LAROCCA, FRANCESCO
 Distribuzione geografica
Continente #
EU - Europa 7.545
NA - Nord America 6.517
AS - Asia 4.060
SA - Sud America 344
Continente sconosciuto - Info sul continente non disponibili 139
AF - Africa 39
OC - Oceania 5
Totale 18.649
Nazione #
US - Stati Uniti d'America 6.416
IT - Italia 2.174
NL - Olanda 1.113
GB - Regno Unito 1.100
SG - Singapore 1.073
CN - Cina 1.049
VN - Vietnam 847
DE - Germania 781
FR - Francia 715
UA - Ucraina 429
RU - Federazione Russa 368
KR - Corea 256
BR - Brasile 251
TR - Turchia 191
HK - Hong Kong 187
IE - Irlanda 152
SE - Svezia 152
AT - Austria 121
IN - India 121
CH - Svizzera 117
FI - Finlandia 91
BE - Belgio 75
JP - Giappone 61
CA - Canada 59
BD - Bangladesh 46
ID - Indonesia 37
AR - Argentina 33
RO - Romania 27
TW - Taiwan 26
PH - Filippine 24
JO - Giordania 23
TH - Thailandia 23
IQ - Iraq 20
EU - Europa 19
CL - Cile 18
ES - Italia 17
BG - Bulgaria 16
MX - Messico 16
MY - Malesia 15
AP - ???statistics.table.value.countryCode.AP??? 14
CO - Colombia 13
EC - Ecuador 11
IL - Israele 11
PK - Pakistan 11
UZ - Uzbekistan 11
IR - Iran 10
ZA - Sudafrica 10
BY - Bielorussia 9
GT - Guatemala 7
PL - Polonia 7
HR - Croazia 6
SA - Arabia Saudita 6
AE - Emirati Arabi Uniti 5
CZ - Repubblica Ceca 5
NP - Nepal 5
PY - Paraguay 5
VE - Venezuela 5
AU - Australia 4
GR - Grecia 4
KE - Kenya 4
LT - Lituania 4
LU - Lussemburgo 4
MA - Marocco 4
NI - Nicaragua 4
PE - Perù 4
AL - Albania 3
DZ - Algeria 3
EG - Egitto 3
HN - Honduras 3
LV - Lettonia 3
SV - El Salvador 3
CI - Costa d'Avorio 2
DK - Danimarca 2
DO - Repubblica Dominicana 2
ET - Etiopia 2
GY - Guiana 2
JM - Giamaica 2
LB - Libano 2
NO - Norvegia 2
RS - Serbia 2
SN - Senegal 2
TG - Togo 2
TN - Tunisia 2
TT - Trinidad e Tobago 2
AM - Armenia 1
AZ - Azerbaigian 1
BB - Barbados 1
BH - Bahrain 1
BO - Bolivia 1
BW - Botswana 1
BZ - Belize 1
CM - Camerun 1
CY - Cipro 1
DJ - Gibuti 1
EE - Estonia 1
GE - Georgia 1
GF - Guiana Francese 1
HU - Ungheria 1
KG - Kirghizistan 1
KW - Kuwait 1
Totale 18.502
Città #
Ashburn 1.466
Amsterdam 955
Southend 917
Singapore 564
San Jose 474
Turin 450
Beijing 362
Seattle 340
Chandler 324
Fairfield 298
Princeton 241
Ho Chi Minh City 215
Hanoi 212
Jacksonville 207
Houston 194
Santa Clara 193
Ann Arbor 180
Woodbridge 180
Hong Kong 154
Cambridge 152
Dublin 147
Berlin 143
Izmir 143
Torino 129
Chicago 126
Bologna 120
Boardman 116
Council Bluffs 115
Milan 110
San Ramon 108
Wilmington 106
Seoul 105
Bern 99
Vienna 98
Helsinki 81
Los Angeles 77
San Donato Milanese 72
Zhengzhou 71
Lauterbourg 69
Shanghai 68
Baltimore 59
Zaporozhye 51
Buffalo 50
Brussels 49
Overberg 45
Pennsylvania Furnace 45
Frankfurt am Main 41
Rome 40
Da Nang 39
Padua 38
San Francisco 38
Dallas 37
Monopoli 36
Guangzhou 33
Des Moines 32
Hangzhou 30
Tokyo 30
Saint Petersburg 29
Catania 28
São Paulo 28
Jakarta 27
New York 26
Atlanta 24
London 23
Haiphong 22
Bordeaux 20
Redwood City 20
Rivoli 20
The Dalles 20
Changzhou 19
Florence 19
Durham 18
Paris 18
Washington 17
Dalian 16
Mountain View 16
Norwalk 16
Orem 16
Frankfurt Am Main 15
Asti 14
Malatya 14
Toronto 14
Chengdu 13
Hefei 13
Nanjing 13
North Bergen 13
Andover 12
Montreal 12
Moscow 12
San Diego 12
Xian 12
Bucharest 11
Canelli 11
San Antonio 11
Tashkent 11
Bangkok 10
Fremont 10
Liège 10
Naples 10
Phoenix 10
Totale 11.579
Nome #
