IRIS
PEZZELLA, Giuseppe
 Distribuzione geografica
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Continente #
EU - Europa 8.170
NA - Nord America 3.560
AS - Asia 3.384
SA - Sud America 791
AF - Africa 52
OC - Oceania 32
Totale 15.989
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Nazione #
RU - Federazione Russa 5.493
US - Stati Uniti d'America 3.487
SG - Singapore 1.343
IE - Irlanda 944
IT - Italia 749
CN - Cina 680
BR - Brasile 672
HK - Hong Kong 527
GB - Regno Unito 376
VN - Vietnam 302
KR - Corea 225
UA - Ucraina 222
DE - Germania 91
IN - India 84
FR - Francia 71
AR - Argentina 41
NL - Olanda 39
FI - Finlandia 38
CA - Canada 36
ID - Indonesia 35
TR - Turchia 35
AU - Australia 32
EC - Ecuador 29
BD - Bangladesh 24
AT - Austria 23
GR - Grecia 23
IQ - Iraq 21
MX - Messico 21
SE - Svezia 19
JP - Giappone 18
PK - Pakistan 18
BE - Belgio 16
VE - Venezuela 15
ES - Italia 13
IR - Iran 13
MA - Marocco 13
PL - Polonia 13
PY - Paraguay 12
ZA - Sudafrica 12
EG - Egitto 9
CO - Colombia 8
CZ - Repubblica Ceca 7
SA - Arabia Saudita 7
AZ - Azerbaigian 6
KE - Kenya 6
PE - Perù 6
PT - Portogallo 6
CH - Svizzera 5
IL - Israele 5
TW - Taiwan 5
BY - Bielorussia 4
CY - Cipro 4
UY - Uruguay 4
UZ - Uzbekistan 4
BB - Barbados 3
BH - Bahrain 3
CL - Cile 3
DZ - Algeria 3
GT - Guatemala 3
JM - Giamaica 3
KZ - Kazakistan 3
LB - Libano 3
NP - Nepal 3
TH - Thailandia 3
AE - Emirati Arabi Uniti 2
CR - Costa Rica 2
DK - Danimarca 2
DO - Repubblica Dominicana 2
KH - Cambogia 2
LT - Lituania 2
LU - Lussemburgo 2
MY - Malesia 2
NO - Norvegia 2
OM - Oman 2
PH - Filippine 2
SN - Senegal 2
TN - Tunisia 2
AL - Albania 1
AO - Angola 1
BA - Bosnia-Erzegovina 1
BG - Bulgaria 1
BO - Bolivia 1
CI - Costa d'Avorio 1
ET - Etiopia 1
GE - Georgia 1
HN - Honduras 1
HR - Croazia 1
HU - Ungheria 1
JO - Giordania 1
LA - Repubblica Popolare Democratica del Laos 1
LV - Lettonia 1
MD - Moldavia 1
MT - Malta 1
MU - Mauritius 1
NI - Nicaragua 1
PA - Panama 1
RO - Romania 1
RS - Serbia 1
TG - Togo 1
Totale 15.989
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Città #
Moscow 1.921
Dublin 940
Santa Clara 661
San Jose 537
Hong Kong 518
Jacksonville 514
Singapore 417
Seoul 208
Chandler 160
Princeton 158
Roxbury 152
Ann Arbor 130
Cambridge 120
Naples 109
Ashburn 102
Ho Chi Minh City 99
Napoli 78
Beijing 71
Hefei 68
Hanoi 64
São Paulo 59
Des Moines 53
Nanjing 51
Medford 47
New York 45
Wilmington 45
Boardman 38
Rome 38
Dallas 29
Aversa 28
Giugliano in Campania 26
The Dalles 24
Xian 24
Bengaluru 23
Rio de Janeiro 23
Sydney 22
Da Nang 21
Atlanta 20
London 19
Milan 18
Redwood City 17
Vienna 15
Woodbridge 15
Brasília 14
Casalnuovo di Napoli 14
Caserta 14
Centro 14
Guayaquil 14
Los Angeles 14
Stella Cilento 14
Belo Horizonte 13
Haiphong 13
San Leucio 13
Shanghai 13
Baghdad 11
Casavatore 11
Porto Alegre 11
Amsterdam 10
Ankara 10
Brussels 10
Guangzhou 10
Hamburg 10
Helsinki 10
Poona 10
Pozzuoli 10
Sala Consilina 10
Biên Hòa 9
Curitiba 9
Guarulhos 9
Hanover 9
Norwalk 9
Thái Bình 9
Thái Nguyên 9
Toronto 9
Viterbo 9
Chicago 8
Houston 8
Nuremberg 8
Santo André 8
Zhengzhou 8
Casoria 7
Frankfurt am Main 7
Jakarta 7
Jinan 7
Kolkata 7
Paris 7
Recife 7
Salerno 7
Villaricca 7
Afragola 6
Baku 6
Betim 6
Brno 6
Campinas 6
Caxias do Sul 6
Cimitile 6
Enschede 6
Hangzhou 6
Jeddah 6
Meudon 6
Totale 8.250
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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
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
