SHAHPAR, Shahrokh
 Distribuzione geografica
Continente #
EU - Europa 3.682
NA - Nord America 109
AS - Asia 52
Totale 3.843
Nazione #
IT - Italia 3.651
US - Stati Uniti d'America 106
SG - Singapore 28
CN - Cina 19
SE - Svezia 15
GB - Regno Unito 7
MX - Messico 3
FI - Finlandia 2
FR - Francia 2
MY - Malesia 2
AT - Austria 1
CZ - Repubblica Ceca 1
DE - Germania 1
HK - Hong Kong 1
IE - Irlanda 1
IN - India 1
RU - Federazione Russa 1
TJ - Tagikistan 1
Totale 3.843
Città #
Cagliari 3.241
Uta 381
Boardman 30
Singapore 20
Nyköping 15
Fairfield 14
Santa Clara 13
Shanghai 13
Quartucciu 6
Woodbridge 5
Seregno 4
Apodaca 3
Ashburn 3
Cambridge 3
Leeds 3
London 3
Milan 3
Ann Arbor 2
Chandler 2
Farmington 2
Fuzhou 2
Helsinki 2
Kuala Lumpur 2
Los Angeles 2
Misterbianco 2
Rome 2
Serramanna 2
Talence 2
Atlanta 1
Beijing 1
Boston 1
Dublin 1
Dushanbe 1
Hangzhou 1
Houston 1
Pune 1
Putignano 1
San Diego 1
Vienna 1
Wilmington 1
Totale 3.794
Nome #
Least squares approximation-based polynomial chaos expansion for uncertainty quantification and robust optimization in aeronautics 757
High-Fidelity Computational Fluid Dynamics Analysis of In-Serviced Shrouded High-Pressure Turbine Rotor Blades 649
Gradient-enhanced Least-square Polynomial Chaos Expansions for Uncertainty Quantification and Robust Optimization 427
HIGH-FIDELITY CFD ANALYSIS OF IN-SERVICED SHROUDED HIGH-PRESSURE TURBINE ROTOR BLADES 370
Extending Highly Loaded Axial Fan Operability Range Through Novel Blade Design 363
EXTENDING HIGHLY LOADED AXIAL FAN OPERABILITY RANGE THROUGH NOVEL BLADE DESIGN 338
MULTI-FIDELITY HEAT TRANSFER ANALYSIS OF SHROUDED HIGH-PRESSURE TURBINE ROTOR BLADES 319
HEAT TRANSFER ANALYSIS OF DAMAGED SHROUDED HIGH-PRESSURE TURBINE ROTOR BLADES 250
Heat Transfer Analysis of Damaged Shrouded High-Pressure Turbine Rotor Blades 227
SECONDARY FLOW CONTROL OF TURBOMACHINERY BLADES USING VORTEX GENERATORS 154
Analysis of the aerothermal performance of modern commercial high-pressure turbine rotors using different levels of fidelity 15
COMBUSTOR TRAVERSE OPTIMIZATION TO LOWER HIGH-PRESSURE TURBINE ROTOR TEMPERATURES 8
MULTI-DISCIPLINARY OPTIMIZATION OF GYROID TOPOLOGIES FOR A COLD PLATE HEAT EXCHANGER DESIGN 6
Totale 3.883
Categoria #
all - tutte 5.682
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 5.682


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021118 0 0 0 5 40 10 15 11 12 9 6 10
2021/2022104 14 1 4 0 4 11 0 1 3 8 23 35
2022/2023572 25 36 16 25 33 74 65 63 60 29 85 61
2023/20241.250 42 43 32 66 117 217 211 111 63 87 107 154
2024/20251.839 382 482 383 422 170 0 0 0 0 0 0 0
Totale 3.883