High-order DG Method for an Implicit LES of a Gas Turbine Cascade 1.101
Turbomachinery design by a swarm-based optimization method coupled with a CFD solver 537
Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines 472
A robust and adaptive recovery-based discontinuous Galerkin method for the numerical solution of convection-diffusion equations 397
Euler-based throughflow method for inverse design and optimization of turbomachinery blades 346
On the aerodynamic design of axial flow turbines by an implicit upwind axisymmetric solver 343
On the aerodynamic design of axial flow turbines by an implicit upwind axisymmetric method 339
Potential of specification of swirl in axisymmetric CFD methods for turbine blade aerodesign 326
An actuator disk model of incidence and deviation for RANS-based throughflow analysis 310
Adaptive CFD schemes for aerospace propulsion 306
Euler inverse axisymmetric solution for design of axial flow multistage turbomachinery 298
Axisymmetric Design of Axial Turbomachines:an inverse method introducing Profile Losses 295
Axisymmetric design of axial turbomachines: an inverse method introducing profile losses. 290
Feedback filtering in discontinuous Galerkin methods for Euler equations 290
Inverse method for axisymmetric Navier-Stokes computations in turbomachinery aerodesign 288
CFD-based analysis of multistage throughflow surfaces with incidence 286
CFD-based analysis of multistage throughflow surfaces with incidence 280
Nozzles and Intakes Interacting with the External Flow: Design and Analysis 276
An actuator disk model of incidence and deviation for RANS-based throughflow analysis 276
Multiple objective optimization and inverse design of axial turbomachinery blades 274
Euler-based throughflow method for inverse design and optimization of turbomachinery blades 265
RANS simulation of secondary flows in a low pressure turbine cascade: Influence of inlet boundary layer profile 264
A Numerical Smith Diagram Revision for Modern Low Pressure Turbine Profiles 261
Design of Multistage AxialFlow Turbines and Compressors 247
Euler Solver for 3D Inverse Problems 246
Transonic Flows About a Circular Cylinder 245
Supersonic Single Stage Gas Turbine AEROTHERMODYNAMICDESIGN 244
A treatment of the leading edge discontinuity for time-marching throughflow analyses 238
Integrated Design and Analysys of Intakes and Nozzles in Air-Breathing Engines. 236
A Contribution on the Numerical Prediction of Transonic Flows 233
Design Method for 2-D TransonicRotational Flows 227
Afterbodies and Nozzles Optimization by UsingInverse Methods 226
Inverse design of high lift cascades by implicit upwind schemes 225
Euler inverse throughflow model based on an implicit upwind time marching technique. 224
Profile Loss Modelling in an Euler Inverse Throughflow Computation 223
Application of a 3-D Inviscid RotationalDesign Procedure for Turbomachinery Bladings 219
Upwind Formulation forthe Numerical Prediction of Hyperbolic Flows 218
Soluzioni Numeriche non Stazionariedelle Equazioni di Eulero in Regime Transonico 212
Optimized inverse design of axial turbomachineryby a Euler axisymmetric solver 210
Mixed Averaging Procedures 207
Decomposition of Domain and UpwindFormulations for the Euler Equations 207
Machine learning methods for the simulation of turbulent flows in turbomachinery 206
