PORTO @ Archivio Istituzionale della Ricerca

CASALINO, LORENZO
 Distribuzione geografica
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Continente #
NA - Nord America 16.712
EU - Europa 15.407
AS - Asia 4.341
SA - Sud America 468
AF - Africa 46
OC - Oceania 15
Continente sconosciuto - Info sul continente non disponibili 8
Totale 36.997
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Nazione #
US - Stati Uniti d'America 16.634
IT - Italia 5.079
DE - Germania 2.541
GB - Regno Unito 2.449
FR - Francia 1.852
CN - Cina 1.787
SG - Singapore 1.172
UA - Ucraina 992
RU - Federazione Russa 559
KR - Corea 415
IE - Irlanda 405
BR - Brasile 395
TR - Turchia 395
NL - Olanda 358
CH - Svizzera 266
SE - Svezia 265
FI - Finlandia 170
HK - Hong Kong 107
BE - Belgio 100
JP - Giappone 85
IN - India 75
ES - Italia 72
IR - Iran 70
AT - Austria 55
CA - Canada 54
VN - Vietnam 50
JO - Giordania 41
MY - Malesia 40
PL - Polonia 37
PT - Portogallo 30
ID - Indonesia 29
IL - Israele 28
RO - Romania 28
AR - Argentina 25
BD - Bangladesh 18
EU - Europa 18
AE - Emirati Arabi Uniti 17
BG - Bulgaria 17
AP - ???statistics.table.value.countryCode.AP??? 12
AU - Australia 11
ZA - Sudafrica 11
CL - Cile 10
EC - Ecuador 10
MX - Messico 10
HR - Croazia 9
UZ - Uzbekistan 9
CO - Colombia 8
IQ - Iraq 8
PY - Paraguay 8
EG - Egitto 6
LT - Lituania 6
MA - Marocco 6
NG - Nigeria 6
PK - Pakistan 6
SA - Arabia Saudita 6
DK - Danimarca 5
GR - Grecia 5
LU - Lussemburgo 5
NP - Nepal 5
AL - Albania 4
BO - Bolivia 4
CZ - Repubblica Ceca 4
EE - Estonia 4
KZ - Kazakistan 4
LV - Lettonia 4
NZ - Nuova Zelanda 4
VE - Venezuela 4
CI - Costa d'Avorio 3
HU - Ungheria 3
PE - Perù 3
RS - Serbia 3
SK - Slovacchia (Repubblica Slovacca) 3
TT - Trinidad e Tobago 3
TW - Taiwan 3
AO - Angola 2
BY - Bielorussia 2
DO - Repubblica Dominicana 2
DZ - Algeria 2
GE - Georgia 2
GP - Guadalupe 2
GT - Guatemala 2
HN - Honduras 2
KE - Kenya 2
NO - Norvegia 2
OM - Oman 2
PH - Filippine 2
SN - Senegal 2
TG - Togo 2
AM - Armenia 1
BH - Bahrain 1
BT - Bhutan 1
CR - Costa Rica 1
CW - ???statistics.table.value.countryCode.CW??? 1
GA - Gabon 1
JM - Giamaica 1
KG - Kirghizistan 1
KW - Kuwait 1
LB - Libano 1
LI - Liechtenstein 1
MD - Moldavia 1
Totale 36.985
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Città #
Ashburn 3.956
Southend 2.083
Seattle 1.747
Des Moines 1.310
Fairfield 1.289
Turin 923
Chandler 638
Singapore 622
Woodbridge 618
Houston 564
Princeton 563
Jacksonville 498
Cambridge 447
Santa Clara 446
Beijing 438
Wilmington 438
Ann Arbor 425
Dublin 381
San Ramon 349
Berlin 338
Milan 306
Izmir 284
Torino 266
Zhengzhou 251
Bern 247
Chicago 239
Shanghai 232
Boardman 230
Rome 220
Frankfurt 219
Dallas 215
San Donato Milanese 151
Helsinki 149
Zaporozhye 126
Pennsylvania Furnace 124
Baltimore 123
Overberg 109
Seoul 108
Denver 107
Herkenbosch 105
Bologna 99
Moscow 97
Brussels 87
Council Bluffs 85
Hefei 79
Hong Kong 75
Bari 72
Monopoli 72
Hangzhou 65
Los Angeles 62
Saint Petersburg 61
Padua 59
Mountain View 53
Redwood City 52
Paris 51
Buffalo 50
New York 49
San Mauro Torinese 49
Munich 44
San Diego 44
Bottanuco 40
Amsterdam 38
Istanbul 38
Guangzhou 34
Naples 34
Vienna 33
Pisa 32
São Paulo 31
Washington 31
Fremont 30
Malatya 30
Norwalk 30
Cuneo 29
Genoa 28
Atlanta 26
Nanjing 26
Varese 26
Frankfurt am Main 25
London 25
Toronto 25
Jakarta 24
Yubileyny 24
