PORTO @ Archivio Istituzionale della Ricerca

PASTRONE, Dario Giuseppe
 Distribuzione geografica
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Continente #
NA - Nord America 16.879
EU - Europa 14.668
AS - Asia 8.670
SA - Sud America 695
Continente sconosciuto - Info sul continente non disponibili 358
AF - Africa 111
OC - Oceania 21
Totale 41.402
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Nazione #
US - Stati Uniti d'America 16.652
IT - Italia 5.399
SG - Singapore 2.414
DE - Germania 2.140
GB - Regno Unito 1.943
CN - Cina 1.914
VN - Vietnam 1.801
FR - Francia 1.524
RU - Federazione Russa 1.078
UA - Ucraina 795
BR - Brasile 549
KR - Corea 536
HK - Hong Kong 394
TR - Turchia 370
NL - Olanda 358
IE - Irlanda 324
IN - India 299
BD - Bangladesh 275
SE - Svezia 223
CH - Svizzera 180
FI - Finlandia 156
JP - Giappone 138
BE - Belgio 125
CA - Canada 124
JO - Giordania 71
ES - Italia 70
TH - Thailandia 59
ID - Indonesia 57
PH - Filippine 55
IR - Iran 53
IQ - Iraq 47
PL - Polonia 47
AT - Austria 46
MY - Malesia 43
TW - Taiwan 43
AR - Argentina 40
BG - Bulgaria 33
EU - Europa 30
MX - Messico 30
PT - Portogallo 30
AE - Emirati Arabi Uniti 27
PK - Pakistan 25
CO - Colombia 24
IL - Israele 24
ZA - Sudafrica 24
RO - Romania 22
AU - Australia 16
CL - Cile 16
VE - Venezuela 16
DZ - Algeria 15
KZ - Kazakistan 15
AP - ???statistics.table.value.countryCode.AP??? 14
EC - Ecuador 14
SA - Arabia Saudita 14
EG - Egitto 13
JM - Giamaica 13
PY - Paraguay 13
HN - Honduras 12
GR - Grecia 11
TT - Trinidad e Tobago 11
CR - Costa Rica 10
MA - Marocco 10
PE - Perù 10
BY - Bielorussia 9
ET - Etiopia 9
NO - Norvegia 9
TN - Tunisia 9
UZ - Uzbekistan 9
BO - Bolivia 8
CI - Costa d'Avorio 8
CZ - Repubblica Ceca 7
GT - Guatemala 7
KE - Kenya 7
LT - Lituania 7
LU - Lussemburgo 7
LV - Lettonia 7
NP - Nepal 7
HR - Croazia 6
LB - Libano 6
NG - Nigeria 6
SN - Senegal 6
AL - Albania 5
OM - Oman 5
EE - Estonia 4
GP - Guadalupe 4
HU - Ungheria 4
IS - Islanda 4
NI - Nicaragua 4
NZ - Nuova Zelanda 4
PR - Porto Rico 4
UY - Uruguay 4
BA - Bosnia-Erzegovina 3
BB - Barbados 3
DK - Danimarca 3
SK - Slovacchia (Repubblica Slovacca) 3
SY - Repubblica araba siriana 3
AZ - Azerbaigian 2
BH - Bahrain 2
DO - Repubblica Dominicana 2
GA - Gabon 2
Totale 41.033
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Città #
Ashburn 3.578
Southend 1.648
Singapore 1.348
Turin 1.239
Seattle 1.226
Des Moines 1.100
San Jose 1.087
Fairfield 950
Chandler 552
Woodbridge 509
Ho Chi Minh City 474
Princeton 449
Beijing 432
Houston 426
Hanoi 422
Milan 419
Jacksonville 390
Santa Clara 390
Wilmington 344
Dublin 318
Ann Arbor 307
Hong Kong 307
Cambridge 304
Rome 288
Council Bluffs 278
San Ramon 274
Berlin 273
Seoul 263
Chicago 257
Torino 255
Dallas 250
Izmir 225
Boardman 208
Hefei 200
Los Angeles 190
Zhengzhou 185
Bern 164
Shanghai 158
Frankfurt 157
Lauterbourg 141
Helsinki 134
Moscow 129
San Donato Milanese 123
Bologna 116
Brussels 116
Herkenbosch 104
Baltimore 99
New York 98
San Mauro Torinese 95
Pennsylvania Furnace 94
Zaporozhye 90
Buffalo 89
Overberg 83
Da Nang 81
Haiphong 77
Denver 74
Naples 64
Hangzhou 63
Monopoli 62
Padua 62
Saint Petersburg 59
Amsterdam 56
Phoenix 55
Frankfurt am Main 51
Istanbul 48
Redwood City 48
Tokyo 46
San Diego 44
Guangzhou 43
Genoa 42
Toronto 42
Mountain View 39
Atlanta 38
São Paulo 38
Savigliano 36
Dearborn 34
Warsaw 34
Nichelino 33
The Dalles 32
Malatya 31
Rotterdam 31
Zogno 31
Brooklyn 30
Hải Dương 30
Chennai 29
Paris 29
San Francisco 29
Vienna 28
Ankara 27
Florence 27
Sofia 27
Jakarta 26
Munich 26
Verona 25
Bangkok 24
Bari 23
Montreal 23
Redmond 23
Shenzhen 23
Washington 23
Totale 25.221
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Nome #
Mission Design and Disposal Methods Comparison for the Removal of Multiple Debris 805
Chemical Rocket Propulsion 518
Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines 515
Combustion Instability Involving Vortex Shedding in Hybrid Rocket Motors 466
