IRIS
CASARSA, Luca
 Distribuzione geografica
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Continente #
NA - Nord America 3.376
EU - Europa 1.046
AS - Asia 214
AF - Africa 5
Continente sconosciuto - Info sul continente non disponibili 4
Totale 4.645
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Nazione #
US - Stati Uniti d'America 3.360
UA - Ucraina 310
IT - Italia 235
DE - Germania 213
CN - Cina 154
FI - Finlandia 97
IE - Irlanda 54
TR - Turchia 39
GB - Regno Unito 35
FR - Francia 29
SE - Svezia 25
RU - Federazione Russa 21
CA - Canada 16
VN - Vietnam 14
BE - Belgio 13
PL - Polonia 10
TG - Togo 5
EU - Europa 4
JP - Giappone 3
AT - Austria 2
NL - Olanda 2
IN - India 1
KR - Corea 1
TH - Thailandia 1
TW - Taiwan 1
Totale 4.645
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Città #
Fairfield 403
Ann Arbor 383
Woodbridge 372
Houston 347
Chandler 268
Jacksonville 215
Ashburn 184
Seattle 178
Wilmington 176
Dearborn 122
Cambridge 118
Beijing 70
Udine 59
Princeton 58
Dublin 54
Izmir 39
Torre Del Greco 23
San Diego 20
Ogden 17
Blacksburg 15
Des Moines 15
Dong Ket 14
Brussels 13
Ottawa 13
Gorizia 12
Boardman 10
Hefei 10
Nanjing 10
Guangzhou 8
Trieste 8
Warsaw 8
Desio 7
Helsinki 7
Kunming 7
Jinan 6
Simi Valley 6
Codroipo 5
Fuzhou 5
Indiana 5
Lomé 5
Milan 5
Norwalk 5
Dallas 4
Duncan 4
Falls Church 4
Zhengzhou 4
Bochum 3
Chongqing 3
Grafing 3
Hackney 3
Mestre 3
Nanchang 3
New York 3
Pieris 3
Brescia 2
Chengdu 2
Hangzhou 2
Lublin 2
Padova 2
Redwood City 2
Rome 2
Ronchis 2
Santa Maria A Vico 2
Shanghai 2
Shaoxing 2
Sunnyvale 2
Tappahannock 2
Tokyo 2
Vienna 2
Wuhan 2
Ürümqi 2
Augusta 1
Bangkok 1
Bergamo 1
Bourg-la-reine 1
Castelfranco Veneto 1
Changsha 1
Chicago 1
Cividale del Friuli 1
Delft 1
Feltre 1
Frankfurt am Main 1
Gavardo 1
Groningen 1
Hebei 1
Langfang 1
London 1
Mirano 1
Montreal 1
Moscow 1
Múggia 1
Novokuznetsk 1
Palermo 1
Phoenix 1
Preganziol 1
Rezzato 1
Roncade 1
Rovellasca 1
Saint Petersburg 1
San Jose 1
Totale 3.408
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Nome #
Rotational effects on the flow field inside a leading edge impingement cooling passage 149
Effects of Rotation at Different Channel Orientations on the Flow Field inside a Trailing Edge Internal Cooling Channel 147
Experimental Investigation of the Effects of Blowing Conditions and Mach number on the Unsteady Behavior of Coolant Ejection through a Trailing Edge Cutback 141
Experimental assessment of the aero-thermal performance of rib roughened trailing edge cooling channels for gas turbine blades 128
Characterization of the velocity and heat transfer fields in an internal cooling channel with high blockage ratio 127
Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation 119
Effects of rotation and channel orientation on the flow field inside a trailing edge internal cooling channel 118
Flow field analysis inside a gas turbine trailing edge cooling channel under static and rotating conditions: Effect of ribs 116
Effects of injection conditions and Mach number on unsteadiness arising within coolant jets over a pressure side vane surface 113
Effects of rotation and buoyancy forces on the flow field behavior inside a triangular rib roughened channel 113
Rotating heat transfer measurements on a multi-pass internal cooling channel - II experimental tests 109
Flow field investigations in rotating facilities by means of stationary PIV systems 108
Flow field analysis inside a gas turbine trailing edge cooling channel under static and rotating conditions 108
Rotating heat transfer measurements on a multi-pass internal cooling channel - I rig development 106
Effect of rotation on a gas turbine blade internal cooling system: Experimental investigation 106
Numerical aero-thermal analysis of a rib-roughened trailing edge cooling channel at different rotation numbers and channel orientations 105
Flow field inside a leading edge cooling channel with turbulence promoters in rotating conditions 103
Experimental investigation of the interaction between showerhead coolant jets and main flow 103
Buoyancy effects at high rotation number on the flow field inside a triangular shaped rib roughened channel 103
Low Reynolds number flow in rectangular cooling channels provided with low aspect ratio pin fins 101
Comparison of rankine cycles for micro-CHP generation based on inward flow radial turbine or scroll expander 96
An efficient numerical model of pulsating combustion and its experimental validation 95
Experimental Investigation of the aerothermal performance of a high blockage rib-roughened cooling channel 94
