IRIS
VIVIANI, Antonio
 Distribuzione geografica
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Continente #
EU - Europa 11.214
NA - Nord America 5.291
AS - Asia 4.212
SA - Sud America 830
AF - Africa 71
OC - Oceania 28
Continente sconosciuto - Info sul continente non disponibili 5
Totale 21.651
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Nazione #
RU - Federazione Russa 7.176
US - Stati Uniti d'America 5.214
SG - Singapore 1.661
IE - Irlanda 1.283
IT - Italia 870
CN - Cina 850
HK - Hong Kong 719
BR - Brasile 710
UA - Ucraina 623
GB - Regno Unito 545
VN - Vietnam 355
DE - Germania 215
KR - Corea 203
FI - Finlandia 162
IN - India 121
TR - Turchia 94
GR - Grecia 85
SE - Svezia 78
FR - Francia 51
AR - Argentina 45
NL - Olanda 41
CA - Canada 38
JP - Giappone 37
BD - Bangladesh 30
ID - Indonesia 30
AU - Australia 28
EC - Ecuador 26
MX - Messico 21
IQ - Iraq 20
PK - Pakistan 16
AT - Austria 15
BE - Belgio 15
DZ - Algeria 15
IR - Iran 15
PY - Paraguay 12
EG - Egitto 11
PL - Polonia 11
ZA - Sudafrica 11
MA - Marocco 10
VE - Venezuela 10
PE - Perù 9
CO - Colombia 8
KE - Kenya 8
SA - Arabia Saudita 8
CH - Svizzera 7
ES - Italia 7
UZ - Uzbekistan 7
ET - Etiopia 6
UY - Uruguay 6
CZ - Repubblica Ceca 5
BH - Bahrain 4
EU - Europa 4
NP - Nepal 4
PT - Portogallo 4
AE - Emirati Arabi Uniti 3
AL - Albania 3
CL - Cile 3
DO - Repubblica Dominicana 3
HN - Honduras 3
IL - Israele 3
JM - Giamaica 3
JO - Giordania 3
LU - Lussemburgo 3
MY - Malesia 3
OM - Oman 3
PH - Filippine 3
TH - Thailandia 3
TN - Tunisia 3
TW - Taiwan 3
AZ - Azerbaigian 2
BY - Bielorussia 2
CR - Costa Rica 2
DK - Danimarca 2
GA - Gabon 2
IS - Islanda 2
KG - Kirghizistan 2
KH - Cambogia 2
KZ - Kazakistan 2
LB - Libano 2
PA - Panama 2
BA - Bosnia-Erzegovina 1
BB - Barbados 1
BG - Bulgaria 1
BN - Brunei Darussalam 1
BO - Bolivia 1
BW - Botswana 1
CG - Congo 1
CI - Costa d'Avorio 1
CU - Cuba 1
GE - Georgia 1
GT - Guatemala 1
HR - Croazia 1
HU - Ungheria 1
LT - Lituania 1
MD - Moldavia 1
MG - Madagascar 1
MM - Myanmar 1
MU - Mauritius 1
NI - Nicaragua 1
NO - Norvegia 1
Totale 21.646
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Città #
Moscow 2.502
Dublin 1.279
Jacksonville 1.019
Santa Clara 783
Hong Kong 711
Singapore 516
San Jose 514
Chandler 428
Princeton 221
Ann Arbor 215
Ashburn 197
Seoul 196
Roxbury 159
Medford 141
Napoli 136
Ho Chi Minh City 125
Naples 107
Cambridge 99
Hefei 93
Boardman 91
Wilmington 85
Beijing 81
Hanoi 69
New York 61
São Paulo 58
San Mateo 50
Rome 48
Caserta 46
Woodbridge 45
The Dalles 41
Bengaluru 39
Sala Consilina 37
Des Moines 35
Dallas 33
Jinan 31
Giugliano in Campania 30
Nanjing 30
Aversa 27
Da Nang 25
Los Angeles 23
Atlanta 22
Rio de Janeiro 22
San Leucio 21
Sydney 21
Norwalk 19
Haiphong 18
Porto Alegre 18
Hamburg 17
Milan 17
Houston 16
Redwood City 16
Brasília 13
Brussels 13
Hangzhou 13
Amsterdam 12
Chennai 12
Düsseldorf 12
Baghdad 11
Battipaglia 11
Casavatore 11
Casoria 11
London 11
Toronto 11
Helsinki 10
Hải Dương 10
Mountain View 10
Orem 10
Poona 10
Pozzuoli 10
Shanghai 10
Tianjin 10
Zhengzhou 10
Ankara 9
Belo Horizonte 9
Curitiba 9
Thái Bình 9
Viterbo 9
Campinas 8
Changsha 8
Manchester 8
Munich 8
Shenyang 8
Vienna 8
Auburn Hills 7
Biên Hòa 7
Calgary 7
Chicago 7
Frankfurt am Main 7
Guarulhos 7
Jeddah 7
Maceió 7
New Delhi 7
Pune 7
Recife 7
Stella Cilento 7
Tashkent 7
Villaricca 7
Wuhan 7
Afragola 6
Bremen 6
Totale 11.074
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Nome #
Aeroshape design of reusable re-entry vehicles by multidisciplinary optimization and computational fluid dynamics 163
A Numerical Procedure for Variable-Pitch Law Formulation of Vertical-Axis Wind Turbines 154
Aerodinamica Numerica e Supercalcolatori 148
A corrected vortex blob method for 3D thermal buoyant flows 146
Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions 141
Aerodynamic analysis of a manned space vehicle for missions to Mars 138
Aerodynamic Performance Analysis of a Winged Re-Entry Vehicle From Hypersonic Down to Subsonic Speed 136
An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles 136
Aerodynamic Analysis with Separation Dynamics of a Launcher at Staging Conditions 135
