IRIS
PEZZELLA, Giuseppe
 Distribuzione geografica
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Continente #
EU - Europa 2.190
NA - Nord America 1.809
AS - Asia 565
OC - Oceania 23
AF - Africa 8
SA - Sud America 6
Totale 4.601
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Nazione #
US - Stati Uniti d'America 1.792
IE - Irlanda 941
IT - Italia 441
GB - Regno Unito 340
UA - Ucraina 217
CN - Cina 213
SG - Singapore 162
KR - Corea 111
DE - Germania 66
FI - Finlandia 36
FR - Francia 27
IN - India 26
AU - Australia 23
GR - Grecia 23
TR - Turchia 22
RU - Federazione Russa 21
NL - Olanda 16
SE - Svezia 15
CA - Canada 14
BE - Belgio 13
IR - Iran 10
CZ - Repubblica Ceca 7
ES - Italia 7
AT - Austria 6
PT - Portogallo 6
CH - Svizzera 5
EG - Egitto 4
HK - Hong Kong 4
IL - Israele 4
KE - Kenya 4
CY - Cipro 3
MX - Messico 3
PE - Perù 3
PK - Pakistan 3
BR - Brasile 2
ID - Indonesia 2
JP - Giappone 2
AE - Emirati Arabi Uniti 1
AR - Argentina 1
LB - Libano 1
LT - Lituania 1
NO - Norvegia 1
RO - Romania 1
SA - Arabia Saudita 1
Totale 4.601
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Città #
Dublin 936
Jacksonville 513
Chandler 160
Princeton 158
Roxbury 152
Ann Arbor 130
Cambridge 119
Seoul 103
Singapore 85
Napoli 78
Des Moines 52
Nanjing 50
Medford 46
Wilmington 45
Boardman 38
New York 38
Naples 29
Rome 27
Xian 24
Beijing 21
Sydney 19
Redwood City 17
Woodbridge 15
Caserta 14
Centro 14
Stella Cilento 14
San Leucio 13
Casavatore 11
Brussels 10
Poona 10
Sala Consilina 10
Ankara 9
Hamburg 9
Hanover 9
Milan 9
Norwalk 9
Helsinki 8
Moscow 8
Casoria 7
Jinan 7
London 7
Salerno 7
Toronto 7
Zhengzhou 7
Brno 6
Enschede 6
Meudon 6
Shanghai 6
Tehran 6
Vienna 6
Fairfield 5
Houston 5
Livorno 5
San Giuseppe Vesuviano 5
San Mateo 5
Vercelli 5
Villaricca 5
Ashburn 4
Groningen 4
Leiria 4
Mountain View 4
Palermo 4
Portici 4
Qualiano 4
The Hague 4
Torre Del Greco 4
Étagnières 4
Andover 3
Arequipa 3
Atlanta 3
Avellino 3
Aversa 3
Dallas 3
Giugliano in Campania 3
Los Angeles 3
Marcianise 3
New Delhi 3
Nicosia 3
Nocera Inferiore 3
Ottawa 3
Potenza 3
Torino 3
Turin 3
Vega 3
Afragola 2
Amsterdam 2
Auburn Hills 2
Barletta 2
Baudour 2
Bologna 2
Bourg-la-reine 2
Bremen 2
Broomfield 2
Casalnuovo di Napoli 2
Casandrino 2
Changsha 2
Gif-sur-yvette 2
Hangzhou 2
Holon 2
Islamabad 2
Totale 3.248
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Nome #
Multidisciplinary Design and Flight Test of the HEXAFLY-INT Experimental Flight Vehicle 77
MINI IRENE - Deployable Heat Shield for Suborbital Flight Test 69
Aerothermodynamic analysis of a space vehicle for manned exploration missions to Mars 64
Aerodynamic analysis of a manned space vehicle for missions to Mars 56
Heat transfer analysis for a winged reentry flight test bed 56
Aerodynamic Performance Analysis of a Winged Re-Entry Vehicle From Hypersonic Down to Subsonic Speed 54
Aeroshape design of reusable re-entry vehicles by multidisciplinary optimization and computational fluid dynamics 54
Aerodynamic Performance Analysis of an Unmanned Re-Entry Vehicle from Hypersonic Down to Subsonic Regime 53
Aerodynamics analysis of a capsule vehicle for a manned exploration mission to Mars 52
Influence of surface catalyticity on reentry aerothermodynamics and heat shield 52
A New Philosophy for the Design of Re-Entry Vehicles 51
Aerodynamic Analysis with Separation Dynamics of a Launcher at Staging Conditions 50
Aerodynamic Analysis of an Unmanned Aerial Vehicle at Hypersonic Speed 50
Effects of finite rate chemical models on the aerothermodynamics of reentry capsules 48