Rotating heat transfer measurements on realistic multi-pass geometry 94
Numerical evaluation of showerhead film cooling aerothermal performance on a first-stage vane 93
Separated flow structures around a cylindrical obstacle in a narrow channel 92
Aero-acoustics in a tangential blower: validation of the CFD flow distribution using advanced PIV Techniques 91
Combined heat transfer and flow field analysis in rib-roughened cooling passages for turbine blades 89
Coriolis Effects on the Flow Field Inside a Rotating Triangular Channel for Leading Edge Cooling 87
Aero-acoustic in a tangential blower: validation of the CFD flow distribution using advanced PIV techniques 85
Experimental study of the three-dimensional flow field in cross-flow fans 84
Aerodynamic behavior under rotation of an advanced leading edge impingement cooling channel 84
Experimental analysis of the velocity field inside a turbine blade cooling channel by means of particle image velocimetry 79
Experimental and numerical investigation on a combustor model for syngas swirl flames 78
Three-dimensional features of the turbulent flow through a planar sudden expansion 76
Aero-thermal performance investigation of an internal cooling channel with high blockage ratio 71
Experimental Investigation of unsteadiness associated with film cooling flow ejection from the vane pressure side 71
Analisi sperimentale del campo di moto in ventilatori a flusso trasversale 67
Gas turbine blades internal cooling: Design, development and validation of a new rig for heat transfer measurements under rotation 62
Flow Field Analysis of a Trailing Edge Internal Cooling Channel 61
Investigation of pyrolysis syngas swirl flames in a combustor model 60
Messa a punto di un sistema di misura 2D-DPIV e primi test sperimentali 59
Misure PIV all’interno di un ventilatore a flusso trasversale 56
Numerical investigation on the flow and heat transfer in a rib-roughened channel with high blockage ratio 52
Rotational effects on the trailing edge cooling passage flow field 51
Misure PIV del flusso all’interno di un canaledi raffreddamento per pale di turbina a gas 50
Analisi sperimentale del campo di moto in un canale di raffreddamento per il bordo d'uscita di pale rotoriche di turbina a gas 44
Analisi sperimentale delle prestazioni aero-termiche di canali di raffreddamento per il bordo d'uscita di pale di turbina a gas 44
Indagine sperimentale del campo di moto in un canale di raffreddamento per il bordo d'uscita di pale rotoriche di tubina a gas 41
Experimental investigation of the aerodynamic and thermal behaviour of the film at the leading edge of a cooled nozzle vane cascade 40
Analisi sperimentale di un dispositivo di combustione pulsante 38
Heat transfer and pressure loss performances for additively manufactured pin fin arrays in annular channels 36
Misure PIV del campo di moto all'interno della girante di ventilatori a flusso trasversale 35
Simulazione numerica e verifica sperimentale di un dispositivo di combustione pulsante 34
Aero-thermodynamic performance investigation of a rib roughened cooling channel flow with high blockage ratio 33
Misure PIV del flusso all'interno di un ventilatore a flusso trasversale 29
Heat transfer characterization inside a rotating rib roughened cooling channel with multiple heated walls 19
Click mechanism for racing car self-levelling flap 17
Validation of the transient liquid crystal thermography technique for heat transfer measurements on a rotating cooling passage 17
Acquisition and integration of differential pressure measurements on sails for boat performances improvement 14
Experimental investigation of heat transfer and pressure losses across staggered Body Centered cubic arrays fabricated by Laser Powder Bed Fusion 10
Effects of different cross-sections of Body Centered Cubic cells on pressure drop and heat transfer of additively manufactured heat sinks 5
Combined heat transfer and flow fields analysis in rib-roughened cooling passages for turbine blades 4
Totale 4.760
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Categoria #
all - tutte 13.620
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 13.620
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019306 0 0 0 0 0 0 0 0 0 0 190 116
2019/20201.304 71 52 43 192 88 201 171 166 90 109 36 85
2020/2021673 34 85 7 94 18 92 34 82 96 25 66 40
2021/2022414 14 46 6 16 7 29 33 29 5 72 95 62
2022/2023572 65 85 11 77 57 139 11 25 58 16 10 18
2023/2024151 22 22 6 2 32 10 4 4 33 12 4 0
Totale 4.760