PEZZELLA, Giuseppe
 Distribuzione geografica
Continente #
NA - Nord America 2.509
EU - Europa 2.369
AS - Asia 1.630
SA - Sud America 121
OC - Oceania 27
AF - Africa 11
Totale 6.667
Nazione #
US - Stati Uniti d'America 2.486
IE - Irlanda 944
SG - Singapore 662
IT - Italia 568
HK - Hong Kong 494
GB - Regno Unito 342
CN - Cina 238
UA - Ucraina 218
KR - Corea 118
BR - Brasile 103
DE - Germania 75
FI - Finlandia 38
IN - India 36
FR - Francia 31
RU - Federazione Russa 28
AU - Australia 27
TR - Turchia 26
GR - Grecia 23
NL - Olanda 22
CA - Canada 16
SE - Svezia 15
BE - Belgio 13
AT - Austria 12
IR - Iran 10
PK - Pakistan 8
CZ - Repubblica Ceca 7
ES - Italia 7
EC - Ecuador 6
MX - Messico 6
PT - Portogallo 6
AR - Argentina 5
CH - Svizzera 5
ID - Indonesia 5
AZ - Azerbaigian 4
BD - Bangladesh 4
EG - Egitto 4
IL - Israele 4
IQ - Iraq 4
KE - Kenya 4
CY - Cipro 3
JP - Giappone 3
PE - Perù 3
PL - Polonia 3
BY - Bielorussia 2
DK - Danimarca 2
KZ - Kazakistan 2
LU - Lussemburgo 2
NO - Norvegia 2
TW - Taiwan 2
AE - Emirati Arabi Uniti 1
AO - Angola 1
BA - Bosnia-Erzegovina 1
BO - Bolivia 1
CL - Cile 1
JM - Giamaica 1
KH - Cambogia 1
LA - Repubblica Popolare Democratica del Laos 1
LB - Libano 1
LT - Lituania 1
MA - Marocco 1
MD - Moldavia 1
PY - Paraguay 1
RO - Romania 1
SA - Arabia Saudita 1
TH - Thailandia 1
TN - Tunisia 1
UZ - Uzbekistan 1
VE - Venezuela 1
Totale 6.667
Città #
Dublin 939
Santa Clara 654
Jacksonville 513
Hong Kong 488
Chandler 160
Princeton 158
Roxbury 152
Ann Arbor 130
Singapore 128
Cambridge 119
Seoul 103
Naples 87
Napoli 78
Des Moines 52
Nanjing 50
Medford 46
Wilmington 45
New York 39
Boardman 38
Rome 31
Xian 24
Beijing 22
Sydney 21
Aversa 19
Redwood City 17
Milan 16
Woodbridge 15
Caserta 14
Centro 14
Stella Cilento 14
San Leucio 13
Casavatore 11
Brussels 10
Hamburg 10
Helsinki 10
Moscow 10
Poona 10
Sala Consilina 10
Shanghai 10
Vienna 10
Ankara 9
Atlanta 9
Hanover 9
Norwalk 9
London 8
Casoria 7
Jinan 7
Los Angeles 7
Salerno 7
Toronto 7
Villaricca 7
Zhengzhou 7
Ashburn 6
Brno 6
Enschede 6
Meudon 6
Tehran 6
Afragola 5
Fairfield 5
Houston 5
Kolkata 5
Livorno 5
San Giuseppe Vesuviano 5
San Mateo 5
Somma Vesuviana 5
São Paulo 5
Vercelli 5
Amsterdam 4
Baku 4
Falkenstein 4
Giugliano in Campania 4
Groningen 4
Guayaquil 4
Jakarta 4
Leiria 4
Mountain View 4
Nuremberg 4
Orta di Atella 4
Palermo 4
Pomigliano d'Arco 4
Portici 4
Qualiano 4
Sant'Anastasia 4
St Petersburg 4
The Hague 4
Torre Del Greco 4
Étagnières 4
Andover 3
Arequipa 3
Avellino 3
Brasília 3
Canberra 3
Dallas 3
Genoa 3
Guangzhou 3
Guarulhos 3
Hangzhou 3
Marcianise 3
Natal 3
New Delhi 3
Totale 4.582
Nome #
Multidisciplinary Design and Flight Test of the HEXAFLY-INT Experimental Flight Vehicle 86
MINI IRENE - Deployable Heat Shield for Suborbital Flight Test 78
Aerothermodynamic analysis of a space vehicle for manned exploration missions to Mars 75
Aeroshape design of reusable re-entry vehicles by multidisciplinary optimization and computational fluid dynamics 73
Aerodynamic Performance Analysis of a Winged Re-Entry Vehicle From Hypersonic Down to Subsonic Speed 70
Hypersonic Vehicles Past, Present and Future Developments 68
Heat transfer analysis for a winged reentry flight test bed 65
Aerodynamic Performance Analysis of an Unmanned Re-Entry Vehicle from Hypersonic Down to Subsonic Regime 65
Aerodynamic analysis of a manned space vehicle for missions to Mars 64
Aerodynamics analysis of a capsule vehicle for a manned exploration mission to Mars 62
Influence of surface catalyticity on reentry aerothermodynamics and heat shield 62
Aerodynamic Analysis with Separation Dynamics of a Launcher at Staging Conditions 62
Effects of finite rate chemical models on the aerothermodynamics of reentry capsules 61
Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles 61
A New Philosophy for the Design of Re-Entry Vehicles 61
Assessment of predictive capabilities for aerodynamic heating in hypersonic flow 60
Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions 59
Aerodynamic Analysis of an Unmanned Aerial Vehicle at Hypersonic Speed 58
LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE RE-ENTRY VEHICLE 58
Aerodynamic analysis of a Mars exploration manned capsule 56
An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles 56
Aerodynamic Performance Analysis of Three Different Vehicle Concepts at Hypersonic Speed 55
Aerodynamic and Aerothermodynamic Database of the HEXAFLYINT Hypersonic Glider 55
Hypersonic Vehicles - Applications, Recent Advances, and Perspectives 55
Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle 54
Aerodynamics and aerothermodynamics assessment of a Mars sample return mission 53
Aerodynamic Analysis of the USV3 Vehicle from Hypersonic to Landing Flight Conditions 52
Hypersonic Aerothermal Environment Assessment of the CIRA FTB-X Reentry Vehicle 52
Introductory Chapter: The Challenge to Fly Faster and Higher 52
Computational flowfield analysis over a blunt body reentry vehicle, Journal of Spacecraft and Rockets 51
Aerodynamic and thermal design of a space vehicle entering the Mars atmosphere 51
Multidisciplinary Design of Reusable Re-Entry Vehicles by Optimization and Computational Fluid Dynamics 51
Aerothermodynamics and thermal design for on-ground and in-flight testing of a deployable heat shield capsule 51
Phase-A design of a reusable re-entry vehicle 51
Analysis of thermochemical modelling and surface catalyticity in space vehicles reentry 50
Preliminary Design of Minimum Weight Configurations for a Reentry Vehicle 50
Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle 50
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 49
Aerothermochemical flowfield around space vehicles for manned missions to Mars 49
Aerothermodynamic analysis of an Apollo-like reentry vehicle 49
Computational analysis of the flowfield past a returning capsule at super-orbital speed 49
Computational Flowfield Analysis of a Planetary Entry Vehicle 48
Sensitivity Analysis for the Numerical Simulation of an Engine Air Cooling System 48
MINI-IRENE: Design of Deployable Heat Shield Capsule for a Sounding Rocket Flight Experiment 48
Fluid Dynamics Analysis of a Space Vehicle Entering the Mars Atmosphere 47
Non-equilibrium Computational Flowfield Analysis for Mars Entry Manned 47
Aerodynamic analysis of a supersonic transport aircraft at landing speed conditions 47
Non-Equilibrium Computational Flowfield Analysis for the Design of Mars Manned Entry Vehicles 46
Nonequilibrium aerothermodynamics for a capsule reentry vehicle 46
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 46
Launcher Aerodynamics: a Suitable Investigation Approach at Phase-A Design Level 46
Ablative Heatshield Design for a Sample Return Vehicle 46
Aerodynamic Performance Analysis of Three Different Vehicle Concepts 45
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 44
Evolution of Aerodynamic Shape for a Concept of Autonomous Re-Entry Vehicle 44
Next Generation Launchers Aerodynamics 44
Aerodynamic Database Development of the ESA Intermediate Experimental Vehicle 44
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 43
Analysis of flowfield past a sample return capsule with heatshield ablation 43
Computational Flow Field Analyses on Aeronautical Oil Cooling Systems 43
An Aerothermal Analysis of an Engine Nacelle for a General Aviation Airplane Model 43
Launcher Aerodynamic Analysis With Plume Effects 43