Falls Church 23
Modena 23
Southampton 23
Melun 22
Shenzhen 22
Shiraz 22
Hanoi 21
Madrid 21
Ningbo 21
Redmond 21
Warsaw 21
Ankara 20
Tokyo 20
Vercelli 20
Andover 18
Putian 18
Rosignano Marittimo 18
Tel Aviv 18
Totale 24.220
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Nome #
Indirect Optimization of Satellite Deployment into a Highly Elliptic Orbit 427
Active Debris Removal Missions with Multiple Targets 389
Genetic Algorithm and Indirect Method Coupling for Low-Thrust Trajectory Optimization 389
Combustion Instability Involving Vortex Shedding in Hybrid Rocket Motors 383
Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage 374
Indirect Optimization of Asteroid Deflection Missions with Electric Propulsion 320
Mars gravity assist to improve missions towards main-belt asteroids 313
Design Trade-offs for Hybrid Rocket Motors 311
Oxidizer Control and Optimal Design of Hybrid Rockets for Small Satellites 309
Optimal Low-Thrust Escape Trajectories Using Gravity Assist 306
1st ACT Global Trajectory Optimisation Competition: Results Found at the Politecnico of Turin 305
Comparison of Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper-Stage 304
Improved Edelbaum's approach to optimize LEO-GEO low-thrust transfers 302
Fast Evaluation and Optimization of Low-Thrust Transfers to Multiple Targets 300
Low-Thrust Trajectories to Mercury with Multiple Gravity Assists 300
Approximate Optimization of Low-Thrust Transfers Between Low-Eccentricity Close Orbits 299
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
Optimization of Hybrid Propellant Mars Ascent Vehicle 274
Optimal design of hybrid rocket motors for microgravity platform 273
Hybrid rocket upper stage optimization: effects of grain geometry 272
Minimum-Fuel Escape from Two-Body Sun-Earth System 271
Optimization of Open Rotor Engines for Civil Aircraft Using a Cooperative Evolutionary Method 271
Acoustic Analysis of Hybrid Rocket Combustion Chambers 270
Analysis of Acoustics and Vortex Shedding Interactions in Hybrid Rocket Motors 269
Acoustic Analysis of Hybrid Rocket Combustion Chambers 266
Resonant Fly-by Missions to Near Earth Asteroids 263
Improved Edelbaum's approach to optimize low earth/geostationary orbits low-thrust transfers 263
Wall Curvature Effects on External Burning in Supersonic Flow 260
Optimization of an Advanced Open Rotor Engine for Civil Transport 258
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
Effects of Limitation of Nozzle Flow Separation on Launcher Performance 252
Optimal Performance of a Dual-Fuel Single-Stage Rocket 252
Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure 252
Simple Strategy for Powered Swingby 251
Effects of limitation of nozzle flow separation on launcher performance 251
Resonant Fly-by Missions to Near Earth Asteroids 250
Numerical Analysis of Grain Burnback in Solid Propellants 248
Hybrid Evolutionary Algorithm for the Optimization of Interplanetary Trajectories 247
Optimal Control Law for Interplanetary Trajectories with Nonideal Solar Sail 247
Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages 246
A Straightforward Approach for Robust Design of Hybrid Rocket Engine Upper Stage 246
Optimal Control of a Grey Solar Sail for Interplanetary Missions 244
Flexible variable-specific-impulse electric propulsion systems for planetary 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
