PORTO @ Archivio Istituzionale della Ricerca

LAROCCA, FRANCESCO
 Distribuzione geografica
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Continente #
EU - Europa 5.849
NA - Nord America 5.084
AS - Asia 1.280
SA - Sud America 24
Continente sconosciuto - Info sul continente non disponibili 6
AF - Africa 3
OC - Oceania 2
Totale 12.248
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Nazione #
US - Stati Uniti d'America 5.053
IT - Italia 1.999
GB - Regno Unito 1.056
DE - Germania 731
CN - Cina 657
FR - Francia 581
UA - Ucraina 422
SG - Singapore 186
TR - Turchia 180
RU - Federazione Russa 167
IE - Irlanda 150
NL - Olanda 149
SE - Svezia 145
CH - Svizzera 111
AT - Austria 103
KR - Corea 101
BE - Belgio 63
FI - Finlandia 58
ID - Indonesia 29
CA - Canada 27
RO - Romania 27
JP - Giappone 24
IN - India 23
JO - Giordania 23
EU - Europa 19
HK - Hong Kong 19
AP - ???statistics.table.value.countryCode.AP??? 14
BG - Bulgaria 14
BR - Brasile 11
MY - Malesia 11
TW - Taiwan 11
IL - Israele 10
IR - Iran 9
CL - Cile 8
BY - Bielorussia 7
HR - Croazia 6
CZ - Repubblica Ceca 4
LU - Lussemburgo 4
MX - Messico 4
VN - Vietnam 4
ES - Italia 3
PE - Perù 3
AU - Australia 2
PH - Filippine 2
ZA - Sudafrica 2
AE - Emirati Arabi Uniti 1
BO - Bolivia 1
DK - Danimarca 1
DZ - Algeria 1
EE - Estonia 1
GR - Grecia 1
GY - Guiana 1
HU - Ungheria 1
KZ - Kazakistan 1
LV - Lettonia 1
NO - Norvegia 1
PK - Pakistan 1
PL - Polonia 1
PT - Portogallo 1
RS - Serbia 1
SK - Slovacchia (Repubblica Slovacca) 1
Totale 12.248
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Città #
Ashburn 1.262
Southend 917
Turin 406
Seattle 340
Chandler 324
Fairfield 298
Beijing 285
Princeton 241
Jacksonville 206
Houston 189
Ann Arbor 180
Woodbridge 180
Cambridge 152
Dublin 146
Berlin 143
Izmir 143
Singapore 140
Santa Clara 129
Torino 129
Chicago 119
Bologna 115
Boardman 114
San Ramon 108
Wilmington 105
Bern 99
Vienna 94
Milan 89
San Donato Milanese 72
Zhengzhou 67
Shanghai 64
Baltimore 57
Helsinki 55
Zaporozhye 51
Council Bluffs 47
Overberg 45
Pennsylvania Furnace 45
Brussels 44
Padua 38
Monopoli 35
San Francisco 35
Des Moines 32
Rome 31
Saint Petersburg 29
Catania 28
Hangzhou 27
Jakarta 26
Guangzhou 21
Redwood City 20
Rivoli 20
Buffalo 18
Changzhou 18
Durham 18
Florence 18
Frankfurt am Main 18
Atlanta 17
Dalian 16
Mountain View 16
Norwalk 16
Frankfurt Am Main 15
Asti 14
London 14
Malatya 14
Nanjing 13
Washington 13
Andover 12
Paris 12
San Diego 12
Xian 12
Bucharest 11
Canelli 11
Chengdu 11
Toronto 11
Fremont 10
Putian 10
San Antonio 10
Sofia 10
Talence 10
Bordeaux 9
Cupertino 9
Fontenay-aux-roses 9
Civitanova Marche 8
Huntingdon 8
Legnano 8
New York 8
Tokyo 8
Yubileyny 8
Zogno 8
Beinasco 7
Hong Kong 7
Istanbul 7
Jinan 7
Kiev 7
Moscow 7
Shenzhen 7
University Park 7
Austin 6
Collegno 6
Foligno 6
Menlo Park 6
Messina 6
Totale 8.091
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Nome #
Turbomachinery design by a swarm-based optimization method coupled with a CFD solver 425
Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines 376
A robust and adaptive recovery-based discontinuous Galerkin method for the numerical solution of convection-diffusion equations 299
On the aerodynamic design of axial flow turbines by an implicit upwind axisymmetric method 283
On the aerodynamic design of axial flow turbines by an implicit upwind axisymmetric solver 281
Potential of specification of swirl in axisymmetric CFD methods for turbine blade aerodesign 278
Euler-based throughflow method for inverse design and optimization of turbomachinery blades 267
Adaptive CFD schemes for aerospace propulsion 257
Axisymmetric Design of Axial Turbomachines:an inverse method introducing Profile Losses 248
An actuator disk model of incidence and deviation for RANS-based throughflow analysis 243
Inverse method for axisymmetric Navier-Stokes computations in turbomachinery aerodesign 240
Axisymmetric design of axial turbomachines: an inverse method introducing profile losses. 240
Multiple objective optimization and inverse design of axial turbomachinery blades 239
Euler inverse axisymmetric solution for design of axial flow multistage turbomachinery 236
Feedback filtering in discontinuous Galerkin methods for Euler equations 231
CFD-based analysis of multistage throughflow surfaces with incidence 228
CFD-based analysis of multistage throughflow surfaces with incidence 223
An actuator disk model of incidence and deviation for RANS-based throughflow analysis 219
Euler-based throughflow method for inverse design and optimization of turbomachinery blades 205
Euler Solver for 3D Inverse Problems 196
A Numerical Smith Diagram Revision for Modern Low Pressure Turbine Profiles 195
Nozzles and Intakes Interacting with the External Flow: Design and Analysis 187
Design of Multistage AxialFlow Turbines and Compressors 186
A Contribution on the Numerical Prediction of Transonic Flows 186
