IRIS
PEZZELLA, Giuseppe
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 2.501
EU - Europa 2.282
AS - Asia 657
OC - Oceania 27
AF - Africa 8
SA - Sud America 7
Totale 5.482
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 2.482
IE - Irlanda 943
IT - Italia 507
GB - Regno Unito 341
CN - Cina 234
UA - Ucraina 217
SG - Singapore 212
KR - Corea 116
DE - Germania 68
FI - Finlandia 38
IN - India 32
FR - Francia 31
AU - Australia 27
GR - Grecia 23
RU - Federazione Russa 22
TR - Turchia 22
NL - Olanda 18
CA - Canada 16
SE - Svezia 15
BE - Belgio 13
IR - Iran 10
AT - Austria 8
CZ - Repubblica Ceca 7
ES - Italia 7
HK - Hong Kong 6
PT - Portogallo 6
CH - Svizzera 5
EG - Egitto 4
ID - Indonesia 4
IL - Israele 4
KE - Kenya 4
CY - Cipro 3
JP - Giappone 3
MX - Messico 3
PE - Perù 3
PK - Pakistan 3
PL - Polonia 3
BR - Brasile 2
DK - Danimarca 2
LU - Lussemburgo 2
NO - Norvegia 2
AE - Emirati Arabi Uniti 1
AR - Argentina 1
AZ - Azerbaigian 1
BY - Bielorussia 1
EC - Ecuador 1
KH - Cambogia 1
KZ - Kazakistan 1
LA - Repubblica Popolare Democratica del Laos 1
LB - Libano 1
LT - Lituania 1
MD - Moldavia 1
RO - Romania 1
SA - Arabia Saudita 1
TH - Thailandia 1
Totale 5.482
Salva come PNG Salva come JPEG
Città #
Dublin 938
Santa Clara 654
Jacksonville 513
Chandler 160
Princeton 158
Roxbury 152
Ann Arbor 130
Singapore 128
Cambridge 119
Seoul 103
Napoli 78
Naples 58
Des Moines 52
Nanjing 50
Medford 46
Wilmington 45
New York 39
Boardman 38
Rome 27
Xian 24
Beijing 22
Sydney 21
Redwood City 17
Aversa 15
Woodbridge 15
Caserta 14
Centro 14
Stella Cilento 14
San Leucio 13
Casavatore 11
Milan 11
Brussels 10
Hamburg 10
Helsinki 10
Poona 10
Sala Consilina 10
Ankara 9
Atlanta 9
Hanover 9
Moscow 9
Norwalk 9
Shanghai 9
London 8
Casoria 7
Jinan 7
Los Angeles 7
Salerno 7
Toronto 7
Vienna 7
Zhengzhou 7
Ashburn 6
Brno 6
Enschede 6
Meudon 6
Tehran 6
Afragola 5
Fairfield 5
Houston 5
Livorno 5
San Giuseppe Vesuviano 5
San Mateo 5
Somma Vesuviana 5
Vercelli 5
Villaricca 5
Amsterdam 4
Giugliano in Campania 4
Groningen 4
Jakarta 4
Leiria 4
Mountain View 4
Palermo 4
Portici 4
Qualiano 4
Sant'Anastasia 4
The Hague 4
Torre Del Greco 4
Étagnières 4
Andover 3
Arequipa 3
Avellino 3
Canberra 3
Dallas 3
Genoa 3
Guangzhou 3
Hangzhou 3
Marcianise 3
New Delhi 3
Nicosia 3
Nocera Inferiore 3
Ottawa 3
Potenza 3
Torino 3
Turin 3
Vega 3
Auburn Hills 2
Barletta 2
Baudour 2
Bhuj 2
Bologna 2
Bourg-la-reine 2
Totale 4.030
Salva come PNG Salva come JPEG
Nome #
Multidisciplinary Design and Flight Test of the HEXAFLY-INT Experimental Flight Vehicle 82
MINI IRENE - Deployable Heat Shield for Suborbital Flight Test 74
Aerothermodynamic analysis of a space vehicle for manned exploration missions to Mars 69
Aeroshape design of reusable re-entry vehicles by multidisciplinary optimization and computational fluid dynamics 64
Aerodynamic analysis of a manned space vehicle for missions to Mars 62
Heat transfer analysis for a winged reentry flight test bed 61
Aerodynamic Performance Analysis of a Winged Re-Entry Vehicle From Hypersonic Down to Subsonic Speed 60
Aerodynamic Performance Analysis of an Unmanned Re-Entry Vehicle from Hypersonic Down to Subsonic Regime 59
Influence of surface catalyticity on reentry aerothermodynamics and heat shield 57
A New Philosophy for the Design of Re-Entry Vehicles 57
Aerodynamics analysis of a capsule vehicle for a manned exploration mission to Mars 56
Aerodynamic Analysis with Separation Dynamics of a Launcher at Staging Conditions 56
Aerodynamic Analysis of an Unmanned Aerial Vehicle at Hypersonic Speed 56