PRELIMINARY DESIGN OF VARIABLE-PITCH SYSTEMS FOR DARREIUS WIND TURBINE USING A GENETIC ALGORITHM BASED OPTIMIZATION PROCEDURE. 135
Aerodynamic analysis of a supersonic transport aircraft at landing speed conditions 135
A Vortex-thermal blobs method for unsteady buoyancy driven flows 134
Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles 132
A Hybrid Model based on POD and Domain Decomposition to Compute the 2-D Aerodynamics Flow Field 130
Aerodynamic Analysis of an Unmanned Aerial Vehicle at Hypersonic Speed 130
Aerodynamic analysis of a Mars exploration manned capsule 128
3D numerical simulations of thermodiffusion experiment for a ternary mixture on-board Foton 127
A Validation of a Hybrid Model for 2D Transonic Flow Field Analysis 127
An optimization-based procedure for self-generation of Re-entry Vehicles shape 126
A non-equilibrium thermochemical model for hypersonic air flow 122
Use of Magnetic Field to Reduce Convection in Low Prandtl Number Liquid Bridges 119
Aerodynamic optimization of airfoils shape for atmospheric flight on Mars planet 118
Aerodynamic Performance Analysis of an Unmanned Re-Entry Vehicle from Hypersonic Down to Subsonic Regime 118
Grid free Lagrangian blobs vortex method with Brinkman layer domain embedding approach for heterogeneous unsteady thermo fluid dynamics problems 117
Design of mass saving configurations for winged reentry vehicles 117
Nonlinear convective oscillations in two-layer systems under the action of the horizontal component of the temperature gradient 114
Effects of Non-Linear Tension on Combined Free Convection in Cavities 114
Spectroscopic determination of chemical species and non-equilibrium temperatures for air flows in a plasma wind tunnel, Journal of Thermophysics and Heat Transfer 113
Aerothermodynamic analysis of a space vehicle for manned exploration missions to Mars 113
Bubbles and Drops behaviour under low-gravity - A space experiment for the IML-2 mission 113
Hypersonic Vehicles Past, Present and Future Developments 113
CFD design capabilities for next generation high-speed aircraft 113
The influence of medium compressibility on chemical reaction rates – Part II: Numerical Experiments 111
Aerodynamic and thermal design of a space vehicle entering the Mars atmosphere 111
Multi-objective optimization for re-entry spacecraft conceptual design using a free-form shape generator 111
Hypersonic Vehicles - Applications, Recent Advances, and Perspectives 111
Application of extended irreversible thermodynamics to the modelling of non-equilibrium hypersonic flows 110
Multidisciplinary Design of Reusable Re-Entry Vehicles by Optimization and Computational Fluid Dynamics 109
Heat transfer analysis for a winged reentry flight test bed 108
WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS 106
Parametric Integral Soft Objects-based Procedure for Thermal Protection System Modeling of Reusable Launch Vehicle 106
LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE RE-ENTRY VEHICLE 106
Torque maximization of vertical axis wind turbines with variable pitch law 106
Phase-A design of a reusable re-entry vehicle 106
Marangoni-Buoyant Boundary Layers 105
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 105
Nonlinear convective oscillations with different symmetry properties in two-layer systems 104
Experimental Study of Surfactant Transfer in Fluid Systems in Microgravity Conditions 104
Threshold onset of Marangoni convection in narrow channels 104
Non-Equilibrium Computational Flowfield Analysis for the Design of Mars Manned Entry Vehicles 104
Experimental considerations of solutocapillary flow initiation on bubble/drop interface in presence of a soluble surfactant 104
Aerodynamics analysis of a capsule vehicle for a manned exploration mission to Mars 104
Airfoil aerodynamic optimization for Mars exploration aircraft 103
Aerodynamic Performance Analysis of Three Different Vehicle Concepts at Hypersonic Speed 103
Oscillatory Marangoni convection around bubbles and drops in heterogeneous solutions of surfactants 102
Symmetric and asymmetric convective oscillations in a multilayer system 102
Influence of surface catalyticity on reentry aerothermodynamics and heat shield 102
