IRIS
PEZZELLA, Giuseppe
 Distribuzione geografica
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Continente #
EU - Europa 4.400
AS - Asia 3.072
NA - Nord America 2.738
SA - Sud America 781
AF - Africa 43
OC - Oceania 32
Totale 11.066
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Nazione #
US - Stati Uniti d'America 2.688
RU - Federazione Russa 1.882
SG - Singapore 1.211
IE - Irlanda 944
BR - Brasile 664
CN - Cina 629
IT - Italia 625
HK - Hong Kong 518
GB - Regno Unito 368
KR - Corea 225
VN - Vietnam 224
UA - Ucraina 222
DE - Germania 90
IN - India 75
FR - Francia 58
AR - Argentina 41
FI - Finlandia 38
ID - Indonesia 34
TR - Turchia 34
AU - Australia 32
NL - Olanda 32
EC - Ecuador 29
CA - Canada 24
AT - Austria 23
GR - Grecia 23
MX - Messico 20
BD - Bangladesh 19
SE - Svezia 19
IQ - Iraq 17
PK - Pakistan 16
BE - Belgio 15
VE - Venezuela 15
JP - Giappone 14
IR - Iran 13
PL - Polonia 12
MA - Marocco 11
PY - Paraguay 11
ZA - Sudafrica 11
ES - Italia 9
EG - Egitto 8
CO - Colombia 7
CZ - Repubblica Ceca 7
AZ - Azerbaigian 6
PE - Perù 6
PT - Portogallo 6
CH - Svizzera 5
IL - Israele 5
KE - Kenya 5
BY - Bielorussia 4
UY - Uruguay 4
UZ - Uzbekistan 4
BH - Bahrain 3
CL - Cile 3
CY - Cipro 3
DZ - Algeria 3
NP - Nepal 3
SA - Arabia Saudita 3
AE - Emirati Arabi Uniti 2
BB - Barbados 2
DK - Danimarca 2
DO - Repubblica Dominicana 2
KH - Cambogia 2
KZ - Kazakistan 2
LB - Libano 2
LT - Lituania 2
LU - Lussemburgo 2
NO - Norvegia 2
OM - Oman 2
SN - Senegal 2
TN - Tunisia 2
TW - Taiwan 2
AL - Albania 1
AO - Angola 1
BA - Bosnia-Erzegovina 1
BG - Bulgaria 1
BO - Bolivia 1
HR - Croazia 1
HU - Ungheria 1
JM - Giamaica 1
JO - Giordania 1
LA - Repubblica Popolare Democratica del Laos 1
LV - Lettonia 1
MD - Moldavia 1
MT - Malta 1
NI - Nicaragua 1
PH - Filippine 1
RO - Romania 1
RS - Serbia 1
TH - Thailandia 1
Totale 11.066
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Città #
Dublin 940
Santa Clara 658
Moscow 593
Jacksonville 514
Hong Kong 512
Singapore 300
Seoul 208
Chandler 160
Princeton 158
Roxbury 152
Ann Arbor 130
Cambridge 119
Naples 92
Napoli 78
Ho Chi Minh City 76
Hefei 68
Beijing 67
São Paulo 58
Des Moines 53
Nanjing 51
Medford 46
Hanoi 45
Wilmington 45
Ashburn 43
New York 42
Boardman 38
Rome 33
Dallas 28
The Dalles 24
Xian 24
Bengaluru 23
Rio de Janeiro 23
Sydney 22
Aversa 19
Milan 17
Redwood City 17
Da Nang 16
London 16
Vienna 15
Woodbridge 15
Brasília 14
Casalnuovo di Napoli 14
Caserta 14
Centro 14
Guayaquil 14
Stella Cilento 14
Atlanta 13
Belo Horizonte 13
San Leucio 13
Shanghai 13
Los Angeles 12
Casavatore 11
Ankara 10
Brussels 10
Guangzhou 10
Haiphong 10
Hamburg 10
Helsinki 10
Poona 10
Porto Alegre 10
Pozzuoli 10
Sala Consilina 10
Baghdad 9
Curitiba 9
Guarulhos 9
Hanover 9
Norwalk 9
Toronto 9
Biên Hòa 8
Nuremberg 8
Santo André 8
Thái Bình 8
Zhengzhou 8
Amsterdam 7
Casoria 7
Chicago 7
Jakarta 7
Jinan 7
Recife 7
Salerno 7
Thái Nguyên 7
Villaricca 7
Viterbo 7
Baku 6
Betim 6
Brno 6
Campinas 6
Caxias do Sul 6
Enschede 6
Frankfurt am Main 6
Hangzhou 6
Houston 6
Kolkata 6
Meudon 6
Tehran 6
Warsaw 6
Afragola 5
Asunción 5
Canoas 5
Changsha 5
Totale 6.059
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Nome #
Aeroshape design of reusable re-entry vehicles by multidisciplinary optimization and computational fluid dynamics 114
Multidisciplinary Design and Flight Test of the HEXAFLY-INT Experimental Flight Vehicle 109
MINI IRENE - Deployable Heat Shield for Suborbital Flight Test 105
Aerodynamic Performance Analysis of a Winged Re-Entry Vehicle From Hypersonic Down to Subsonic Speed 99
Aerodynamic analysis of a manned space vehicle for missions to Mars 98
A Numerical Procedure for Variable-Pitch Law Formulation of Vertical-Axis Wind Turbines 96
Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles 95