Effects of finite rate chemical models on the aerothermodynamics of reentry capsules 53
Aerodynamic analysis of a Mars exploration manned capsule 52
Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles 52
Aerodynamic Performance Analysis of Three Different Vehicle Concepts at Hypersonic Speed 51
LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE RE-ENTRY VEHICLE 51
An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles 51
Aerodynamic and Aerothermodynamic Database of the HEXAFLYINT Hypersonic Glider 50
Hypersonic Vehicles Past, Present and Future Developments 50
Aerodynamics and aerothermodynamics assessment of a Mars sample return mission 49
Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions 48
Hypersonic Vehicles - Applications, Recent Advances, and Perspectives 48
Aerodynamic and thermal design of a space vehicle entering the Mars atmosphere 47
Aerodynamic Analysis of the USV3 Vehicle from Hypersonic to Landing Flight Conditions 47
Computational flowfield analysis over a blunt body reentry vehicle, Journal of Spacecraft and Rockets 46
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 46
Analysis of thermochemical modelling and surface catalyticity in space vehicles reentry 46
Aerothermochemical flowfield around space vehicles for manned missions to Mars 46
Aerothermodynamics and thermal design for on-ground and in-flight testing of a deployable heat shield capsule 46
Multidisciplinary Design of Reusable Re-Entry Vehicles by Optimization and Computational Fluid Dynamics 45
Non-Equilibrium Computational Flowfield Analysis for the Design of Mars Manned Entry Vehicles 44
Preliminary Design of Minimum Weight Configurations for a Reentry Vehicle 44
Phase-A design of a reusable re-entry vehicle 44
Sensitivity Analysis for the Numerical Simulation of an Engine Air Cooling System 43
MINI-IRENE: Design of Deployable Heat Shield Capsule for a Sounding Rocket Flight Experiment 43
Ablative Heatshield Design for a Sample Return Vehicle 43
Introductory Chapter: The Challenge to Fly Faster and Higher 43
Aerothermodynamic analysis of an Apollo-like reentry vehicle 41
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 41
Aero-thermal Trade-off Analysis of the Italian USV Re-Entry Flying Test Bed 41
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 40
Aerodynamic Performance Analysis of Three Different Vehicle Concepts 40
Nonequilibrium aerothermodynamics for a capsule reentry vehicle 39
Fluid Dynamics Analysis of a Space Vehicle Entering the Mars Atmosphere 39
Computational Flowfield Analysis of a Planetary Entry Vehicle 39
Analysis of flowfield past a sample return capsule with heatshield ablation 39
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 39
Aerodynamic analysis of a supersonic transport aircraft at landing speed conditions 39
A Numerical Procedure for Variable-Pitch Law Formulation of Vertical-Axis Wind Turbines 38
Non-equilibrium Computational Flowfield Analysis for Mars Entry Manned 38
Launcher Aerodynamics: a Suitable Investigation Approach at Phase-A Design Level 38
Additive Layer Manufacturing For Entry Capsules 38
Next Generation Launchers Aerodynamics 37
An Aerothermal Analysis of an Engine Nacelle for a General Aviation Airplane Model 37
Overview of design analysis of a space mission for sample returning from Mars 36
A Fast Pod-Based Aerothermal Design Environment Tool 36
Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle 36
Computational Flowfield Analysis of a Next Generation Launcher 36
