10 29 25 11 9 17 16 28 0 3 33 10
2024/202572 51 21 0 0 0 0 0 0 0 0 0 0
Totale 2.255