IRIS
PEZZELLA, Giuseppe
 Distribuzione geografica
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Continente #
EU - Europa 8.433
NA - Nord America 4.818
AS - Asia 3.515
SA - Sud America 793
Continente sconosciuto - Info sul continente non disponibili 381
AF - Africa 53
OC - Oceania 34
Totale 18.027
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Nazione #
RU - Federazione Russa 5.494
US - Stati Uniti d'America 4.690
SG - Singapore 1.447
IT - Italia 966
IE - Irlanda 944
CN - Cina 690
BR - Brasile 674
HK - Hong Kong 529
GB - Regno Unito 388
VN - Vietnam 302
KR - Corea 231
UA - Ucraina 222
DE - Germania 102
IN - India 86
FR - Francia 72
CA - Canada 58
AR - Argentina 41
NL - Olanda 40
FI - Finlandia 38
ID - Indonesia 35
TR - Turchia 35
AU - Australia 34
EC - Ecuador 29
BD - Bangladesh 25
AT - Austria 23
GR - Grecia 23
JP - Giappone 23
MX - Messico 22
IQ - Iraq 21
SE - Svezia 19
BE - Belgio 18
PK - Pakistan 18
VE - Venezuela 15
ES - Italia 14
JM - Giamaica 14
PL - Polonia 14
IR - Iran 13
MA - Marocco 13
PY - Paraguay 12
ZA - Sudafrica 12
PT - Portogallo 11
CR - Costa Rica 10
EG - Egitto 9
CO - Colombia 8
CZ - Repubblica Ceca 7
SA - Arabia Saudita 7
AZ - Azerbaigian 6
CH - Svizzera 6
KE - Kenya 6
LV - Lettonia 6
PE - Perù 6
TW - Taiwan 6
BB - Barbados 5
GT - Guatemala 5
IL - Israele 5
BY - Bielorussia 4
CY - Cipro 4
DZ - Algeria 4
UY - Uruguay 4
UZ - Uzbekistan 4
BH - Bahrain 3
CL - Cile 3
DK - Danimarca 3
KZ - Kazakistan 3
LB - Libano 3
NI - Nicaragua 3
NP - Nepal 3
RO - Romania 3
TH - Thailandia 3
AE - Emirati Arabi Uniti 2
DO - Repubblica Dominicana 2
EE - Estonia 2
HN - Honduras 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
AI - Anguilla 1
AL - Albania 1
AO - Angola 1
BA - Bosnia-Erzegovina 1
BG - Bulgaria 1
BO - Bolivia 1
BS - Bahamas 1
CI - Costa d'Avorio 1
CU - Cuba 1
DM - Dominica 1
ET - Etiopia 1
GD - Grenada 1
GE - Georgia 1
HR - Croazia 1
HU - Ungheria 1
JO - Giordania 1
LA - Repubblica Popolare Democratica del Laos 1
MD - Moldavia 1
Totale 17.640
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Città #
Moscow 1.921
Dublin 940
San Jose 725
Santa Clara 716
Hong Kong 518
Jacksonville 515
Singapore 419
Council Bluffs 392
Ashburn 320
Seoul 214
Chandler 160
Princeton 158
Roxbury 152
Ann Arbor 130
Naples 122
Cambridge 120
Ho Chi Minh City 99
Napoli 78
Beijing 77
Milan 73
Hefei 68
Hanoi 64
São Paulo 59
Des Moines 53
New York 52
Nanjing 51
Rome 49
Medford 47
Wilmington 45
Boardman 39
Dallas 35
Aversa 33
Atlanta 26
Giugliano in Campania 26
The Dalles 24
Xian 24
Bengaluru 23
Miano 23
Rio de Janeiro 23
Sydney 22
Da Nang 21
London 19
Los Angeles 19
Redwood City 17
Frankfurt am Main 16
Caserta 15
Vienna 15
Woodbridge 15
Brasília 14
Casalnuovo di Napoli 14
Centro 14
Guayaquil 14
Shanghai 14
Stella Cilento 14
Belo Horizonte 13
Haiphong 13
San Leucio 13
Brussels 12
Baghdad 11
Casavatore 11
Porto Alegre 11
Afragola 10
Amsterdam 10
Ankara 10
Guangzhou 10
Hamburg 10
Helsinki 10
Poona 10
Pozzuoli 10
Sala Consilina 10
Tokyo 10
Biên Hòa 9
Casoria 9
Chicago 9
Curitiba 9
Guarulhos 9
Hanover 9
Norwalk 9
Thái Bình 9
Thái Nguyên 9
Toronto 9
Viterbo 9
Boston 8
Houston 8
Montreal 8
Nuremberg 8
Phoenix 8
Santo André 8
Zhengzhou 8
Jakarta 7
Jinan 7
Kolkata 7
Palermo 7
Paris 7
Recife 7
Salerno 7
San José 7
Villaricca 7
Warsaw 7
Baku 6
Totale 9.271
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Nome #
Aeroshape design of reusable re-entry vehicles by multidisciplinary optimization and computational fluid dynamics 175
A Numerical Procedure for Variable-Pitch Law Formulation of Vertical-Axis Wind Turbines 162
Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions 150
Aerodynamic analysis of a manned space vehicle for missions to Mars 147
Aerodynamic analysis of a supersonic transport aircraft at landing speed conditions 147
Aerodynamic Performance Analysis of a Winged Re-Entry Vehicle From Hypersonic Down to Subsonic Speed 146