Aerodynamic and Aerothermodynamic Trade-off Analysis of a Small Hypersonic Flying Test Bed 36
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 35
Effects of surface catalyticity on computed heat transfer over a reentry vehicle 35
A simplified methodology to simulate a heat exchanger in an aircraft's oil cooler by means of a Porous Media model 35
Launcher Aerodynamic Analysis With Plume Effects 35
High and Low Speed Analysis of a Re-usable Unmanned Re-entry Vehicle 35
A POD-Based Reduced Order Model for the Simulation of Scirocco PWT Nozzles 35
MINI-IRENE: Design of a Capsule with Deployable Heat Shield for a Sounding Rocket Flight Experiment 35
Low speed longitudinal aerodynamics of a blended wing-body re-entry vehicle 35
Assessment of predictive capabilities for aerodynamic heating in hypersonic flow 34
Overview of research activities on Hypersonic Vehicles at the Department of Engineering of the University of Campania “L. Vanvitelli” 34
Thermal investigation of a nacelle internal and external fields in pusher configuration 33
Aerodynamic and Aerothermodynamic Analysis of High Speed Earth Re-Entry Capsule 33
An aerothermodynamic design optimization framework for hypersonic vehicles 33
A Spline Based Algorithm for the Analysis of the Flow in Scirocco Plasma Wind Tunnel Nozzle 33
Re-entry Aerodynamics and Aerothermodynamics Analyses of the Flying Test Bed USV-X in the Framework of a High Lift Return 33
Aerodynamic and Aerothermodynamic design of Future Launchers Preparatory Program Concepts 33
Hypersonic Aerothermal Environment Assessment of the CIRA FTB-X Reentry Vehicle 33
Aerodynamic Database Development of the ESA Intermediate Experimental Vehicle 33
Aerodynamic and Aerothermodynamic of the USV3 Re-entry Vehicle 33
Design Analysis of the High-Speed Experimental Flight Test Vehicle HEXAFLY-International 33
Catalytic effects on non-equilibrium aerothermodynamics of a reentry vehicle 32
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 32
A reduced Order Model for a Rapid Evaluation of Scirocco PWT Nozzles Flowfield 32
Overview of Design Approach for a Sample Return Capsule 32
Introductory Chapter: Hypersonic Vehicles - Past, Present, and Future Insights 32
Low Speed Aerodynamic Analysis of the N2A Hybrid Wing–Body 32
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 31
Numerical and Experimental Research on Aerodynamics of High Speed Passenger Vehicle within the Hexafly-Int Project 31
Computational analysis of the flowfield past a returning capsule at super-orbital speed 31
Numerical Analysis of the Flowfield Past a Next Generation Launcher 31
Aerothermodynamics Study of an Advanced Thermal Protection System 31
Analisi di un Veicolo Rientrante a Bordi d'Attacco Aguzzi 31
Airfoil aerodynamic optimization for Mars exploration aircraft 30
Aerodynamic Characterization of HEXAFLY Scramjet Propelled Hypersonic Vehicle 30
Supersonic Combustion Ram-Jet Configuration with Hydrocarbon Fue 30
Computational Flowfield Analyses of hypersonic Problems with Reacting Boundary Layer 30
Aerothermodynamic Design of an Ablative Heat Shield for a Sample Return Vehicle 30
Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle 29
Flap Effectiveness Appraisal for Winged Re-Entry Vehicles 29
Totale 4.148
Salva come PNG Salva come JPEG
Categoria #
all - tutte 30.658
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 30.658
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020263 0 0 0 0 0 5 164 16 19 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
2024/20251.043 21 114 93 49 396 370 0 0 0 0 0 0
Totale 5.828