TRAINELLI, LORENZO
 Distribuzione geografica
Continente #
EU - Europa 6.464
NA - Nord America 6.432
AS - Asia 1.095
OC - Oceania 60
SA - Sud America 56
AF - Africa 27
Continente sconosciuto - Info sul continente non disponibili 7
Totale 14.141
Nazione #
US - Stati Uniti d'America 5.985
IT - Italia 3.184
DE - Germania 773
GB - Regno Unito 465
CA - Canada 432
CN - Cina 299
UA - Ucraina 277
SE - Svezia 241
FI - Finlandia 210
VN - Vietnam 201
ES - Italia 197
AT - Austria 188
NL - Olanda 188
FR - Francia 150
IE - Irlanda 149
CH - Svizzera 104
TR - Turchia 85
HK - Hong Kong 76
PH - Filippine 59
SG - Singapore 59
KR - Corea 56
RU - Federazione Russa 54
BE - Belgio 53
IN - India 52
JP - Giappone 52
SI - Slovenia 48
AU - Australia 46
RS - Serbia 45
IR - Iran 44
BR - Brasile 43
JO - Giordania 35
PT - Portogallo 32
NO - Norvegia 20
PK - Pakistan 18
RO - Romania 17
PL - Polonia 16
NZ - Nuova Zelanda 14
TH - Thailandia 13
TW - Taiwan 12
GR - Grecia 11
CZ - Repubblica Ceca 8
ID - Indonesia 8
SK - Slovacchia (Repubblica Slovacca) 8
EU - Europa 7
CI - Costa d'Avorio 6
DK - Danimarca 6
MX - Messico 6
MY - Malesia 6
ZA - Sudafrica 6
AE - Emirati Arabi Uniti 5
BG - Bulgaria 5
CO - Colombia 5
HR - Croazia 5
IL - Israele 5
CR - Costa Rica 4
LT - Lituania 4
NP - Nepal 4
TN - Tunisia 3
AR - Argentina 2
EC - Ecuador 2
EG - Egitto 2
HU - Ungheria 2
KE - Kenya 2
MA - Marocco 2
PE - Perù 2
SY - Repubblica araba siriana 2
TT - Trinidad e Tobago 2
ZW - Zimbabwe 2
AL - Albania 1
BW - Botswana 1
CL - Cile 1
CM - Camerun 1
DZ - Algeria 1
EE - Estonia 1
GG - Guernsey 1
GL - Groenlandia 1
JM - Giamaica 1
LK - Sri Lanka 1
LV - Lettonia 1
OM - Oman 1
PA - Panama 1
QA - Qatar 1
SA - Arabia Saudita 1
SC - Seychelles 1
VE - Venezuela 1
Totale 14.141
Città #
Milan 1.077
Fairfield 563
Chandler 546
Woodbridge 525
Houston 399
Ann Arbor 391
Wilmington 368
Munich 324
Ashburn 279
Seattle 230
Mcallen 217
Redwood City 204
Montréal 198
Cambridge 185
Vienna 181
Ottawa 173
Málaga 151
Jacksonville 150
Dublin 144
Dearborn 138
Rome 138
Lawrence 126
Dong Ket 110
Helsinki 99
Beijing 98
Bovisio Masciago 84
Medford 76
Bern 74
Princeton 52
Davao City 50
Delft 48
Des Moines 39
Columbus 38
Brussels 37
Amman 35
Belgrade 33
London 33
Novara 32
Zibido San Giacomo 32
San Diego 30
Gavirate 28
Central 25
Napoli 24
Luft 23
Cranfield 22
Jinan 22
Naples 22
Torino 22
Istanbul 21
Norwalk 21
Robbiate 21
Seoul 21
Xian 21
Madrid 20
Redmond 20
Scafati 20
Tokyo 20
Carate Brianza 19
Los Angeles 19
Legnano 18
Melbourne 18
New York 18
Samara 18
Berlin 16
Chicago 16
Dallas 16
Dresden 16
San Donato Milanese 16
Toulouse 16
Amsterdam 15
Central District 15
Como 15
Shanghai 15
Zurich 15
Bresso 14
Firat 14
Maribor 14
Mountain View 14
Atlanta 13
Auburn Hills 13
Changsha 13
Verona 13
Bareggio 12
Genoa 12
Palosco 12
Paris 12
Rho 12
Adelaide 11
Ankara 11
Bergamo 11
Gothenburg 11
Stuttgart 11
Zhengzhou 11
Busto Arsizio 10
Kingston 10
Luleå 10
Newton 10
Singapore 10
Taipei 10
Bangkok 9
Totale 8.664
Nome #
A General Preliminary Sizing Procedure for Pure-Electric and Hybrid-Electric Airplanes 512
Preliminary weight sizing of light pure-electric and hybrid-electric aircraft 406
Aircraft with electric batteries, in particular a hybrid aircraft 306
MAHEPA – A Milestone-Setting Project in Hybrid-Electric Aircraft Technology Development 290
Real Time Contactless Sensor for Helicopter Blade Angle Measurement 285
Conceptual Design of a Structural-Battery Hybrid-Electric Aircraft 283
A General Approach to the Conceptual Design of All-Electric and Hybrid-Electric Aircraft 261
Design of Airport Infrastructures in Support of the Transition to a Hybrid-Electric Fleet 246
Distributed Electric Propulsion Aircraft Simulating a Single Propeller Aircraft 223
A Novel Contactless Sensor for Helicopter Blade Motion In-Flight Measurements 212
Optimal Definition of a Short-Haul Air Transportation Network for Door-to-Door Mobility 187
Evaluating The Impact Of Fleet Switching To Hybrid-Electric Aircraft On Airport Infrastructures 184