An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles 145
Aerodynamic Analysis with Separation Dynamics of a Launcher at Staging Conditions 144
Aerodynamic analysis of a Mars exploration manned capsule 142
Multidisciplinary Design and Flight Test of the HEXAFLY-INT Experimental Flight Vehicle 141
MINI IRENE - Deployable Heat Shield for Suborbital Flight Test 138
Aerodynamic Analysis of an Unmanned Aerial Vehicle at Hypersonic Speed 137
Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles 137
A New Philosophy for the Design of Re-Entry Vehicles 129
Aerodynamic optimization of airfoils shape for atmospheric flight on Mars planet 128
CFD design capabilities for next generation high-speed aircraft 127
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 123
Aerodynamic Performance Analysis of an Unmanned Re-Entry Vehicle from Hypersonic Down to Subsonic Regime 122
Aerothermodynamic analysis of a space vehicle for manned exploration missions to Mars 121
Multidisciplinary Design of Reusable Re-Entry Vehicles by Optimization and Computational Fluid Dynamics 121
Ablative Heatshield Design for a Sample Return Vehicle 120
Hypersonic Vehicles Past, Present and Future Developments 120
Aerodynamic and thermal design of a space vehicle entering the Mars atmosphere 119
Aerodynamic Analysis of the USV3 Vehicle from Hypersonic to Landing Flight Conditions 119
Heat transfer analysis for a winged reentry flight test bed 118
A Fast Pod-Based Aerothermal Design Environment Tool 118
Hypersonic Vehicles - Applications, Recent Advances, and Perspectives 118
Assessment of predictive capabilities for aerodynamic heating in hypersonic flow 117
LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE RE-ENTRY VEHICLE 117
Phase-A design of a reusable re-entry vehicle 116
Aerodynamics analysis of a capsule vehicle for a manned exploration mission to Mars 114
Additive Layer Manufacturing For Entry Capsules 114
Low Speed Aerodynamic Analysis of the N2A Hybrid Wing–Body 114
WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS 113
Influence of surface catalyticity on reentry aerothermodynamics and heat shield 113
Aeroshape Design and Low speed Aerodynamic Analysis of a Crew Return Vehicle 112
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 112
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 112
Airfoil aerodynamic optimization for Mars exploration aircraft 111
Non-Equilibrium Computational Flowfield Analysis for the Design of Mars Manned Entry Vehicles 111
Aerodynamic Performance Analysis of Three Different Vehicle Concepts at Hypersonic Speed 111
Aerothermodynamic analysis of an Apollo-like reentry vehicle 110
Preliminary Design of Minimum Weight Configurations for a Reentry Vehicle 110
A simplified methodology to simulate a heat exchanger in an aircraft's oil cooler by means of a Porous Media model 110
Aero-thermal Trade-off Analysis of the Italian USV Re-Entry Flying Test Bed 109
Aerodynamic Analysis of a High-Speed Aircraft from Hypersonic down to Subsonic Speeds 108
Experimental Analysis of a Space Re-Entry Vehicle at Landing Conditions 108
Effects of finite rate chemical models on the aerothermodynamics of reentry capsules 108
Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 108
A POD-Based Reduced Order Model for the Simulation of Scirocco PWT Nozzles 107
Introductory Chapter: The Challenge to Fly Faster and Higher 107
MINI-IRENE: Design of Deployable Heat Shield Capsule for a Sounding Rocket Flight Experiment 106
Aerodynamic Performance Analysis of Three Different Vehicle Concepts 106
Aerodynamic and Aerothermodynamic Database of the HEXAFLYINT Hypersonic Glider 106
Analysis of Subsonic/Hypersonic Aerodynamics of a High-Speed Aircraft 105
Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle 105
Launcher Aerodynamics: a Suitable Investigation Approach at Phase-A Design Level 105
