IRIS
CASARSA, Luca
 Distribuzione geografica
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Continente #
NA - Nord America 4.078
AS - Asia 1.486
EU - Europa 1.336
SA - Sud America 263
AF - Africa 22
Continente sconosciuto - Info sul continente non disponibili 4
Totale 7.189
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Nazione #
US - Stati Uniti d'America 4.024
SG - Singapore 694
CN - Cina 376
UA - Ucraina 315
IT - Italia 270
DE - Germania 237
BR - Brasile 219
HK - Hong Kong 170
RU - Federazione Russa 148
FI - Finlandia 101
VN - Vietnam 92
GB - Regno Unito 57
IE - Irlanda 54
TR - Turchia 44
FR - Francia 41
CA - Canada 34
SE - Svezia 32
KR - Corea 23
PL - Polonia 22
AR - Argentina 18
JP - Giappone 14
BE - Belgio 13
IN - India 13
MX - Messico 13
PK - Pakistan 12
BD - Bangladesh 11
NL - Olanda 10
IQ - Iraq 9
EC - Ecuador 8
CH - Svizzera 7
ZA - Sudafrica 6
ES - Italia 5
LT - Lituania 5
TG - Togo 5
AT - Austria 4
CO - Colombia 4
EU - Europa 4
ID - Indonesia 4
VE - Venezuela 4
CZ - Repubblica Ceca 3
JO - Giordania 3
MA - Marocco 3
PE - Perù 3
PY - Paraguay 3
AL - Albania 2
CL - Cile 2
DO - Repubblica Dominicana 2
DZ - Algeria 2
HU - Ungheria 2
IL - Israele 2
KZ - Kazakistan 2
LK - Sri Lanka 2
NP - Nepal 2
OM - Oman 2
PA - Panama 2
AE - Emirati Arabi Uniti 1
AZ - Azerbaigian 1
BG - Bulgaria 1
BY - Bielorussia 1
CI - Costa d'Avorio 1
EE - Estonia 1
EG - Egitto 1
ET - Etiopia 1
GE - Georgia 1
GR - Grecia 1
GT - Guatemala 1
GY - Guiana 1
HN - Honduras 1
IM - Isola di Man 1
JM - Giamaica 1
KE - Kenya 1
KG - Kirghizistan 1
KW - Kuwait 1
LA - Repubblica Popolare Democratica del Laos 1
NO - Norvegia 1
PS - Palestinian Territory 1
PT - Portogallo 1
SK - Slovacchia (Repubblica Slovacca) 1
SN - Senegal 1
SY - Repubblica araba siriana 1
TH - Thailandia 1
TW - Taiwan 1
UY - Uruguay 1
UZ - Uzbekistan 1
ZM - Zambia 1
Totale 7.189
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Città #
Fairfield 403
Ann Arbor 383
Woodbridge 372
Houston 351
Ashburn 340
Singapore 299
Chandler 268
Jacksonville 215
Beijing 212
Seattle 180
Wilmington 176
Hong Kong 170
Dearborn 122
Cambridge 118
Boardman 74
Udine 60
Princeton 58
Los Angeles 55
Dublin 54
Izmir 39
Buffalo 28
Ho Chi Minh City 27
Dallas 26
New York 26
São Paulo 25
Hefei 24
Torre Del Greco 23
Seoul 21
San Diego 20
Hanoi 19
Warsaw 19
Redondo Beach 18
Santa Clara 18
Ogden 17
Blacksburg 15
Des Moines 15
Dong Ket 14
Ottawa 14
Brussels 13
Tokyo 13
Gorizia 12
Montreal 12
Rio de Janeiro 12
Düsseldorf 11
Nanjing 10
Atlanta 9
Belo Horizonte 9
Guangzhou 9
Brooklyn 8
Denver 8
Helsinki 8
Lahore 8
Milan 8
Phoenix 8
Trieste 8
Chicago 7
Desio 7
Kunming 7
London 7
Stockholm 7
Boston 6
Brasília 6
Frankfurt am Main 6
Jinan 6
Johannesburg 6
Norwalk 6
Orem 6
Secaucus 6
Simi Valley 6
Chennai 5
Codroipo 5
Fuzhou 5
Haiphong 5
Indiana 5
Lomé 5
Padova 5
Rome 5
San Francisco 5
Amsterdam 4
Baghdad 4
Duncan 4
Falls Church 4
Guarulhos 4
Manchester 4
Newark 4
Porto Alegre 4
Povoletto 4
Salvador 4
St Petersburg 4
São Gonçalo 4
Venice 4
Vienna 4
Zhengzhou 4
Amman 3
Ankara 3
Asunción 3
Augusta 3
Bochum 3
Chongqing 3
Da Nang 3
Totale 4.699
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Nome #
Rotational effects on the flow field inside a leading edge impingement cooling passage 190
Effects of Rotation at Different Channel Orientations on the Flow Field inside a Trailing Edge Internal Cooling Channel 187
Characterization of the velocity and heat transfer fields in an internal cooling channel with high blockage ratio 171
Effects of injection conditions and Mach number on unsteadiness arising within coolant jets over a pressure side vane surface 169
Experimental assessment of the aero-thermal performance of rib roughened trailing edge cooling channels for gas turbine blades 168
Flow field analysis inside a gas turbine trailing edge cooling channel under static and rotating conditions: Effect of ribs 163
Experimental Investigation of the Effects of Blowing Conditions and Mach number on the Unsteady Behavior of Coolant Ejection through a Trailing Edge Cutback 162
Flow field analysis inside a gas turbine trailing edge cooling channel under static and rotating conditions 160
Effects of rotation and channel orientation on the flow field inside a trailing edge internal cooling channel 156
Effects of rotation and buoyancy forces on the flow field behavior inside a triangular rib roughened channel 152
Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation 151
Flow field investigations in rotating facilities by means of stationary PIV systems 149
Rotating heat transfer measurements on a multi-pass internal cooling channel - I rig development 149
Rotating heat transfer measurements on a multi-pass internal cooling channel - II experimental tests 146
Effect of rotation on a gas turbine blade internal cooling system: Experimental investigation 144
Combined heat transfer and flow field analysis in rib-roughened cooling passages for turbine blades 143
Buoyancy effects at high rotation number on the flow field inside a triangular shaped rib roughened channel 141
Low Reynolds number flow in rectangular cooling channels provided with low aspect ratio pin fins 140
Coriolis Effects on the Flow Field Inside a Rotating Triangular Channel for Leading Edge Cooling 139
