CUBEDA, SIMONE
 Distribuzione geografica
Continente #
NA - Nord America 709
EU - Europa 605
AS - Asia 303
AF - Africa 15
OC - Oceania 12
SA - Sud America 1
Totale 1.645
Nazione #
US - Stati Uniti d'America 709
RU - Federazione Russa 299
IT - Italia 120
CN - Cina 107
HK - Hong Kong 90
IE - Irlanda 55
SG - Singapore 42
SE - Svezia 35
JO - Giordania 28
PL - Polonia 27
FI - Finlandia 24
IN - India 15
DE - Germania 13
AU - Australia 12
DZ - Algeria 10
AT - Austria 9
GB - Regno Unito 9
JP - Giappone 9
NL - Olanda 4
IR - Iran 3
TR - Turchia 3
VN - Vietnam 3
BG - Bulgaria 2
CH - Svizzera 2
CI - Costa d'Avorio 2
FR - Francia 2
KR - Corea 2
MD - Moldavia 2
PT - Portogallo 2
BR - Brasile 1
ID - Indonesia 1
MU - Mauritius 1
NG - Nigeria 1
ZA - Sudafrica 1
Totale 1.645
Città #
Santa Clara 418
Hong Kong 76
Dublin 55
Ashburn 32
Singapore 31
Beijing 28
Warsaw 26
Florence 24
Helsinki 22
Fairfield 21
Prato 20
Moscow 19
Chandler 16
Seattle 16
Houston 14
Melbourne 12
Shanghai 12
Tong 11
Woodbridge 11
Kent 10
Mumbai 10
Wilmington 10
Cambridge 9
Vienna 9
Kurita 8
Milan 8
Princeton 8
Boston 7
Modena 6
West Jordan 6
Altamura 5
Prad am Stilfser Joch 5
Redwood City 5
Andover 4
Cagliari 4
Lawrence 4
Loughborough 4
Ponte San Pietro 4
Boardman 3
Guangzhou 3
Hillsboro 3
Karaj 3
Pune 3
Abidjan 2
Ann Arbor 2
Bergamo 2
Bern 2
Central 2
Correggio 2
Dong Ket 2
Falkenstein 2
Gavorrano 2
Jiujiang 2
Khenchela 2
Lappeenranta 2
Lisbon 2
Los Angeles 2
Luft 2
Medford 2
Munich 2
Nanjing 2
Parma 2
Reggio Emilia 2
Romola 2
San Diego 2
Seoul 2
Vercelli 2
Xi'an 2
Yubileyny 2
Aberdeen 1
Annaba 1
Batna City 1
Bethesda 1
Bien Hoa 1
Buffalo 1
Changsha 1
Clifton 1
Frankfurt am Main 1
Groningen 1
Handan 1
Hyderabad 1
Jakarta 1
Johannesburg 1
La Spezia 1
Laojunmiao 1
Leawood 1
Mülheim 1
Naples 1
Norwalk 1
Orta di Atella 1
Paris 1
Rui'an 1
Sesto Fiorentino 1
Soltau 1
Stevenage 1
Studio City 1
Sulzbach am Main 1
São Paulo 1
Urmston 1
Viareggio 1
Totale 1.088
Nome #
Impacts of gas-turbine combustors outlet flow on the aero-thermal performance of film-cooled first stage nozzles 236
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled HPT vanes 127
Non-reactive test rig for combustor-turbine interaction studies in industrial gas turbines 115
Impact of predicted combustor outlet conditions on the aerothermal performance of film-cooled high pressure turbine vanes 108
Design of a Non-Reactive Warm Rig With Real Lean-Premix Combustor Swirlers and Film-Cooled First Stage Nozzles 103
DEVELOPMENT AND APPLICATION OF A CONCENTRATION PROBE FOR MIXING FLOWS TRACKING IN TURBOMACHINERY APPLICATIONS 100
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 97
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 91
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 85
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 84
Film Cooling and Cold Streaks Tracking on a Fully Cooled Nozzle Guide Vane Under Representative Combustor Outflow Conditions 77
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions 74
Development and Application of a Concentration Probe for Mixing Flows Tracking in Turbomachinery Applications 67
External heat transfer on nozzle guide vanes under highly swirled combustor outlet flow 67
Heat Transfer Coefficient and Adiabatic Effectiveness on a Film-Cooled Pressure Side: Results and Assessment of the IR-Based Measurement Technique Reliability 65
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS MEASUREMENTS ON A NOZZLE GUIDE VANE WITH A SINGLE ROW OF CYLINDRICAL HOLES 59
Heat Transfer Coefficient and Adiabatic Effectiveness Measurements on a Nozzle Guide Vane With a Single Row of Cylindrical Holes 59
NUMERICAL PREDICTION OF THE HEAT LOADS ON A NON-REACTIVE TEST RIG FOR COMBUSTOR-TURBINE INTERACTION BY USING HYBRID RANS-LES APPROACH 57
Totale 1.671
Categoria #
all - tutte 6.019
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 6.019


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/202019 0 0 0 0 0 0 0 4 4 2 1 8
2020/202166 8 8 1 5 4 7 5 3 7 8 4 6
2021/202291 1 2 0 18 13 8 3 13 2 4 9 18
2022/2023227 16 18 22 6 6 36 50 7 42 4 10 10
2023/2024273 7 24 25 14 12 23 22 62 20 17 38 9
2024/2025960 29 116 73 170 323 182 18 49 0 0 0 0
Totale 1.671