Overview of research activities on Hypersonic Vehicles at the Department of Engineering of the University of Campania “L. Vanvitelli” 105
Low speed longitudinal aerodynamics of a blended wing-body re-entry vehicle 104
Computational flowfield analysis over a blunt body reentry vehicle, Journal of Spacecraft and Rockets 103
Aerodynamics and aerothermodynamics assessment of a Mars sample return mission 103
A Spline Based Algorithm for the Analysis of the Flow in Scirocco Plasma Wind Tunnel Nozzle 103
Hypersonic Aerothermal Environment Assessment of the CIRA FTB-X Reentry Vehicle 103
Effects of thermochemical modelling and surface catalyticity on an earth reentry vehicle 102
Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle 102
MINI-IRENE: Design of a Capsule with Deployable Heat Shield for a Sounding Rocket Flight Experiment 102
Multi-disciplinary optimization of a space re-entry vehicle using skeleton-based integral soft objects 101
Nonequilibrium aerothermodynamics for a capsule reentry vehicle 101
Fluid Dynamics Analysis of a Space Vehicle Entering the Mars Atmosphere 101
Aerodynamic Characterization of HEXAFLY Scramjet Propelled Hypersonic Vehicle 101
An aerothermodynamic design optimization framework for hypersonic vehicles 101
An Aerothermal Analysis of an Engine Nacelle for a General Aviation Airplane Model 101
Aerothermodynamics and thermal design for on-ground and in-flight testing of a deployable heat shield capsule 100
Overview of design analysis of a space mission for sample returning from Mars 99
Analysis of thermochemical modelling and surface catalyticity in space vehicles reentry 99
A reduced Order Model for a Rapid Evaluation of Scirocco PWT Nozzles Flowfield 99
Multidisciplinary optimization and cfd validation for the design of a next generation re-entry glider 99
High and Low Speed Analysis of a Re-usable Unmanned Re-entry Vehicle 98
Sonic Boom generation using open source CFD approach 97
Computational Flowfield Analysis of a Planetary Entry Vehicle 97
Computational analysis of the flowfield past a returning capsule at super-orbital speed 97
Aerodynamic and Aerothermodynamic Trade-off Analysis of a Small Hypersonic Flying Test Bed 97
SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT 96
Launcher Aerodynamic Analysis With Plume Effects 96
Introductory Chapter: Hypersonic Vehicles - Past, Present, and Future Insights 96
Sensitivity Analysis for the Numerical Simulation of an Engine Air Cooling System 95
Next Generation Launchers Aerodynamics 95
Hypersonic Aerothermal Environment Preliminary Definition of the CIRA FTB-X Reentry Vehicle 95
Aerodynamic and Aerothermodynamic design of Future Launchers Preparatory Program Concepts 95
LOW SPEED AERODYNAMICS OF SIX OPTIMISED AND UNCONVENTIONAL RE-ENTRY VEHICLE AEROSHAPES 94
Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories 94
Aerothermochemical flowfield around space vehicles for manned missions to Mars 94
Numerical Rebuilding of High and Low Enthalpy Hypersonic Flow Test Over a Double Wedge Model 94
Subsonic Aerodynamic Analysis of an Unconventional Re-entry Vehicle 94
Multidisciplinary Optimization and Experimental Aerodynamic Assessment of a Crew Return Vehicle 93
ENGINEERING-BASED TOOL FOR THREE-DIMENSIONAL ESTIMATIONS OF RE-ENTRY VEHICLES AEROTHERMODYNAMICS 93
Overview of Design Approach for a Sample Return Capsule 93
Supersonic Combustion Ram-Jet Configuration with Hydrocarbon Fue 93
Computational Analysis of Shock Wave Boundary Layer Interactions in Non-equilibrium Hypersonic Flow 93
Non-equilibrium Computational Flowfield Analysis for Mars Entry Manned 92
Totale 11.129
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Categoria #
all - tutte 68.068
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 68.068
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022882 0 0 0 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
2026/20271.656 71 343 807 435 0 0 0 0 0 0 0 0
Totale 18.027