Cooperative Evolutionary Algorithm for Space Trajectory Optimization 241
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
Integrated Design of Hybrid Rocket Upper Stage and Launcher Trajectory 237
Evolutionary optimization of interplanetary trajectories: improvements from initial diversification 236
One-Dimensional Analysis of Parabolic-Profile MPD Thrusters 236
Approximate optimal LEO transfers with J2 perturbation and dragsail 236
Channel Geometry for Optimal MPD Acceleration 235
Comparison of Robust Design Approaches for Hybrid Rocket Engines 234
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
Optimal Performance of a Tripropellant Single-Stage Rocket 225
Tentative Solutions for Indirect Optimization of Spacecraft Trajectories 225
Minimum-fuel escape from two-body earth-sun system 225
Asteroid Rendezvous Missions with Departure From Earth-Sun L4 and L5 223
Simple Strategy for Powered Swingby 222
Optimization of rocket ascent trajectories using an indirect procedure 221
Trajectories Towards Near-Earth-Objects Using Solar Electric Propulsion 221
Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages 220
A Parametric Analysis of Hybrid Rocket Motors for Sounding Rockets 219
Indirect Optimization of Low-Thrust Capture Trajectories 219
Optimization of DeltaV-Earth-Gravity-Assist Trajectories 218
Optimization of Civil Turbofan with Evolutionary Algorithms 218
Optimal Robust Design of Hybrid Rocket Engines 218
Numerical Tracking of the Solid-Gas Interface in Rocket Motors 217
Analisi Unidimensionale di Flussi Choked in Propulsori MPD 216
Indirect Optimization of Three-Dimensional Multiple-Impulse Moon-to-Earth Transfers 215
Optimal Three-Dimensional Trajectories for Manned Mars Missions 215
Optimal Design of Hybrid Rockets for Small Satellites 214
Optimal performance of a dual-fuel single-stage rocket 214
Optimization of DV-Earth-Gravity-Assist Trajectories 214
Flexible variable-specific-impulse electric propulsion systems for planetary missions 213
Optimization of Variable-Specific-Impulse Interplanetary Trajectories 213
Optimal Design and Control of Hybrid Rockets for Access to Space 213
Optimization of Hybrid Sounding Rockets for Hypersonic Testing 213
Design of High-Energy Escape Trajectories with Lunar Gravity Assist 212
Indirect Optimization Method for Low-Thrust Interplanetary Trajectories 212
Optimal Cooperative Deployment of a Two-Satellite Formation into a Highly Elliptic Orbit 211
Oxidizer Control and Optimal Design of Hybrid Rockets for Small Satellites 211
A New Mission Concept to Reach Near-Earth Planets 209
Fast Evaluation and Optimization of Low-Thrust Transfers to Multiple Targets 208
Totale 25.492
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Categoria #
all - tutte 104.577
article - articoli 42.974
book - libri 0
conference - conferenze 53.423
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 8.180
Totale 209.154
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.881 0 0 0 376 161 260 130 241 153 281 191 88
2021/20222.185 118 98 304 93 95 127 128 71 123 201 301 526
2022/20234.210 279 460 72 207 254 433 1.512 194 318 55 94 332
2023/20241.233 64 107 65 88 122 144 86 135 54 98 108 162
2024/20253.403 43 508 207 367 412 213 142 212 444 201 270 384
2025/20261.762 538 579 645 0 0 0 0 0 0 0 0 0
Totale 37.262