Two-Dimensional Inviscid Unsteady Flows inMultiple Blade Rows 202
FIELD INVERSION AND MACHINE LEARNING STRATEGIES FOR IMPROVING RANS MODELLING IN TURBOMACHINERY 202
Integrazione Numerica delle Equazioni di NavierStokes 200
Inverse Method for Complex FlowConfigurations 200
Metodo Inverso per Configurazioni Complesse del Campo di MotoConfigurations 200
Inverse Methods for 3-D Internal Flow 197
Treatment of the leading edge discontinuity in time-marching throughflow Models 197
Numerical Method for Designing 3D Turbomachinery Blade Rows 192
A Numerical Study of the Spanwise Turbulence Past a Cylinder Flow 192
Problemi Inversi Relativi a Flussi Comprimibili,Rotazionali e non Viscosi 186
Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction 185
Field inversion for data-augmented RANS modelling in turbomachinery flows 181
Multiple Objective Optimization of Axial Turbomachines Based on Inverse Method 180
The role of uncertainty in data-driven turbulence modelling 177
Contribution to Case C1.2b: Flow over the NACA0012 airfoil ­ transonic case 173
Simulation of secondary flows in turbomachinery by the discontinuous Galerkin method 172
Contribution to Case C1.3: Flat plate boundary layer 172
Integrazione numerica delle equazioni di Navier-Stokes e di Eulero: Test Cases 170
RANS closure approximation by artificial neural networks 169
Research on Inverse Design Methods and Optimizationin Italy 168
Time-Dependent Solution of MultidimensionalInverse Problem 167
REYNOLDS STRESS CORRECTION BY MACHINE LEARNING METHODS WITH PHYSICAL CONSTRAINTS 164
A Comparison of Local and Global Strategies for Exploiting Field Inversion on Separated Flows at Low Reynolds Number 158
Contribution to Case C1.6: Vortex transport 157
Contribution to Case C1.2: Transonic Ringleb flow 155
Reynolds stress correction by data assimilation methods with physical constraints 153
Global and local POD models for the prediction of compressible flows with DG methods 152
Design of Air Intakes and Nozzles forTransonic Rotational Flows 150
Problemi Inversi Relativi a FlussiComprimibili Rotazionali e non Viscosi 149
Contribution to Case C1.1: Inviscid Flow through a Channel with a Smooth Bump 149
The Filtering Approach as a Tool for Modeling and Analyzing Turbulence 148
Uncertainty propagation in field inversion for turbulence modelling in turbomachinery 146
A study on the statistical convergence of turbulence simulations around a cylinder 145
Unstructured discretisation of a non-local transition model for turbomachinery flows 140
Enhancing turbulence modeling with data-driven approaches: a focus on the field inversion and machine learning paradigm 139
Reduced order modelling for turbomachinery shape design 131
A penalisation approach to simulate root compressors 118
Totale 18.649
Categoria #
all - tutte 53.686
article - articoli 19.264
book - libri 0
conference - conferenze 28.808
curatela - curatele 0
other - altro 4.959
patent - brevetti 0
selected - selezionate 0
volume - volumi 655
Totale 107.372


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022900 0 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
2024/20251.598 38 213 101 195 182 90 88 91 240 78 79 203
2025/20265.166 288 226 219 323 233 268 626 339 1.902 520 63 159
2026/2027238 146 92 0 0 0 0 0 0 0 0 0 0
Totale 18.649