Aerodynamic Performance Analysis of Three Different Vehicle Concepts at Hypersonic Speed 47
Aerodynamic analysis of a Mars exploration manned capsule 46
Aerodynamic and Aerothermodynamic Database of the HEXAFLYINT Hypersonic Glider 46
LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE RE-ENTRY VEHICLE 46
Hypersonic Vehicles Past, Present and Future Developments 46
Aerodynamics and aerothermodynamics assessment of a Mars sample return mission 45
Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles 45
An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles 45
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 42
Analysis of thermochemical modelling and surface catalyticity in space vehicles reentry 42
Aerothermochemical flowfield around space vehicles for manned missions to Mars 42
Hypersonic Vehicles - Applications, Recent Advances, and Perspectives 42
Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions 41
Computational flowfield analysis over a blunt body reentry vehicle, Journal of Spacecraft and Rockets 41
Aerodynamic Analysis of the USV3 Vehicle from Hypersonic to Landing Flight Conditions 41
Aerodynamic and thermal design of a space vehicle entering the Mars atmosphere 40
Multidisciplinary Design of Reusable Re-Entry Vehicles by Optimization and Computational Fluid Dynamics 40
Non-Equilibrium Computational Flowfield Analysis for the Design of Mars Manned Entry Vehicles 39
Preliminary Design of Minimum Weight Configurations for a Reentry Vehicle 39
Sensitivity Analysis for the Numerical Simulation of an Engine Air Cooling System 39
MINI-IRENE: Design of Deployable Heat Shield Capsule for a Sounding Rocket Flight Experiment 39
Phase-A design of a reusable re-entry vehicle 39
Aerothermodynamics and thermal design for on-ground and in-flight testing of a deployable heat shield capsule 38
Introductory Chapter: The Challenge to Fly Faster and Higher 38
Aerothermodynamic analysis of an Apollo-like reentry vehicle 37
Ablative Heatshield Design for a Sample Return Vehicle 37
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 36
Aerodynamic Performance Analysis of Three Different Vehicle Concepts 36
Nonequilibrium aerothermodynamics for a capsule reentry vehicle 35
Fluid Dynamics Analysis of a Space Vehicle Entering the Mars Atmosphere 35
Computational Flowfield Analysis of a Planetary Entry Vehicle 35
Analysis of flowfield past a sample return capsule with heatshield ablation 35
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 35
Aero-thermal Trade-off Analysis of the Italian USV Re-Entry Flying Test Bed 35
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 33
Next Generation Launchers Aerodynamics 33
Aerodynamic analysis of a supersonic transport aircraft at landing speed conditions 33
Overview of design analysis of a space mission for sample returning from Mars 32
Non-equilibrium Computational Flowfield Analysis for Mars Entry Manned 32
Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle 32
Computational Flowfield Analysis of a Next Generation Launcher 32
Additive Layer Manufacturing For Entry Capsules 32
Effects of surface catalyticity on computed heat transfer over a reentry vehicle 31
Aerodynamic and Aerothermodynamic Trade-off Analysis of a Small Hypersonic Flying Test Bed 31
Low speed longitudinal aerodynamics of a blended wing-body re-entry vehicle 31
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 30
A Fast Pod-Based Aerothermal Design Environment Tool 30