Performance of a small-scale turbojet engine fed with traditional and alternative fuels 436
Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage 422
Active Debris Removal Missions with Multiple Targets 421
Rheological and Mechanical Characterization of 3D Printable Solid Propellant Slurry 396
Solid Rocket Propellant Photo-Polymerization with an In-House LED-UV Prototype 390
Design Trade-offs for Hybrid Rocket Motors 382
An Italian network to improve hybrid rocket performance: Strategy and results 375
Risposta dinamica di presa d'aria supersonica a disturbi generati a monte e a valle dell'onda d'urto retta 362
Comparative specific energy consumption between air transport and high-speed rail transport: A practical assessment 362
Advancements in Photocurable Solid Propellantsfor Additive Manufacturing 359
Oxidizer Control and Optimal Design of Hybrid Rockets for Small Satellites 353
Comparison of Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper-Stage 347
Il problema di Goddard 344
Dual-bell nozzle with fluidic control of transition for space launchers 343
Optimal Low-Thrust Escape Trajectories Using Gravity Assist 342
Effects of Limitation of Nozzle Flow Separation on Launcher Performance 337
Optimization Procedure for Preliminary Design of Opposition-Class Mars Missions 337
Analysis of Air-Turborocket Performance 337
Optimal design of hybrid rocket motors for microgravity platform 329
IMPACT OF AN OPTIMIZED POWER TURBINE DISKS CAVITY ON GEARED OPEN ROTOR PERFORMANCE – A MULTIDISCIPLINARY APPROACH IN THE PRELIMINARY DESIGN 329
Optimization of Open Rotor Engines for Civil Aircraft Using a Cooperative Evolutionary Method 329
Mixture-Ratio Control to Improve Hydrogen-Fuel Rocket Performance 327
Optimal Low-Thrust Trajectories Using Flyby 326
Hybrid rocket upper stage optimization: effects of grain geometry 324
An Indirect Method for the Optimization of Finite-Thrust Non-Coplanar Rendezvous Maneuvers 319
Acoustic Analysis of Hybrid Rocket Combustion Chambers 311
Analysis of Acoustics and Vortex Shedding Interactions in Hybrid Rocket Motors 307
Photo-polymerization for additive manufacturing of composite solid propellants 305
Optimal Performance of a Dual-Fuel Single-Stage Rocket 304
Acoustic Analysis of Hybrid Rocket Combustion Chambers 302
Indirect Optimization Method for Round-Trip Mars Trajectories 301
Simple Strategy for Powered Swingby 300
Optimization of Hybrid Propellant Mars Ascent Vehicle 300
Wall Curvature Effects on External Burning in Supersonic Flow 299
Effects of limitation of nozzle flow separation on launcher performance 299
Numerical Analysis of Grain Burnback in Solid Propellants 299
An Improved Acoustic Analysis of a Subscale Rocket Motor 294
Optimal Aeroassisted GEO-to-LEO Transfer by an Indirect Method 289
Indirect Optimization Method for Impulsive Transfers 289
Evaluation of UV-Curable Solid Rocket Propellants’ Properties for Advanced 3D Printing Technologies 284
Analysis of a Thermally Actuated Vuilleumier Refrigerator 284
Optimization of an Advanced Open Rotor Engine for Civil Transport 284
Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure 283
A Straightforward Approach for Robust Design of Hybrid Rocket Engine Upper Stage 282
Multiphysics Modeling for Combustion Instability in Paraffin-Fueled Hybrid Rocket Engines 281
Assessment of Mission Capabilities of a Reusable Heavy-lift Launch Vehicle Concept with Aerospike Engine 280
Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages 280
Numerical Analysis of Grain Burnback in Solid Propellants 279
Modeling Combustion Instability in Aluminized Hybrid Propellants 279
Mission opportunities for human exploration of Mars 278
Design Optimization of a Mg/CO2 Hybrid Rocket Engine for Mars Ascent Vehicles 277
Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance 276
Integrated Design of Hybrid Rocket Upper Stage and Launcher Trajectory 275
