IRIS
CINNELLA, Paola
 Distribuzione geografica
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Continente #
EU - Europa 4.086
AS - Asia 3.223
NA - Nord America 2.739
SA - Sud America 543
Continente sconosciuto - Info sul continente non disponibili 60
AF - Africa 49
OC - Oceania 2
Totale 10.702
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Nazione #
US - Stati Uniti d'America 2.622
IT - Italia 1.495
SG - Singapore 1.460
IE - Irlanda 1.125
CN - Cina 603
RU - Federazione Russa 559
HK - Hong Kong 471
BR - Brasile 449
VN - Vietnam 297
UA - Ucraina 253
FR - Francia 176
IN - India 137
SE - Svezia 126
GB - Regno Unito 104
FI - Finlandia 96
KR - Corea 63
BD - Bangladesh 51
CA - Canada 51
MX - Messico 45
AR - Argentina 36
DE - Germania 35
PL - Polonia 29
ID - Indonesia 25
IQ - Iraq 25
ES - Italia 23
JP - Giappone 21
EC - Ecuador 19
ZA - Sudafrica 16
BE - Belgio 13
AE - Emirati Arabi Uniti 12
CH - Svizzera 12
LT - Lituania 11
TR - Turchia 11
CO - Colombia 9
SN - Senegal 9
NL - Olanda 8
PK - Pakistan 8
PY - Paraguay 8
UZ - Uzbekistan 8
VE - Venezuela 7
CR - Costa Rica 6
RO - Romania 6
AT - Austria 5
CL - Cile 5
JM - Giamaica 5
UY - Uruguay 5
AZ - Azerbaigian 4
DZ - Algeria 4
EG - Egitto 4
EU - Europa 4
IL - Israele 4
JO - Giordania 4
KE - Kenya 4
MA - Marocco 4
PE - Perù 4
KZ - Kazakistan 3
NP - Nepal 3
BG - Bulgaria 2
DO - Repubblica Dominicana 2
HN - Honduras 2
OM - Oman 2
PH - Filippine 2
RS - Serbia 2
SA - Arabia Saudita 2
TN - Tunisia 2
AL - Albania 1
AU - Australia 1
AW - Aruba 1
BF - Burkina Faso 1
BN - Brunei Darussalam 1
BO - Bolivia 1
BW - Botswana 1
BY - Bielorussia 1
EE - Estonia 1
ET - Etiopia 1
GE - Georgia 1
GT - Guatemala 1
IR - Iran 1
LB - Libano 1
LK - Sri Lanka 1
LV - Lettonia 1
MD - Moldavia 1
ML - Mali 1
NG - Nigeria 1
NI - Nicaragua 1
NZ - Nuova Zelanda 1
PA - Panama 1
PR - Porto Rico 1
PS - Palestinian Territory 1
PT - Portogallo 1
SY - Repubblica araba siriana 1
TG - Togo 1
TT - Trinidad e Tobago 1
XK - ???statistics.table.value.countryCode.XK??? 1
Totale 10.647
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Città #
Lecce 1.425
Dublin 1.125
Singapore 455
Hong Kong 431
San Jose 263
Ashburn 236
Chandler 197
Council Bluffs 197
Moscow 179
Beijing 167
Jacksonville 165
Ho Chi Minh City 98
New York 97
Wayanad 89
Dallas 83
Los Angeles 82
Princeton 82
Lauterbourg 77
Hanoi 66
Seoul 62
Des Moines 55
São Paulo 47
Santa Clara 38
Ann Arbor 37
Denver 36
Central District 32
Wilmington 30
Montreal 27
Warsaw 25
Ogden 23
Mexico City 21
Rio de Janeiro 20
Stockholm 20
Chicago 19
Tokyo 19
Brooklyn 18
Haiphong 17
Orem 16
Poplar 16
Phoenix 15
Atlanta 14
Chennai 14
Houston 14
Boston 13
Brussels 13
Boardman 12
Columbus 12
Da Nang 12
Seattle 12
Baghdad 11
Hải Dương 11
Norwalk 10
Zurich 10
Dakar 9
Frankfurt am Main 9
London 9
Milan 9
Mumbai 9
Quito 9
Rome 9
San Francisco 9
Turku 9
Belo Horizonte 8
Thái Bình 8
West Jordan 8
Manchester 7
Querétaro 7
Ribeirão Preto 7
The Dalles 7
Biên Hòa 6
Curitiba 6
Dhaka 6
Johannesburg 6
Shanghai 6
São Gonçalo 6
Amsterdam 5
Ankara 5
Brasília 5
Buenos Aires 5
Campinas 5
Dubai 5
Goiânia 5
Guangzhou 5
Paris 5
Porto Alegre 5
Raleigh 5
Secaucus 5
Toronto 5
Baku 4
Cape Town 4
Caraguatatuba 4
Charlotte 4
Guayaquil 4
Helsinki 4
Louisville 4
Miami 4
Montevideo 4
New Delhi 4
Nuremberg 4
San José 4
Totale 6.547
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Nome #
Multi-fidelity optimization strategy for the industrial aerodynamic design of helicopter rotor blades 212
Aerodynamic performance of transonic dense gas flows past an airfoil 171
A third-order accurate centered scheme for turbulent compressible flow calculations in aerodynamics 168
Airfoil shape optimization for transonic flows of Bethe-Zel’dovich-Thompson fluids 167
Accurate simulation of turbulent transonic flows over oscillating airfoils 166
Inviscid and viscous aerodynamics of dense gases 165