A New Philosophy for the Design of Re-Entry Vehicles 95
Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions 94
Aerodynamic Analysis of an Unmanned Aerial Vehicle at Hypersonic Speed 94
Aerothermodynamic analysis of a space vehicle for manned exploration missions to Mars 91
Aerodynamic Analysis with Separation Dynamics of a Launcher at Staging Conditions 91
Aerodynamic analysis of a Mars exploration manned capsule 88
Hypersonic Vehicles Past, Present and Future Developments 85
Aerodynamic Analysis of the USV3 Vehicle from Hypersonic to Landing Flight Conditions 84
Aerodynamic Performance Analysis of an Unmanned Re-Entry Vehicle from Hypersonic Down to Subsonic Regime 84
Assessment of predictive capabilities for aerodynamic heating in hypersonic flow 84
An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles 84
Aerodynamics analysis of a capsule vehicle for a manned exploration mission to Mars 83
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 81
Aerodynamic Performance Analysis of Three Different Vehicle Concepts at Hypersonic Speed 80
Influence of surface catalyticity on reentry aerothermodynamics and heat shield 79
Multidisciplinary Design of Reusable Re-Entry Vehicles by Optimization and Computational Fluid Dynamics 79
Heat transfer analysis for a winged reentry flight test bed 78
LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE RE-ENTRY VEHICLE 78
Aerodynamic analysis of a supersonic transport aircraft at landing speed conditions 78
Aerodynamic and thermal design of a space vehicle entering the Mars atmosphere 77
Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle 77
Hypersonic Vehicles - Applications, Recent Advances, and Perspectives 77
Aerodynamic optimization of airfoils shape for atmospheric flight on Mars planet 76
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 76
Aerothermodynamic analysis of an Apollo-like reentry vehicle 75
Preliminary Design of Minimum Weight Configurations for a Reentry Vehicle 75
Aerodynamic and Aerothermodynamic Database of the HEXAFLYINT Hypersonic Glider 75
Additive Layer Manufacturing For Entry Capsules 75
WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS 74
MINI-IRENE: Design of Deployable Heat Shield Capsule for a Sounding Rocket Flight Experiment 74
Ablative Heatshield Design for a Sample Return Vehicle 74
Aero-thermal Trade-off Analysis of the Italian USV Re-Entry Flying Test Bed 73
Hypersonic Aerothermal Environment Assessment of the CIRA FTB-X Reentry Vehicle 73
Introductory Chapter: The Challenge to Fly Faster and Higher 73
Nonequilibrium aerothermodynamics for a capsule reentry vehicle 72
Effects of finite rate chemical models on the aerothermodynamics of reentry capsules 72
A Fast Pod-Based Aerothermal Design Environment Tool 72
Launcher Aerodynamics: a Suitable Investigation Approach at Phase-A Design Level 72
A POD-Based Reduced Order Model for the Simulation of Scirocco PWT Nozzles 71
Low Speed Aerodynamic Analysis of the N2A Hybrid Wing–Body 71
Analysis of Subsonic/Hypersonic Aerodynamics of a High-Speed Aircraft 70
Aerodynamics and aerothermodynamics assessment of a Mars sample return mission 70
Fluid Dynamics Analysis of a Space Vehicle Entering the Mars Atmosphere 70
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 70
A Spline Based Algorithm for the Analysis of the Flow in Scirocco Plasma Wind Tunnel Nozzle 70
Aerothermodynamics and thermal design for on-ground and in-flight testing of a deployable heat shield capsule 70
Phase-A design of a reusable re-entry vehicle 70
Computational flowfield analysis over a blunt body reentry vehicle, Journal of Spacecraft and Rockets 69
Computational Flowfield Analysis of a Planetary Entry Vehicle 69
Computational analysis of the flowfield past a returning capsule at super-orbital speed 69