Aerodynamic analysis of a supersonic transport aircraft at landing speed conditions 135
Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles 132
Multidisciplinary Design and Flight Test of the HEXAFLY-INT Experimental Flight Vehicle 131
Aerodynamic Analysis of an Unmanned Aerial Vehicle at Hypersonic Speed 130
MINI IRENE - Deployable Heat Shield for Suborbital Flight Test 130
Aerodynamic analysis of a Mars exploration manned capsule 128
A New Philosophy for the Design of Re-Entry Vehicles 123
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
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 114
Aerothermodynamic analysis of a space vehicle for manned exploration missions to Mars 113
Hypersonic Vehicles Past, Present and Future Developments 113
CFD design capabilities for next generation high-speed aircraft 113
Aerodynamic Analysis of the USV3 Vehicle from Hypersonic to Landing Flight Conditions 112
Aerodynamic and thermal design of a space vehicle entering the Mars atmosphere 111
Ablative Heatshield Design for a Sample Return Vehicle 111
Hypersonic Vehicles - Applications, Recent Advances, and Perspectives 111
A Fast Pod-Based Aerothermal Design Environment Tool 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
Additive Layer Manufacturing For Entry Capsules 107
WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS 106
LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE RE-ENTRY VEHICLE 106
Phase-A design of a reusable re-entry vehicle 106
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 105
Assessment of predictive capabilities for aerodynamic heating in hypersonic flow 105
Non-Equilibrium Computational Flowfield Analysis for the Design of Mars Manned Entry Vehicles 104
Aerodynamics analysis of a capsule vehicle for a manned exploration mission to Mars 104
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 104
Airfoil aerodynamic optimization for Mars exploration aircraft 103
Aerodynamic Performance Analysis of Three Different Vehicle Concepts at Hypersonic Speed 103
Influence of surface catalyticity on reentry aerothermodynamics and heat shield 102
Experimental Analysis of a Space Re-Entry Vehicle at Landing Conditions 101
Preliminary Design of Minimum Weight Configurations for a Reentry Vehicle 101
Aero-thermal Trade-off Analysis of the Italian USV Re-Entry Flying Test Bed 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
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 100
Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle 100
A POD-Based Reduced Order Model for the Simulation of Scirocco PWT Nozzles 100
Low Speed Aerodynamic Analysis of the N2A Hybrid Wing–Body 100
Aerodynamic and Aerothermodynamic Database of the HEXAFLYINT Hypersonic Glider 99
Launcher Aerodynamics: a Suitable Investigation Approach at Phase-A Design Level 98
Aerothermodynamic analysis of an Apollo-like reentry vehicle 97
MINI-IRENE: Design of Deployable Heat Shield Capsule for a Sounding Rocket Flight Experiment 97
A simplified methodology to simulate a heat exchanger in an aircraft's oil cooler by means of a Porous Media model 97
Hypersonic Aerothermal Environment Assessment of the CIRA FTB-X Reentry Vehicle 96
Analysis of Subsonic/Hypersonic Aerodynamics of a High-Speed Aircraft 95
Effects of finite rate chemical models on the aerothermodynamics of reentry capsules 95
A Spline Based Algorithm for the Analysis of the Flow in Scirocco Plasma Wind Tunnel Nozzle 95
Overview of research activities on Hypersonic Vehicles at the Department of Engineering of the University of Campania “L. Vanvitelli” 95
