PORTO @ Archivio Istituzionale della Ricerca

COLASURDO, GUIDO
 Distribuzione geografica
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Continente #
NA - Nord America 12.057
EU - Europa 8.787
AS - Asia 2.430
SA - Sud America 262
AF - Africa 19
Continente sconosciuto - Info sul continente non disponibili 17
OC - Oceania 6
Totale 23.578
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Nazione #
US - Stati Uniti d'America 12.023
IT - Italia 2.193
GB - Regno Unito 1.714
DE - Germania 1.468
FR - Francia 1.105
CN - Cina 931
UA - Ucraina 763
SG - Singapore 697
RU - Federazione Russa 356
TR - Turchia 325
NL - Olanda 280
KR - Corea 233
BR - Brasile 223
IE - Irlanda 212
CH - Svizzera 183
SE - Svezia 175
FI - Finlandia 118
AT - Austria 67
JP - Giappone 50
VN - Vietnam 34
JO - Giordania 30
MY - Malesia 30
HK - Hong Kong 29
CA - Canada 25
ES - Italia 24
EU - Europa 22
IR - Iran 18
AP - ???statistics.table.value.countryCode.AP??? 16
RO - Romania 16
IN - India 15
BE - Belgio 12
PL - Polonia 12
BD - Bangladesh 11
AE - Emirati Arabi Uniti 10
AR - Argentina 10
EC - Ecuador 9
ID - Indonesia 9
IL - Israele 9
LU - Lussemburgo 9
CL - Cile 8
GR - Grecia 7
HR - Croazia 6
SA - Arabia Saudita 6
AU - Australia 5
HU - Ungheria 5
MX - Messico 5
UZ - Uzbekistan 5
ZA - Sudafrica 5
IQ - Iraq 4
KZ - Kazakistan 4
MA - Marocco 4
PY - Paraguay 4
TW - Taiwan 4
CO - Colombia 3
EE - Estonia 3
NG - Nigeria 3
VE - Venezuela 3
DZ - Algeria 2
NP - Nepal 2
PE - Perù 2
PH - Filippine 2
AO - Angola 1
AZ - Azerbaigian 1
BG - Bulgaria 1
BY - Bielorussia 1
CI - Costa d'Avorio 1
CR - Costa Rica 1
DO - Repubblica Dominicana 1
EG - Egitto 1
GE - Georgia 1
HN - Honduras 1
JM - Giamaica 1
KE - Kenya 1
NZ - Nuova Zelanda 1
PK - Pakistan 1
PT - Portogallo 1
QA - Qatar 1
RS - Serbia 1
SN - Senegal 1
TJ - Tagikistan 1
XK - ???statistics.table.value.countryCode.XK??? 1
Totale 23.578
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Città #
Ashburn 2.776
Des Moines 1.913
Southend 1.553
Seattle 1.483
Fairfield 760
Santa Clara 462
Jacksonville 381
Chandler 372
Princeton 358
Woodbridge 358
Singapore 348
Houston 302
Wilmington 261
Izmir 258
Turin 257
Cambridge 251
San Ramon 249
Ann Arbor 236
Beijing 232
Frankfurt 222
Berlin 214
Dublin 207
Chicago 195
Bern 173
Rome 145
Boardman 136
Shanghai 113
Helsinki 110
Herkenbosch 110
Zhengzhou 108
San Donato Milanese 106
Pennsylvania Furnace 105
Overberg 101
Baltimore 100
Zaporozhye 87
Milan 84
Monopoli 69
Padua 69
Bologna 63
Moscow 61
Vienna 55
Seoul 52
Torino 50
Saint Petersburg 46
Los Angeles 40
Malatya 37
Redwood City 35
Paris 33
Buffalo 32
Dallas 31
Hangzhou 31
Hong Kong 27
Mountain View 27
Munich 24
Pisa 24
Rotterdam 24
San Diego 24
Norwalk 22
Murrieta 20
Yubileyny 19
Tokyo 18
Atlanta 17
Hanoi 17
San Francisco 17
Council Bluffs 16
Modena 16
Naples 16
Ningbo 16
Toronto 16
Bari 15
Guangzhou 15
Hefei 15
Monselice 15
Verona 15
Washington 15
Cuneo 14
London 14
Shenzhen 14
Melun 13
Santa Cruz 13
Brussels 12
Ho Chi Minh City 12
Jinan 12
Putian 12
São Paulo 12
Amsterdam 11
Nanjing 11
New York 11
Frankfurt Am Main 10
Altopascio 9
Genoa 9
Kocaeli 9
Loano 9
Madrid 9
Redmond 9
Samara 9
Alba 8
Andover 8
Arlington 8
Brasília 8
Totale 16.546
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Nome #
Indirect Optimization of Satellite Deployment into a Highly Elliptic Orbit 427
Risposta dinamica di presa d'aria supersonica a disturbi generati a monte e a valle dell'onda d'urto retta 321
Mars gravity assist to improve missions towards main-belt asteroids 313
Optimal Low-Thrust Escape Trajectories Using Gravity Assist 306
1st ACT Global Trajectory Optimisation Competition: Results Found at the Politecnico of Turin 305