The Influence of the horizontal component of the temperature gradient on nonlinear convective oscillations in two-layer systems 102
Experimental Analysis of a Space Re-Entry Vehicle at Landing Conditions 101
Preliminary Design of Minimum Weight Configurations for a Reentry Vehicle 101
Free topology generation of thermal protection system for reusable space vehicles using integral soft objects 101
Introductory Chapter: The Challenge to Fly Faster and Higher 101
Aeroshape Design and Low speed Aerodynamic Analysis of a Crew Return Vehicle 100
Aerodynamic Analysis of a High-Speed Aircraft from Hypersonic down to Subsonic Speeds 100
Low Speed Aerodynamic Analysis of the N2A Hybrid Wing–Body 100
Thermocapillary bubble migration in confined medium 99
Different types of nonlinear convective oscillations in a multilayer system 99
Buoyant vortex ring impinging on a porous layer 99
Vortex Ring Buoyant Plume on Porous Bodyin Thermal Non-Equilibrium 99
Thermocapillary Flows in Two-Fluids Liquid Bridges 98
Launcher Aerodynamics: a Suitable Investigation Approach at Phase-A Design Level 98
Effects of Variable Transport Properties on Thermal Marangoni Flows 97
Equilibrium Instability, Internal Flows, Motion and Overturn of Dissolving Drops 97
Aerothermodynamic analysis of an Apollo-like reentry vehicle 97
Similar solutions of double-diffusive dissipative layers along free surface 96
Nonlinear convective flows in multilayer fluid system 96
Coupling between flow velocity and non-equilibrium internal processes in hypersonic flow aerothermochemistry 96
Analysis of Subsonic/Hypersonic Aerodynamics of a High-Speed Aircraft 95
Experimental Studies of Marangoni Convection in Thin Liquid Layers Caused by Soluble Surfactant 95
On thermal stress and thermal creep convection in vapour crystal growth under microgravity 95
Effects of finite rate chemical models on the aerothermodynamics of reentry capsules 95
Overview of research activities on Hypersonic Vehicles at the Department of Engineering of the University of Campania “L. Vanvitelli” 95
The Influence of the Horizontal Component of the Temperature Gradient on nonlinear Oscillatory Convective Regimes in Multilayer System 94
Aerodynamics and aerothermodynamics assessment of a Mars sample return mission 94
Fluid Dynamics Analysis of a Space Vehicle Entering the Mars Atmosphere 94
Standing Oscillations and Traveling Waves in Two - Layer Systems with an Inclined Temperature Gradient 94
Fluid dynamic modelling of crystal growth from vapour 93
Nonequilibrium aerothermodynamics for a capsule reentry vehicle 93
Double diffusion convection under sinusoidal modulations of low frequency vibrations 93
Overview of design analysis of a space mission for sample returning from Mars 93
Aerodynamic Performance Analysis of Three Different Vehicle Concepts 93
Oscillatory Marangoni convection around the air bubble in a vertical surfactant stratification. 92
Non linear regimes of anticonvection, thermocapillarity, and Rayleigh-Benard convection in two-layer systems 92
Computational flowfield analysis over a blunt body reentry vehicle, Journal of Spacecraft and Rockets 92
Computational analysis of the flowfield past a returning capsule at super-orbital speed 92
Low speed longitudinal aerodynamics of a blended wing-body re-entry vehicle 92
Multi-disciplinary optimization of a space re-entry vehicle using skeleton-based integral soft objects 91
Experimental study of Marangoni bubble migration in normal gravity 91
Nonlinear development of oscillatory instability in a three-layer system under the joint action of buoyancy and thermocapillary effect 91
Thermal and concentrational Marangoni convection at the liquid/air bubble interface 91
Totale 10.869
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Categoria #
all - tutte 80.508
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 80.508
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202119 0 0 0 0 0 0 0 0 0 0 0 19
2021/20221.212 62 7 21 5 457 21 6 30 49 18 132 404
2022/20232.033 273 12 25 108 164 126 0 120 1.147 14 21 23
2023/20241.012 66 21 36 83 328 64 8 23 14 18 64 287
2024/20253.195 16 131 107 52 528 382 273 208 393 785 171 149
2025/202611.106 262 318 558 718 914 6.666 476 311 489 241 118 35
Totale 22.000