IRIS
PEZZELLA, Giuseppe
 Distribuzione geografica
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Continente #
EU - Europa 8.199
NA - Nord America 3.725
AS - Asia 3.438
SA - Sud America 793
Continente sconosciuto - Info sul continente non disponibili 380
AF - Africa 52
OC - Oceania 33
Totale 16.620
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Nazione #
RU - Federazione Russa 5.493
US - Stati Uniti d'America 3.644
SG - Singapore 1.387
IE - Irlanda 944
IT - Italia 770
CN - Cina 687
BR - Brasile 674
HK - Hong Kong 527
GB - Regno Unito 380
VN - Vietnam 302
KR - Corea 228
UA - Ucraina 222
DE - Germania 93
IN - India 84
FR - Francia 71
AR - Argentina 41
CA - Canada 40
NL - Olanda 40
FI - Finlandia 38
ID - Indonesia 35
TR - Turchia 35
AU - Australia 33
EC - Ecuador 29
BD - Bangladesh 24
AT - Austria 23
GR - Grecia 23
MX - Messico 22
IQ - Iraq 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
PT - Portogallo 7
SA - Arabia Saudita 7
AZ - Azerbaigian 6
KE - Kenya 6
PE - Perù 6
CH - Svizzera 5
IL - Israele 5
JM - Giamaica 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
CR - Costa Rica 3
DZ - Algeria 3
GT - Guatemala 3
KZ - Kazakistan 3
LB - Libano 3
NP - Nepal 3
TH - Thailandia 3
AE - Emirati Arabi Uniti 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 16.240
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Città #
Moscow 1.921
Dublin 940
Santa Clara 687
San Jose 537
Hong Kong 518
Jacksonville 514
Singapore 417
Seoul 211
Chandler 160
Princeton 158
Roxbury 152
Ashburn 146
Ann Arbor 130
Cambridge 120
Naples 113
Ho Chi Minh City 99
Napoli 78
Beijing 74
Hefei 68
Hanoi 64
São Paulo 59
Des Moines 53
Council Bluffs 51
Nanjing 51
Medford 47
New York 45
Wilmington 45
Rome 39
Boardman 38
Aversa 33
Dallas 29
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 19
Redwood City 17
Los Angeles 15
Vienna 15
Woodbridge 15
Brasília 14
Casalnuovo di Napoli 14
Caserta 14
Centro 14
Guayaquil 14
Shanghai 14
Stella Cilento 14
Belo Horizonte 13
Haiphong 13
San Leucio 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
Frankfurt am Main 9
Guarulhos 9
Hanover 9
Norwalk 9
Thái Bình 9
Thái Nguyên 9
Toronto 9
Viterbo 9
Afragola 8
Chicago 8
Houston 8
Nuremberg 8
Santo André 8
Zhengzhou 8
Casoria 7
Jakarta 7
Jinan 7
Kolkata 7
Paris 7
Recife 7
Salerno 7
Villaricca 7
Baku 6
Betim 6
Brno 6
Campinas 6
Caxias do Sul 6
Cimitile 6
Enschede 6
Fairfield 6
Hangzhou 6
Totale 8.388
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Nome #
Aeroshape design of reusable re-entry vehicles by multidisciplinary optimization and computational fluid dynamics 167
A Numerical Procedure for Variable-Pitch Law Formulation of Vertical-Axis Wind Turbines 155
Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions 143
Aerodynamic analysis of a supersonic transport aircraft at landing speed conditions 140
Aerodynamic analysis of a manned space vehicle for missions to Mars 139
Aerodynamic Performance Analysis of a Winged Re-Entry Vehicle From Hypersonic Down to Subsonic Speed 139
Aerodynamic Analysis with Separation Dynamics of a Launcher at Staging Conditions 138
An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles 137
Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles 134
MINI IRENE - Deployable Heat Shield for Suborbital Flight Test 132
Aerodynamic Analysis of an Unmanned Aerial Vehicle at Hypersonic Speed 131
Multidisciplinary Design and Flight Test of the HEXAFLY-INT Experimental Flight Vehicle 131
Aerodynamic analysis of a Mars exploration manned capsule 130
A New Philosophy for the Design of Re-Entry Vehicles 124
Aerodynamic Performance Analysis of an Unmanned Re-Entry Vehicle from Hypersonic Down to Subsonic Regime 120
Aerodynamic optimization of airfoils shape for atmospheric flight on Mars planet 119
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 117
Hypersonic Vehicles Past, Present and Future Developments 115
CFD design capabilities for next generation high-speed aircraft 115
Aerothermodynamic analysis of a space vehicle for manned exploration missions to Mars 114
Aerodynamic and thermal design of a space vehicle entering the Mars atmosphere 114
Hypersonic Vehicles - Applications, Recent Advances, and Perspectives 114
Aerodynamic Analysis of the USV3 Vehicle from Hypersonic to Landing Flight Conditions 113
Multidisciplinary Design of Reusable Re-Entry Vehicles by Optimization and Computational Fluid Dynamics 112
A Fast Pod-Based Aerothermal Design Environment Tool 111
Ablative Heatshield Design for a Sample Return Vehicle 111
Heat transfer analysis for a winged reentry flight test bed 108
Additive Layer Manufacturing For Entry Capsules 108
LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE RE-ENTRY VEHICLE 108
WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS 107
Assessment of predictive capabilities for aerodynamic heating in hypersonic flow 107
Phase-A design of a reusable re-entry vehicle 107
Non-Equilibrium Computational Flowfield Analysis for the Design of Mars Manned Entry Vehicles 106
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 106
Aerodynamic Performance Analysis of Three Different Vehicle Concepts at Hypersonic Speed 106
Airfoil aerodynamic optimization for Mars exploration aircraft 105