Analysis of Air-Turborocket Performance 304
Il problema di Goddard 302
Improved Edelbaum's approach to optimize LEO-GEO low-thrust transfers 302
Low-Thrust Trajectories to Mercury with Multiple Gravity Assists 300
Mixture-Ratio Control to Improve Hydrogen-Fuel Rocket Performance 294
Optimization of Variable-Specific-Impulse Interplanetary Trajectories 294
Optimal Geometry of Self-Field Magnetoplasmadynamic Thrusters 291
Indirect Methods for the Optimization of Spacecraft Trajectories 290
Optimization Procedure for Preliminary Design of Opposition-Class Mars Missions 288
Deployment of a Two-Spacecraft Formation into a Highly Elliptic Orbit with Collision Avoidance 278
Tour of Jupiter Galilean moons: Winning solution of GTOC6 276
Minimum-Fuel Escape from Two-Body Sun-Earth System 271
An Indirect Method for the Optimization of Finite-Thrust Non-Coplanar Rendezvous Maneuvers 268
Resonant Fly-by Missions to Near Earth Asteroids 263
Improved Edelbaum's approach to optimize low earth/geostationary orbits low-thrust transfers 263
Indirect Optimization Method for Impulsive Transfers 255
Caratteristiche cinematiche di elementi di tenuta in macchine KKM-ka 3/2 254
Indirect Optimization Method for Round-Trip Mars Trajectories 253
Numerical Analysis of Grain Burnback in Solid Propellants 253
Optimal Low-Thrust Trajectories Using Flyby 252
Optimal Performance of a Dual-Fuel Single-Stage Rocket 252
Simple Strategy for Powered Swingby 251
Resonant Fly-by Missions to Near Earth Asteroids 250
Unsteady Compressible Flow: A Computational Method Consistent with the Physical Phenomena 249
Numerical Analysis of Grain Burnback in Solid Propellants 248
Optimal Control Law for Interplanetary Trajectories with Nonideal Solar Sail 247
A Physically Consistent Time-Dependent Method for the Solution of the Euler Equations in Transonic Flow 246
Optimal Control of a Grey Solar Sail for Interplanetary Missions 244
Optimal Aeroassisted GEO-to-LEO Transfer by an Indirect Method 244
Optimal Performance of Enthalpy Rocket 243
Mission opportunities for human exploration of Mars 243
Analysis of a Thermally Actuated Vuilleumier Refrigerator 242
Energy Management in Rocket Propulsion 238
Missions to Asteroids Using Solar Electric Propulsion 238
Mars gravity assist to improve missions towards main-belt asteroids 237
One-Dimensional Analysis of Parabolic-Profile MPD Thrusters 236
Channel Geometry for Optimal MPD Acceleration 235
A Contribution to the Prediction of Distorted Flow in Axial Compressors 233
Characteristics of Electric Propulsion Systems for Optimal Interplanetary Trajectories 231
Optimal control law for interplanetary trajectories with solar sail 226
GTOC5: Results from the Politecnico di Torino and Università di Roma Sapienza 226
Traiettorie ottimali di ascesa in orbita 226
Optimal Low-Thrust Maneuvers in Presence of Earth Shadow 226
Mixture-Ratio Control to Improve LOX/LH2 Rocket Performance 225
Tentative Solutions for Indirect Optimization of Spacecraft Trajectories 225
Minimum-fuel escape from two-body earth-sun system 225
Simple Strategy for Powered Swingby 222
Axisymmetric Swirling Flows in Underexpanded Jets 221
Optimization of rocket ascent trajectories using an indirect procedure 221
Trajectories Towards Near-Earth-Objects Using Solar Electric Propulsion 221
Contributo al miglioramento della caratteristica di regolazione dei motori ad accensione comandata 220
Optimization of DeltaV-Earth-Gravity-Assist Trajectories 218
An Analysis of Air-Turborocket Performance 218
Numerical Tracking of the Solid-Gas Interface in Rocket Motors 217
Optimal Finite-Thrust Spacecraft Trajectories: an Indirect Approach 216