Aerothermodynamics and thermal design for on-ground and in-flight testing of a deployable heat shield capsule 95
Aerodynamics and aerothermodynamics assessment of a Mars sample return mission 94
Fluid Dynamics Analysis of a Space Vehicle Entering the Mars Atmosphere 94
Nonequilibrium aerothermodynamics for a capsule reentry vehicle 93
Overview of design analysis of a space mission for sample returning from Mars 93
Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle 93
Aerodynamic Performance Analysis of Three Different Vehicle Concepts 93
An aerothermodynamic design optimization framework for hypersonic vehicles 93
An Aerothermal Analysis of an Engine Nacelle for a General Aviation Airplane Model 93
Computational flowfield analysis over a blunt body reentry vehicle, Journal of Spacecraft and Rockets 92
Aerodynamic Characterization of HEXAFLY Scramjet Propelled Hypersonic Vehicle 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
Computational Flowfield Analysis of a Planetary Entry Vehicle 91
Aerodynamic and Aerothermodynamic Trade-off Analysis of a Small Hypersonic Flying Test Bed 91
SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT 90
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 90
Analysis of thermochemical modelling and surface catalyticity in space vehicles reentry 90
A reduced Order Model for a Rapid Evaluation of Scirocco PWT Nozzles Flowfield 90
Hypersonic Aerothermal Environment Preliminary Definition of the CIRA FTB-X Reentry Vehicle 90
MINI-IRENE: Design of a Capsule with Deployable Heat Shield for a Sounding Rocket Flight Experiment 90
Multidisciplinary optimization and cfd validation for the design of a next generation re-entry glider 90
High and Low Speed Analysis of a Re-usable Unmanned Re-entry Vehicle 89
Aerodynamic and Aerothermodynamic design of Future Launchers Preparatory Program Concepts 89
Numerical Rebuilding of High and Low Enthalpy Hypersonic Flow Test Over a Double Wedge Model 89
Computational Analysis of Shock Wave Boundary Layer Interactions in Non-equilibrium Hypersonic Flow 89
LOW SPEED AERODYNAMICS OF SIX OPTIMISED AND UNCONVENTIONAL RE-ENTRY VEHICLE AEROSHAPES 88
Sensitivity Analysis for the Numerical Simulation of an Engine Air Cooling System 88
Next Generation Launchers Aerodynamics 88
Non-equilibrium Computational Flowfield Analysis for Mars Entry Manned 87
Aerothermochemical flowfield around space vehicles for manned missions to Mars 87
Launcher Aerodynamic Analysis With Plume Effects 87
Aerodynamic Database Development of the ESA Intermediate Experimental Vehicle 87
Sonic Boom generation using open source CFD approach 86
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 86
Introductory Chapter: Hypersonic Vehicles - Past, Present, and Future Insights 86
Phase-A design of a Mars exploration aerial vehicle 86
Subsonic Aerodynamic Analysis of an Unconventional Re-entry Vehicle 85
Supersonic Combustion Ram-Jet Configuration with Hydrocarbon Fue 84
Numerical investigations of classical hypersonic problems; comparison with experimental data 84
Totale 10.273
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Categoria #
all - tutte 59.954
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 59.954
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20216 0 0 0 0 0 0 0 0 0 0 0 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
2025/20268.946 235 274 581 630 767 5.063 257 412 367 237 103 20
Totale 16.361