Aerodynamics analysis of a capsule vehicle for a manned exploration mission to Mars 105
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 105
Aero-thermal Trade-off Analysis of the Italian USV Re-Entry Flying Test Bed 104
Aerodynamic Analysis of a High-Speed Aircraft from Hypersonic down to Subsonic Speeds 103
Influence of surface catalyticity on reentry aerothermodynamics and heat shield 103
Introductory Chapter: The Challenge to Fly Faster and Higher 103
Experimental Analysis of a Space Re-Entry Vehicle at Landing Conditions 102
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 102
Aeroshape Design and Low speed Aerodynamic Analysis of a Crew Return Vehicle 101
Preliminary Design of Minimum Weight Configurations for a Reentry Vehicle 101
Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle 101
Low Speed Aerodynamic Analysis of the N2A Hybrid Wing–Body 101
A POD-Based Reduced Order Model for the Simulation of Scirocco PWT Nozzles 100
Aerodynamic and Aerothermodynamic Database of the HEXAFLYINT Hypersonic Glider 100
A simplified methodology to simulate a heat exchanger in an aircraft's oil cooler by means of a Porous Media model 99
Launcher Aerodynamics: a Suitable Investigation Approach at Phase-A Design Level 99
Aerothermodynamic analysis of an Apollo-like reentry vehicle 98
MINI-IRENE: Design of Deployable Heat Shield Capsule for a Sounding Rocket Flight Experiment 98
Aerodynamic Performance Analysis of Three Different Vehicle Concepts 98
Hypersonic Aerothermal Environment Assessment of the CIRA FTB-X Reentry Vehicle 98
Analysis of Subsonic/Hypersonic Aerodynamics of a High-Speed Aircraft 97
Aerodynamics and aerothermodynamics assessment of a Mars sample return mission 97
Effects of finite rate chemical models on the aerothermodynamics of reentry capsules 97
A Spline Based Algorithm for the Analysis of the Flow in Scirocco Plasma Wind Tunnel Nozzle 97
Overview of research activities on Hypersonic Vehicles at the Department of Engineering of the University of Campania “L. Vanvitelli” 97
Nonequilibrium aerothermodynamics for a capsule reentry vehicle 95
Fluid Dynamics Analysis of a Space Vehicle Entering the Mars Atmosphere 95
Aerothermodynamics and thermal design for on-ground and in-flight testing of a deployable heat shield capsule 95
Overview of design analysis of a space mission for sample returning from Mars 94
An Aerothermal Analysis of an Engine Nacelle for a General Aviation Airplane Model 94
Aerodynamic Characterization of HEXAFLY Scramjet Propelled Hypersonic Vehicle 93
Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle 93
Computational analysis of the flowfield past a returning capsule at super-orbital speed 93
An aerothermodynamic design optimization framework for hypersonic vehicles 93
Aerodynamic and Aerothermodynamic Trade-off Analysis of a Small Hypersonic Flying Test Bed 93
Low speed longitudinal aerodynamics of a blended wing-body re-entry vehicle 93
Multidisciplinary optimization and cfd validation for the design of a next generation re-entry glider 93
SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT 92
Multi-disciplinary optimization of a space re-entry vehicle using skeleton-based integral soft objects 92
Computational flowfield analysis over a blunt body reentry vehicle, Journal of Spacecraft and Rockets 92
A reduced Order Model for a Rapid Evaluation of Scirocco PWT Nozzles Flowfield 92
Hypersonic Aerothermal Environment Preliminary Definition of the CIRA FTB-X Reentry Vehicle 92
Computational Flowfield Analysis of a Planetary Entry Vehicle 91
Analysis of thermochemical modelling and surface catalyticity in space vehicles reentry 91
High and Low Speed Analysis of a Re-usable Unmanned Re-entry Vehicle 91
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 90
Computational Analysis of Shock Wave Boundary Layer Interactions in Non-equilibrium Hypersonic Flow 90
MINI-IRENE: Design of a Capsule with Deployable Heat Shield for a Sounding Rocket Flight Experiment 90
Sonic Boom generation using open source CFD approach 89
LOW SPEED AERODYNAMICS OF SIX OPTIMISED AND UNCONVENTIONAL RE-ENTRY VEHICLE AEROSHAPES 89
Sensitivity Analysis for the Numerical Simulation of an Engine Air Cooling System 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
Next Generation Launchers Aerodynamics 88
Aerodynamic Database Development of the ESA Intermediate Experimental Vehicle 88
Phase-A design of a Mars exploration aerial vehicle 88
Subsonic Aerodynamic Analysis of an Unconventional Re-entry Vehicle 88
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 87
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
Introductory Chapter: Hypersonic Vehicles - Past, Present, and Future Insights 87
Numerical investigations of classical hypersonic problems; comparison with experimental data 86
Supersonic Combustion Ram-Jet Configuration with Hydrocarbon Fue 85
Totale 10.419
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Categoria #
all - tutte 63.816
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 63.816
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022910 0 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
2025/20268.956 235 274 581 630 767 5.063 257 412 367 237 103 30
2026/2027249 71 178 0 0 0 0 0 0 0 0 0 0
Totale 16.620