Analisi Unidimensionale di Flussi Choked in Propulsori MPD 216
Optimal Three-Dimensional Trajectories for Manned Mars Missions 215
Optimal performance of a dual-fuel single-stage rocket 214
Optimization of DV-Earth-Gravity-Assist Trajectories 214
Optimization of Variable-Specific-Impulse Interplanetary Trajectories 213
Un metodo numerico per la soluzione del problema inverso nell'aerodinamica esterna 213
Indirect Optimization Method for Low-Thrust Interplanetary Trajectories 212
Optimal Cooperative Deployment of a Two-Satellite Formation into a Highly Elliptic Orbit 211
A New Mission Concept to Reach Near-Earth Planets 209
An Indirect Method for Fixed-Time Finite-Thrust Optimal Orbit Transfer 206
Optimal Trajectories Towards Near-Earth-Objects using Solar Electric Propulsion (SEP) and Gravity Assisted Maneuver 205
Optimal DV-Earth-Gravity-Assist Trajectories in the Restricted Three-Body Problem 205
Numerical Analysis of Reacting Nonequilibrium Two-dimensional Nozzle Flows Including Boundary Layer and Shock Waves 204
Optimal Propellant Control in Hybrid Rocket Engines 200
Trajectory Options for a Mars Sample Return Mission 198
Heat Transfer Analysis in Pressurizer Tank Under Microgravity 198
Optimal Orbit Transfer Using a Canonical Transformation and an Indirect Method 197
Trade-off Between Payload and Trip-Time for EP Interplanetary Trajectories 195
Optimal Geometry of Self-Field Magnetoplasmadynamic Thrusters 194
Heat Transfer Analysis in Pressurizer Tank Under Microgravity 192
A Finite Difference Method Based on Bicharacteristics for Solving Multidimensional Hyperbolic Flows 192
A New Configuration of the Thermally Actuated Vuilleumier Refrigerator 187
Optimal Finite-Thrust Spacecraft Trajectories 187
Three-Dimensional Inviscid Compressible Rotational Flows. Numerical Results and Comparison with Analytical Solutions 185
Indirect Optimization of Multi-Flyby Mercury Rendezvous Missions 180
Indirect Approach for Minimum-Fuel Aeroassisted Transfer 177
Missions to Asteroids Using Solar Electric Propulsion 172
Optimal Low-Thrust Escape from the Solar System 172
Campo di moto potenziale incompressibile attorno a un profilo alare in una galleria di forma arbitraria 170
On the Performance of the Air-TurboRocket 168
3D Optimal Orbit Transfer 168
Optimal Transfer to Non-Coplanar Geostationary Orbit 167
Trasformazione conforme per la generazione di griglie per il calcolo del flusso attraverso schiere palettate 166
Trasferimento orbitale con spinta finita 165
Indirect Optimization Method for Interplanetary Trajectories Using Electric Propulsion and Gravity Assist 162
Optimal Time-Constrained Missions to Near-Earth Asteroids 157
Nozzle Effects on Linear Stability Behaviour of Combustors 149
Numerical Investigations on the Generation and Development of Rotating Stalls 146
Operation Modes of Constant-Area MPD Thrusters 145
On the Benefit of Variable-Specific-Impulse Operation forInterplanetary Trajectories 140
Totale 22.849
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Categoria #
all - tutte 69.399
article - articoli 20.210
book - libri 0
conference - conferenze 33.722
curatela - curatele 0
other - altro 2.629
patent - brevetti 0
selected - selezionate 0
volume - volumi 12.838
Totale 138.798
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.005 0 0 58 194 63 130 67 121 82 131 110 49
2021/20221.015 53 67 145 18 13 46 62 28 38 47 194 304
2022/20233.400 135 268 7 91 128 256 2.022 69 158 9 58 199
2023/2024353 28 27 10 12 47 40 8 34 8 31 27 81
2024/20251.797 22 349 113 150 381 135 54 58 197 60 95 183
2025/2026881 287 281 313 0 0 0 0 0 0 0 0 0
Totale 23.609