Innovative Helicopter In-Flight Noise Monitoring Systems Enabled by Rotor-State Measurements 173
Demonstration and Testing of the Pilot Acoustic Indicator on a Helicopter Flight Simulator 171
ROTOR FOR A HOVER-CAPABLE AIRCRAFT AND METHOD FOR DETECTING THE ATTITUDE OF A BLADE WITH RESPECT TO A HUB OF SUCH A ROTOR 171
Laser and vision-based measurements of helicopter blade angles 169
A Powertrain Sizing Method for Hydrogen-Driven Aircraft 161
On the Design of an Electric-Powered Micro-Feeder Aircraft 157
Assessing the Effect of Hybrid-Electric Power-Trains on Chemical and Acoustic Pollution 149
Experiences in Academic Flight Testing Education 147
Contactless Rotor Flapping Sensor Design, Implementation and Testing 139
An Optimization Model for Airport Infrastructures in Support to Electric Aircraft 138
Velivolo plurimotore simulante un monomotore via hardware e software 137
Capturing the Demand for an Electric-Powered Short-Haul Air Transportation Network 135
Velivolo con Batterie Elettriche, in Particolare Velivolo Ibrido (Aircraft with Electric Battery, in Particular Hybrid Aircraft) 133
Recent Developments in Electric Aircraft Conceptual Design 132
Flybrid: Envisaging the Future Hybrid-Powered Regional Aviation 131
A Preliminary Sizing Tool for Evtol Personal Air Vehicles 127
An Attempt at the Classification of Energy Decaying Schemes for Structural and Multibody Dynamics 126
Optimization of the Demand Satisfied by a “Micro-Feeder” Hybrid-Electric Air Transport Service 126
Structural Batteries in Aviation: A Preliminary Sizing Methodology 126
An Invariant-Preserving Approach to Robust Finite-Element Multibody Simulation 121
Flynk - the Future All-Electric Commuter Concept for Metropolitan Areas 121
A Noise Estimation Procedure for Electric and Hybrid-Electric Aircraft 120
Methodologies for the initial design studies of an innovative community-friendly miniliner 118
Sizing of Airport Recharging Infrastructures in Support to a Hybrid-Electric Fleet 114
Project Caurus 'Nibbio' - A Novel Tilt Rotor Concept for Very High Speed Applications 113
On the Optimal Scaling of Index Three DAEs in Multibody Dynamics 112
Reliable and Cost-Effective Flight Testing of Ultralight Aircraft 109
Developing a Novel Contactless Sensor for Helicopter Rotor State Measurements 108
The Embedded Projection Method: a General Index Reduction Procedure for Constrained System Dynamics 107
A Vision-Based Technique for in-Flight Measurement of Helicopter Blade Motion 106
Aero-servo-elastic Modeling and Control of Wind Turbines Using Finite-Element Multibody Procedures 104
Overview and Preliminary Results of the Scalability Investigation of Hybrid Electric Concepts for Next-Generation Aircraft (SIENA) Project 103
Implementation of Effective Procedures for Unilateral Contact Modeling in Multibody Dynamics 103
An Index Reduction Method in Non-Holonomic System Dynamics 101
Dynamic Properties of Some Gimbal and Teetering Two-Blade Helicopter Rotor Heads 99
Switching to Electric Propulsion: Aero Club Fleet and Infrastructure Sizing 99
Dynamic Characterization of a Novel Gimbal Two-Blade Helicopter Rotor 97
Integration of Elastic Multibody Systems by Invariant Conserving/Dissipating Algorithms. I. Formulation 96
A Novel Momentum-Preserving Energy-Decaying Algorithm for Finite Element Multibody Procedures 94
Robust Integration Schemes for Flexible Multibody Systems 94
A Simple Framework for the Study of Airplane Trim and Stability 94
Finite-State Acoustoaeroelasticity 93
Flight Testing of a New Ultralight Airplane for LTF-UL Certification 93
Hybris – An Innovative Concept for Future General Aviation 91
On the Non-Linear Effects of the Gimbal Design on the Aeroelastic Behavior of a Tilt Rotor 90
An Index Reduction Method in Holonomic System Dynamics 90
A Finite-State BEM Method for Acoustoaeroelasticity of Shells 86
Design of the Series Hybrid Reconfiguration of a General Aviation Aircraft 85
Optimal Recharging Infrastructure Sizing and Operations for a Regional Airport 85
In-Flight Demonstration of a Novel Contactless Sensor for Helicopter Blade Motion Measurement 84