High and Low Speed Analysis of a Re-usable Unmanned Re-entry Vehicle 43
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 42
Aero-thermal Trade-off Analysis of the Italian USV Re-Entry Flying Test Bed 42
Computational Analysis of Shock Wave Boundary Layer Interactions in Non-equilibrium Hypersonic Flow 42
Sounding Hypersonic Atmospheric Reentry Capsule Shark. Design Realization Flight and Data Interpretation 41
A Fast Pod-Based Aerothermal Design Environment Tool 41
Aerodynamic and Aerothermodynamic Trade-off Analysis of a Small Hypersonic Flying Test Bed 41
Additive Layer Manufacturing For Entry Capsules 41
Low speed longitudinal aerodynamics of a blended wing-body re-entry vehicle 41
A Numerical Procedure for Variable-Pitch Law Formulation of Vertical-Axis Wind Turbines 40
Overview of design analysis of a space mission for sample returning from Mars 40
Catalytic effects on non-equilibrium aerothermodynamics of a reentry vehicle 40
MINI-IRENE: Design of a Capsule with Deployable Heat Shield for a Sounding Rocket Flight Experiment 40
CFD design capabilities for next generation high-speed aircraft 40
Effects of surface catalyticity on computed heat transfer over a reentry vehicle 39
Aerodynamic and Aerothermodynamic Analysis of High Speed Earth Re-Entry Capsule 39
Computational Flowfield Analysis of a Next Generation Launcher 39
A Spline Based Algorithm for the Analysis of the Flow in Scirocco Plasma Wind Tunnel Nozzle 39
Re-entry Aerodynamics and Aerothermodynamics Analyses of the Flying Test Bed USV-X in the Framework of a High Lift Return 39
Aerodynamic and Aerothermodynamic design of Future Launchers Preparatory Program Concepts 39
A POD-Based Reduced Order Model for the Simulation of Scirocco PWT Nozzles 39
Design Analysis of the High-Speed Experimental Flight Test Vehicle HEXAFLY-International 39
Analysis of Subsonic/Hypersonic Aerodynamics of a High-Speed Aircraft 38
Aerodynamic Characterization of HEXAFLY Scramjet Propelled Hypersonic Vehicle 38
An aerothermodynamic design optimization framework for hypersonic vehicles 38
Aerodynamic and Aerothermodynamic of the USV3 Re-entry Vehicle 38
Numerical Rebuilding of High and Low Enthalpy Hypersonic Flow Test Over a Double Wedge Model 38
Overview of research activities on Hypersonic Vehicles at the Department of Engineering of the University of Campania “L. Vanvitelli” 38
A simplified methodology to simulate a heat exchanger in an aircraft's oil cooler by means of a Porous Media model 37
Numerical investigations of classical hypersonic problems; comparison with experimental data 37
Analisi di un Veicolo Rientrante a Bordi d'Attacco Aguzzi 37
Introductory Chapter: Hypersonic Vehicles - Past, Present, and Future Insights 37
Low Speed Aerodynamic Analysis of the N2A Hybrid Wing–Body 37
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 36
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 36
A reduced Order Model for a Rapid Evaluation of Scirocco PWT Nozzles Flowfield 36
Numerical and Experimental Research on Aerodynamics of High Speed Passenger Vehicle within the Hexafly-Int Project 36
Thermal investigation of a nacelle internal and external fields in pusher configuration 36
Totale 4.819
Categoria #
all - tutte 35.647
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 35.647


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/202059 0 0 0 0 0 0 0 0 0 22 25 12
2020/2021562 38 10 51 28 61 23 159 41 62 40 43 6
2021/2022928 18 6 22 5 318 21 10 22 47 29 110 320
2022/20231.260 186 13 16 24 93 60 1 47 779 5 19 17
2023/2024802 43 19 35 45 264 44 4 13 15 18 48 254
2024/20252.248 21 114 93 49 396 384 321 130 289 451 0 0
Totale 7.033