An Aerothermal Analysis of an Engine Nacelle for a General Aviation Airplane Model 30
Assessment of predictive capabilities for aerodynamic heating in hypersonic flow 30
High and Low Speed Analysis of a Re-usable Unmanned Re-entry Vehicle 30
Thermal investigation of a nacelle internal and external fields in pusher configuration 29
Aerodynamic and Aerothermodynamic Analysis of High Speed Earth Re-Entry Capsule 29
A simplified methodology to simulate a heat exchanger in an aircraft's oil cooler by means of a Porous Media model 29
An aerothermodynamic design optimization framework for hypersonic vehicles 29
Re-entry Aerodynamics and Aerothermodynamics Analyses of the Flying Test Bed USV-X in the Framework of a High Lift Return 29
Launcher Aerodynamic Analysis With Plume Effects 29
Aerodynamic and Aerothermodynamic design of Future Launchers Preparatory Program Concepts 29
Hypersonic Aerothermal Environment Assessment of the CIRA FTB-X Reentry Vehicle 29
A POD-Based Reduced Order Model for the Simulation of Scirocco PWT Nozzles 29
Aerodynamic and Aerothermodynamic of the USV3 Re-entry Vehicle 29
Design Analysis of the High-Speed Experimental Flight Test Vehicle HEXAFLY-International 29
Overview of research activities on Hypersonic Vehicles at the Department of Engineering of the University of Campania “L. Vanvitelli” 29
A Numerical Procedure for Variable-Pitch Law Formulation of Vertical-Axis Wind Turbines 28
Catalytic effects on non-equilibrium aerothermodynamics of a reentry vehicle 28
Overview of Design Approach for a Sample Return Capsule 28
Launcher Aerodynamics: a Suitable Investigation Approach at Phase-A Design Level 28
Aerodynamic Database Development of the ESA Intermediate Experimental Vehicle 28
Introductory Chapter: Hypersonic Vehicles - Past, Present, and Future Insights 28
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 27
Numerical and Experimental Research on Aerodynamics of High Speed Passenger Vehicle within the Hexafly-Int Project 27
Computational analysis of the flowfield past a returning capsule at super-orbital speed 27
Numerical Analysis of the Flowfield Past a Next Generation Launcher 27
Aerothermodynamics Study of an Advanced Thermal Protection System 27
Analisi di un Veicolo Rientrante a Bordi d'Attacco Aguzzi 27
A Spline Based Algorithm for the Analysis of the Flow in Scirocco Plasma Wind Tunnel Nozzle 27
MINI-IRENE: Design of a Capsule with Deployable Heat Shield for a Sounding Rocket Flight Experiment 27
Aerodynamic Characterization of HEXAFLY Scramjet Propelled Hypersonic Vehicle 26
A reduced Order Model for a Rapid Evaluation of Scirocco PWT Nozzles Flowfield 26
Supersonic Combustion Ram-Jet Configuration with Hydrocarbon Fue 26
Computational Flowfield Analyses of hypersonic Problems with Reacting Boundary Layer 26
Low Speed Aerodynamic Analysis of the N2A Hybrid Wing–Body 26
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 25
Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle 25
Flap Effectiveness Appraisal for Winged Re-Entry Vehicles 25
Aerodynamic Performance Analysis of the IXV Vehicle 25
Numerical Simulation of Liquid-structure Interaction Problem in a Tank of a Space Re-entry Vehicle 25
Totale 3.639
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Categoria #
all - tutte 25.791
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 25.791
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020517 0 147 5 16 86 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
2024/2025131 21 110 0 0 0 0 0 0 0 0 0 0
Totale 4.916