Optimal Sizing and Operation of Airport Infrastructures in Support of Electric-Powered Aviation 84
Preliminary Weight Sizing of Light Pure-Electric and Hybrid-Electric Aircraft 83
An Investigation of the Micro-Feeder Aircraft Concept 83
An Attempt at a Systematic Framework for the Parameterization of Rotation and Rigid Motion 81
Trimming a High-Fidelity Multibody Helicopter Model for Performance and Control Analysis 81
Test in Operative Environment of an Artificial Neural Network for Aerodynamic Angles Estimation 81
Aeroelastic Modeling and Control of Wind Turbine Generators Using Finite Element Multibody Procedures 80
Basic Aeroelastic Stability Studies of Hingeless Rotor Blades in Hover Using Geometrically Exact Beam and Finite-State Inflow 80
MANOEUVRES - an Effort Towards Quieter, Reliable Rotorcraft Terminal Procedures 79
Innovative Rotor-State Measurements Enabling Helicopter In-Flight Noise Monitoring and Enhanced Attitude Control 78
Finite Element Procedures for Non-Linear Aeroelastic Problems 77
Sizing and Performance of Hydrogen-Driven Airplanes 76
Developing an Observation Methodology for Non-Measurable Rotorcraft States 76
Conceptual Design of a Near-Zero Emission and Cost-Efficient Regional Air Mobility Solution 76
A Simplified Approach to Basic Airplane Equilibrium and Stability 75
Predicting the effect of electric and hybrid-electric aviation on acoustic pollution 75
Experiences in Flight Mechanics Education: Getting the Students Hands on the Real Thing 74
An Attempt at the Classification of Energy Decaying Schemes for Structural and Multibody Dynamics 71
Preliminary Sizing and Energy Management of Serial Hybrid-Electric Airplanes 71
Concept Study of an Innovative Aerial Component for The Italian Firefighting System 70
Conceptual Studies of Hybrid-Electric Passenger Airplanes 69
Integration of Elastic Multibody Systems by Invariant Conserving/Dissipating Algorithms. II. Numerical Schemes and Applications 68
Development and Testing of Innovative Solutions for Helicopter In-Flight Noise Monitoring and Enhanced Control Based on Rotor State Measurements 68
A Sizing Procedure for Structural Batteries in Hybrid-Electric Aircraft 68
Modelling and Characterization of a Novel Gimbal Two-Blade Helicopter Rotor 67
A Cost-Effective Approach to Ultralight Machine Flight Testing - an Academic Perspective 66
Project MANOEUVRES - Towards Real-Time Noise Monitoring and Enhanced Rotorcraft Handling Based on Rotor State Measurements 66
Award-Winning Innovative Aircraft Design Projects at Politecnico di Milano 66
An Embedded Projection Method for Constrained Dynamics 65
On the Modeling of Rotorcraft Systems Using Finite Element Multibody Dynamics 64
Sviluppo di Strumenti per la Simulazione di Moderne Turbine Eoliche : Aeroelastic Analysis and Control of Wind Turbine Generators 64
On the Optimal Scaling of Index Three DAEs in Multibody Dynamics 62
Nonlinear Unconditional Stability in the Integration of Flexible Multibody Systems 62
The Pilot Acoustic Indicator: a Novel Cockpit Instrument for the Greener Helicopter Pilot 61
Acoustic Prediction of Helicopter Unsteady Manoeuvres 61
Hybrid-Electric Power-Train Modelling for Airplane Performance Analysis and Sizing 60
Basic Airplane Equilibrium and Stability Revisited 59
Energy Preserving/Decaying Schemes for Holonomic/Non-Holonomic Non-Linear Multibody Systems 59
Totale 11.979
Categoria #
all - tutte 31.442
article - articoli 6.674
book - libri 0
conference - conferenze 22.624
curatela - curatele 0
other - altro 0
patent - brevetti 1.610
selected - selezionate 0
volume - volumi 423
Totale 62.773


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019519 0 0 0 0 0 0 0 0 0 127 201 191
2019/20202.029 148 136 53 114 226 186 209 116 232 150 269 190
2020/20212.891 265 259 248 236 291 187 255 210 184 253 175 328
2021/20222.222 130 261 148 171 279 133 138 173 148 200 181 260
2022/20232.102 162 180 119 179 201 233 84 138 275 235 155 141
2023/20241.194 73 189 146 158 173 191 119 73 37 35 0 0
Totale 14.362