Analysis of High-Order Residual-Based Dissipation for Unsteady Compressible Flows 159
Optimal airfoil shapes for viscous transonic flows of Bethe—Zel’dovich—Thompson fluids 158
Numerical Solver for Dense Gas Flows 157
A study of turbulent compressible flows over oscillating airfoils by a high-order accurate numerical scheme 156
A numerical method for turbomachinery aeroelasticity 155
Caratterizzazione del sito di interesse nazionale di Brindisi- Modellazione numerica della fluidodinamica di falda e del trasporto di inquinanti 154
Accurate and Computationally Efficient Equations of State for the Numerical Simulation of Dense Gas Flows 150
Shape optimization for dense gas flows in turbine cascades 147
A numerical method for turbomachinery aeroelasticity 147
Optimal airfoil shapes for viscous transonic flows of dense gases 144
A centred numerical scheme for dense gas flows 143
Computationally efficient models for the numerical simulation of thermodynamically complex flows 143
Aerodynamic rotor blade optimization at Eurocopter - a new way of industrial rotor blade design 143
GA-hardness of Aerodynamic Optimization Problems: Analysis and Proposed Cures 141
Analysis and optimization of viscous dense gas flows 141
Effcient numerical simulation of dense gas flows past airfoils and wings 141
An accurate finite-volume formulation of a residual-based compact scheme for unsteady compressible flows 141
A fully implicit third-order scheme in time and space for unsteady turbulent compressible flow simulations 139
Efficient numerical simulation of three-dimensional Bethe-Zel'dovich-Thompson fluid flows 139
Investigation of BZT transonic flows past an airfoil using a 5th power virial equation of state 138
A numerical method for 3D turbomachinery aeroelasticity 138
Third-order finite volume schemes for Euler computations on curvilinear meshes 137
An assessment of a fifth-order residual-based compact scheme for steady and unsteady compressible flows 137
Future directions for computing compressible flows : higher order centering versus multidimensional upwinding 132
GA-Hardness of dense-gas flow optimization problems 132
A study of turbulent compressible flows over oscillating airfoils by a high-order accurate numerical scheme 131
Effects of Modeling Uncertainties in Condensing Wet-Steam Flows through Supersonic Nozzles 131
Transonic flows of BZT fluids through turbine cascades 127
A numerical method for dense gas flows 127
Assessment of a high-order shock-capturing central-difference scheme for hypersonic turbulent flow simulations 125
Roe-type schemes for dense gas flow computations 124
Optimal blade shapes for viscous dense gas flows through turbine cascades 122
Development of a residual-based-compact scheme in elsAfor the computation of complex turbomachinery flows 121
Transonic flows of dense gases over finite wings 117
Robust Optimization of Dense Gas Flows under Uncertain Operating Conditions 117
Numerical Method for Wet-Steam Flows in Turbine Cascades 115
Direct numerical simulation of subharmonic second-mode breakdown in hypersonic boundary layers with finite-rate chemistry 113
Un metodo numerico di elevata accuratezza per flussi non stazionari nelle turbomacchine 113
Numerical Method for Wet-Steam Flows with Polydispersed Droplet Spectra 112
Assessment of automatic Hybrid RANS/LES Models for Industrial CFD 112
Bayesian estimates of parameter variability in the k-e turbulence model 111
Evaluation of a high-order central-difference solver for highly compressible flows out of thermochemical equilibrium 110
Nozzle Shape Optimization for Wet-Steam Flows 109
Hybrid Adjoint-based Robust Optimization Approach for Fluid-Dynamics Problems 109
Turbulence 108
Coupled/Uncoupled solutions of RANS equations using a Jacobian-free Newton-Krylov method 108