A simplified methodology to simulate a heat exchanger in an aircraft's oil cooler by means of a Porous Media model 69
An Aerothermal Analysis of an Engine Nacelle for a General Aviation Airplane Model 69
High and Low Speed Analysis of a Re-usable Unmanned Re-entry Vehicle 69
CFD design capabilities for next generation high-speed aircraft 69
Airfoil aerodynamic optimization for Mars exploration aircraft 68
Non-Equilibrium Computational Flowfield Analysis for the Design of Mars Manned Entry Vehicles 68
Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle 68
Aerodynamic and Aerothermodynamic design of Future Launchers Preparatory Program Concepts 68
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 67
Analysis of thermochemical modelling and surface catalyticity in space vehicles reentry 67
Sensitivity Analysis for the Numerical Simulation of an Engine Air Cooling System 67
Aerodynamic Performance Analysis of Three Different Vehicle Concepts 67
Next Generation Launchers Aerodynamics 67
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 66
Launcher Aerodynamic Analysis With Plume Effects 66
Aerodynamic and Aerothermodynamic Trade-off Analysis of a Small Hypersonic Flying Test Bed 66
Low speed longitudinal aerodynamics of a blended wing-body re-entry vehicle 66
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 65
Aerodynamic Performance Analysis of the IXV Vehicle 65
Experimental Analysis of a Space Re-Entry Vehicle at Landing Conditions 64
Non-equilibrium Computational Flowfield Analysis for Mars Entry Manned 64
A reduced Order Model for a Rapid Evaluation of Scirocco PWT Nozzles Flowfield 64
Numerical Rebuilding of High and Low Enthalpy Hypersonic Flow Test Over a Double Wedge Model 64
Computational Analysis of Shock Wave Boundary Layer Interactions in Non-equilibrium Hypersonic Flow 64
Aerothermochemical flowfield around space vehicles for manned missions to Mars 63
Numerical investigations of classical hypersonic problems; comparison with experimental data 63
Aerodynamic Database Development of the ESA Intermediate Experimental Vehicle 63
Overview of research activities on Hypersonic Vehicles at the Department of Engineering of the University of Campania “L. Vanvitelli” 63
Multi-disciplinary optimization of a space re-entry vehicle using skeleton-based integral soft objects 62
Computational Flow Field Analyses on Aeronautical Oil Cooling Systems 62
Aerodynamic Characterization of HEXAFLY Scramjet Propelled Hypersonic Vehicle 62
Overview of Design Approach for a Sample Return Capsule 62
Supersonic Combustion Ram-Jet Configuration with Hydrocarbon Fue 62
Evolution of Aerodynamic Shape for a Concept of Autonomous Re-Entry Vehicle 61
An aerothermodynamic design optimization framework for hypersonic vehicles 61
Analysis of flowfield past a sample return capsule with heatshield ablation 60
Sounding Hypersonic Atmospheric Reentry Capsule Shark. Design Realization Flight and Data Interpretation 60
Computational Flowfield Analysis of a Next Generation Launcher 60
MINI-IRENE: Design of a Capsule with Deployable Heat Shield for a Sounding Rocket Flight Experiment 60
Aerodynamic Analysis of a High-Speed Aircraft from Hypersonic down to Subsonic Speeds 59
Overview of design analysis of a space mission for sample returning from Mars 59
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 59
Introductory Chapter: Hypersonic Vehicles - Past, Present, and Future Insights 59
Totale 7.334
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Categoria #
all - tutte 49.081
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 49.081
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021374 0 0 0 0 0 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
2024/20252.630 21 114 93 49 396 384 321 130 289 563 139 131
2025/20264.020 235 274 581 630 767 1.533 0 0 0 0 0 0
Totale 11.435