Comparison of rankine cycles for micro-CHP generation based on inward flow radial turbine or scroll expander 139
An efficient numerical model of pulsating combustion and its experimental validation 138
Flow field inside a leading edge cooling channel with turbulence promoters in rotating conditions 135
Separated flow structures around a cylindrical obstacle in a narrow channel 135
Aero-acoustics in a tangential blower: validation of the CFD flow distribution using advanced PIV Techniques 134
Numerical aero-thermal analysis of a rib-roughened trailing edge cooling channel at different rotation numbers and channel orientations 134
Aero-acoustic in a tangential blower: validation of the CFD flow distribution using advanced PIV techniques 133
Aerodynamic behavior under rotation of an advanced leading edge impingement cooling channel 133
Experimental investigation of the interaction between showerhead coolant jets and main flow 133
Experimental Investigation of the aerothermal performance of a high blockage rib-roughened cooling channel 129
Rotating heat transfer measurements on realistic multi-pass geometry 129
Analisi sperimentale del campo di moto in ventilatori a flusso trasversale 121
Numerical evaluation of showerhead film cooling aerothermal performance on a first-stage vane 120
Experimental analysis of the velocity field inside a turbine blade cooling channel by means of particle image velocimetry 116
Aero-thermal performance investigation of an internal cooling channel with high blockage ratio 115
Experimental and numerical investigation on a combustor model for syngas swirl flames 113
Experimental study of the three-dimensional flow field in cross-flow fans 111
Experimental Investigation of unsteadiness associated with film cooling flow ejection from the vane pressure side 110
Gas turbine blades internal cooling: Design, development and validation of a new rig for heat transfer measurements under rotation 101
Heat transfer and pressure loss performances for additively manufactured pin fin arrays in annular channels 100
Messa a punto di un sistema di misura 2D-DPIV e primi test sperimentali 99
Three-dimensional features of the turbulent flow through a planar sudden expansion 97
Flow Field Analysis of a Trailing Edge Internal Cooling Channel 93
Analisi sperimentale delle prestazioni aero-termiche di canali di raffreddamento per il bordo d'uscita di pale di turbina a gas 92
Misure PIV del flusso all’interno di un canaledi raffreddamento per pale di turbina a gas 91
Investigation of pyrolysis syngas swirl flames in a combustor model 90
Rotational effects on the trailing edge cooling passage flow field 90
Indagine sperimentale del campo di moto in un canale di raffreddamento per il bordo d'uscita di pale rotoriche di tubina a gas 86
Analisi sperimentale del campo di moto in un canale di raffreddamento per il bordo d'uscita di pale rotoriche di turbina a gas 85
Analisi sperimentale di un dispositivo di combustione pulsante 84
Numerical investigation on the flow and heat transfer in a rib-roughened channel with high blockage ratio 83
Misure PIV all’interno di un ventilatore a flusso trasversale 79
Experimental investigation of heat transfer and pressure losses across staggered Body Centered cubic arrays fabricated by Laser Powder Bed Fusion 75
Aero-thermodynamic performance investigation of a rib roughened cooling channel flow with high blockage ratio 74
Experimental investigation of the aerodynamic and thermal behaviour of the film at the leading edge of a cooled nozzle vane cascade 70
Acquisition and integration of differential pressure measurements on sails for boat performances improvement 67
Simulazione numerica e verifica sperimentale di un dispositivo di combustione pulsante 64
Misure PIV del campo di moto all'interno della girante di ventilatori a flusso trasversale 61
Click mechanism for racing car self-levelling flap 59
Heat transfer characterization inside a rotating rib roughened cooling channel with multiple heated walls 55
Combined heat transfer and flow fields analysis in rib-roughened cooling passages for turbine blades 53
Effects of different cross-sections of Body Centered Cubic cells on pressure drop and heat transfer of additively manufactured heat sinks 50
Validation of the transient liquid crystal thermography technique for heat transfer measurements on a rotating cooling passage 50
Misure PIV del flusso all'interno di un ventilatore a flusso trasversale 49
Heat Transfer and Pressure Loss Performance of Additively Manufactured Metamaterials in Annular Channels 48
Experimental investigation of heat transfer and pressure losses across additively manufactured Body Centered Cubic arrays: effects of cell shape and array arrangement 15
Totale 7.318
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Categoria #
all - tutte 26.707
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 26.707
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021435 0 0 0 0 0 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
2023/2024201 22 22 6 2 32 10 4 4 33 12 10 44
2024/20251.171 39 77 100 15 39 65 96 72 133 59 191 285
2025/20261.337 231 224 161 304 390 27 0 0 0 0 0 0
Totale 7.318