Quantification of thermodynamic uncertainties in real-gas flows 107
Robust Optimization of Dense Gas Flows under Uncertain Operating Conditions 107
Numerical study of transonic shock/boundary layer interactions on an oscillating airfoil using a third-order scheme and nonlinear turbulence models 106
Convergence behaviours of Genetic Algorithms for Aerodynamic Optimisation Problems 106
High-order and conservative method for patched grid interfaces 106
Metodi avanzati per la Fluidodinamica Numerica 104
Numerical Simulation of external transonic flows of Bethe-Zel’dovich-Thompson fluids 104
Multi-zone quasidimensional combustion models for Spark Ignition engines 104
Multiblock computations of complex turbomachinery flows using residual-based compact schemes 103
GAMM Annual Meeting - Lecce 2015 Overview of the Sections 101
EFFICIENT ROBUST OPTIMIZATON TECHNIQUES FOR UNCERTAIN DENSE GAS FLOWS 100
Comparison of the Stability Properties of Round and Square Liquid Jets 99
Viscous performance of transonic dense gas flows 98
Simulation numérique d’écoulements compressibles turbulents fortement décollés autour de profils oscillants par un schéma de haute précision 98
Multiblock Residual-Based Compact Schemes for the Computation of Complex Turbomachinery Flows 98
Predictive RANS simulations via Bayesian model-scenario averaging 98
Numerical Investigation of High-Speed Turbulent Boundary Layers of Dense Gases 97
Efficient Implementation of Short Fundamental Equations of State for the Numerical Simulation of Dense Gas Flows 97
Robust Shape Optimization of Uncertain Dense Gas Flows Through a Plane Turbine Cascade 97
Numerical study of multistage transcritical ORC axial turbines 96
On the design of high order residual-based dissipation for unsteady compressible flows 95
Finite volume formulation of a third-order residual-based compact scheme for unsteady flow computations 93
High order residual-based compact schemes for aerodynamics and aeroacoustics 92
Effets des approximations numériques et de la modélisation de la turbulence sur la dynamique fine échelle d'un tourbillon de Taylor-Green 91
The high-order dynamic computational laboratory for CFD research and applications 91
Convergence of Fourier-based time methods for turbomachinery wake passing problems 91
A priori tests of turbulence models for compressible flows 89
Numerical study of multistage transcritical ORC axial turbines 89
Bayesian quantification of thermodynamic uncertainties in dense gas flows 89
High-order residual-based compact schemes for compressible flows on overset grids 88
Development of Numerical Schemes for Hybrid Turbulence Modelling in an Industrial CFD Solver 86
Thermochemical non-equilibrium effects in turbulent hypersonic boundary layers 84
Numerical investigation of dense-gas effects in turbomachinery 84
Spectral properties of high-order residual-based compact schemes for unsteady compressible flows 84
Shock impingement on a transitional hypersonic high-enthalpy boundary layer 80
Finite-rate chemistry effects in turbulent hypersonic boundary layers: A direct numerical simulation study 76
Toward improved simulation tools for compressible turbomachinery: assessment of Residual-Based Compact schemes for the transonic compressor NASA Rotor 37 76
Sensitivity Analysis of Dense Gas Flow Simulations to Thermodynamic Uncertainties 75
Totale 10.702
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Categoria #
all - tutte 51.251
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 51.251
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022312 0 6 29 14 44 5 14 33 13 7 34 113
2022/20231.776 90 50 29 75 61 105 6 74 1.202 9 48 27
2023/2024354 34 7 13 14 9 39 5 7 59 100 52 15
2024/20251.301 13 17 25 24 117 122 55 45 479 80 120 204
2025/20264.664 464 498 542 868 487 233 390 154 568 249 155 56
2026/2027316 107 209 0 0 0 0 0 0 0 0 0 0
Totale 10.702