INSINNA, MASSIMILIANO
 Distribuzione geografica
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Continente #
NA - Nord America 1.148
EU - Europa 835
AS - Asia 242
OC - Oceania 3
AF - Africa 1
Continente sconosciuto - Info sul continente non disponibili 1
Totale 2.230
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Nazione #
US - Stati Uniti d'America 1.142
PL - Polonia 394
IT - Italia 172
CN - Cina 105
IE - Irlanda 99
SE - Svezia 59
HK - Hong Kong 52
SG - Singapore 39
RU - Federazione Russa 29
JO - Giordania 24
FI - Finlandia 19
GB - Regno Unito 19
BE - Belgio 13
FR - Francia 9
UA - Ucraina 8
VN - Vietnam 8
IN - India 7
CA - Canada 6
DE - Germania 5
JP - Giappone 5
ES - Italia 4
AU - Australia 3
CH - Svizzera 3
RS - Serbia 2
EU - Europa 1
IR - Iran 1
MU - Mauritius 1
TR - Turchia 1
Totale 2.230
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Città #
Warsaw 394
Fairfield 210
Woodbridge 116
Dublin 99
Seattle 86
Ashburn 80
Florence 78
Cambridge 76
Chandler 70
Houston 67
Ann Arbor 66
Wilmington 59
Beijing 47
Altamura 35
Lawrence 34
Princeton 34
Hong Kong 28
Singapore 26
Shanghai 17
Medford 13
Boston 12
Harbin 11
Brussels 10
Kent 10
San Diego 9
Buffalo 8
Dong Ket 8
Falls Church 6
Boardman 5
Central 5
Scandicci 5
Barcelona 4
Cagliari 4
Guangzhou 4
Milan 4
Norwalk 4
Redwood City 4
Bern 3
Detroit 3
Melbourne 3
Ottawa 3
Phoenix 3
Prato 3
Rui'an 3
Tong 3
Toronto 3
Toulouse 3
Bagno a Ripoli 2
Belgrade 2
Dearborn 2
Hillsboro 2
London 2
New York 2
Prad am Stilfser Joch 2
Ravenna 2
Redmond 2
Rome 2
Spoleto 2
Wigan 2
Wilsonville 2
Xian 2
Absecon 1
Andover 1
Bethesda 1
Bordes 1
Boulder 1
Bruges 1
Brugherio 1
Catania 1
Cecina 1
Cerreto Guidi 1
Changsha 1
Chennai 1
Chiusi 1
Comun Nuovo 1
Dallas 1
Dongyang 1
Genova 1
Grevenbroich 1
Hefei 1
Hounslow 1
Izmir 1
Jacksonville 1
Larciano 1
Lastra a Signa 1
Laurel 1
Longmont 1
Montecchio Maggiore 1
Napoli 1
Nürnberg 1
Paderno Dugnano 1
Palermo 1
Rignano Sull'arno 1
Romano Di Lombardia 1
Salerno 1
Samara 1
San Mateo 1
Stevenage 1
Tappahannock 1
Tokyo 1
Totale 1.845
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Nome #
Investigation of the Aero-Thermal Aspects of Combustor/Turbine Interaction in Gas Turbines 228
On the Effect of an Aggressive Inlet Swirl Profile on the Aero-thermal Performance of a Cooled Vane 226
On the CFD Analysis of a Stratified Taylor-Couette System Dedicated to the Fabrication of Nanosensors 166
Development of a One-Dimensional Model for the Prediction of Leakage Flows in Rotating Cavities Under Non-Uniform Tangential Pressure Distribution 125
Hybrid RANS-LES modeling of the aerothermal field in an annular hot streak generator for the study of combustor-turbine interaction 119
Conjugate Heat Transfer Analysis of a Film Cooled High-Pressure Turbine Vane Under Realistic Combustor Exit Flow Conditions 112
Clocking effects of inlet nonuniformities in a fully cooled high-pressure vane: A conjugate heat transfer analysis 109
Analysis of Combustor/Vane Interaction with Decoupled and Loosely Coupled Approaches 104
Film Cooling Performance in a Transonic High-Pressure Vane: Decoupled Simulation and Conjugate Heat Transfer Analysis 103
Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors 101
Uncertainty Quantification and Stochastic Variations of Renewable Fuels 99
Aerodynamic Characterization of Conical Diffusers for Radial Turboexpanders Under Realistic Inlet Conditions 86
Optical fibre nanotips fabricated by a dynamic chemical etching for sensing applications 85
Hybrid rans-les modeling of the aero-Thermal field in an annular hot streak generator for the study of combustor-Turbine interaction 77
One-Dimensional Prediction and Three-Dimensional CFD Simulation of the Fluid Dynamics of Regenerative Pumps 74
Hybrid RANS-LES Modeling of a Hot Streak Generator Oriented to the Study of Combustor-Turbine Interaction 73
Simulation of Combustor/NGV Interaction Using Coupled RANS Solvers: Validation and Application to a Realistic Test Case 66
Effects of realistic inflow conditions on the aero-thermal performance of a film-cooled vane 60
Whispering Gallery Mode Aptasensors for Detection of Blood Proteins 58
Whispering Gallery Mode Aptasensors for Detection of Blood Proteins 57
Numerical Prediction of Cavitation Inception in Centrifugal Impellers 44
Numerical Analysis of Combustor/Vane Interaction 42
On the Effect of Inlet Swirl and Temperature Profiles on the Aero-Thermal Performance of a Heavily Film-Cooled Vane 37
Totale 2.251
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Categoria #
all - tutte 6.051
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 6.051
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020558 0 38 25 44 67 66 69 67 64 54 54 10
2020/2021260 23 30 8 38 12 22 16 20 30 31 16 14
2021/2022167 3 13 12 5 6 15 9 13 13 12 19 47
2022/2023435 52 82 24 20 30 63 58 14 62 6 18 6
2023/2024171 6 20 25 11 13 7 23 43 2 1 11 9
2024/202572 46 26 0 0 0 0 0 0 0 0 0 0
Totale 2.251