Supersonic Single Stage Gas Turbine AEROTHERMODYNAMICDESIGN 184
Inverse design of high lift cascades by implicit upwind schemes 179
Integrated Design and Analysys of Intakes and Nozzles in Air-Breathing Engines. 178
Afterbodies and Nozzles Optimization by UsingInverse Methods 177
Profile Loss Modelling in an Euler Inverse Throughflow Computation 176
A treatment of the leading edge discontinuity for time-marching throughflow analyses 175
Design Method for 2-D TransonicRotational Flows 174
Application of a 3-D Inviscid RotationalDesign Procedure for Turbomachinery Bladings 172
Soluzioni Numeriche non Stazionariedelle Equazioni di Eulero in Regime Transonico 167
Euler inverse throughflow model based on an implicit upwind time marching technique. 167
Transonic Flows About a Circular Cylinder 163
Optimized inverse design of axial turbomachineryby a Euler axisymmetric solver 161
Treatment of the leading edge discontinuity in time-marching throughflow Models 152
Problemi Inversi Relativi a Flussi Comprimibili,Rotazionali e non Viscosi 150
Upwind Formulation forthe Numerical Prediction of Hyperbolic Flows 148
Decomposition of Domain and UpwindFormulations for the Euler Equations 144
Multiple Objective Optimization of Axial Turbomachines Based on Inverse Method 143
Two-Dimensional Inviscid Unsteady Flows inMultiple Blade Rows 141
Integrazione Numerica delle Equazioni di NavierStokes 141
Inverse Method for Complex FlowConfigurations 141
RANS simulation of secondary flows in a low pressure turbine cascade: Influence of inlet boundary layer profile 140
Metodo Inverso per Configurazioni Complesse del Campo di MotoConfigurations 139
Numerical Method for Designing 3D Turbomachinery Blade Rows 138
Integrazione numerica delle equazioni di Navier-Stokes e di Eulero: Test Cases 133
Inverse Methods for 3-D Internal Flow 132
FIELD INVERSION AND MACHINE LEARNING STRATEGIES FOR IMPROVING RANS MODELLING IN TURBOMACHINERY 130
Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction 123
Contribution to Case C1.2b: Flow over the NACA0012 airfoil ­ transonic case 119
Machine learning methods for the simulation of turbulent flows in turbomachinery 116
Design of Air Intakes and Nozzles forTransonic Rotational Flows 115
Time-Dependent Solution of MultidimensionalInverse Problem 114
Research on Inverse Design Methods and Optimizationin Italy 113
Problemi Inversi Relativi a FlussiComprimibili Rotazionali e non Viscosi 111
Contribution to Case C1.6: Vortex transport 108
Contribution to Case C1.2: Transonic Ringleb flow 107
Contribution to Case C1.3: Flat plate boundary layer 105
A Numerical Study of the Spanwise Turbulence Past a Cylinder Flow 105
Contribution to Case C1.1: Inviscid Flow through a Channel with a Smooth Bump 101
Unstructured discretisation of a non-local transition model for turbomachinery flows 99
RANS closure approximation by artificial neural networks 95
The role of uncertainty in data-driven turbulence modelling 88
Global and local POD models for the prediction of compressible flows with DG methods 77
Field inversion for data-augmented RANS modelling in turbomachinery flows 72
Simulation of secondary flows in turbomachinery by the discontinuous Galerkin method 66
REYNOLDS STRESS CORRECTION BY MACHINE LEARNING METHODS WITH PHYSICAL CONSTRAINTS 66
Mixed Averaging Procedures 65
Uncertainty propagation in field inversion for turbulence modelling in turbomachinery 65
The Filtering Approach as a Tool for Modeling and Analyzing Turbulence 60
A penalisation approach to simulate root compressors 58
Reduced order modelling for turbomachinery shape design 56
Reynolds stress correction by data assimilation methods with physical constraints 51
A study on the statistical convergence of turbulence simulations around a cylinder 40
High-order DG Method for an Implicit LES of a Gas Turbine Cascade 31
A Comparison of Local and Global Strategies for Exploiting Field Inversion on Separated Flows at Low Reynolds Number 17
L. Muscarà, M. Cisternino, A. Ferrero, A. Iob, F. Larocca, K. Samouchos, H. Telib "Enhancing turbulence modeling with data-driven approaches: a focus on the field inversion and machine learning paradigm. " 15
Totale 12.371
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Categoria #
all - tutte 36.192
article - articoli 13.179
book - libri 0
conference - conferenze 19.084
curatela - curatele 0
other - altro 3.422
patent - brevetti 0
selected - selezionate 0
volume - volumi 507
Totale 72.384
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020781 0 0 0 0 129 105 69 161 125 97 77 18
2020/2021946 150 146 37 121 22 84 49 71 63 109 65 29
2021/2022923 23 55 13 28 22 85 87 52 42 83 184 249
2022/20231.363 101 224 15 85 122 190 112 70 164 38 95 147
2023/2024506 26 52 45 16 49 33 29 41 33 30 66 86
2024/2025724 38 213 101 195 177 0 0 0 0 0 0 0
Totale 12.371