Analysis of Conical Detonation Waves 266
Optimal Robust Design of Hybrid Rocket Engines 266
GTOC5: Results from the Politecnico di Torino and Università di Roma Sapienza 264
Blockage Corrections at High Angles of Attack in a Wind Tunnel 264
Comparison of Robust Design Approaches for Hybrid Rocket Engines 263
N2O-Cooled Aerospike for a Hybrid Rocket Motor: Nitrous Oxide Characterization and Additive Manufacturing 263
Multi physics modelling for a hybrid rocket engine with liquefying fuel: a sensitivity analysis on combustion instability 260
Optimization of DeltaV-Earth-Gravity-Assist Trajectories 260
Optimization of rocket ascent trajectories using an indirect procedure 260
Mixture-Ratio Control to Improve LOX/LH2 Rocket Performance 259
Modeling of Saturated and Superheated N2O Heat Transfer Rates, with Experimental Verification 257
Multi-objective Optimization of Electric Pumps for Hybrid Rocket Engines 256
Optimal Performance of a Tripropellant Single-Stage Rocket 256
Simple Strategy for Powered Swingby 255
Optimization of DV-Earth-Gravity-Assist Trajectories 255
Hybrid rocket engine design optimization at politecnico di torino: A review 254
Traiettorie ottimali di ascesa in orbita 253
Optimal Design and Control of Hybrid Rockets for Access to Space 253
Optimal Finite-Thrust Spacecraft Trajectories: an Indirect Approach 252
Analysis of a Stator-Rotor-Stator Spinning Disk Reactor in Single-Phase and Two-Phase Boiling Conditions Using a Thermo-Fluid Flow Network and CFD 252
Optimal Design of Hybrid Rocket Small Satellite Launchers: Ground Versus Airborne Launch 251
Optimal Three-Dimensional Trajectories for Manned Mars Missions 250
An Analysis of Air-Turborocket Performance 249
A Parametric Analysis of Hybrid Rocket Motors for Sounding Rockets 248
An Indirect Method for Fixed-Time Finite-Thrust Optimal Orbit Transfer 248
Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages 248
Numerical Tracking of the Solid-Gas Interface in Rocket Motors 248
Optimization of Hybrid Sounding Rockets for Hypersonic Testing 247
Emission-Driven Hybrid Rocket Engine Optimization for Small Launchers 245
Optimal Design of Hybrid Rockets for Small Satellites 245
Optimal performance of a dual-fuel single-stage rocket 244
Optimization of Civil Turbofan with Evolutionary Algorithms 244
Multi-Objective Optimization of Rocket-Based Combined-Cycle Engine Performance Using a Hybrid Evolutionary Algorithm 243
AN ITALIAN NETWORK TO IMPROVE HYBRID ROCKET PERFORMANCE: THE STRATEGY, THE PROGRAM, THE RESULTS 243
Viability of an Electrically Driven Pump-Fed Hybrid Rocket for Small Launcher Upper Stages 243
External burning on curved surfaces in supersonic flow - Problems and limitations 242
Optimal Orbit Transfer Using a Canonical Transformation and an Indirect Method 241
An Air-Turborocket Exergy Analysis 240
Oxidizer Control and Optimal Design of Hybrid Rockets for Small Satellites 240
Deterministic and Robust Optimization of Hybrid Rocket Engines for Small Satellite Launchers 239
Numerical investigation of different configurations for hydrogen fuelled jet engine combustors 237
Evolutionary Algorithm Based Approach for RBCC Engines Optimization 236
Optimal Propellant Control in Hybrid Rocket Engines 236
Totale 30.128
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Categoria #
all - tutte 112.825
article - articoli 38.889
book - libri 0
conference - conferenze 62.878
curatela - curatele 0
other - altro 723
patent - brevetti 565
selected - selezionate 0
volume - volumi 9.770
Totale 225.650
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.558 0 0 197 50 45 90 189 77 110 121 262 417
2022/20233.574 222 393 66 168 210 360 1.272 179 300 57 120 227
2023/20241.422 60 102 58 94 124 194 117 245 47 119 125 137
2024/20253.625 48 444 166 342 363 205 224 264 451 222 379 517
2025/202610.341 520 510 678 774 477 588 1.504 796 2.245 1.084 430 735
2026/20271.530 1.017 389 124 0 0 0 0 0 0 0 0 0
Totale 41.402